20050627000042005062700004EA 2005 6 27 SWIA200515090 120050530A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07720SW 7297 OVERHEAD EMERGENCY LIGHT IN CABIN INOPERATIVE. RELAMPED OVERHEAD FWD EMERGENCY LAMP. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050627001552005062700155NM 2005 6 27 QXEA200501064 120050617A5230 HANDLE BOMBDRDHC8 DHC8402 1390042NM PAX DOOR UNSECURE A QXEAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 NM09408QX 4050 SEA - ON FLIGHT 2438, RETURNED TO FIELD SEA-GEG, (MASTER WARNING) BAGGAGE DOOR LIGHT AND LOSS OF PRESSURIZATION AT 3000 FEET. INSPECTED AND FOUND LATCH HANDLE EXTENDED. OPENED DOOR AND INSPECTED. FOUND NO DEFECTS. RESET LATCH. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050623000022005062300002NM 2005 6 23 AALA20050385 120050611A3350 LIGHT BOEING777 777223 1385213NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW21774AN 29581 MIA - EMERGENCY LIGHT ASSEMBLY AT FIRST CLASS CLOSET IN FORWARD GALLEY BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY AT FIRST CLASS CLOSET IN FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050317000922005031700092NM 2005 3 17 2005UALA00206 120050302A5322 SHEAR TIE BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29582UA 26702 AFT PIT STA 1440 SHEAR TIE CORRODED BETWEEN STR 29L AND 30L. A REPLACEMENT SHEAR TIE WAS FABRICATED AND INSTALLED. 2L72 4F4 FRTA2NM E17NE 20050209001362005020900136NM 2005 2 9 MASA200500024 120050109A33501317 BULB DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHTSBURNED OUT A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07989HA 427 FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING SYSTEM HAS A LIGHT THAT IS OUT. MAINTENANCE RELAMPED THE LIGHT. 2H72 4T RTA13NM 20050324001352005032400135NM 2005 3 24 F3LA200500007 120050308A5320 SILL BOEING737 7373L9 1384470NM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03313FL 4372 26442 DURING C-4 CHECK INSPECTION, REPORTED R2 DOOR MOP SILL CORRODED. REPLACED R2 DOOR MOP SILL PER SRM 51-40-02. 2L72 4F RTA16WE 20050324001692005032400169EA 2005 3 24 SWIA200514640 120050223A27604916405 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA SPOILER MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TXTAXI/GRND HDL 1 NM07924SW8400 8400 7681 DURING TAXI OUT, GOT SPOILERONS FAULT MESSAGE. REPLACED NR 2 SECU IAW MM 27-61-05, OPERATIONAL CHECKS GOOD. 2L72 4F RTA21EA 20050324001712005032400171EA 2005 3 24 SWIA200514642 120050224A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAP MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 NM07919SW6589 6589 7657 SELECTED FLAPS TO 8 DEGREES, THEN FLAPS FAIL CAUTION MESSAGE. REMOVED AND REPLACED FECU IAW CRJ 200 MM CHAPTER 27-51-05, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050325000222005032500022EU 2005 3 25 05FDEA00587 120050317A5730A5724279520100 PANEL AIRBUS310 A310222 3930315EU RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 RIGHT WING T/E PANEL LANDING FOR ACCESS PANEL 675CB HAS 1.0 INCH CRACK. REMOVED AND REPLACED LANDING PLATE IAW SRM 51-72-10. 2L72 4F RTA35EU 20050325000592005032500059WP 2005 3 25 DHL2005805504 120050220A5531 FRAME DOUG DC8 DC873F 302199FWP VERTICAL STAB CRACKED A DHLAK NONE P NO WARNING INDICATION ININSP/MAINT 1 SO01805DH80855 46125 VERTICAL STAB L/E FORMER CRACKED 1.000, STA ZFS 114.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (AL7075-T6 0.032) IAW SRM 55-2-0 PG 7-8 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED ANGLE DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1 PG 2A TABLE II. 2L74 4F RT4A25 20050325001022005032500102EA 2005 3 25 SWIA200514736 120050314A2711 TRIM SYSTEM CNDAIRCL600 CL6002C10 1390015EA AILERONS MALFUNCTIONED A SWIAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 NM07732SK 10194 AILERON TRIM RANAWAY DURING TAKEOFF ROLL. TAKEOFF CONFIG AILERON TRIM MOVES LWD. CLEANED TRIM SWITCHES & PANEL CONNECTOR. OHM'ED AND MEGGED WIRING BETWEEN AILERON TRIM ACTUATOR AND JB10. WIRING ALL OHM'ED OUT NORMAL. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050325001052005032500105 2005 3 25 SWAA050865 420050321A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29795SW 30606 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. SLIDE DID NOT DEPLOY. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20050325001272005032500127NM 2005 3 25 SWAA050782 120050314A57546546486 WEDGE BOEING737 7373H4 1384600NM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND RT WING, NR 4 L/E SLAT, INBOARD END T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM. 2L72 4F RTA16WE 20050328001782005032800178NM 2005 3 28 HNAA0500028 120050323A7797 WIRE DHAV DHC8 DHC8102 2809003NM SPEED SENSE DAMAGED A HNAAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 EA07907HA 011 RT AC BUSS LIGHT ILLUMINATED IN FLT WITH ASSOCIATED RT TRU, RIGHT ELEVATOR HEAT AND RIGHT STALL WARNING. REMOVED AND REPLACED CONNECTOR 2421-P6 AT A/C CONTACTOR BOX, REPLACED WIRES 2022B22, 2023B22, 2021B22, 2024B22, 10024G22, 10023G22, 10022G22, 10021M22, 20015G22, 20045C22, 20044C22, 20043C22, 2442-2009D2, 20011B22, 20010B22 NO FIX, PROBLEM RETURNED ON 25 MARCH 2005. R & R RT AC GENERATOR AND GCU NO FIX PROBLEM RETURNED 02 APRIL 2005. REPAIRED SPEED SENSE WIRES NEAR RT AC CONTACTOR BOX. OPS CHECK GOOD 2H72 4T RTA13NM 20050328001792005032800179NM 2005 3 28 BB05020 120050321A3397 WIRE BOEING767 767201 1385125NM EMERGENCY LIGHT DETACHED A USAAK NONE O OTHER ININSP/MAINT 1 EA19648US 23900 PHL FOUND A BROKEN WIRE FOR THE EMERGENCY FLOOR TRACK LIGHTING NEAR SEAT ROWS 22 AND 23. MAINTENANCE RE-ATTACHED THE WIRE TO THE HOUSING. 2L72 4F RTA1NM 20050623000092005062300009EA 2005 6 23 MASA200500395 120050525A5210 HAND RAIL CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OBSTRUCTED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07154SF 7154 ASH 2628 CLT. THE CREW REPORTED THAT THE PASSENGER DOOR WOULD NOT CLOSE IN THE DOOR FRAME. AFTER SEVERAL HOURS OF RIGGING, MAINTENANCE REMOVED THE DEBRIS FROM THE HAND RAILS. OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA21EA 20050929000012005092900001NM 2005 9 29 05FDEA02993 120050919A5230 WEB BOEING727 727200 138407ENM CARGO DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21674 FWD CARGO DOOR INNER WEB CRACKED AT UPPER MIDDLE RIVNUT. REPAIRED FWD CARGO DOOR INNER WEB PER FED EX EA 7-5230-91364. 2L73 4F RTA3WE 20060210000082006021000008SO 2006 2 10 MASA200500620 120050807A3350 SWITCH EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMRG LIGHT SYS NOT CLOSED A MASAO OTHER O OTHER NRNOT REPORTED 1 SW07853MJ 145464 ASH 2674 GSP ROW 12 D,F EMERG EXIT LIGHT WILL NOT ILLUMINATE. CONTRACT MX PLACED EMERG LIGHT SW TO ARM FOR CHARGING FOR 1 HOUR. OPS NML. NO OTHER DEFECTS NOTED. 2L72 4T4 FRTT00011ATTE6CH 20050323001952005032300195WP 2005 3 23 AALA20050209 120050321A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217543A 53025 PHX - EMERGENCY LIGHTS AT OVERHEAD MID CABIN INOPERATIVE. REPLACED BATTERY CHARGER FOR EMERGENCY LIGHTS AT MID CABIN OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050324000412005032400041NM 2005 3 24 WRLA2005027 120050216A5512 SKIN DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098 FOUND CORROSION IN HST LT BARREL NUT HOLE NR 21. 2L73 4F4 FRTA22WE E24NE 20050324001212005032400121CE 2005 3 24 20030802 120050226A5320 STRUCTURE BEECH 1900 1900D 1154162CE FUSELAGE DAMAGED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03150GL UE150 ON ROUTINE INSPECTION, A SMALL LIGHTNING HOLE FOUND ON BOTTOM SIDE OF FUSELAGE DIRECTLY IN FRONT OF AFT PRESS BULKHEAD AT FS 545.50. REPAIRED, AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050324001262005032400126NM 2005 3 24 P5CA0501322 120050212A5230 SKIN BOEING747 74746NF 13848BTNM CARGO DOOR DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 EA15451PA 30809 ON WALK AROUND FOUND PUNCTURE DAMAGE ON OUTERSKIN OF BULK CARGO DOOR. DAMAGE WAS .7500 ROUND IN DIAMETER 10 INCHES FROM FRONT EDGE, 6 INCHES FROM LOWER EDGE. REPAIRED PER SRM 52-00-01. COI 451-008 RAISED FOR INTERIM REPAIR. 2L74 4F RTA20WE 20050324001542005032400154EA 2005 3 24 QXEA200500194 120050123A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - RIGHT INBOARD SEAT RAIL, AT STATION X478 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-00-001-001-A01, REO 670-53-00-060, REV B AND HORIZON AIR EA R -53-266. 2L72 4F RTA21EA 20050324001562005032400156NM 2005 3 24 WRLA2005080 120050226A5340 ANGLE DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE OVERWING TANK CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11276 48632 DURING "C04" CHECK INSPECTION, FOUND OVERWING TANK REAR SPAR LOWER CHORD REINFORCE ANGLE SURFACE CORROSION AT STA 1376 BETWEEN X=37.5 AND X=-37.5 (LENGTH = 57"). 2L73 4F4 FRTA22WE E24NE 20050324001612005032400161NM 2005 3 24 WRLA2005019 120050131A5347 SEAT TRACK DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11273 48519 DURING "C2" CHECK FOUND CABIN SEAT TRACK CORROSION BETWEEN STA 858 AND STA 873 X=27.5. CUT AND REMOVED CORRODED SECTION BETWEEN STA 832 AND 909 X=27.5, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION AND SPLICE HAT. CONDITION CHECK SATISFACTORY REF MD11 SRM 53-70-00 FIG 1 REV 36 VOL I. 2L73 4F4 FRTA22WE E24NE 20050324001732005032400173SO 2005 3 24 C2XA05SH008 120050215A532014530644401 FLOOR SUPPORT EMB 145 EMB145ER 3260211SO FUSLEAGE DAMAGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714940 145033 SHV - DURING C-CHECK, THE LT OMEGA BEAM AT FRAME 48 HAS DAMAGED SEAT TRACK SCREW HOLE. 2L72 4F RTT00011AT 20050324002002005032400200EU 2005 3 24 05FDEA00583 120050317A5347 SEAT TRACK AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 MAIN DECK CARGO COMPT LEFT NR 3 SEAT TRACK, FR48, FR49.5, FR51.5, FR53.5, 4 EA AREAS OF CORROSION INSIDE SCALLOP HOLES AS MARKED. REMOVED AND REPLACED SEAT TRACK SECTION BETWEEN FRAME 50.5 TO 54 IAW A310-200 SRM 53-10-16. 2L72 4F RTA35EU 20050325000432005032500043EA 2005 3 25 SWIA200514753 120050309A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07953SW 7813 LEFT FLOORBEAM ANGLE AT FS 621.00 IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. CRACKED FLOOR SUPPORT REPAIRED IAW CRJ REO 601R-53-61-117 REV B. 2L72 4F RTA21EA 20050325000552005032500055EU 2005 3 25 05FDEA00603 120050318A5230 STRUCTURE AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 CORROSION FOUND UNDER THE NR 9 LATCH ROLLER FOR FWD CARGO DOOR. COMPLIED WITH EA 6-5310-86132. 2L72 4F RTA35EU 20050325000732005032500073WP 2005 3 25 DHL2005805521 120050308A534774529523 CARGO TRACK DOUG DC8 DC873F 302199FWP CARGO BAY DETERIORATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT NR 5 TRACK PLUG DETERIORATED AT STA 158.000. REMOVED DETERIORATED NR 5 TRACK PLUG IAW SRM 51-3-0 PG 1-2. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK PLUG IAW SRM 51-3-0 PG 1-2. TORQUED IAW SRM 51-3-1. 2L74 4F RT4A25 20050325001222005032500122EU 2005 3 25 05FDEA00418 120050308A5730 PANEL AIRBUS310 A310222 3930315EU RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 UPON REMOVAL OF LANDING AT RT WING HINGE PANEL ON L/E FOUND PANEL LANDING CRACKED REF N00915. REMOVED AND REPLACED PANEL LANDING IAW SRM 51-40-21 AND DRW A572-434548. 2L72 4F RTA35EU 20050328000072005032800007SO 2005 3 28 SWIA200514764 120050207A5315 FLOORBEAM EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 RIGHT FLOOR SUPPORT ANGLE AT FRAME 44-47 IS CORRODED. ITEM FOUND AT C-CHECK INSPECTION. SUPPORT ANGLE REPLACED IAW EMB 120 SRM 57-40-02, 57-25-00, 51-23-00. 2L72 4T RTA31SO 20050328000202005032800020SO 2005 3 28 SWIA200514777 120050207A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 LT AFT SEAT TRACK AT YL 479.00 IS CORRODED. (ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED SEAT TRACK IAW EMB 120 SRM 51-22-00, 51-40-02, 51-25-00. 2L72 4T4 TRTA31SO E20NE 20050328000542005032800054WP 2005 3 28 AALA20050192 120050303A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21297AA 49309 OVERHEAD EMERGENCY LIGHT AT ROW 20 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT AT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20050328000552005032800055WP 2005 3 28 AALA20050193 120050313A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217535A 49989 ATL FORWARD ENTRY AND FORWARD GALLEY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD LIGHTS AT FORWARD ENTRY AND FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2L72 4F A6WE 20050328000802005032800080 2005 3 28 2005F00040 420050303A6122DCFS290D7 GOVERNOR CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO RT ENGINE PROP SEIZED E DUFAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL273796C 1464 402B0803 WHILE IN CRUISE FLIGHT, THE RT ENGINE BEGAN TO LOSE RPM. THE PILOT PUSHED THE PROPELLER CONTROL LEVER ALL THE WAY FORWARD TO MAX RPM WITH NO CHANGE. THE PILOT DESCENDED AND MADE AN UNEVENTFUL LANDING. THE RT ENGINE QUIT ON ROLL OUT AND THE RT PROPELLER WENT INTO FEATHER. THE PROPELLER GOVERNOR WAS REMOVED AND APPEARED TO HAVE AN INTERNAL FAILURE. A SERVICEABLE GOVERNOR WAS INSTALLED AND OPS CHECKED OK. 1L72 3O3 O A7CE E8CE 20050328001072005032800107NM 2005 3 28 ASMF200503016 120050319A2410 CSD DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE RIGHT OVERHEATED W ASMFA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW23861LF 49826 AIRCRAFT RETURNED, TEMPERATURE IN RT CSD INCREASED HIGHLY AFTER TAKE OFF AND BATTERIES CIRCUIT BREAKER POPPED OUT. RT CSD WAS SERVICED IAW MM 24-10-1, TESTED CORRECT. DURING OVERNIGHT SERVICE CSD FILTERS AND OIL WERE REPLACED IAW MM 24-10-01 AND CSD WAS SERVICED IAW MM 24-10-02. ADDITIONALLY, CIRCUIT BREAKER B1-146 WAS REPLACED AND BATTERIES CHARGER WAS TESTED IAW MM24-30-2, ALL CORRECT. 2L72 4F4 FRT E9NE 20050328001152005032800115NE 2005 3 28 ASMF200503014 220050314A720097980611 CONTROL VALVE BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE LT ENGINE FAILED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23806AM6983 4275 26273 726731 AIRCRAFT RETURNED TO PLATFORM AFTER ENGINES STARTED WITH CROSSED FEEDING, EICAS MESSAGES R HYD R SUR PRESS, R ENG REV CONE, L ENG REV CONE, L ENG FIRE LOOP 2, EPR DET LOOP 2 INCHES AND (RT ENGINE EPR OUT OF SERVICE) WERE SHOWN AND PNEUMATIC AUXILIARY POWER UNIT FAIL. THE ENGINES WERE TURNED OFF AND FIM 71-00-00 FIGURE 110, SHEET 1, CODE 352-17 AND 352-15 PROCEDURES WERE PERFORMED AND ENGINES WERE RESTARTED IAW MM 71-00-00, TESTED CORRECT. DURING OVERNIGHT SERVICE, THE SURGE CONTROL VALVE OF AUXILIARY POWER UNIT WAS REPLACED IAW MM 49-53-01, TESTED CORRECT. 2L72 4F4 FRTA2NM E17NE 20050328001162005032800116CE 2005 3 28 AL200501485 120050228A5340680501A BRACKET CESSNA206 U206G 2073356CE CONT O520 IO520F 17032SO FLOW TRANSDUCER BROKEN B HJBRK NONE O OTHER ININSP/MAINT 1 AL055428U450 U20605290 DURING SCHEDULED INSPECTION, FOUND MOUNTING BRACKET FOR FUEL FLOW TRANSDUCER INSTALLED IAW STC NR SE443GL CRACKED ON ALL FLANGES WITH ONE FLANGE BROKEN OFF COMPLETELY. 1H71 3O3 O A4CE E5CE 20050328001192005032800119NM 2005 3 28 SWAA050894 120050323A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727 E + 16, STR 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050328001202005032800120NM 2005 3 28 SWAA050895 120050323A55236959227 BUSHING BOEING737 7373H4 1384600NM RT ELEVATOR TAB WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29380SW 26587 DURING SCHEDULED C2 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR NR 1 TAB HINGE BOLT & BUSHING PER MM. 2L72 4F RTA16WE 20050328001212005032800121NM 2005 3 28 SWAA050896 120050323A3350101073 LENS BOEING737 7377H4 1384404NM R2 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29459WN 32497 R2 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LENS ASSY PER MM. 2L72 4F RTA16WE 20050328001222005032800122NM 2005 3 28 SWAA050897 120050323A53306545769 SKIN BOEING737 7375H4 138449DNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29510SW 24187 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 378, LBL 2. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050328001332005032800133 2005 3 28 CHQA200500060 420050322A34177014700626 ADC EMB 135 EMB135LR 3260305SO COCKPT FAILED A CHQAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL11834RP 145696 DESCENT FL360 APPROX 2-3,000 FPM, PILOTS NOTICED HIGH WIND NOISE, 5 SEC LATER CAPTAIN'S AIRSPEED INDICATOR ROSE 130 KTS TO 285 KTS. RECEIVED HIGH SPEED WARNING & SPS ADVANCE CAUTION MESSAGE. ACFT LEVELED OFF, AFTER LEVEL OFF BOTH AIRSPEED INDICATORS BEGAN WORKING NORMALLY AS COMPARED TO THE ISIS. DESCENT NORMAL UNTIL 13,000 FT, SMOKE BEGAN TO FILL COCKPIT FROM BEHIND AVIONIC PANELS. EMERGENCY DECLARED. SMOKE CLEARED WITHIN 5 MINUTES AND ACFT LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED ALL AVIONICS PANELS ON GLARESHIELD & WIRES ON WINDSHIELD, NO DEFECTS NOTED. A PITOT STATIC TEST WAS PERFORMED. SYS 2 FOUND TO BE LOOSING 12 FT PER MINUTE. REMOVED & REPLACED NR 2 ADC COMPUTER, OPS CHECK GOOD. 2L72 4F RTT00011AT 20050328001342005032800134SO 2005 3 28 CHQA200500061 120050322A2611FDS765A2 SMOKE DETECTOR EMB 145 EMB145LR 3260212SO CABIN MALFUNCTIONED A CHQAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL11971RP 145426 FLIGHT 3223 PHL-ABE - AFTER DEPARTURE AT APPROXIMATELY 500 FT MSL RECEIVED AN EICAS MESSAGE LAV SMOKE. THE FLIGHT ATTENDANT INVESTIGATED THE LAVATORY AND INFORMED THAT ALL WAS NORMAL IN THE LAVATORY WITH NO INDICATIONS OF FIRE OR SMOKE AT ALL. PHL OPERATIONS WAS NOTIFIED AND THE AIRCRAFT RETURNED TO THE FIELD NON-EMERGENCY LANDING. THE AIRCRAFT WAS VECTORED FOR A VISUAL APPROACH TO RUNWAY 27R AND LANDED UNEVENTFULLY. THE AIRCRAFT WAS FERRIED TO IND WHERE MAINTENANCE REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR. ENGINE RUNS WERE PERFORMED WITH NO DEFECTS NOTED IAW EMB 145 AMM 26-14-01. 2L72 4T RTT00011AT 20050711000112005071100011CE 2005 7 11 DXTA200500818 120050704A3350 LIGHT CESSNA500 560CESSNA 2076750CE CABIN MALFUNCTIONED E DXTAK NONE N FALSE WARNING ININSP/MAINT 1 GL07341QS 5600341 EMERGENCY LIGHTS WILL NOT EXTINGUISH DUE TO A HARD LANDING. ITEM IS UNDER INVESTIGATION. 2L72 4F RTA22CE 20081024 NM 2008 10 24 DL76G081358 120050630A5751 SKIN BOEING767 7673P6 1385105NM LT AILERON DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27156DL 25354 SPARE REMOVED FROM A/C 1506. LT OTBD AILERON UPPER SKIN, LOWER SKIN, CORE AND TAILING EDGE WEDGE DAMAGED AT WS 1025. A NEW SECTION OF CORE WAS INSTALLED, UPPER AND LOWER SKINS REPAIRED WITH REPAIR PLIES AND ADDED PLIES AND TRAILING EDGE WEDGE SPLICED IN. 2L72 4F RTA1NM 20050323002012005032300201NM 2005 3 23 SWAA050765 120050312A33507003661 BALLAST BOEING737 7375H4 138449DNM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29502SW 24179 DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST ASSY PER MM. 2L72 4F RTA16WE 20050324000122005032400012EA 2005 3 24 QXEA200500189 120050124A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - RIGHT INBOARD SEAT RAIL, AT STATION X396, HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01, REO 670-53-00-060, REV B. AND HORIZON AIR EA R-53-266. 2L72 4F RTA21EA 20050324000292005032400029CE 2005 3 24 DELA200500003 120050214A750067469 GASKET LEAR 55 55LEAR 5170702CE BLEED AIR DUCT LEAKING E DELAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03903JC 081 RIGHT ENGINE FIRE WARNING ILLUMINATED IN FLIGHT AT FL250. AFM PROCEDURES FOLLOWED, THROTTLE RETARDED TO IDLE AND WARNING CEASED. THROTTLE SLOWLY RETURNED TO CRUISE POWER WITHOUT INCIDENT. MAINTENANCE FOUND LEAKING BLEED AIR PIPE GASKET NEAR PYLON FIRE DETECTION LOOP. GASKET WAS REPLACED AND GROUND RUN, LEAK CHECKS AND OPERATIONAL CHECKS SATISFACTORY. 2L72 4F A10CE 20050324000682005032400068NM 2005 3 24 WRLA2005020 120050131A5313 LONGERON DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11273 48519 DURING "C2" CHECK, FOUND CORROSION ON LONGERON L46L BETWEEN STA 5-73 AND STA 5-93. CUT AND REMOVED CORRODED SECTION BETWEEN STA 5-63 AND 5-103, CUT FRAME STA 5-73 TO STA 5-93 TO PROVIDE ACCESS FOR REMOVAL/INSTALLATION OF LONGERON L46L. FABRICATED NEW LONGERON SECTION FROM 1D0865T, 7150-T61511 EXTRUSION, FABRICATED LONGERON SPLICE FITTING FROM 7150-T61511 EXTRUSION PER MD11 SRM 53-10-00 VOL I. INSTALLED REPAIR PARTS. FABRICATED FRAME REPAIR PARTS AND HEATED THE REPAIR PARTS TO T6. CONDITION CHECK SATISFACTORY REF MD11 SRM 53-30-00 VOL I. 2L73 4F4 FRTA22WE E24NE 20050324001632005032400163NM 2005 3 24 ASMF200503009 120050312A71105930645509 NOSE COWL DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE RIGHT DAMAGED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23831LF10043 53050 716778 DURING TRANSIT CHECK, DETECTED DAMAGE IN RIGHT ENGINE NOSE COWLING BY FOREIGN OBJECT DAMAGE WITH LIP DENT DEPTH OF 0.150 PER 1 DIAMETER AT 03:00 POSITION. AIRCRAFT WAS SENT TO THE HANGAR AND NOSE COWLING WAS REPLACED IAW MM 71-10-01 PAGE 201, ALL CORRECT. 2L72 4F4 FRT E9NE 20050325000462005032500046NM 2005 3 25 05FDEA00614 120050321A5710 STIFFENER BOEING727 727200 138407ENM FUEL CELL CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 RIGHT WING INTERNAL FUEL CELL UPPER STIFFENER NR 9 IS CRACKED AT WS 656.5. REPAIRED PER E.A. 7-5710-86251. 2L73 4F RTA3WE 20050325000712005032500071NM 2005 3 25 QXEA200500427 120050129A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFTHAND WING, LEFTHAND FUEL PANEL REBATE AT 522AT HAS CORROSION AROUND SCREW HOLES, TOP SURFACE. REPAIRED IAW Q400 SRM SUB TASK 57-10-30-940-002. 2H72 4T RTA13NM 20050325001032005032500103EA 2005 3 25 COMA0560195 120050321A2750 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS SYS ILLUMINATED A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01470CA 7650 FLIGHT 5393 FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20050325001212005032500121EU 2005 3 25 05FDEA00417 120050308A5347 SEAT TRACK AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 MDCC NR 4 SEAT TRACK RT OF CENTER FROM FR 16 TO FR 19 CORRODED REF N00517. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-21. 2L72 4F RTA35EU 20050325001242005032500124EU 2005 3 25 05FDEA00420 120050308A5347 SEAT TRACK AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25446FE 224 MDC NR 4 SEAT TRACK RT OF CENTER AT FR19 ON I/B SPLICE HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED SPLICE ANGLE AT FR19 IAW SRM 51-40-21. 2L72 4F RTA35EU 20050325001262005032500126NM 2005 3 25 SWAA050781 120050314A53206546833 WEB BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29605SW 27956 DURING SCHEDULED D-CHECK, FOUND 2 EA FLOOR WEB CRACKS BETWEEN BS 188 TO BS 196, LBL 29 & RBL 29, WL 208. REMOVED AND REPLACED WEB SECTION PER SRM. 2L72 4F RTA16WE 20050325001352005032500135NM 2005 3 25 QXEA200500386 120050124A5340 STOP FITTING BOMBDRDHC8 DHC8401 1390041NM ZONE 200 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - AFT FUSELAGE - AFT ENTRY DOOR SURROUND STRUCTURE FORWARD STOP FITTING GOUGED AT STATION 668.900 AND STRINGER 19P. 2H72 4T RTA13NM 20050328000522005032800052CE 2005 3 28 TZR2005F00001 120050304A3211509410 ATTACH FITTING CESSNA401 401A 207590DCE CONT O520 TSIO520E 17040SO MLG CRACKED E TZRAK NONE O OTHER ININSP/MAINT 1 SW05409TE8875 401A0118 THE LT AND RT MAIN LANDING GEAR HAD CRACKS ON THE BOSS AREA WHERE THE TORQUE LINKS ATTACH. THE CRACKS WERE ABOUT .2500 INCH LONG AND LACATED NEXT TO WHERE THE BOSS CONNECTS TO THE TUBE. (SW05200506155) (K) 1L72 3O3 O A7CE E8CE 20050328001942005032800194EA 2005 3 28 SWIA200514758 120050322A27508004301 DETECTOR CNDAIRCL600 CL6002B19 1900309EA UNIT-SKEW MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED TOTAKEOFF 1 NM07463SW2891 2891 7820 AFTER T/O, THE GEAR AND FLAP INDICATORS REMAINED ILLUMINATED ON ED1 FOR APPROX 20 MINUTES. GEAR AND FLAPS INDICATED NORMAL (UP & 0 DEGREES). REPLACED SKEW DETECTOR UNIT IAW MM 27-51-15, OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050328002002005032800200NM 2005 3 28 SWAA050881 120050322A21216454051 FAN BOEING737 7373H4 1384600NM COCKPIT FAULTY A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SW29602SW 27953 ELECTRICAL ODOR IN CABIN WHEN RECIRCULATING FAN ON. ODOR DISPENSES WHEN TURNED OFF. REMOVED AND REPLACED FAN PER MM. 2L72 4F RTA16WE 20050328002022005032800202NM 2005 3 28 SWAA050883 120050322A53116546533 FRAME BOEING737 7373H4 1384600NM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29395SW 27689 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, STR 24R. REPAIRED FRAME PER PAE ER. 2L72 4F RTA16WE 20050328002102005032800210NM 2005 3 28 SWAA050891 120050322A53306545765 SKIN BOEING737 7373G7 1384595NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29691WN 23781 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 10, STR 14R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050328002162005032800216NM 2005 3 28 SWAA050875 120050322A53306545774 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E + 6, STR 25R. REPAIRED SKIN PER SWA EA & SRM. 2L72 4F RTA16WE 20050328002182005032800218NM 2005 3 28 SWAA050877 120050322A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 948.5, L2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050328002212005032800221SO 2005 3 28 SWIA200514761 120050207A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 RIGHT OUTBOARD AFT SEAT TRACK CORRODED AT FR38 TO FR34 (SIDEWALL). ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK REPLACED IAW EMB 120 SRM 51-25-00, 51-22-00, 51-40-02. 2L72 4T RTA31SO 20050329000032005032900003WP 2005 3 29 ASAA0580133 120050227A5230 SKIN DOUG DC9 DC983 3022083WP CARGO DOOR BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 HV-CHECK, FORWARD CARGO BAY DOOR IS BENT AROUND DOOR HANDLE. REMOVED DAMAGED SECTION. INSTALLED REPAIR SCUFF PLATE. (M) 2L72 4F RTA6WE 20050329000062005032900006WP 2005 3 29 ASAA0580136 120050227A5230 SKIN DOUG DC9 DC983 3022083WP CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - HV-CHECK, MID CARGO BAY DOOR IS DENTED. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050329000102005032900010WP 2005 3 29 ASAA0580131 120050227A532199366391 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - HV-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050329000422005032900042CE 2005 3 29 S2YA05019 120050225A2750 SWITCH BEECH 1900 1900D 1154162CE TE FLAPS MALFUNCTIONED A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL1385SK UE85 FLT 1071 - SDF-MKE - AFTER TAKEOFF, THE CREW WAS UNABLE TO RAISE THE FLAPS, PERFORMED AIR TURN BACK TO SDF. THE FLAPS WHERE RETRACTED USING THE BYPASS SWITCH AND THE SYSTEM WAS MEL'D. THE MEL WAS CLEAR BY ADJUSTING THE RT FLAP SAFETY SWITCH AND REPLACING THE FLAP SWITCH ARM ASSEMBLY. (M) 2L72 4T RTA24CE 20050302001652005030200165NM 2005 3 2 USAA050075 120050101A5320 STIFFENER BOEING737 7373B7 1384580NM MLG WW CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19522AU49282 23857 PIT - FOUND STIFFENER CRACKED .75 INCH, MAIN LANDING GEAR WHEEL WELL BS 663.75 AT LBL 6.15. REPLACED STIFFENER PER EA 75002 AND BOEING DWG 65-45402. (M) 2L72 4F RTA16WE 20050324000622005032400062EU 2005 3 24 AWXA200500263 120050215A5315D5347209800000 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28647AW 762 MCN - MAJOR REPAIR - DURING 8-DAY CHECK, CORROSION WAS FOUND ON FLOORBEAM Y35 AT FS 64. MAINTENANCE REMOVED CORRODED FLOORBEAM Y35 AT FS 64; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW A320 SRM 51-49-00. 2L72 4F RTA28NM 20050324000662005032400066WP 2005 3 24 05FDEA00485 120050310A5310AJC7207181 DOOR FRAME DOUG DC10 DC1030 3023501WP ZONE 100 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25311FE 46871 C/W EA8-5310-55459 FUSELAGE-MAIN FRAME-AFT ENTRY DOOR JAMB REPAIR (P/N AJC7207- 181). CLOSING ACTION 03/10/05 C/W EA8-5310-55459. ON NO. S00017. 2L73 4F A22WE 20050324001162005032400116 2005 3 24 DJFA2005057 420050210A3425 DISPLAY BEECH MU300 400A 1155402CE COCKPIT MALFUNCTIONED E DJFAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA23792TA RK264 SHORTLY AFTER TAKEOFF CREW NOTICED AN INCREASING TREND OF A BURNING ELECTRICAL SMELL. AFTER APROXIMATELY 15 MINUTES THE NR 2 PRIMARY FLIGHT DISPLAY FAILED WITH A "DISPLAY TEMP" FLAG. THE APPROPRIATE CIRCUIT BREAKER WAS PULLED, AND AIRCRAFT RETURNED TO KAPA WITHOUT FURTHER INCIDENT. MAINTENANCE VERIFIED THE FAULT AND FOUND LOW AIR FLOW TO THE NR 2 PRIMARY FLIGHT DISPLAY. AFTER REMOVING AN INK PEN FROM THE COOLING FAN AIRFLOW WAS BACK TO A NORMAL STRONG FLOW. THE NR 2 PRIMARY FLIGHT DISPLAY WAS REINSTALLED, AND OPERATIONALLY CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4F RTA16SW 20050328001372005032800137SO 2005 3 28 C2XA05IA049 120050321A3397375921 CONNECTOR EMB 145 EMB145XR 3260214SO EMERGENCY SIGN LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2734110 145658 IAH - FLIGHT 2339, DURING POSTFLIGHT INSPECTION THE CREW REPORTED THE EMERGENCY EXIT LIGHT IN THE EXIT ROW TO BE INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR TO THE EMERGENCY LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THIS PART IS NOT SERIALIZED, AND TIMES ARE NOT AVAILABLE. 2L72 4F RT 20050328001392005032800139NM 2005 3 28 UPS05444179 120050314A5347 SEAT TRACK BOEING747 747121 1384871NM FUSLEAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D- BS 2040 - 2140 LBL 65 SEAT TRACK FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.050 X 1 X 10 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20050328001472005032800147NE 2005 3 28 BA05007 220050322A752052G225 SOLENOID AIRBUS330 A330323 3930335EU PWA 4168 PW4168A NE RT ENGINE FAILED A USAAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CLCLIMB 1 EA19670UW 315 733501 AFTER TAKEOFF, CREW RECEIVED MULTIPLE ECAM WARNINGS: ENGINE NR 1 BLEED LOW TEMP, APU AFT FUEL PUMP, PACK NR 2 AIR INLET FLAP ACTUATOR FAIL, PACK 2 INLET PRESSURE SENSOR AND NAC COOL VALVE FAILURE. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RESET THE SDAC'S AND FWC'S AND PERFORMED AN ENGINE RUN. THE BLEED AND PACK PROBLEMS DID NOT RETURN. HOWEVER, THE PACK INLET PRESSURE SENSOR IS TARGETED FOR TROUBLESHOOTING. THE APU AFT FUEL PUMP PROBLEM COULD NOT BE DUPLICATED. MAINTENANCE REPLACED THE RIGHT TVBC AIR VALVE. SUBSEQUENTLY, THE AFT FUEL PUMP AND THE RIGHT PACK INLET FLAP ACTUATOR WERE REPLACED. 2L72 4F4 FRTA46NM 20050328001602005032800160NM 2005 3 28 UPS05544196 120050222A5347 CARGO TRACK BOEING757 75724APF 1384969NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01439UP 25470 CORROSION AROUND ALL RT CARGO TIE DOWNS IN FWD CARGO BAY BS 620 820 RBL 25. BLENDED CORROSION IN 11 AREAS TO BE OUT OF LIMITS PER SRM 53-00-53-1 FIG 101. BLENDED AREAS BS 620-BS 820 RBL 25. 2L72 4F RTA2NM 20050328001682005032800168SO 2005 3 28 C2XA05SD017 120050323A335066903 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714558 145598 SDF - FWD FRONT EMERGENCY LIGHT STRIP INOP. REMOVED AND REPLACED EMERGENCY LIGHT STRIP, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2L72 4T RTT00011AT 20050328001762005032800176NM 2005 3 28 AALA20050217 120050228A5313 LONGERON BOEING767 767323 1385205NM FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21357AA 24038 AFW - RIGHT HAND UPPER LONGERON WEB AT STRINGER 12 RIGHT JUST FORWARD OF STATION 1809 CRACKED. CUT OUT DAMAGED WEB AT APPROXIMATELY STATION 1798 AND FABRICATED A REPAIR WEB FROM .032 7075T6 CLAD. DOUBLER FROM .040 7075T6 CLAD AND FILLER FROM 0.080 7075T6 AND MACHINE SPLICE. ALODINE AND PRIME ALL ALUMINUM SURFACES PER 767 SRM. INSTALLED WEB SPLICES WITH BMS595 SEALANT AND INSTALLED BACR15FTC7K6 AT ALL RIVET LOCATIONS AND BACB30VT OR BACB30NX AT ALL HIL OK LOCATIONS IN TRANSITION FIT. 2L72 4F RTA1NM 20050328001772005032800177NM 2005 3 28 AALA20050219 120050311A1430 FASTENER BOEING767 767323 1385205NM WING FUEL TANK CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21357AA 24038 AFW - SEVEN LOCK FASTENER COLLARS CRACKED INSIDE FUEL TANKS AT WING STATION 261.2 LEFT HAND 394.2 LEFT HAND, 308.1 RT, 798.2 RIGHT HAND. REPLACED SEVEN EACH LOCK FASTENER COLLARS. NO LOOSE OR LEAKING LOCK FASTENERS AFTER REPLACEMENT OF COLLARS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050328001802005032800180NM 2005 3 28 AALA20050214 120050323A3397 WIRE BOEING757 757223 1384957NM EMERGENCY LIGHT BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21601AN 27052 DFW - AFT LOWER RIGHT HAND LAVATORY EMERGENCY FLOOD LIGHT WITH ARROW IS INOPERATIVE. REPAIRED BREAKS IN FEED WIRES WITH ENVIRONMENTAL SPLICES FOR AFT LOWER RIGHT HAND LAVATORY FLOOD LIGHT WITH ARROWS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20050328001872005032800187NE 2005 3 28 IXXA0500025O 220050322A72009026M70G01 ENGINE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C1 13802NE NR 3 FLAMED OUT A IXXAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SW11605AL385354668 46106 692502 ON CLIMB NR 3 ENG FLAMED OUT 32,000 FT, NO AUDIBLE/VISUAL ENG STALL OR VIBRATION. WEATHER VMC THROUGHOUT CLIMB. ENG FLAMED OUT N1 30%, N2 15% & OIL PRESSURE 3 PSI. GEN WENT OFF LINE, IGNITION NOT ON. FUEL CONFIG NORMAL, FUEL TEMP TANK -5C & FUEL PRESSURE AFTER FLAMEOUT 7 PSI ENG MOTORING 18% N2. ATTEMPTED RESTART AFTER RUNNING ABNORMAL ENGINE CHECKLIST. RECYCLED FIRE HANDLE, ATTEMPTED RESTART DESCENDING 21,000 FT, STARTER RESET & ALL 4 CROSSFEEDS IN POSITION. ENG RESTARTED 17,000, PARAMETERS NORMAL. LANDED WITH ALL 4 MOTORS RUNNING AND NO FURTHER PROBLEMS THROUGHOUT FLIGHT. MX PERFORMED CFM MM 71-00-00 FAULT 51, T/S TREE, PERFORMED POWER RUN. ENGINE INDICATIONS NORMAL, NO DEFECTS NOTED. 2L74 4F4 FRT4A25 E2GL 20050328001912005032800191SO 2005 3 28 SWIA200514755 120050322A2120 SMOKE EMB 120 EMB120ER 3260203SO CABIN DETECTED A SWIAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DEDESCENT 1 NM07236SW 120312 F/A REPORTED LIGHT SMOKE AND BURNING SMELL DURING DESCENT IN BOTH AUTO & LOW. RAN RIGHT AND LEFT PACKS ON GROUND FROM APU BLEED. NO SMOKE NOTED AT THIS TIME. 2L72 4T RTA31SO 20050324001062005032400106EU 2005 3 24 SSHA099270 120050210A6320704A34412009 HOSE AEROSPAS355 AS355* EU OIL COOLER FAILED E SSHAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP133607P 1249 PILOT MADE A PRECAUTIONARY LANDING DUE TO ILLUMINATION OF THE MGB PRESSURE LIGHT, INSPECTION REVEALED THE MGB OIL COOLER LINE HAD BURST AT THE JOINT BETWEEN THE HOSE AND THE METAL CRIMPEND END. THE HOSE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1G72 3U H11EU 20050324001172005032400117EA 2005 3 24 QXEA200500265 120050212A5330 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09609QX 10031 YYC - FUSELAGE EXTERIOR, CROWN STATION 773 AND STRINGER 2R HAS NICK ON FUSELAGE SKIN. REPAIRED IAW CRJ700 SRM 51-26-00-01-001-A01, 51-12-00-001-001-A01 AND SRM 51-25-01-001-001-A01. 2L72 4F RTA21EA 20050324001702005032400170EA 2005 3 24 SWIA200514641 120050224A2760C13045BA03 CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA SPOILER MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07742SK 10197 "RUD LIMIT FAULT" STATUS MSG CAME ON DURING FLIGHT. REMOVED AND REPLACED SSCU NR 1 AND PERFORMED OPERATIONAL CHECK IN IAW AMM 27-61-05. 2L72 4F RTA21EA 20050325000792005032500079WP 2005 3 25 05FDEA00610 120050321A5310 STRUCTURE DOUG DC10 DC1010 3022110WP FUSELAGE CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25571FE 47830 DURING INSPECTION FOUND AT STA 1741 STRUCTURE X=-17; X= 17 WITH CORROSION AND RETAINER X= 17 WITH CORROSION. REMOVED CORROSION FROM AFFECTED AREA PER SRM 51-21-01. PERFORMED CHECK LIMITS; THE MATERIAL REMOVED IS WITHIN LIMITS PER SRM 53-00-01. PROTECTED AREA PER SRM 51-21-01. 2L73 4F A22WE 20050325000892005032500089EA 2005 3 25 SWIA200514733 120050319A3397 WIRE CNDAIRCL600 CL6002C10 1390015EA EMERGENCY SIGN DAMAGED A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07744SK 10200 EMERGENCY LIGHT EXIT SIGN ON AFT OF BULKHEAD SEPARATING 1ST CLASS & COACH (RT SIDE) IS INOPERATIVE. REPAIRED WIRES ON EMERGENCY LGIHT EXIT SIGN. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050324001772005032400177EA 2005 3 24 SWIA200514499 120050122A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07954SW 7815 FS 621 FLOOR SUPPORT ANGLE LBL 42 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. FLOOR SUPPORT ANGLE REPAIRED IAW CRJ REO 601R-53-61-117 REV B. 2L72 4F RTA21EA 20050324001822005032400182EA 2005 3 24 SWIA200514741 120050110A5340 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07439SW 7578 FS 280 BL RIGHT INBOARD ANGLE BRACKET CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ 200 SRM 51-42-06 PG 4 & 18 & 51-42-20 PG 3 & 16. 2L72 4F RTA21EA 20050324001852005032400185EA 2005 3 24 SWIA200514726 120050319A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA TRIM STUCK A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07978SW 7953 REMOVE AND REPLACE F/O'S TRIM SWITCH DUE TO COMPLAINT OF STICKING. REPLACED F/O TRIM SWITCH AS REQUIRED PER CRJ MM 27-41-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050324001982005032400198EU 2005 3 24 05FDEA00581 120050317A3040 CONTROLLER AIRBUS300 A300F4605R 3930327EU WINDOW TEMP MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25660FE 759 AFTER TAKEOFF GOT RIGHT AND RIGHT LATERAL WINDOW HEAT FAULT. C/W ECAM AND RESET, FAULTED SECOND TIME AND REMAINED OFF FOR REMAINDER OF FLIGHT. NOTE: NO ECAM CHIME. REPLACED RIGHT WINDOW TEMP CONTROLLER, REF M/M 32-42-11. OPS CHECKS OK. MFG 6664157. 2L72 4F RTA35EU 20050325000302005032500030EA 2005 3 25 SWIA200514746 120050307A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07442SW 7609 MAIN FUSELAGE FS 280 LBL 9.0 LOWER FLANGE CRACKED ON TRANSVERSE BEAM. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR IAW CRJ REO 601R-53-11-138 REV NC. 2L72 4F RTA21EA 20050325000322005032500032EA 2005 3 25 SWIA200514748 120050307A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07442SW 7609 FUSELAGE PULLEY INTERCOSTAL HAS A PREVIOUS REPAIRED CRACKED ANGLE FS 484.00 LBL 36.0. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ REO 601R-53-41-059 REV A. 2L72 4F RTA21EA 20050328000122005032800012NM 2005 3 28 72300085 120050315A5313 STRINGER BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1.5 X 18 INCH AREA OF CORROSION ON STRINGER. 2L73 4F4 FRTA3WE E2EA 20050328000142005032800014SO 2005 3 28 SWIA200514771 120050207A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO PWA 118 PW118 NE FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 SEAT RAIL, LT OB CORRODED IN SEVERAL SPOTS AROUND THE SCREW HEADS. FR 15A AND FR32. (ITEM FOUND AT C-CHECK INSPECTION.) SEAT TRACK REPLACED IAW EMB 120 SRM 51-22-00, 51-25-00, 51-40-02. 2L72 4T4 TRTA31SO E20NE 20050328000572005032800057WP 2005 3 28 ASMF200503008 120050309A2910 SERVO VALVE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE HYD SYSTEM LEAKING W ASMFK NONE K FLUID LOSS ININSP/MAINT 1 SW23753RA 49587 DURING TRANSIT CHECK WAS DETECTED HYDRAULIC LEAK IN THE DUAL SERVO VALVE OF LT WHEEL WELL . THE DUAL SERVO VALVE AND HYDRAULIC LINES WERE ADJUSTED IAW MM 32-43-03, TESTED CORRECT. 2L72 4F4 FRTA6WE E9NE 20050328000682005032800068CE 2005 3 28 2005F00039 120050308A531057111451 DOOR FRAME CESSNA414 414A 2075907CE CONT O520 TSIO520NB 17040SO FUSELAGE CRACKED D LZ2RK NONE O OTHER ININSP/MAINT 1 GL274057C3000 414A0848 LOWER DOOR FRAME CRACKING BY THE REAR HINGE. 1L72 3O3 O A7CE E8CE 20050328000812005032800081 2005 3 28 2005F00041 420050303A6122DCFS290D7 GOVERNOR CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO ZONE 600 SEIZED E DUFAO OTHER R PARTIAL RPM/PWR LOSS CRCRUISE 1 GL273796C 1464 402B0803 WHILE IN CRUISE FLIGHT, THE RT ENGINE BEGAN TO LOSE RPM. THE PILOT PUSHED THE PROPELLER CONTROL LEVER ALL THE WAY FORWARD TO MAX RPM WITH NO CHANGE. THE PILOT DESCENDED AND MADE AN UNEVENTFUL LANDING. THE RT ENGINE QUIT ON ROLL OUT AND THE RT PROPELLER WENT INTO FEATHER. THE PROPELLER GOVERNOR WAS REMOVED AND APPEARED TO HAVE AN INTERNAL FAILURE. A SERVICABLE GOVERNOR WAS INSTALLED AND OPS CHECKED OK. 1L72 3O3 O A7CE E8CE 20050329000432005032900043NM 2005 3 29 USAA050330 120050216A5322 SHEAR TIE BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US 24560 PIT - FOUND SHEAR TIE CRACKED .5 INCH, STRINGER 2R STATION 578. REMOVED AND REPLACED WITH NEW PART PER SRM 51-40-02. (M) 2L72 4F RTA16WE 20050329000452005032900045NM 2005 3 29 USAA050303 120050223A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US40275 24841 CLT - FOUND FLOORBEAM CORRODED 10.9 INCHES BY 2 INCHES, STATION 328 ENTIRE T-CAP. INSTALLED T-CAP REPAIR PER SRM 53-10-51. (M) 2L72 4F RTA16WE 20050329000532005032900053NM 2005 3 29 USAA050335 120050223A53151137215 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US40959 24560 PIT - FOUND FLOORBEAM CORRODED 8 INCHES, STATION 312. CORROSION LEVEL 1, TASK C53-107-01. REMOVED AND REPLACED PER SRM AND IPC 53-4200 FIG 2. (M) 2L72 4F RTA16WE 20050329000652005032900065NM 2005 3 29 USAA050305 120050224A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19387US54352 22959 CLT - FOUND SKIN CRACKED 3.375 INCH STATION 883 STRINGER 25R. INSTALLED DOUBLER IAW SRM 53-00-01. (M) 2L72 4F RTA16WE 20050328001122005032800112SO 2005 3 28 X6PA200500001 120050115A1430 BOLT PIPER PA32 PA32300 7103212SO LYC O540 IO540* 41532EA SEAT BACK BROKEN E X6PAK NONE O OTHER ININSP/MAINT 1 SO33631BW 327340041 PILOT'S SEAT BACK ADJUST BOLTS BROKE, ALLOWING SEAT BACK TO RECLINE. 1L71 3O3 O A3SO 1E4 20050328001242005032800124NM 2005 3 28 SWAA050899 120050323A33506574550 LIGHT BOEING737 7373Q8 1384670NM L2 DOOR BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER SRM. 2L72 4F RTA16WE 20050328001292005032800129NM 2005 3 28 UPS05444175 120050313A5347BAC15201566 SEAT TRACK BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C, M/D- BS 1920 - 2040 LBL 95 SEAT TRACK & FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.045 X 1 X 3 INCH, EXCEED SRM 53-10-01 FIG 1 LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9. 2L74 4F A20WE 20050328001402005032800140NM 2005 3 28 UPS05444180 120050314A5315BAC1505101047 FLOORBEAM BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE: C M/D- BS 1500 RBL 83-89 FLOORBEAM UPPER CHORD LWR SURFACE CRACKED CRACK, LENGTH .375 INCH. FLOORBEAM REPAIRED AS PER SRM 51-40-04 FIG 1. 2L74 4F A20WE 20050328001452005032800145NM 2005 3 28 UPS05444185 120050313A5320 WEB BOEING747 747121 1384871NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D- STA 1220 LBL 116-118 BELOW FLOOR SUPPORT WEB CRACKED, LENGTH 2 INCHES. FLOOR SUPPORT WEB REPAIRED AS PER SRM 51-40-02 FIG 1. 2L74 4F A20WE 20050328001532005032800153NM 2005 3 28 UPS05444187 120050313A534065B386001427 STRINGER CLIP BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D- BS 1960 LT STR 2L TIE CLIP CRACKED, LENGTH .375 INCH. TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9 & SRM 51-30-02. 2L74 4F A20WE 20050328001632005032800163 2005 3 28 BB05021 420050322A2565 LIGHT BOEING767 7672B7 1385107NM ESCAPE SLIDE INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19651US PA0199 24764 BFM DURING ANNUAL SLIDE INFLATION CHECK, THE EMERGENCY LIGHTS DID NOT ILLUMINATE. MAINTENANCE REPLACED THE SLIDE. FURTHER INFORMATION PENDING. 2L72 4F RTA1NM 20050328001652005032800165NE 2005 3 28 DXTA200500640 220050321A7200 ENGINE CESSNA560 560XL 2076702CE PWA 545 PW545A NE RIGHT MALFUNCTIONED E DXTAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL07670QS 5605170 PCEDB0371 AFTER APPLYING TAKEOFF POWER, RIGHT EEC REVERTED TO MANUAL MODE, ABORTED TAKEOFF. ITEM IS UNDER INVESTIGATION. 2L72 4F4 FRTA22CE E00059EN 20050328001692005032800169SO 2005 3 28 153303132005 120050313A32501159SCH4023 SHUTOFF VALVE GULSTMG1159 GIV 3980115SO NLG STEERING FAILED E N93AO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO13467QS114 1533 NWS FAILED PRIOR TO TAXI. 2L72 4F RTA12EA 20050328001712005032800171NM 2005 3 28 AALA20050212 120050320A3350 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21785AN 30005 DFW - FIRST CLASS SEAT EMERGENCY ESCAPE PATH LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS SEAT EMERGENCY ESCAPE PATH LIGHT AT RT NR 1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050324001342005032400134NM 2005 3 24 TSAA0529012 120050307A2910 LINE BOEING737 7372T4 1384492NM HYD SYSTEM LEAKING A TSAAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 WP13808AL 23445 LOST A SYSTEM HYDRAULICS ON SHORT FINAL. MAINTENANCE MET THE AIRCRAFT ON THE RUNWAY. MAINTENANCE REPLACED THE NOSE GEAR DOWN ACTUATOR LINE PER AMM 32-3-11. SERVICED HYDRAULIC SYSTEM TO FULL. LEAK CHECK OKAY. REPLACED THE NR 1 AND NR 2 CASE DRAIN FILTERS, LEAK CHECK OK PER AMM 29-11-91. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A16WE 20050324001552005032400155EA 2005 3 24 QXEA200500190 120050124A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09610QX 10033 YYC - RIGHT INBOARD SEAT RAIL, AT STATION X418, HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-00-001-001-A01, REO 670-53-00-060, REV B. AND HORIZON AIR EA R-53-266. 2L72 4F RTA21EA 20050324001652005032400165NE 2005 3 24 ASMF200503010 220050313A732176960615 FUEL CONTROL DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE RIGHT FAILED W ASMFO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SW23753RA9120 2761 49587 718196 AFTER LANDING RIGHT ENGINE FREQUENCY WAS BELOW 390 AND BUS WAS OFF, THE RIGHT ENGINE WAS STARTED AND PARAMETERS WERE VERIFIED; N2 STABILIZED IN 40 PERCENT AND BUSS WAS OFF. N2 WAS ADJUSTED TO 56 PERCENT BUT RIGHT ENGINE DID NOT STABILIZED. AIRCRAFT WAS SENT TO THE HANGAR AND THE FUEL CONTROL UNIT AND RELAY R2-8 WERE REPLACED IAW MM 73-20-01 AND WDM 73-23-01 RESPECTIVELY. ENGINES TRIM AND OPERATIONAL CHECK WERE PERFORMED IAW MM 71-00-00 AND MPCM 71-00-00, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20050325000092005032500009NM 2005 3 25 CALA0500083 120050322A5313BAC1498156 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2759302 23353 INSPECTION FOUND SKIN BULGING AT STA 360 MINUS 6 INCHES TO 360 WITH CORROSION ON STRINGER 25L. REPAIRED STRINGER IAW ECRA 5311-01219. 2L72 4F RTA16WE 20050325000602005032500060WP 2005 3 25 DHL2005805505 120050223A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 LEFT OUTER WING INBOARD L/E UPPER FORMER CRACKED 0.500, XFS 678.750. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. FABRICATED (2EA) ANGLE DOUBLERS (AL7075-T6 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLERS WITH FASTENERS IAW SRM 51-1-20D PG 9, SRM 51-1-21 PG 1. TORQUED IAW SRM 51-3-1 PG 2A. 2L74 4F RT4A25 20050325000972005032500097NM 2005 3 25 05FDEA00516 120050315A5322 SHEAR TIE BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25481FE 21463 CORROSION ON SHEAR TIE BS 950E, STR 26L. *S/D* REPAIRED PER SRM 53-10-4. 2L73 4F RTA3WE 20050328000092005032800009EA 2005 3 28 COMA0560201 120050323A301060059122223 SENSOR CNDAIRCL600 CL6002B19 1900309EA WING OVERHEAT MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01435CA 7473 FLIGHT 5060 RECEIVED A WING OVERHEAT WARNING DURING CRUISE FLIGHT. CREW DECLARED AN EMERGENCY AND RETURNED TO CVG. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED WING OVERHEAT SENSOR. 2L72 4F RTA21EA 20050328001752005032800175NM 2005 3 28 AALA20050216 120050323A3350 REFLECTOR BOEING767 767323 1385205NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21385AM 27059 DFW - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LIGHT REFLECTOR ASSEMBLY FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20050328001852005032800185NM 2005 3 28 P5CA0501331 120050320A783019600263 DOOR BOEING747 747283B 1384867NM PWA JT9 JT9D70A 52054NE THRUST REVERSER MISSING A P5CAK NONE O OTHER ININSP/MAINT 1 EA15921FT 21575 688856 ON POST FLIGHT NR 3 ENGINE REVERSER PANEL MISSING. ACCOMPLISHED INTERIM REPAIR PER SRM 51-00-04 AND SRM 51-40-16, ALSO GMM 3-17-1. TRANSFERRED TO C/O ITEM 921-179. 2L74 4F4 F A20WE E3NE 20050328001962005032800196NM 2005 3 28 DHL2005745006 120050325A2120 SMOKE BOEING727 727224 1384076NM CABIN DETECTED A DHLAGB O2 MASK DEPLOYED EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO01745DH 20665 SMOKE IN COCKPIT BEGAN SHORTLY AFTER INITIAL DESCENT INTO SLC. COMPLETED SMOKE SOURCE I.D. EMERGENCY CHKLST & AIR CON SYS SMOKE EMERGENCY CHKLST. SMOKE BEGAN TO DISSIPATE AFTER ENG 1 & 2 BLEEDS REVERSED. RAN NR 1, 2 & 3 ENGINES WITH BLEEDS & PACKS ON, NO EVIDENCE OF SMOKE OR FIRE. RAN ENGINES AT ALL PWR SETTINGS AND MIX VALVES AT ALL SETTINGS TO DUPLICATESMOKE COND, NO SMOKE NOTED EXCEPT FOR SLIGHT CARBON ODOR. INSPECTED AIR COND BAY AND BOTH PACKS AND FOUND LH WATER SEPERATOR COALESCER BAG FILTER CONTAMINATED WITH OIL AND CARBON RESIDUE. R AND R LH WATER SEPERATOR FILTER AND RAN PACKS WITH ENG AND APU BLEED AIR, SYST CKS GD. MX 2L73 4F A3WE 20050328002032005032800203NM 2005 3 28 SWAA050884 120050322A53116546539 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, LBL 64, WL 202. REPAIRED FRAME PER PAE ER. 2L72 4F RTA16WE 20050328002052005032800205NM 2005 3 28 SWAA050886 120050322A55116573782 SPAR BOEING737 7373Q8 1384670NM HORIZONTAL STAB CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29663SW 23256 DURING SCHEDULED D-CHECK, FOUND LT HORIZONTAL STAB, AFT SPAR, UPPER CHORD CORRODED AT STA 276.70. REPAIRED LT HORIZONTAL STAB PER SRM & SB. 2L72 4F RTA16WE 20050328002192005032800219NM 2005 3 28 SWAA050878 120050322A57536546435 SKIN BOEING737 7373H4 1384600NM LT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED C1 CHECK, FOUND LT WING INBOARD AFT FLAP T/E DELAMINATED. REPAIRED FLAP PER SRM. 2L72 4F RTA16WE 20050328002202005032800220NM 2005 3 28 SWAA050879 120050322A5310907822 FITTING BOEING737 7373H4 1384600NM L1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29625SW 27701 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR LOWER FUSELAGE HINGE BOX FITTING CRACKED. REMOVED AND REPLACED HINGE BOX FITTING PER SRM & SAM 326. 2L72 4F RTA16WE 20050329000022005032900002WP 2005 3 29 ASAA0580132 120050227A532199365451 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 HV-CHECK, CABIN FLOOR PANEL HAS CORRODED FASTENERS. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050329000112005032900011WP 2005 3 29 ASAA0580134 120050227A53305912494501 SKIN DOUG DC9 DC983 3022083WP FUSELAGE BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 HV-CHECK, FORWARD CARGO BAY DOOR CUTOUT IS GOUGED FORWARD OF UPPER DOOR STOP. REMOVED DAMAGE, AND INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050329000282005032900028WP 2005 3 29 ASAA0580124 120050227A53219936537501 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - HV-CHK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050329000392005032900039SO 2005 3 29 SIMA200506605 120050302A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21801AE 145469 DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUTOUT TO REMOVE THE CORROSION. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 28 CHAPTERS 53-21-10 FIG 201. (M) 2L72 4F RTT00011AT 20050329000402005032900040CE 2005 3 29 S2YA05015 120050211A3297 WIRE BEECH 1900 1900D 1154162CE NLG CORRODED A S2YAO OTHER J WARNING INDICATION CLCLIMB 1 GL1392SK UE92 FLT 1851 - GRR-MKE - AFTER TAKEOFF, THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AND THE INSTRANSIT LIGHTS REMAINED ILLUMINATED. THE CREW CONTINUED TO MKE WITH THE GEAR DOWN. MAINTENANCE INSPECTED THE SYSTEM AND FOUND A CORRODED JUMPER WIRE AT A325P1 IN THE NOSE WHEEL WELL. THE JUMPER WAS REPLACED AND THE GEAR OPERATIONALLY CHECKED GOOD. WITH NO FURTHER DISCREPANCIES NOTED THE A/C WAS RETURNED TO SERVICE. (M) 2L72 4T RTA24CE 20050329000412005032900041NE 2005 3 29 S2YA05014 220050210A751002ND362033 VALVE DORNERDO32 DO328300 NM PWA 306 PW306B NE ANTI ICE SYSTEM MALFUNCTIONED A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13359SK 3202 APPROXIMATELY 80 KNOTS RECEIVED AN ENGINE ANTI-ICE OVERHEAT AND A SINGLE WARNING CHIME. CREW ABORTED TAKEOFF AND MESSAGE CLEARED DURING ROLLOUT. CREW UNABLE TO DUPLICATE THE PROBLEM AND THE A/C WAS CLEAR TO LAUNCH. DURING FLT 2265, MKE-BNA, THE SAME PROBLEM OCCURRED. THE CREW MADE AN AIR TURN BACK TO MKE. MAINTENANCE REPLACED THE BLEED AIR SHUTOFF VALVE AND WITH ALL OPERATIONAL CHECKS WERE GOOD THE A/C WAS RETURNED TO SERVICE. LATER THAT DAY BEFORE FLIGHT 2127 - CLE-MKE, THE SAME PROBLEM OCCURRED. THE CREW ABORTED THE TAKEOFF AND AGAIN THE MESSAGE CLEARED AND WAS UNABLE TO BE DUPLICATED. ON RETURN TO MKE, MAINTENANCE INSPECTED THE RIGHT ANTI-ICE VALVE AND CONNECTOR, ALL OPERATIONAL CHECK WERE GOOD. (M)2H72 4T4 FRTA55NM E35NE 20050627000012005062700001EA 2005 6 27 SWIA200515087 120050520A2597 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA FLAP SCEW INOPERATIVE A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07905SW 7437 FLAP SKEW DETECTION SYSTEM INOPERATIVE. REPLACED CONNECTOR 1J9CE IAW WDM 27-51-00. OPERATIONAL CHECK GOOD IAW MM 27-51-00. 2L72 4F RTA21EA 20051003001152005100300115EU 2005 10 3 2005UALA01005 120050921A5313 STRINGER AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE FR 55-57 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29415UA 475 STR 42L HAS CORROSION BETWEEN FR 55 AND FR 57. 2L72 4F4 FRTA28NM E40NE 20060210000072006021000007SO 2006 2 10 MASA200500619 120050807A3350 SWITCH EMB 145 EMB145LR 3260212SO ALLSN AE300 AE3007A GL EMRG LIGHT SYS NOT CLOSED A MASAK NONE O OTHER NRNOT REPORTED 1 SW07853MJ 145464 ASH 2674 GSP. FIRST FLOOR EMERG PATH EXIT LIGHT WILL NOT ILLUMINATE. CONTRACT MX PLACED EMERG LIGHT SW TO ARM FOR CHARGING FOR 1 HOUR. OPS NML. NO OTHER DEFECTS NOTED. 2L72 4T4 FRTT00011ATTE6CH 20050801000822005080100082EA 2005 8 1 A6WA200540248 120050717A5246 DOOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE FUEL TANK DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31420AW 7640 RT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT FOR PANEL 640BB HAS FRETTING DAMAGE. 2 INCH LONG X .125 INCH WIDE. REPAIRED BY BLENDING AND TREATING DAMAGED AREA IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20050705000092005070500009EU 2005 7 5 USAA050691 120050518A5315D5347209300000 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSLEAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19716UW 1055 PIT - FOUND FLOORBEAM CORRODED 3 FT BY 3 INCHES, FLOORBEAM AT -Y31 BETWEEN FRAME 67-70. REPLACED FLOORBEAM PER AIRBUS DWG D53471815 AND TR 51-40-01. (M) 2L72 4F RTA28NM 20060609001132006060900113CE 2006 6 9 DBCA122DA 120050515A3230 CONTROL UNIT CESSNA650 650 2076802CE MLG FAILED E DBCAO OTHER O OTHER NRNOT REPORTED 1 GL13605SA 2744 6500152 AFTER DEPARTING, THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO DEPARTURE, LANDING WAS UNEVENTFUL. RECEIVING SPECIAL FLIGHT PERMIT DATED 8 MAY 06 FROM FSDO SW01. FERRIED AIRCRAFT, LANDING GEAR CONTROL REPLACED. OPERATION CHECKED GOOD. (K) 2L72 4F A9NM 20050324001432005032400143SO 2005 3 24 C2XA05SH010 120050215A531114527703001 FRAME EMB 145 EMB145ER 3260211SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714940 145033 SHV - DURING C-CHECK, SEVERAL GOUGES FOUND ON LEFT HAND EMERGENCY EXIT DOOR LOWER INTERNAL FRAME. 2L72 4F RTT00011AT 20050325000062005032500006NM 2005 3 25 QXEA200500417 120050128A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFTHAND WING LEFTHAND PANEL 523AT BOTTOM SURFACE OF PANEL PITTING AND FRETTING CORROSION AROUND PANEL ATTACH HOLES. REPAIRED IAW RD 8/4-57-421. 2H72 4T RTA13NM 20050325000642005032500064NM 2005 3 25 QXEA200500426 120050127A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFTHAND WING LEFTHAND FUEL TANK AT 521BT HAS CORROSION AROUND PANEL REBATE TOP SURFACE. REPAIRED IAW Q400 SRM 57-10-35-940-001. 2H72 4T RTA13NM 20050325000872005032500087NM 2005 3 25 QXEA200500429 120050127A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 600 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - RIGHT WING FUEL PANEL AT 621AT LOWER SURFACE HAS AREA OF CORROSION, AROUND SCREW HOLES. REPAIRED IAW Q400 SRM SUB TASK 57-10-35-940-001. 2H72 4T RTA13NM 20050325000952005032500095NM 2005 3 25 SWAA050873 120050321A56105893543129 WINDOW BOEING737 7373Q8 1384670NM COCKPIT ARCED A SWAAO OTHER O OTHER NRNOT REPORTED 1 SW29688SW 23254 ARCING OBSERVED ON L1 COCKPIT WINDOW IN TOP RT CORNER. WINDOW HEAT SWITCHED OFF. OUTER PANE L1 COCKPIT WINDOW CRACKED. REMOVED AND REPLACED L1 COCKPIT WINDOW AND HEAT CONTROLLER. 2L72 4F RTA16WE 20050325001082005032500108NM 2005 3 25 SWAA050867 120050321A3350101073 LENS BOEING737 7375H4 138449DNM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29512SW 24189 LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20050325001302005032500130NM 2005 3 25 SWAA050785 120050314A3350612825 BATTERY PACK BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29741SA 29277 DURING SCHEDULED MV2 CHECK, FOUND 2 EA EMERGENCY EXIT LIGHTS INOP IN CABIN & 1 EA EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20050328000592005032800059NM 2005 3 28 TZR2005F00000 120050104A3210400054001 TRUNNION PIPER PA60 PA60600 7106001NM LYC O540 IO540K1J5 41532EA HARTZLHCC3Y HCC3YR2 NE LT MLG CRACKED E TZRAK NONE O OTHER ININSP/MAINT 1 SW05604TE7533 600320118 LT MLG, TRUNION CRACKED AT TOP WHERE TUBE GOES INTO MOUNTING BOSS. (SW05200506154) (K) 1M72 3O3 ORTA17WE 1E4 5 CP25EA 20050328001412005032800141NM 2005 3 28 UPS05444181 120050313A5315BAC1505101045 FLOORBEAM BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D- BS 1580 RBL 83-96 FLOORBEAM UPPER CHORD CORROSION. CORROSION BLEND OUT 0.060 X 2 X 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. M/D BS 1580 RBL 83-96 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 1. 2L74 4F A20WE 20050329000762005032900076EA 2005 3 29 A6WA200540093 120050311A5414 SKIN CNDAIRCL600 CL6002B19 1900309EA NACELLE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31419AW 7633 DURING POST FLIGHT WALK AROUND, RIGHT ENGINE COWLING DISCOVERED POSSIBLY OPENED IN FLIGHT. DAMAGED NOTED. (M) REMOVED AND REPLACED DOOR INSTALL LOWER CORE COWL. OPS CHECK GOOD. (K) 2L72 4F RTA21EA 20050329000772005032900077SO 2005 3 29 SIMA200506606 120050302A532014525381003 FLOOR SUPPORT EMB 135 EMB135KL 3260302SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21801AE 145469 ABI - DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM AT FRAMES 23 AND 25 WERE FOUND CORRODED. BLENDED THE CORRODED AREAS TO REMOVED THE CORROSION AND PERFORMED NDT INSPECTION AND FABRICATED AN EXTERNAL DOUBLER FOR REPAIR. REPAIR DONE IAW EMB REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/0976, PARA 3 DATED FEB 24, 2005. (M) 2L72 4F RTT00011AT 20050329000792005032900079SO 2005 3 29 SIMA200506802 120050308A335066367 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21636AE 145160 DFW - FLT 3358 - DURING POSTFLIGHT, CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS BETWEEN ROWS 7 THROUGH 10 APPEARS TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT STRIP IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTT00011AT 20050329000922005032900092NM 2005 3 29 S2YA05010 120050201A21504067B000004 SHUTOFF VALVE DORNERDO32 DO328300 NM LT A/C PACK FAILED A S2YAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL13356SK 3163 FLT 2265 - MKE-GRR - DURING TAKEOFF, THE CREW GOT A LEFT PACK INOPERATIVE CAS MESSAGE, CONSULTED WITH MAINTENANCE BUT WERE UNABLE TO GET THE MESSAGE TO CLEAR. THE A/C RETURNED TO THE GATE. MAINTENANCE REPLACED THE LEFT HIGH PRESSURE VALVE (PRSOV) BUT THE PROBLEM REMAINED. MAINTENANCE THEN REPLACED THE OXYGEN/ECS PANEL AND ALL OPERATIONAL CHECKS WERE GOOD. WITH NO FURTHER DISCREPANCIES NOTED THE A/C WAS RETURNED TO SERVICE. (M) 2H72 4T RTA55NM 20050329000942005032900094EA 2005 3 29 A6WA200540095 120050313A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE GOUGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31407AW 7424 FOUND SKIN GOUGED AT PANEL B2AL ATTACH SCREW AT 1 O'CLOCK POSITION. BLENDED AREA, PERFORMED EDDY CURRENT AND TREATED BARE MATERIAL. (M) 2L72 4F RTA21EA 20050329001002005032900100NM 2005 3 29 S2YA05020 120050227A2621335000121 FIRE BOTTLE DORNERDO32 DO328300 NM LEFT DISCHARGED A S2YAFA ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13356SK 3163 MKE-BDL - DURING TAKEOFF, THE CREW RECEIVED A FIRE BOTTLE DISCHARGE LIGHT INDICATION. THE CREW PERFORMED AN AIR TURN BACK TO MKE. MAINTENANCE REPLACED THE LEFT FIRE BOTTLE AND WITH OPERATIONAL CHECKS GOOD THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T RTA55NM 20050329001072005032900107NM 2005 3 29 SWAA050900 120050326A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED C4 CHECK, FOUND 2 EA FUSELAGE CRACKS AT AFT PRESSURE BULKHEAD, BS 1016, STR 4L & BETWEEN STR 6R TO STR 7R. REPAIRED AFT PRESSURE BULKHEAD PER SWA EA. 2L72 4F RTA16WE 20050329001132005032900113NM 2005 3 29 SWAA050906 120050324A335070036611 BALLAST BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29426WN 29830 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST PER MM. 2L72 4F RTA16WE 20050330001702005033000170 2005 3 30 S2YA05007 420050120A34577015327905 GPS DORNERDO32 DO328300 NM PWA 306 PW306B NE AUTO PILOT INOPERATIVE A S2YAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL13355SK113322628 3124 SHORTLY AFTER TAKEOFF, THE CREW DECLARED AN EMERGENCY DUE TO THE SMELL OF SMOKE ACCOMPANIED BY WITH THE LIGHT RESEMBLANCE OF SMOKE IN THE COCKPIT. THE CREW MADE AN AIR-TURN-BACK. MECHANIC REPLACED THE GPS-300 FLIGHT DIRECTOR AND AUTO PILOT CONTROL PANEL. OPERATIONAL CHECK REVEALED THE AUTO PILOT NOW DID NOT WORK WITH THE NEW PANEL. THE AUTO PILOT FUNCTION WAS MELED. ON 01/23/05 THE MEL WAS CLEARED BY REPLACING THE GPS-300 PANEL AGAIN. WITH NO FURTHER DISCREPANCIES NOTED THE AC WAS RETURNED TO SERVICE. (K) 2H72 4T4 FRTA55NM E35NE 20050330001932005033000193NM 2005 3 30 72300095 120050323A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 3 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050330002312005033000231NM 2005 3 30 EIA2005041 120050222A5314 KEELBEAM BOEING747 747SR46 1384816NM FUSELAGE CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09478EV 21033 KEEL BEAM RIGHT LOWER CHORD CORROSION BS 1335-1345 WL 100 RBL 10. CORROSION REMOVED PER SRM 53-10-01, REPAIR PARTS FABBED AND INSTALLED PER ECRA 478-51-173-1. 2L74 4F RTA20WE 20050331000682005033100068NM 2005 3 31 05FDEA00684 120050328A5347AEA75791 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 MAIN DECK, SEAT TRACK 47.5 CORRODED AT STA 1531. CARRIED OUT REPAIR IAW SRM 53-70-00 VOLUME I FIGURE 1. 2L73 4F RTA22WE 20050331000782005033100078EA 2005 3 31 COMA0560207 120050326A3620356024310 SENSOR CNDAIRCL600 CL6002B19 1900309EA E/E BAY FAULTY A COMAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO01814CA 7387 FLIGHT 5138 RECEIVED A LEFT 14TH STAGE DUCT MESSAGE CLIMBOUT OF CAE, CREW DECLARED AN EMERGENCY, LEFT ENGINE WAS SHUT DOWN AND RETURNED TO THE FIELD, AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE 14TH STAGE HEAT SENSING ELEMENT. 2L72 4F RTA21EA 20050331001012005033100101SO 2005 3 31 SWIA200514791 120050325A5210 ROD END EMB 120 EMB120ER 3260203SO PAX DOOR OUT OF ADJUST A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07579SW 120347 MAIN CABIN DOOR VERY HARD TO OPEN & CLOSE. ADJUSTED 2 ROD ENDS AND LUBRICATED ALL MOVING PARTS AS NECESSARY. DOOR NOW OPERATIONALLY CHECKS GOOD. 2L72 4T RTA31SO 20050401000302005040100030NM 2005 4 1 USAA050357 120050222A552365C2638415A SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU LT ELEVATOR TAB DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US40959 24560 PIT - Q4 - EXT COMPOSITE SURFACE, .500 INCH AREA OF DELAMINATION, LT ELEVATOR TAB TOP IB CORNER. PREPARED DAMAGED AREA, INSTALLED REPAIR PLYS, HARDWARE, REFINISHED IAW SRM 55-20-01 AND 51-70-05. (K) 2L72 4F4 FRTA16WE E21EU 20050401000312005040100031NM 2005 4 1 USAA050359 120050218A5320 SUPPORT BRACKET BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US40959 24560 PIT - Q4 - BRACKETS, 1 INCH X 3 INCH CORROSION, 4 BRACKETS. CORROSION; LEVEL 1; TASK C53-107-02 THRESHOLD SUPPORT BRAKETS, FWD DOOR ENTRY FLOOR STRUCTURE. PARTS REPLACED IAW MFG DWG. (K) 2L72 4F4 FRTA16WE E21EU 20050404000032005040400003EU 2005 4 4 M7K2005F00000 120050316A2913704A44310027 PUMP UROCOPEC130 EC130B4 8680989EU TMECA ARRIELARRIEL2B NE HYDRAULIC SYS INOPERATIVE E M7KAK NONE O OTHER ININSP/MAINT 1 WP19804MH 3750 23072 DURING RUNUP, IT WAS NOTICED THAT HYDRAULIC PRESSURE WARNING FAILED TO EXTINGUISH UNTIL AIRCRAFT WAS RUN-UP ABOVE IDLE TO FLIGHT IDLE SPEED. SUBSEQUENT INVESTIGATION REVEALED NO FLUID RETURN TO THIS PUMPS RESERVOIR. REPLACEMENT OF THE PUMP CORRECTED THE PROBLEM. EXTERNALLY THE REMOVED PUMP APPEARED NORMAL. PUMP RETURNED TO MFG FOR INSPECTION. THIS IS A 2-PUMP HYDRAULIC SYSTEM. (K) 1G72 3U3 U H9EU E00054EN 20050404000482005040400048CE 2005 4 4 MXI2005F00002 120050309A212166082672 MOTOR LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP COCKPIT FAN FAILED E MXIAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 EA21804TF 404 THE COCKPIT FAN MOTOR FAILED AND CAUSED SMOKE TO COME OUT OF THE OVERHEAD AIR VENTS. AFTER REPLACEMENT IT WAS NOTED THE FAN MOTOR WAS VERY HARD TO TURN. THERE IS NO TIME CHANGE FOR THIS MOTOR LISTED IN CHAPTER 5. (EA21200504524) (K) 2L72 4F4 F A10CE E6WE 20050404000682005040400068WP 2005 4 4 K2D2005F00000 120050128A6410HTC500P3100101 BLADE HUGHES369 369E 4470707WP ALLSN 250C 250C20B 03013GL TAIL ROTOR DAMAGED E K2DAA UNSCHED LANDING D INFLIGHT SEPARATION CRCRUISE 1 WP13142MK2379 0187E REF: K2DA320J TAIL ROTOR BLADE ABRASION STRIP AND TIP CAP DEPARTED BLADE ASSY, INFLIGHT. (WP13200506018) (K) 1G71 3U3 U H3WE E4CE 20050404001102005040400110EU 2005 4 4 KBM2005F00038 120050202A6520350A33215300 BEARING SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE TAIL ROTOR WORN E KBMAK NONE O OTHER ININSP/MAINT 1 WP191188P448 2347 LAMINATED BEARING, WORN. REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050404001132005040400113WP 2005 4 4 DHL2005805582 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (2EA) MISDRILLED HOLES AT STA 1260.00 L-10R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-07-05, EO AST 050201 DATED 02-17-05. PERFORMED DETAIL VISUAL INSPECTION, NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST 050201, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001202005040400120WP 2005 4 4 DHL2005805626 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME (2EA) MISDRILLED HOLES AT STA 702.000 L-9L TO L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 02-25-05 EO AST 050203 DATED 02-18-05. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. PERFORMED DETAIL VISUAL INSPECTION NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD5-4) IAW EO AST050203 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001332005040400133WP 2005 4 4 DHL2005805565 120050321A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT L-12L HOLES (8EA) MISDRILLED BETWEEN FRAME STA 520.000 AND FRAME STA 540.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-15-05 EO AST 050216 DATE 03-02-05. PERFORMED DETAILED VISUAL INSPECTION NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST 050216, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050404001482005040400148NM 2005 4 4 05FDEA00635 120050325A5312 BULKHEAD BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25272FE 22037 LOWER CHORD OF BS 950 CANTED BULKHEAD IS CORRODED, RBL 23. REPLACED BS 950 LOWER CHORD PER SRM 51-40-3 & 51-30-2. 2L73 4F RTA3WE 20050404001522005040400152EU 2005 4 4 2005UALA00261 120050325A3610 DUCT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE BLEED AIR DISCONNECTED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29404UA 450 LT WING LEAK DISPLAYED ON UPPER ECAM. FOUND DUCT DISCONNECTED AT GROUND BLEED AIR CONNECTOR. RECONNECTED DUCT. 2L72 4F4 FRTA28NM E40NE 20050404001552005040400155EU 2005 4 4 05FDEA00637 120050325A5730A57350005201 SKIN AIRBUS310 A310203 3930313EU ZONE 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25401FE 191 PANEL LAND AT 650HB HAS 9 EA ELONGATED HOLES. REPAIRED 5 EA HOLES IAW A310-200 SRM 51-40-44 FIG 1. COMPLIED WITH EA 6-5710-87184 BY INSTALLING 4 EA REPAIR BUSHINGS FOR REMAINING 4 HOLES. 2L72 4F RTA35EU 20050404000112005040400011NE 2005 4 4 KBM2005F00011 220050203A7532 BLEED VALVE SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE ENGINE STICKING E KBMAK NONE O OTHER ININSP/MAINT 1 WP191188P 2347 BLEED VALVE STICKS, REMOVED AND REPLACED. (K) 1G71 3U3 UNCH9EU E19EU 20050404000872005040400087NE 2005 4 4 GAIA05013OP 220050303A7200C25455 AIR CLEANER BOEING727 727214 138407RNM PWA JT8 JT8D9 52048NE NR 1 ENGINE CRACKED A GAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07750US 21512 DURING CLIMBOUT THE LOWER AFT BODY OVERHEAT LIGHT CAME ON. THE AC RETURNED TO AIRPORT AND AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED THE NR 1 ENGINE AIR CLEANER DUE TO CRACKED FLANGES. LEAK CHECK AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (SW07200503890) (K) 2L73 4F4 F A3WE E2EA 20050404000982005040400098 2005 4 4 KBM2005F00046 420050321A3422103002201 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE DIRECTIONAL MALFUNCTIONED E KBMAK NONE O OTHER ININSP/MAINT 1 WP19345SH226 3345 TUMBLES IN FLIGHT. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050404001312005040400131WP 2005 4 4 DHL2005805623 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT Z-FRAME INBOARD FLANGE HOLES (2EA) MISDRILLED AT STA 1020.000 L-12 L-13L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05 EO AST 050205 DATE 02-21-05. CLEANED, TREATED AND PRIMED AREA (MISDRILLED HOLES) IAW SRM 51-1-8B. PERFORMED DETAILED VISUAL INSPECTION NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD6-4) IAW EO AST 050205 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050325001012005032500101EA 2005 3 25 SWIA200514735 120050317A2740 SWITCH CNDAIRCL600 CL6002B19 1900309EA PITCH TRIM INOPERATIVE A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07907SW 7511 F/O TRIM MOSTLY INOPERATIVE. REPLACED F/O'S PITCH TRIM SWITCH IAW CRJ MM 27-41-05. OPERATIONAL CHECKS GOOD. 2L72 4F RTA21EA 20050325001072005032500107 2005 3 25 SWAA050866 420050321A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20050325001092005032500109NM 2005 3 25 DHL2005781534 120050214A5330 SKIN BOEING727 727227 1384078NM FUSELAGE GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01781DH 21996 DURING A C-CHECK, 4 HAND FUSELAGE 4 E AREA IS GOUGED APPROX STA 720E (MARKED) STR 19L. REMOVED PREVIOUS AT LT/HAND FUSELAGE L/E AREA STA 720E STR 19L IAW B727 SRM 51-30-2. FABRICATED DOUBLER REPAIR MAT USED 2024T3 .071 PO 9001978 DIM 17 X 12 INCH AND 1 EA FILLER MAT USED 2024T3 .063 PO 9001684 DIM 10 X 17 INCH IAW B727 SRM 53-30-2 FIG 2 AND 53-30-3 FIG 14. ALODINED AND PRIMED AREA AND PARTS IAW 13 727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 53-30-3 FIG 14. THIS REPAIR IS CATEGORY-B. 2L73 4F A3WE 20050325001162005032500116NM 2005 3 25 05FDEA00511 120050314A5347AEA7579501 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25592FE 48550 MAIN DECK CARGO - SEAT TRACK CORRODED AT STA 1351 RT 76 INCHES. SEAT TRACK REPAIRED AS PER SRM 53-70-00 VOL 1 FIG 1, AT STA 1269 TO 1391. 2L73 4F RTA22WE 20050328000292005032800029CE 2005 3 28 02021105 120050311A324006111800 BRAKE CESSNA208 208B 2073701CE PWA PT6 PT6A114 52043NE RT MLG UNSERVICEABLE E HSYAD RETURN TO BLOCK C F.O.D. TXTAXI/GRND HDL 1 NM05963FE 208B0080 WHILE TAXIING OUT TO PERFORM A FLIGHT TEST REQUIRED FOR UNRELATED MAINTENANCE (STALL WARNING), THE PILOT EXPERIENCED A LOSS OF ABILITY TO STEER THE AIRCRAFT TO THE RT. UPON INSPECTION OF AIRCRAFT BY MAINTENANCE, THE RT MAIN BRAKE CALIPER WAS FOUND TO BE HANGING OFF THE AIRCRAFT BY THE BRAKE LINE. MAINTENANCE FOUND THAT THE GUIDE PINS HAD BEEN SHEARED OFF. CAUSE UNDER INVESTIGATION. REMOVED ALL AFFECTED PARTS AND REPLACED WITH SERVICEABLE COMPONENTS. HIDDEN DAMAGE INSPECTION CARRIED OUT WITH NO FURTHER DAMAGE FOUND. ALL SYSTEMS AFFECTED, OPS CHECKED SATISFACTORILY. 1H71 3T3 T A37CE E4EA 20050328001502005032800150NM 2005 3 28 UPS05244167 120050309A5230 SKIN BOEING727 72722C 138400FNM FWD CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE: C FWD CARGO DOOR CRACKED AT AFT UPPER FRAME BETWEEN LWR ATTACH BOLT FOR BALANCE MECHANISM. REPAIR CARRIED OUT IAW AAAE EO 2005-021-002. 2L73 4F A3WE 20050328001522005032800152NM 2005 3 28 UPS05244169 120050311A5740 FITTING BOEING727 72722C 138400FNM RT TRUNNION CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE:C EXTENSIVE CRACKING SROUND BOTH I/B B & C HOLES FOR A LARGE AREA OF THE RT TRUNNION FITTING ON RT REAR SPAR. REMOVED MLG FWD TRUNNION HOUSING ATTACHMENT FITTING ON REAR SPAR IAW SRM 51-30-2. REPAIR CARRIED OUT IAW SRM 51-30-2, DRAWING 65-19297 & AAA E EO 2005-021-001. 2L73 4F A3WE 20050328001982005032800198NM 2005 3 28 SWAA050880 120050322A3350BR2013 LIGHT BOEING737 7377H4 1384404NM FWD CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29402WN 29814 FWD CABIN EEPLS COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20050328001992005032800199SO 2005 3 28 SWIA200514770 120050207A5347 SEAT TRACK EMB 120 EMB120ER 3260203SO FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 RIGHT SEAT RAIL CORRODED IN SEVERAL SPOTS AROUND SCREW HEADS FROM FRAME 13A- FR.32 OUTBOARD SIDEWALL. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK REPLACED IAW EMB 120 SRM 51-25-00, 51-22-00, 51-40-02. 2L72 4T RTA31SO 20050328002152005032800215NM 2005 3 28 SWAA050874 120050322A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050328002172005032800217NM 2005 3 28 SWAA050876 120050322A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29355SW 25250 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 948.5, R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050329000092005032900009WP 2005 3 29 ASAA0580130 120050227A53219936639501 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - HV-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050329000142005032900014WP 2005 3 29 ASAA0580139 120050227A523059101573 SKIN DOUG DC9 DC983 3022083WP CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - HV-CHECK, AFT CARGO BAY DOOR IS DENTED. COLD-WORKED TO ORIGINAL CONTOUR, INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050329000342005032900034WP 2005 3 29 ASAA0580140 120050227A523059101573 SKIN DOUG DC9 DC983 3022083WP AFT CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - HV-CHECK, AFT CARGO BAY DOOR IS DENTED. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050329000542005032900054NM 2005 3 29 USAA050324 120050220A5315BAC1505100296 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US40959 24560 PIT - FOUND BEAM WITH CORROSION 48 INCH LONG SEVERAL AREAS, FS 312, UPPER CAP FLOORBEAM. CORROSION LEVEL 1, TASK C53-107-01. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-10-51, FIG 205. (M) 2L72 4F RTA16WE 20050328001722005032800172NM 2005 3 28 AALA20050211 120050320A3350 BATTERY PACK BOEING777 777223 1385213NM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21785AN 30005 DFW - EMERGENCY ESCAPE PATH LIGHT AT COACH R3 DOOR FORWARD AND AFT SEAL INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY ESCAPE PATH LIGHT AT COACH R3 DOOR FORWARD AND AFT SEAL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20050329000362005032900036EA 2005 3 29 A6WA200540101 120050316A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31413AW 7585 RIGHT INTERCOSTAL AT FS 484 AT RBL 36 CRACKED 1 INCH LONG. (M) PERFORMED A REPAIR AT FS484, RBL 36 BY CUTTING OUT DAMAGED AREA AND INSTALLING NEW ANGLE IAW REO. (K) 2L72 4F RTA21EA 20050329000442005032900044NM 2005 3 29 USAA050306 120050228A5754 SKIN BOEING737 7373B7 1384580NM NR 5 SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU50516 23705 CLT - FOUND NR 5 SLAT WITH 4 INCH CRACK, LOWER LE SKIN NR 5. INSTALLED REPAIR DOUBLER IAW SRM 57-43-01. (M) 2L72 4F RTA16WE 20050329000492005032900049NM 2005 3 29 USAA050328 120050223A5320 CHANNEL BOEING737 7374B7 1384702NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US40959 24560 PIT - FOUND CARGO FLOOR CHANNEL AND SUPPORT ANGLE WITH CRACKS, APPROX .5 INCH CRACKS, FS 500G, RBBL 6. MANUFACTURED AND INSTALLED CARGO FLOOR CHANNEL AND SUPPORT ATTACH ANGLE PER SRM 53-00-53. (M) 2L72 4F RTA16WE 20050329000582005032900058NM 2005 3 29 USAA050329 120050220A5320 ANGLE BOEING737 7374B7 1384702NM FUSLEAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US40732 24560 PIT - FOUND ANGLE CRACKED .25 INCH, S14R TO S15R AT BS 360 ANGLE BETWEEN STRINGERS. CUTOUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-00-07 FIG 207. (M) 2L72 4F RTA16WE 20050329000642005032900064NM 2005 3 29 USAA050309 120050218A5330 SKIN BOEING737 7373B7 1384580NM FUSELAGE CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND SKIN CHAFED .013 INCH BY .011 INCH DEEP BY 20 INCHES LONG, BS 867-887 LT/RT SIDE OF SKIN UNDER DORSAL FIN. CUT AREA OUT, INSTALLED FILLER, DOUBLER AND TRIPLER AND CHAFED STRAPS PER SRM 53-60-01 FIG 201 PAGE 241. (M) 2L72 4F RTA16WE 20050329000672005032900067NM 2005 3 29 USAA050307 120050222A575535759 SKIN BOEING737 7374B7 1384702NM NR 2 SPOILER CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19440US39212 24811 PIT - FOUND NR 2 SPOILER CRACKED .125 INCH, AND .5 INCH BY .5 INCH AREA DELAMINATED. REMOVED AND REPLACED PER M/M 27-61-11 AND 27-61-11 AND 27-61-51. (M) 2L72 4F RTA16WE 20050329000842005032900084NM 2005 3 29 UIEA200500014 120050308A541465B940512 SKIN BOEING747 7472D7B 1384803NM NR 2 PYLON CRACKED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15527MC 22471 DURING INSPECTION, NR 2 PYLON, CRACK DAMAGE WAS FOUND AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT NACELLE STATION 248. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW STEEL LOWER REPAIR ANGLE FROM NS 235 TO STA 254. THE RIB INSTALLATION AT NACELLE STATION 248 WAS MODIFIED TO ACCOMMODATE THE NEW STEEL LOWER REPAIR ANGLE INSTALLATION ON THE NR 3 STIFFENER. (M) 2L74 4F RTA20WE 20050329000862005032900086NM 2005 3 29 UIEA200500017 120050308A542065B941001 CAP BOEING747 7472D7B 1384803NM STRUT CHAFED A UIEAK NONE O OTHER ININSP/MAINT 1 EA15527MC 22471 DURING SCHEDULED MAINTENANCE, CHAFING MARK WAS FOUND ON THE LEFT SIDE OF THE SKIN ASSEMBLY AT NACELLE STATION 270. AFFECTED FASTENERS WERE REMOVED AND FASTENER HOLES WERE HFEC INSPECTED TO ENSURE CRACK AND DAMAGE FREE CONDITION. THE CHAFING DAMAGE WAS REMOVED BY BLENDING TO A SMOOTH CONTOUR. ENSURED MINIMUM MATERIAL REMOVED. THE BLENDED SURFACE WAS REFINISHED AND DESIGN TYPE OVERSIZE FASTENERS WERE INSTALLED PER SRM REQUIREMENTS. THE REPAIR CONFORMS TO DESIGN REQUIREMENTS. (M) 2L74 4F RTA20WE 20050711000312005071100031NM 2005 7 11 WRLA2005125 120050622A5510 STRUCTURE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE HORIZONTAL STAB CORRODED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277 48743 DURING C-04 CHECK, WHILE PERFORMING INSPECTION PER EO 02-5510-098, FOUND CORROSION IN HST LT BARREL NUT HOLE NR 36. 2L73 4F4 FRTA22WE E24NE 20050323001932005032300193WP 2005 3 23 AALA20050210 120050320A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW217532A 49924 DTW - OVERHEAD EMERGENCY LIGHTS AT ROW 6 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROW 6. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050323001972005032300197NM 2005 3 23 SWAA050764 120050313A53206517590 WEB BOEING737 7373L9 1384470NM COCKPIT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29657SW 23331 DURING SCHEDULED SPECIAL VISIT, FOUND FLOOR WEB CRACKED RT SIDE BETWEEN BS 188 & BS 196, WL 208. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20050323001992005032300199NM 2005 3 23 SWAA050754 120050311A276065463607 MIXER BOX BOEING737 7373A4 1384585NM LT WING W/W FAULTY A SWAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW29679AA 23291 AIR TURNBACK IMMEDIATELY AFTER TAKEOFF, NOTED HEAVY ROLL TO LT, ACCOMPANIED BY CONSIDERABLE RUMBLING. REQUIRED 5 UNITS OF RUDDER TRIM & UNKNOWN AILERON TRIM AT 1/2 YOKE DEFLECTION TO LEVEL WINGS. REMOVED AND REPLACED SPOILER MIXER & NR 3 SPOILER ACTUATOR PER MM. 2L72 4F RTA16WE 20050324000442005032400044SO 2005 3 24 C2XA05CL010 120050215A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714960 145100 CLE FLIGHT NR 2107, CREW REPORTED THAT THE GALLEY AND BULKHEAD EMERGENCY LIGHTS WERE INOP. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM, AND DID NOT FIND AND DEFECTS. SYSTEM OPERATIONALLY CHECKED GOOD. 2L72 4T RTT00011AT 20050324000712005032400071CE 2005 3 24 2003793 120050214A5330 SKIN BEECH 1900 1900D 1154162CE FUSELAGE CORRODED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03179GL UE179 DURING ROUTINE STRUCTURAL INSPECTION, CORROSION WAS FOUND ON INSIDE SKIN NEAR MAIN PAX DOOR HANDLE DOUBLER APPROX 2" BY 2" AREA. AREA REPAIRED, AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050324000852005032400085NM 2005 3 24 2005UALA00245 120050314A2613 OVERHEAT LOOP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE NR 1 ENGINE MALFUNCTIONED A UALAE ENGINE SHUTDOWN N FALSE WARNING DEDESCENT 1 WP29935UA 26663 SHUT DOWN NR 2 ENG DUE TO OVERHEAT INDICATION. CREW REPORTED NR 2 ENG OVERHEAT LIGHT CAME ON WITH NO ABNORMAL ENGINE INDICATION. OVERHEAT LIGHT STAYED ON AFTER THE CHECKLIST. CREW SHUT DOWN NR 2 ENGINE. OVERHEAT LIGHT WENT OUT. UPON ARRIVAL AT THE GATE BOTH A & B LOOPS TESTED NORMAL. FOUND LOWER FAN DETECTOR M1121, LOOPS A & B WITH LOW RESISTANCE. ALSO REPLACED UPPER FAN DETECTOR M1120, LOOP A. ENG OVERHEAT DETECTION SYSTEM TESTED NORMAL AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E2GL 20050324001802005032400180EA 2005 3 24 SWIA200514739 120050110A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07439SW 7578 FS 625 STRINGER 14, LT AND RT SIDE ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED LT AND RT STRINGER 14 SIDE-ANGLES IAW CRJ 200 SRM 51-10-6 PG 3 PARA D & CRJ 200 SRM 51-42-06. 2L72 4F RTA21EA 20050324001872005032400187EA 2005 3 24 SWIA200514728 120050318A2741 SWITCH CNDAIRCL600 CL6002B19 1900309EA TRIM STUCK A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07927SW 7693 CAPTAIN`S TRIM SWITCH STICKS. REMOVED AND REPLACED CAPTAIN'S SIDE TRIM SWITCH IAW MM 27-41-05. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 20050325000152005032500015NM 2005 3 25 UPS05444153 120050312A532269B028032 SHEAR TIE BOEING747 747121 1384871NM M/D CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D - BS 1780 BETWEEN S10-11R FRAME ATTACH SHEAR TIE FOUND CRACKED, CRACK LENGTH .375 INCH. M/D - BS 1780 BETWEEN S10-11R FRAME ATTACH SHEAR TIE REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02. 2L74 4F A20WE 20050325000502005032500050NM 2005 3 25 QXEA200500419 120050203A5730 PANEL BOMBDRDHC8 DHC8401 1390041NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09539DS 4016 YYC - LEFT WING PANEL 522BT BOTTOM SURFACE OF PANEL PITTING AND FRETTING CORROSION AROUND PANEL ATTACH HOLES. REPAIRED IAW RD 8/4-87-422. 2H72 4T RTA13NM 20050325000672005032500067EU 2005 3 25 MALA050286 120050319A3030QR5OV SENSOR SAAB SF340 340B 7860101EU PITOT HEAT MALFUNCTIONED A MALAO OTHER J WARNING INDICATION CRCRUISE 1 GL15446XJ 340B446 LT PITOT HEAT ILLUMINATED INFLIGHT. CREW DECIDED TO RETURN TO MSP RATHER THAN BYPASS EAU TO RHI. REPLACED 5HG CURRENT SENSOR P/N ON/OFF QR5OV. LT PITOT HEAT CHECKS GOOD IAW SF340 MM CH 30. 2L72 4T RTA52EU 20050325000772005032500077WP 2005 3 25 05FDEA00608 120050318A29101489951 SHUTOFF VALVE DOUG DC10 DC1030 3023501WP HYD SYSTEM LEAKING A FDEAJ DUMP FUEL K FLUID LOSS CLCLIMB 1 SO25302FE 46801 APPROXIMATELY 5 MINUTES AFTER TAKEOFF, MASTER CAUTION LIGHT ILLUMINATED AND OBSERVED BOTH LT & RT NR 2 EDP LIGHT ON, PRESSURE AND QUANTITY RAPIDLY WENT TO ZERO. FOUND 1-2 NONREVERSIBLE MOTOR PUMP SHUTOFF VALVE LEAKING FROM BACKUP RING. 2L73 4F A22WE 20050328000932005032800093CE 2005 3 28 HYI2005F00001 120050103A801199103971 RELAY CESSNA402 402C 207590RCE CONT O520 TSIO520* 17040SO RT STARTER STUCK E HYIAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 NE01812AN 402C0229 AIRCRAFT LOST ELECTRICAL POWER SHORTLY AFTER TAKEOFF. AIRCRAFT LANDED W/O INCIDENT. MECHANIC FOUND RT STRAT RELAY STUCK ON. REMOVED AND REPLACED LT AND RT RELAYS, RT STARTER. AIRCRAFT IS EQUIPPED WITH STAART WARNING LIGHT SYSTEM. MX DETERMINED THAT THE SYSTEM WORKED PROPERLY. PILOT MUST NOT HAVE NOTICED WARNING LIGHT. (K) 1L72 3O3 O A7CE E8CE 20050328001282005032800128NM 2005 3 28 UPS05444174 120050313A5347BAC15201566 SEAT TRACK BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D - BS 1528-1532 RBL 75 SEAT TRACK LT FLANGE CORROSION. CORROSION BLEND OUT 0.045 X 1 X 1 INCH, EXCEED SRM 53-10-01 FIG 1 LIMIT. SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02. 2L74 4F A20WE 20050328001432005032800143NM 2005 3 28 UPS05444183 120050313A5320 FLOOR SUPPORT BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C M/D- BS 1580 - 1600 LBL 118 FLOOR SUPPORT CORRODED. CORROSION BLEND OUT 0.035 X 1 X 3 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2. 2L74 4F A20WE 20050328001572005032800157NM 2005 3 28 UPS05444192 120050309A55327075T60080IN SKIN BOEING747 747121 1384871NM VERTICAL FIN CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C VERTICAL FIN RT LWR EDGE FWD SECTION FX SKIN CHAFING MARK FOUND WITH ONE LOCATION OF SKIN BLEND OUT EXCEED EO LIMIT. CHAFE BLEND OUT 0.029 INCH. SKIN REPAIRED AS PER SRM 53-30-03 FIG 1A AT STA 2360 TO 2394 STR 3R AREA. 2L74 4F A20WE 20050328001582005032800158NM 2005 3 28 UPS05444193 120050309A55327075T60080IN SKIN BOEING747 747121 1384871NM VERTICAL FIN CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 INSPECTION TYPE:C VERTICAL FIN LT LWR EDGE FWD SECTION FX SKIN CHAFING MARK FOUND WITH 2 LOCATIONS CHAFE BLEND OUT EXCEED EO LIMIT. CHAFE BLEND OUT DEPTH 0.025 & 0.022 INCH. SKIN REPAIRED AT BS 2310-2360 STR 3L AREA AS PER SRM 53-30-03 FIG 1 & BS 2360 - 2380 STR 3L AREA AS PER SRM 53-30-03 FIG 1A. 2L74 4F A20WE 20050328001622005032800162SO 2005 3 28 RAIA00503011 120050321A3097 CONNECTOR EMB 145 EMB145LR 3260212SO PITOT HEAT LOOSE A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03812HK 145373 ERI - AT 10 KTS ON TAKEOFF ROLL, PITOT 3 INOP MESSAGE ILLUMINATED. MAINTENANCE CLEANED AND SECURED PITOT 3 HEAT CONNECTOR AND OPS CHECKED GOOD. 2L72 4T RTT00011AT 20050328001672005032800167SO 2005 3 28 RAIA00503010 120050318A213122250N030301 CONTROLLER EMB 145 EMB145LR 3260212SO CABIN PRESSURE MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03817HK8845 39 145058 STL - AUTO PRESSURIZATION FAULT INDICATION. MAINTENANCE REMOVED AND REPLACED AUTO PRESSURE CONTROLLER. 2L72 4T RTT00011AT 20050328001842005032800184EU 2005 3 28 SA05031 120050320A5610NP1653115 WINDSHIELD AIRBUSA319 A319112 3930323EU COCKPIT CRACKED A USAAH DEACTIVATE SYST/CIRCUITS A FLAME/FIRE CRCRUISE 1 EA19744US13830 1287 PHL FLT 1174 EN ROUTE PVD TO PHL. DURING THE FLIGHT, THE CAPTAIN'S WINDSHIELD BEGAN TO ARC, AND THEN CRACK. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CAPTAIN'S WINDSHIELD. OK FOR SERVICE. 2L72 4F RTA28NM 20050329000482005032900048NM 2005 3 29 USAA050331 120050216A5322 SHEAR TIE BOEING737 7374B7 1384702NM FUSLEAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US 24560 PIT - FOUND SHEAR TIE CRACKED .25 INCH, STRINGER 1 STATION 578. REMOVED AND REPLACED WITH NEW PART PR SRM 51-40-02. (M) 2L72 4F RTA16WE 20050329000552005032900055NM 2005 3 29 USAA050311 120050216A5320 CHANNEL BOEING737 7373B7 1384580NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND U-CHANNEL WITH 1 INCH CRACK, BS 747-767. FABRICATED AND INSTALLED NEW U-CHANNEL SUPPORT. (M) 2L72 4F RTA16WE 20050329000602005032900060NM 2005 3 29 USAA050322 120050211A554265C2584151 SKIN BOEING737 7373B7 1384580NM RUDDER DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND EXT COMPOSITE SURF 4 INCH LONG BY .125 INCH SINGLE LAYER DAMAGE, RUDDER RT SIDE 64 INCHES FROM BOTTOM 34 INCHES FROM T/E. INSTALLED REPAIR PLYS, SEALED AND REFINISHED PER BOEING SRM 51-70-17, EA 79999. (M) 2L72 4F RTA16WE 20050329000622005032900062NM 2005 3 29 USAA050320 120050211A554265C2584151 SKIN BOEING737 7373B7 1384580NM RUDDER DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU 23706 PIT - FOUND EXT COMPOSITE SURF WITH 1 INCH SINGLE LAYER DAMAGE DELAMINATION, RUDDER RT SIDE 41 INCHES FROM BOTTOM, 8 INCH FROM T/E. INSTALLED REPAIR PLYS, SEALED AND REFINISHED PER BOEING SRM 51-70-17, EA 79999. (M) 2L72 4F RTA16WE 20050329000632005032900063NM 2005 3 29 USAA050310 120050217A5720 SUPPORT ANGLE BOEING737 7373B7 1384580NM RT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19520AU50570 23706 PIT - FOUND SUPPORT ANGLE CRACKED 1 INCH, TRAILING EDGE OF SUPPORT PANEL, RT WING JUST ABOVE INBOARD EDGE OF NR 5 FLAP. FABRICATED AND INSTALLED NEW SUPPORT ANGLE PER BOEING DWG 69-47542 AND SRM 57-51-02. (M) 2L72 4F RTA16WE 20050329000702005032900070NM 2005 3 29 S2YA05016 120050218A2421ALT3524 GENERATOR DORNERDO32 DO328300 NM AC SYSTEM INOPERATIVE A S2YAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL13355SK9994 3124 FLT 2380 - MKE-PIT - DURING TAKOFF ROLL, THE RIGHT ALTERNATOR FAILED AND ALONG WITH THAT THE WINDSHIELD HEAT FAILED AND THE RT AC VOLT FAILED, THE CREW ABORTED THE TAKEOFF. THE ALTERNATOR REMAINED FAIL THROUGH SEVERAL ATTEMPTS TO RESET SO THE CREW RETURNED THE A/C TO THE GATE. MAINTENANCE REPLACED THE RT AC GENERATOR (ALTERNATOR) AND WITH OPERATIONAL CHECK GOOD THE A/C WAS RETURNED TO SERVICE. (M) 2H72 4T RTA55NM 20050329000892005032900089NM 2005 3 29 USAA050301 120050223A5315 FLOORBEAM BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US40275 24841 CLT - FOUND FLOORBEAM CORRODED 2 INCH BY 78 INCH AREA OF CORROSION, STATION 294 ENTIRE T-CAP. INSTALLED NEW SECTION OF FLOORBEAM PER SRM 53-10-51. (M) 2L72 4F RTA16WE 20050329001082005032900108NM 2005 3 29 SWAA050901 120050324A53306545776 SKIN BOEING737 7373H4 1384600NM FUSLAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED C4 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 908 & BS 920, STR 23L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20050329001092005032900109NM 2005 3 29 SWAA050902 120050325A3350101331 LENS BOEING737 7377AD 1384502NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29798SW 28436 OVERWING CENTER AISLE EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS COVER PER MM. 2L72 4F RTA16WE 20050329001102005032900110NM 2005 3 29 SWAA050903 120050324A57546573714 WEDGE BOEING737 7373H4 1384600NM RT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 6 L/E SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED SLAT PER MM. 2L72 4F RTA16WE 20050330001862005033000186NM 2005 3 30 72300102 120050328A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 6 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050330001952005033000195NM 2005 3 30 72300093 120050323A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 3 X 1 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050330001962005033000196NM 2005 3 30 72300092 120050323A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 4 X 1 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050330002042005033000204SO 2005 3 30 LR7A05031 120050306A5311 FRAME LKHEED382 382G 526414USO FUSELAGE MISDRILLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 444, WL 148, RBL 65. REPAIRED IAW LAC MEA 382-53-04-074 R1. 2H74 4T A1SO 20050331000722005033100072NM 2005 3 31 05FDEA00688 120050328A5347AFA7795510 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 MAIN DECK, SEAT TRACK RBL 27.5 CORRODED AT STA 1691. REPAIRED IAW SRM 53-70-00 FIGURE 1 VOLUME I. 2L73 4F RTA22WE 20050329000562005032900056NM 2005 3 29 USAA050334 120050219A53201138222 CHANNEL BOEING737 7374B7 1384702NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US40959 24560 PIT - FOUND ZEE CHANNEL CORRODED 1 INCH BY 12 INCH AREA, RIGHT SIDE ZEE CHANNEL STATION 294-362. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02, 51-20-01, 51-40-00. (M) 2L72 4F RTA16WE 20050329000712005032900071NM 2005 3 29 S2YA05021 120050227A1420 CONNECTOR DORNERDO32 DO328300 NM SHUTOFF VALVE DIRTY A S2YAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL13351SK 3108 FLT 2297 - YYZ-MKE - TAKEOFF ROLL THE CREW GOT A RT BLEED SOV CAS MESSAGE, THEY CONSULTED WITH MX AND WHERE ABLE TO GET IT TO CLEAR. THE CREW ATTEMPTED TAKEOFF AGAIN BUT AGAIN RECEIVED A RT BLEED SOV CAS MESSAGE. THE A/C RETURNED TO THE GATE. OUTSTATION MX CLEANED THE CONNECTOR FO THE LOW PRESSURE PRSOV. WITH NO FURTHER DISCREPANCIES NOTED THE A/C WAS RETURNED TO SERVICE. (M) 2H72 4T RTA55NM 20050329000732005032900073NM 2005 3 29 S2YA05013 120050206A24218160121 GENERATOR DORNERDO32 DO328300 NM LEFT OVERHEATED A S2YAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL13359SK 3202 FLT 2380 - MKE-PIT - DURING FLIGHT, THE CREW NOTICED A LEFT GENERATOR OVERHEAT CAS MESSAGE, CONSULTED WITH MX BUT WAS UNABLE TO GET THE MESSAGE TO CLEAR. THE CREW MADE AN AIR TURN BACK TO MKE. MAINTENANCE INSPECTED THE A/C AND REPLACED THE LEFT GENERATOR, AFTER OPERATIONAL CHECKS WERE GOOD THE A/C WAS RETURNED TO SERVICE WITH NO OTHER DISCREPANCIES NOTED. (M) 2H72 4T RTA55NM 20050329000752005032900075EA 2005 3 29 A6WA200540092 120050309A3220 STRUT CNDAIRCL600 CL6002B19 1900309EA NLG UNDERSERVICED A A6WAO OTHER WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 GL31409AW 7447 NLG WOULD NOT RETRACT ON DEPARTURE. CYCLED GEAR AND COMPLIED WITH QRH. GEAR DISAGREE RED CAS. AMBER NWS CAS AND AMBER WOW INPUT CAS. SERVICED NLG STRUT IAW AMM 32-21-30. OPS GOOD IAW 32-33-00. (M) 2L72 4F RTA21EA 20050329000812005032900081EA 2005 3 29 A6WA200540084 120050303A215032156222 RELIEF VALVE CNDAIRCL600 CL6002B19 1900309EA A/C PACK FAILED A A6WAO OTHER J WARNING INDICATION DEDESCENT 1 GL31438AW 7748 DURING DESCENT WITH POWER AT IDLE BOTH PACKS DROP OFF LINE. REMOVED AND REPLACED RT AND LT PRESSURE RELIEF VALVES IAW 21-51-43. (M) 2L72 4F RTA21EA 20050329000832005032900083NM 2005 3 29 S2YA05018 120050222A3246AHA22252 WHEEL DORNERDO32 DO328300 NM NLG VIBRATION A S2YAA UNSCHED LANDING E VIBRATION/BUFFET TOTAKEOFF 1 GL13355SK8404 718 3124 FLT 2265 - MKE-BNA - DURING TAKEOFF, THE CREW NOTICED A NOSEWHEEL VIBRATION JUST BEFORE TAKEOFF. THE CREW ELECTED TO CONTINUE WITH THE TAKEOFF AND CALLED MX IN THE AIR FOR A CONSULATION WHERE A DECISION WAS MADE TO PERFORM AN AIR TURN BACK TO MKE. MAINTENANCE REPLACED BOTH NOSE WHEEL ASSEMBLIES FOR TIRES BEING OUT OF ROUND AND THE A/C WAS RETURNED TO SERVICE. (M) 2H72 4T RTA55NM 20050329000852005032900085NM 2005 3 29 GAIA05012OP 120050302A311031892 SOCKET BOEING727 727224 1384076NM ANNUNCIATOR SMOKE A GAIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW0769740 20668 FLT 754 - FWA-IND - DURING CLIMB FROM F/L 230 TO F/L 280. SMOKE WAS NOTICED COMING FROM THE FIRST OFFICERS INSTRUMENT PANEL. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO IND WHERE A LANDING WAS MADE WITHOUT INCIDENT. REMOVED AND REPLACED BELOW G/S PUSH TO TEST INHIBIT AND GPWS ANNUNCIATOR. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20050329000932005032900093EA 2005 3 29 A6WA200540104 120050316A5313 RIB CNDAIRCL600 CL6002B19 1900309EA LT MLG WW CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31413AW 7585 LEFT MLG WHEEL WELL AT SS 48.30 FS 523.8 BATT RIB IS CRACKED 1.25 INCH LONG. (M) REPAIRED LT WING BATT RIB AT WS 53.60 IAW MFG REO. (K) 2L72 4F RTA21EA 20050329001032005032900103NM 2005 3 29 S2YA05011 120050203A5280001A3221A500000 ROD DORNERDO32 DO328300 NM MLG DOOR SHEARED A S2YAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL13352SK 3111 FLT 2343 - MKE-CMH - AFTER TAKEOFF, THE CREW NOTICED A NOSE VIBRATION BELIEVING THAT THE GEAR DOOR MIGHT NOT BE FULLY CLOSE. THE CREW MADE AN AIR TURN BACK TO MKE. MAINTENANCE INSPECTED THE A/C AND REPLACED THE LEFT FORWARD NOSE LANDING GEAR DOOR SHEAR ROD. AFTER OPERATIONAL AND RIG CHECKS WERE GOOD THE A/C WAS RETURNED TO SERVICE WITH NO OTHER DISCREPANCIES NOTED. (M) 2H72 4T RTA55NM 20050329001122005032900112 2005 3 29 SWAA050905 420050324A25656970843 HOOK BOEING737 7377H4 1384404NM R1 DOOR GIRT BARLOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29420WN 29825 R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR STOW HOOK LOOSE. SECURED HOOK PER MM. 2L72 4F RTA16WE 20050330000372005033000037 2005 3 30 KBM2005F00010 420050211A34225050031904 GYRO SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE COCKPIT INTERMITTENT E KBMAK NONE O OTHER ININSP/MAINT 1 WP19966SH 3787 DG INTERMITTENT IN FLIGHT, 2 KNOBS LOOSE, REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050330001822005033000182NM 2005 3 30 72300106 120050328A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 6 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050330001902005033000190NM 2005 3 30 72300098 120050328A5340 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 A 1 X 3 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050330001992005033000199SO 2005 3 30 LR7A05036 120050306A5311 FRAME LKHEED382 382G 526414USO FUSELAGE MISDRILLED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 782E, WL 148, LBL 65. REPAIRED IAW LAC MEA 382-53-04-074 R1. 2H74 4T A1SO 20050330002212005033000221SO 2005 3 30 LR7A05014 120050306A5310 BEAM LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03404LC 2850 4763 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND CW REAR BEAM WEB CRACKED AT FS 597, WL 276, CWS 52L. REPAIRED IAW LAC MEA 382-57-05-025. 2H74 4T A1SO 20050328001862005032800186EU 2005 3 28 SA05032 120050321A3230 PIN AIRBUSA319 A319112 3930323EU NLG INSTALLED A USAAA UNSCHED LANDING WJ INADEQUATE Q C WARNING INDICATION CLCLIMB 1 EA19719US 1084 BOS FLT 2035 EN ROUTE BOS TO DCA. AFTER TAKEOFF, THE NOSE GEAR WOULD NOT RETRACT. FLIGHT RETURNED TO FIELD IN BOS AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED A NOSE GEAR PIN. OK FOR SERVICE. 2L72 4F RTA28NM 20050328001892005032800189SO 2005 3 28 139203172005 120050317A78301159PM4156143 LINK GULSTM GULSTMG1159 GIV 3980115SO THRUST REVERSER DAMAGED E N93AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO13492QS4814 0399 1392 RIGHT THRUST REVERSER UNLOCK LIGHT ILLUMINATED CLIMBING THRU 17,000 FEET. 2L72 4F RTA12EA 20050329000982005032900098 2005 3 29 A6WA200540091 420050308A22106229815704 COMPUTER CNDAIRCL600 CL6002B19 1900309EA AUTOFLIGHT MALFUNCTIONED A A6WAO OTHER F FLT CONT AFFECTED CLCLIMB 1 GL31418AW 7618 RUDDER FLUTTER INFLIGHT, ALL CONDITIONS, AUTOPILOT ENGAGES. REMOVED AND REPLACED FCC NR 1 IAW 22-12-14. PERFORMED OPS TEST IAW AMM 22-11-00. OPS CHECK GOOD. AIRCRAFT CERTIFIED FOR RVSM. (M) 2L72 4F RTA21EA 20050329001022005032900102EA 2005 3 29 A6WA20050090 120050308A21707536893 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA RIGHT CONTAMINATED A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL31453AW 7838 SMOKE TOILET MESSAGE INFLIGHT. COMPLIED WITH QRH. FLIGHT ATTENDANT REPORTS HAZE IN CABIN. SMOKE NO LONGER PRESENT. RESET C/B, TESTED TOILET SMOKE DETECTORS, SYSTEM CHECK GOOD. TROUBLESHOT AND FOUND PACK NR 2 ACM DEFECTIVE. NR 2 ACM OIL CHECKED NORMAL. REPLACED RIGHT WATER SEPARATOR SOC GROUND RAN ECS PACK NR 2 AND ACM CHECKS NORMAL. NO SMOKE VISIBLE. (M) 2L72 4F RTA21EA 20050329001112005032900111NM 2005 3 29 SWAA050904 120050324A57536546486 WEDGE BOEING737 7373H4 1384600NM RT WING FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29324SW 23414 DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARDD MIDFLAP OUTBOARD T/E WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PER MM. 2L72 4F RTA16WE 20050331000112005033100011WP 2005 3 31 ASAA0580016 120050123A5320991555415 INTERCOSTAL DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02964AS 53078 OKC - HV-CHECK, SEAT TRACK SUPPORT HAS CORRODED FASTENERS ON ATTACHING ANGLE INTERCOSTAL. REPLACED INTERCOSTAL. (M) 2L72 4F RTA6WE 20050331000332005033100033WP 2005 3 31 DHL2005805571 120050322A574037048412 FITTING DOUG DC8 DC873F 302199FWP NR 2 FUEL TANK CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 NR 2 MAIN TANK INTERIOR FITTING CRACKED 2.000 AT STA 740.000 S-51 (FWD PORT). REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. INSTALLED NEW FITTING IAW SRM 51-1-20D PG 9. TORQUED IAW SRM 51-3-1. REFER TO NR 028714 FOR LEAK CHECK. 2L74 4F RT4A25 20050331000362005033100036EU 2005 3 31 05FDEA00670 120050328A5347 SEAT TRACK AIRBUS310 A310222 3930315EU FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25419FE 345 MAIN CABIN FRAME 34 TO 37 SEAT TRACK YB77 HAS 2EA AREAS OF CORROSION NR 4 SEAT TRACK RT. REMOVED CORROSION IAW A310 SRM 51-74-10, OUT OF LIMITS IAW A310 SRM 53-10-16 FIG 101. FABBED NEW REPAIR SECTION OF SEAT TRACK IAW A310 SRM 53-10-16 FIG 208. REMOVED AND REINSTALLED SPICES AND SUPPORT BRACKET IAW A310-200 SRM 51-72-10. REMOVE BAD SECTION OF TRACK FROM FR33.5 TO 36.5 AND INSTALLED NEW REPAIR SECTION IAW A310-200 SRM 51-72-10 AND 53-10-16 FIG 208. 2L72 4F RTA35EU 20050331000432005033100043WP 2005 3 31 DHL2005805553 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME WORN, STA 700.000 L-8 L-9R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-04-05, EO AST 050217 DATE 03-03-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST050217, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331000562005033100056NM 2005 3 31 05FDEA00680 120050328A5347ABA7680505 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 MAIN DECK, SEAT TRACK LBL 107 CORRODED AT STA. REMOVED AND REPLACED AS IAW SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050401000152005040100015NM 2005 4 1 USAA050338 120050302A5340 ATTACH ANGLE BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US40275 24841 CLT - Q6 - ATTACH ANGLE, .250 INCH CRACK, STATION 578 BETWEEN STRINGERS 8R AND 9R. REPLACED ATTACH ANGLE WITH FABRICATED PART IAW DWG. 2L72 4F4 FRTA16WE E21EU 20050404000072005040400007CE 2005 4 4 XRR2005F00000 120050211A56105042006930 WINDSHIELD BEECH 100 B100 1152919CE GARRTTTPE331TPE331* 01514WP COCKPIT CRACKED E XRRAK NONE O OTHER ININSP/MAINT 1 CE01564CA3902 BE58 INNER PANE OF CO-PILOTS WINDSHIELD CRACKED WHILE AT ALTITUDE. 1L72 4T3 T A14CE E2WE 20050404000312005040400031CE 2005 4 4 ALG2005F00016 120050114A6340206075545001 SENSOR CESSNASTC STC206C 1182107CE ALLSN 250C 250C30P 03013GL MAIN ROTOR CORRODED E ALGAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW032611 45417 JUST AFTER TAKEOFF, THE LOW ROTOR CAUTION LIGHT ILLUMINATED. 2 OR 3 SECONDS LATER, THE LOW ROTOR RPM HORN SOUNDED. ROTOR TACH INDICATIONS WERE NORMAL, PILOT RETURNED TO BASE. UPON LANDING, THE MECHANIC REMOVED AND REPLACED BOTH THE LOW ROTOR RPM AND ENGINE OUT SENSORS DUE TO CORROSION AND AC WAS OPS CHECKED AND RETURNED TO SERVICE. (K) 1H71 3O3 UNTA4CE E1GL 20050404000322005040400032NM 2005 4 4 GAIA05014ST 120050319A5753652163223 SKIN BOEING727 727243 138408DNM PWA JT8 JT8D7B 52053NE LT TE FLAP DELAMINATED A GAIAK NONE O OTHER ININSP/MAINT 1 SW071269Y 21269 DURING A-CHECK, NO FLIGHT, FWA: FOUND LT IB MID-FLAP OB T/E MISSING 6 INCHES OF SKIN. REMOVED AND REPLACED LT IB MID-FLAP AND AFT FLAPS ASSY. OPS CHECKED NORMAL IAW MM 27-51. AIRCRAFT WAS RETURNED TO SERVICE. (SW07200506017) (K) 2L73 4F4 FRTA3WE E2EA 20050404000542005040400054CE 2005 4 4 AZN2005F00000 120050201A324016400806 BRAKE DISC CESSNA310 310R 2074245CE CONT O520 IO520* 17032SO LT BRAKES CRACKED E AZNAK NONE O OTHER ININSP/MAINT 1 GL131761G 310R1223 NOTICED NUMEROUS OF OUR MFG BRAKE DISC, PN 164-00806 BEING CRACKED. THE CRACKS BEGIN WHERE MFG NAME IS STAMPED ON THE BRAKE DISC. FOUND 3 CRACKS WHERE THE LETTER (P) IS STAMPED AND ONE CRACK WHERE THE LETTER (R) IS STAMPED. PROBABLE CAUSE IS THE STAMPING LOCATION SETS UP A STRESS POINT. RECOMMEND DIFFERENT STAMPING LOCATION TO PREVENT RECURRENCE. (K) 1L72 3O3 O 3A10 E5CE 20050331000862005033100086WP 2005 3 31 DHL2005805632 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT INBOARD FLANGE Z-FRAME (1) HOLE MISDRILLED AT STA 340.000 L-8 L-9R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-04-05 EO AST 050217 DATE 03-03-05. PERFORMED NDT INSPECTION (DETAILED). NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST 050217 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050331001122005033100112SO 2005 3 31 SWIA200514796 120050314A2797 CONNECTOR EMB 120 EMB120ER 3260203SO TE FLAP CONTROL FAILED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07584SW 120352 FLAP CONTROL FAULT. REPLACED CONNECTOR ON LEFT AND RIGHT OUTBOARD ACTUATOR. OPERATIONAL CHECK GOOD IAW MM 27-50-00. 2L72 4T RTA31SO 20050401000012005040100001CE 2005 4 1 ZH92005F00000 120050323A3110BAS350352831 SWITCH LEAR 35 35A 5170602CE GARRTTTFE731TFE731* 01518WP INSTRUMENT PANELSHORTED E ZH9AO OTHER O OTHER NRNOT REPORTED 1 EA27326HG 501 WHILE RETURNING TO AIRPORT, THE COPILOTS ALTIMETER BREAKER POPPED, WHICH IN TURN DISABLED THE NR2 ALTIMETER/ADDU. THE AC LANDED 10 MINUTES LATER WITHOUT INCIDENT AND THE NR2 ALTIMETER FAILURE WAS REPORTED TO MAINTENANCE. WHEN THIS PROBLEM WAS INVESTIGATED IT WAS FOUND THAT BOTH ALTIMETER BREAKERS WERE POPPED AND BOTH ALTIMETER/ADDU WERE INOPERATIVE. THE PROBLEM WAS EVENTUALLY TRACED TO A SHORTED AIR DATA SWITCH PANEL WHICH WAS INSTALLED IN THE INSTRUMENT PANEL AS NEW DURING THE STC MODIFICATION. FAILURE OF THIS COMPONENT CAUSED BOTH ALTIMETERS, BOTH ADDUS, ALL MODE C TRANSPONDER INFO, AND THE AUTOPILOT TO BECOME INOPERATIVE. 2L72 4F4 F A10CE E6WE 20050401000032005040100003 2005 4 1 KBM2005F00043 420050312A34225040017901 GYRO SNIAS 350 AS350B2 8680813EU ALLSN 250C 250C20B 03013GL ATTITUDE MALFUNCTIONED A KBMAK NONE O OTHER ININSP/MAINT 1 WP19751H 729 3403 ATTITUDE INDICATOR WOULD NOT CAGE PROPERLY. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E4CE 20050401000162005040100016NM 2005 4 1 USAA050342 120050307A5754 WEDGE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU NR4 SLAT WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU50516 23705 CLT - Q2 - NR 4 SLAT, 2 INCH X 2 INCH, WEAR. NR 4 SLAT T/E WEDGE LOWER SKIN IB. ACCOMPLISHED COMPOSITE REPAIR IAW EA. (K) 2L72 4F4 FRTA16WE E21EU 20050401001042005040100104NM 2005 4 1 USAA050354 120050310A5743 SUPPORT FITTING BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU LT MLG CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19519AU50516 23705 CLT - Q2 - SUPPORT FITTING, .1250 INCH CRACK. LT WING MLG SUPPORT FITTING. ACCOMPLISHED REPAIR IAW TR 57-40-13. (K) 2L72 4F4 FRTA16WE E21EU 20050404000082005040400008 2005 4 4 TVD2005F00000 420050215A3417 LINE PILATSPC12 PC12 7090550EU ADC DETERIORATED E TVDAO OTHER N FALSE WARNING CRCRUISE 1 NM01156SB3430 156 WHILE FLYING AT 170 KIAS, THE PILOT NOTED HE HAD TO REDUCE POWER TO MAINTAIN 170 KIAS. SHORTLY AFTER THAT THE AIRCRAFT`S (STICK SHAKER) ACTIVATED. INSPECTION REVEALED SEVERELY DETERIORATED PLASTIC TUBING FROM FWD PRESSURE BULKHEAD TO AIR DATA COMPUTER. LINES WERE REPLACED. (K) 1L71 3T RTA78EU 20050404000212005040400021EA 2005 4 4 A6WA200540107 120050317A5730 ACCESS PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31415AW 7593 RT LOWER WING PLANK FUEL TANK ACCESS PANEL CUT-OUT BETWEEN SS 50.54 AND WS 66.2 HAS MINOR FRETTING AND FAYING SURFACE LESS THAT .006 INCH DEEP. (K) BLEED MINOR FRETTING ON RT LOWER WING PLANK BETWEEN WS 50-54 AND 66.2 IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20050404000302005040400030EA 2005 4 4 A6WA200540106 120050317A5730 ACCESS PANEL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE LT WING CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31415AW 7593 LT LOWER WING PLANK FUEL TANK ACCESS PANEL CUT-OUT BETWEEN SS 0.00 AND WS 29.42 HAS MINOR FRETTING ON FAYING SURFACE LESS THAN .006 INCH DEEP. C/A PENDING (K) 2L72 4F4 FRTA21EA E15NE 20050404000412005040400041EA 2005 4 4 A6WA200540034 120050125A5712 RIB CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31412AW 7582 MWC 60. RT WING STATION 53.6 BUTT RIB IS CRACKED .5000 INCH LONG IN UPPER AFT RADIUS. REPAIRED RT WING STATION 53.60 BATT RIB IAW MFG EO 601R-57-51-046, REV B. 2L72 4F4 FRTA21EA E15NE 20050404000422005040400042WP 2005 4 4 ASAA0580106 120050215A53219936651505 FLOOR PANEL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE PAX CABIN PEELING A ASAAK NONE O OTHER ININSP/MAINT 1 NM02943AS 53018 OKC C-CHECK - PAX CABIN FLOOR PANEL PEELED. FIBERGLASS BOND REPAIRED. (K) 2L72 4F4 FRTA6WE E9NE 20050404000672005040400067SO 2005 4 4 QTL2005F00000 220050204A741410357584 DISTRIBUTOR GEARCONT CESSNA182 182H 2072718CE CONT O470 O470R 17026SO MAGNETO FAILED E QTLAK NONE O OTHER ININSP/MAINT 1 NM051904X D279801DR 18256004 1309324R MAGNETO REMOVED FOR FAILURE, 24 TEETH MISSING ON DISTRIBUTOR GEAR. REPLACED WITH NEW GEAR NR 10-357586. (K) 1H71 3O3 ONT3A13 E273 20050404001182005040400118WP 2005 4 4 DHL2005805602 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (2EA) MISDRILLED HOLES AT STA 1160.000 L-12R TO L-13R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-07-05, EO AST050201 DATED 02-17-05. PERFORMED DETAIL VISUAL INSPECTION NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST050201, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001212005040400121WP 2005 4 4 DHL2005805531 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT INBOARD FLANGE Z-FRAME HOLES (3EA) MISDRILLED STA 100.000 L-11L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05, EO AST 050205 DATE 02-21-05. CLEANED, TREATED AND PRIMED (AREA) MISDRILLED HOLES IAW SRM 51-1-8B. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD5-6) IAW EO AST 050205, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050404001342005040400134WP 2005 4 4 DHL2005805568 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME (2EA) MISDRILLED HOLES AT STA 440.000 L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-05-05 EO AST 050205 DATED 02-21-05. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA AT STA 440.000 L-10L IAW SRM 51-1-8B. PERFORMED DETAIL VISUAL INSPECTION NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD5-6) IAW EO AST050205, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050331000772005033100077EA 2005 3 31 COMA0560206 120050326A3620356072310 SENSOR CNDAIRCL600 CL6002B19 1900309EA E/E BAY FAULTY A COMAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO01814CA 7387 FLIGHT 5138 RECEVIED A LEFT 14TH STAGE DUCT MESSAGE DURING CLIMBOUT OF CAE, CREW DECLARED AN EMERGENCY, LEFT ENGINE WAS SHUT DOWN AND RETURNED TO THE FIELD, AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE 14TH STAGE HEAT SENSING ELEMENT. 2L72 4F RTA21EA 20050401000982005040100098EA 2005 4 1 A6WA200540110 120050316A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT SIDE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31415AW 7593 FLOOR SUPPORT ANGLE AT FS 621 RT SIDE IS CRACKED 1 INCH. PERFORMED REPAIR TO RT FS621, FLOOR SUPPORT ANGLE IAW REO. (K) 2L72 4F4 FRTA21EA E15NE 20050404000012005040400001CE 2005 4 4 VLI2005F00000 120050127A322026430623 SPRING CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL NLG CRACKED E VLIAK NONE O OTHER ININSP/MAINT 1 SO21335VL1922 208B0964 PCEPC0975 020393 PILOT REPORTED, NOSE GEAR COLLAPSED. DURING RUN-UP SPRING NOSE GEAR CRACKED. (SO21200503223) 1H71 3T3 T A37CE E4EA 5 CP60GL 20050404000282005040400028CE 2005 4 4 LQY2005F00000 120050207A273058151036CR CONTROL CABLE CESSNA441 441 2076020CE GARRTTTPE331TPE331* 01514WP RT ELEVATOR FRAYED E LQYAK NONE O OTHER ININSP/MAINT 1 CE07258VB4000 4410258 RT AFT ELEVATOR CABLE WAS FRAYED THROUGH 4 OF THE 7 STRANDS - FAILURE WAS IMMINENT. THIS CABLE SHOWED NO SIGNS OF WEAR ON THE PREVIOUS INSPECTION 500 HOURS BEFORE AND IT ONLY TAKES A 20 DEGREE BEND AT THIS PULLEY. PROBABLY SHOULD BE INSPECTED EVERY 300 HOURS INSTEAD OF THE FACTORY INSPECTION SCHEDULE OF 600 HOURS. SUGGEST THAT CORROSION RESISTANT STAINLESS STEEL CABLES SEEM TO BE MORE BRITTLE THAN THE STANDARD STEEL CABLES. (K) 1L72 3T3 TRTA28CE E2WE 20050404000662005040400066CE 2005 4 4 L1K2005F00000 120050209A3243054113922 MASTER CYLINDER CESSNA185 A185F 2072821CE CONT O520 IO520D 17032SO MCAULY2A34C D2A34C58 GL BRAKE SYSTEM CONTAMINATED E L1KCO OTHER O OTHER LDLANDING 1 AL01185MF5034 18503268 1588618D AC LANDING AT BELOW FREEZING TEMP, HAD BRAKES LOCKING UP (FROZE UP) ON LANDING. INSP AFTER INCIDENT FOUND DIRT AND DEBRIS ALONG WITH CONTAMINATED FLUID (WATER) IN BOTTOM OF BOTH RT AND LT BRAKE MASTER CYL PN 0541139-22 WHEN REMOVED. CYL BODIES SHOWED NO SIGN OF EVER BEING REMOVED. NEW AT FACTORY ON 1-31-1977 AND WITH TT 5034.0. REVIEW OF AC RECORDS SHOWED THAT CYL HAVE HAD SEAL REPLACED BEFORE WITH NO MENTION OF BODIES BEING REMOVED AND CLEANED IN 27 YEARS 11MONTHS IN SERVICE. NOTE: INNER PART OF CYL CAN BE REMOVED AND SEAL REPLACED WITHOUT REMOVING CYL BODY. PROB CAUSE: BRAKE CYLINDER CONTAMINATION. RECOMMEND: IF CYL SEALS ARE REPLACED, ENTIRE BODY SHOULD BE REMOVED AND CLEANED. (AL01200502421) 1H71 3O3 O 3A24 E5CE 5 CP3EA 20050404000762005040400076EU 2005 4 4 YVB2005F00000 120050125A3260D228580001 PROXIMITY SWITCH AMD FALC50FALCON900 2700160EU NLG WARPED E YVBAO OTHER J WARNING INDICATION CLCLIMB 1 EA11990BB 42 (CNTRL NR 0501) DURING TAKEOFF, LANDING GEAR WOULD NOT COME UP (HANDLE WOULD). WHEN GEAR HANDLE WAS PUT DONW, 3 GREEN DOWN AND LOCK AND AUTO SLAT LIGHT ON THE GEAR HANDLE WAS LOCKED (GROUND MODE). AIRCRAFT JACKED, GEAR SWUNG NORMALLY IN HANGAR. FOUND NOSE GEAR PROX SWITCHES WEAK. REPAIRED PROXIMITY SWITCH AND TESTED IAW MM. OK, EVERYTHING DONE IAW MM. (EA11200502913) (EA11200502879) (K) 2L73 4F RTA46EU 20050404000852005040400085EU 2005 4 4 KBM2005F00036 120050304A6520350A33215300 BEARING SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE TAIL ROTOR WORN E KBMAK NONE O OTHER ININSP/MAINT 1 WP19345SH4464 3345 LAMINATED BEARINGS, WORN. REMOVED AND REPLACED. (K) 1G71 3U3 U H9EU E19EU 20050404001292005040400129WP 2005 4 4 DHL2005805617 120050320A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT (8EA) MISDRILLED HOLES IN L-12R (STA 600.000 - 620.000). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-15-05 EO AST 050216 DATED 03-02-05. PERFORMED DETAIL VISUAL INSPECTION, NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST 050216 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001322005040400132WP 2005 4 4 DHL2005805563 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 702.000 L-11L TO L-12L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 02-25-05, EO AST 050202 DATED 02-17-05. PERFORMED DETAIL VISUAL INSPECTION NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO AST050202, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001372005040400137WP 2005 4 4 DHL2005805581 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (2EA) MISDRILLED HOLES, STA 1420.000 L-12R TO L-13R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-07-05, EO AST 050201 DATED 02-17-05. PERFORMED DETAIL VISUAL INSPECTION NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST 050201, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001422005040400142EU 2005 4 4 F3LA200500014 120050322A2121EVT3454H FAN AIRBUSA319 A319112 3930323EU CABIN INOPERATIVE A F3LAO OTHER EB VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM03916FR8118 4311 1876 FLIGHT CREW REPORTED VENT EXTRACT FAULT. NOTICED AIRCRAFT VIBRATION, FRONT RIGHTSIDE, AND SMELL OF ELECTRICAL SMOKE FRONT TO BACK OF AIRCRAFT. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE VERIFIED VENT EXTRACT FAN FAILURE AS CAUSE OF ODOR PER TSM 24-00-00-810-823 AND PLACARD PER MEL 21-26-02A. UPON ARRIVAL IN DEN, REPLACED VENT EXTRACT FAN PER MM 21-26-51-000-001 AND 21-26-51-400-001. PERFORMED TEST OF SYSTEM VIA MCDU PER MM 21-26-00-710-001. 2L72 4F RTA28NM 20050404001502005040400150NE 2005 4 4 2005UALA00259 220050323A7510 VALVE BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE LT ENGINE STUCK A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29218UA 30222 LEFT ENG ANTI-ICE VALVE STUCK CLOSED. MAINTENANCE REPLACED LH ENGINE ANTI-ICE VALVE. OP CHECKED OK AFTER REACTIVATING VALVE. 2L72 4F4 FRTT0001SE E46NE 20050404001062005040400106NM 2005 4 4 USAA050356 120050218A5340 ATTACH ANGLE BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU FUSELAGE WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19438US40959 24560 PIT - Q4 - ATTACH ANGLE, 1 INCH X 2 INCH WEAR AREA, BS 1288 AT S2R. FABRICATED NEW ANGLE IAW TYP REP 53-20-05A. (K) 2L72 4F4 FRTA16WE E21EU 20050404001262005040400126WP 2005 4 4 DHL2005805564 120050320A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 702.000 L-12L TO L-13L 1EA (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 02-25-05, EO AST 050202 DATED 02-17-05. PERFORMED DETAIL VISUAL INSPECTION NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO AST050202, SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001282005040400128WP 2005 4 4 DHL2005805614 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT Z-FRAME INBOARD FLANGE HOLES (2EA) MISDRILLED STA 1140.000 L-9L L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05 EO AST 050205 DATE 02-21-05. CLEANED, TREATED AND PRIMED (AREA) MISDRILLED HOLES IAW SRM 51-1-8B. PERFORMED DETAILED VISUAL INSPECTION NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD5-4) IAW EO AST 050205 SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050404001302005040400130WP 2005 4 4 DHL2005805619 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT INBOARD FLANGE J-FRAME HOLES (2EA) MISDRILLED AT STA 960.000 L-10L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 02-25-05 EO AST 050203 DATE 02-18-05. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. PERFORMED DETAILED VISUAL INSPECTION, NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST 050203, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050404001362005040400136WP 2005 4 4 DHL2005805539 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (01EA) HOLE MISDRILLED STA 620.000 L-12.5R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-07-05 EO AST050201 DATE 02-17-05. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIVET (MS20470AD) IAW EO AST 050201, SRM 51-1-21 PAGE 1. 2L74 4F RT4A25 20050404001402005040400140WP 2005 4 4 DHL2005805529 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE HOLES (2EA) MISDRILLED AT STA 1340.000 L-12L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 03-05-05 EO AST050205 DATE 02-21-05. CLEANED, TREATED AND PRIMED (AREA) MISDRILLED HOLES IAW SRM 51-1-8B. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST050205 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001462005040400146NM 2005 4 4 2005UALA00257 120050321A2613 OVERHEAT LOOP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 2 ENGINE MALFUNCTIONED A UALAEA ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 WP29341UA 24245 RETURNED TO ORD DUE TO NR 2 ENGINE OVERHEATED AND SHUTDOWN. CREW REPORTED NR 2 ENGINE OVERHEAT INDICATION AT CLIMB. CREW SHUT DOWN NR 2 ENGINE PER QRC. PERFORMED TROUBLESHOOTING OF THE OVERHEAT DETECTION SYSTEM. FOUND NR 2 ENGINE CORE DETECTOR M1122, LOOPS A & B WITH LOW RESISTANCE SHORT TO GROUND. REMOVED AND REPLACED OVERHEAT DETECTOR CORE LOOPS A & B. ENGINE OVERHEAT DETECTION SYSTEM TESTED NORMAL. 2L72 4F4 FRTA16WE E2GL 20050401001012005040100101EA 2005 4 1 A6WA200540121 120050319A57112024T3 SPAR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT WING MISDRILLED A A6WAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL31413AW 7585 DUE TO HOLES SPACING ON RT LOWER WING SPAR AT WS 148, JOINT STRAP 601R100465-4 S/B CANNOT BE INSTALLED IAW SB 601R-57-037. REPAIRED RT WING SPAR AT WS 148, SHIFTED CUTLINE ON T/E RT WING AT WS 148. FABRICATED A NEW DOUBLE JOINT STRAP OUT OF 2024-T3.050 PO NR 46952/7 IAW BRAS 601R-57-6125. (K) 2L72 4F4 FRTA21EA E15NE 20050404000152005040400015EA 2005 4 4 O2G2005F00004 120050314A2497OCDB9A023 CONTACTOR CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF34* NE FUSELAGE FAILED E O2GAA UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 NE03601VH4858 2532 5043 NR1 THRU FAILED INFLIGHT CAUSING LOSS OF NR 1 DC BUSS AND UTILITY BUSS. REPLACED THE NR 1 LINE CONTACTOR AND NR1 TRU. 2L72 4F4 FRTA21EA E15NE 20050404001232005040400123WP 2005 4 4 DHL2005805567 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME (2EA) MISDRILLED HOLES AT STA 540.000 L-12L TO L-13L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-05-05, EO AST 050205 DATED 02-21-05. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA AT STA 540.000 L-12L TO L-13L IAW SRM 51-1-8B. PERFORMED DETAIL VISUAL INSPECTTION NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD6-5) IAW EO AST 050205 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001432005040400143EU 2005 4 4 2005UALA00254 120050318A4990 SEPARATOR AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE APU OIL SYSTEM WORN A UALAA UNSCHED LANDING KH FLUID LOSS ELECT. POWER LOSS-50 PC CRCRUISE 1 WP29442UA 780 AUTO SHUTDOWN OF APU WITH NR 2 ENG DRIVEN GENERATOR ALREADY INOPERATIVE. CONFIRMED NO EXTERNAL OIL LEAKAGE. GEARBOX MODULE 756407J, S/N SP-G 970369 WAS PARTIALLY DISASSEMBLED FOR INSPECTION AND REPLACEMENT OF THE BEARING TABS AND AIR-OIL SEPARATOR SEAL. AIR-OIL SEPARATOR LIP SEAL WAS WORN, ALLOWING OIL TO BLOW BY. 2L72 4F4 FRTA28NM E40NE 20050404001542005040400154EU 2005 4 4 U30A200500002 120050312A2910D2901005201300 PIPE AIRBUS320 A320214 3930316EU ZONE 413 LEAKING A U30AA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA17264AV7663 7663 1867 CREW RECEIVED AN ECAM MESSAGE, GREEN HYD LOW PRESS. TURNED OFF PUMP & PTU. STATUS PG INDICATED LOW PRESS & NIL QTY. DIVERTED, DECLARED AN EMERGENCY. ECAM GENERATED APPROACH LIST INSTRUCTS TO TURN PTU BACK ON TO TRY TO RESTORE PRESSURE, PRESSURE RESTORED. CANCELED THE EMERGENCY. FLT CREW ELECTED TO MAKE AN OVERWEIGHT LANDING & LANDED AT LESS THAN 50 FPM VERTICAL SPEED. MAINTENANCE REPLACED A LEAKING (PINHOLE) GREEN HYD RETURN LINE IN THE NR 1 ENGINE PYLON. SERVICED THE GREEN HYD SYSTEM PER AMM 12-12-00, LEAK CK'D AND OP'S CK'D THE GREEN HYD SYSTEM OK PER AMM 29-11-06. THE OVERWEIGHT LANDING WAS FOUND TO BE WITHIN ALLOWABLE LIMITS PER AMM 05-51-11. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA28NM 20050404001642005040400164NM 2005 4 4 05FDEA00660 120050326A2612 WARNING LIGHT BOEING727 727200 138407ENM CARGO BAY SMOKE ILLUMINATED A FDEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO25258FE 20940 LOWER CARGO SMOKE LIGHT ILLUMINATED ON T/O AT 70 KTS, RTO NO OTHER INDICATIONS LIGHT WENT OUT DURING DECELERATION. RELEASED FOR SERVICE PER MEL/CDL: 26-19-A CATEGORY: C EXPIRATION: 05APR05 MEL 26-19-A: SMOKE DETECTION IN THE FWD LOWER CARGO COMPARTMENT INOP. OHMED AND MEGGED WIRING TO THE FWD LIGHT L9109 TO THE CONTROL PANEL REF 727-200 WDM 26-23-00, ALL CKS GOOD. CHECKED THE LIGHT SOCKET, CHECKS GOOD. REMOVED AND REPLACED CSCP, OPS CKS GOOD PER 727-200 M/M 26-17-001-5. OK FOR SERVICE. 2L73 4F RTA3WE 20050404001752005040400175NM 2005 4 4 AWXA200500374 120050321A5730654783852 SKIN BOEING737 7373G7 1384595NM RT WING CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 MCN - MAJOR REPAIR - DURING C-16 CHECK A .375 INCH CRACK WAS FOUND IN PREVIOUS REPAIR OF RT WING SKIN AT INBOARD MID FLAP LEADING EDGE CUTOUT FOR FORE FLAP CONTROL ROD RS 176.0. MAINTENANCE REMOVED PREVIOUS REPAIR OF RT WING SKIN AT RS 176.0; FABRICATED A NEW SECTION OF REPLACEMENT SKIN AND REPAIR SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-53-01 FIG 202. 2L72 4F RTA16WE 20050405000472005040500047WP 2005 4 5 ASAA0580072 120050131A571299374639 RIB DOUG DC9 DC983 3022083WP RT WING CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, FOUND RIGHT WING LEADING EDGE RIB CRACKED. REPLACED DAMAGE. INSTALLED REPAIR ANGLE, SHIM, RADIUS, AND FILLER. (M) 2L72 4F RTA6WE 20050405000792005040500079WP 2005 4 5 ASAA0580055 120050131A532199365821 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL HAS BROKEN INSERTS. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050405001352005040500135EA 2005 4 5 QXEA200500458 120050304A5347 SEAT TRACK CNDAIRCL600 CL6002C10 1390015EA ZONE 200 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - LEFT HAND INBOARD SEAT RAIL AT STATION X663 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND HORIZON AIR EA R-53-083. 2L72 4F RTA21EA 20050404001812005040400181CE 2005 4 4 DXTA200500628 120050312A3260 UPLOCK SWITCH CESSNA750 750 2076810CE MLG OUT OF ADJUST E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07936QS 7500036 UPON GEAR RETRACTION, HEARD THUMP GEAR UNLOCK LIGHT WOULD NOT EXTINGUISH. FOUND NOSE LANDING GEAR UPLOCK SWITCH OUT OF ADJUSTMENT. ADJUSTED NLG UPLOCK SWITCH IAW CE 750 MM 32-30-05. OPS CHECK GOOD IAW CE 750 MM CH 32-00-01. 2L72 4J RTT00007WI 20050404001842005040400184SO 2005 4 4 SWIA200514768 120050207A5340 FITTING EMB 120 EMB120ER 3260203SO FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM0758733 120197 RIGHT SIDE FIN TO FUSELAGE FITTING IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. FIN TO FUSE ANGLE REPAIRED IAW EMB 120 SB 120-53-0074 & EMBRAER EST-504/96. 2L72 4T RTA31SO 20050404001862005040400186NM 2005 4 4 SWAA050740 120050310A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29300SW 22940 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, BELOW STR 12R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20050405000052005040500005EU 2005 4 5 ASOA05192 120050205A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE INBOARD AND OUTBOARD SEAT TRACKS BETWEEN FRAME 28-29 RT WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INBOARD AND OUTBOARD SEAT TRACKS BETWEEN FRAME 28-29 RT IAW SRM 53-00-00 FIG 434. (M) 2H72 4T RTA53EU 20050405000062005040500006EA 2005 4 5 ASOA05207 120050304A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27880AS 7606 DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072B. (M) 2L72 4F RTA21EA 20050405000492005040500049WP 2005 4 5 ASAA0580050 120050131A532199365831 FLOOR PANEL DOUG DC9 DC983 3022083WP FUSELAGE PUNCTURED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, PAX CABIN FLOOR PANEL IS PUNCTURED AT TWO LOCATIONS. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050405001702005040500170NM 2005 4 5 AALA20050223 120050328A33970201875001 WIRE HARNESS BOEING737 737823 13844BZNM EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21967AN 29545 LGA - EMERGENCY LIGHT AT SEATS 19DEF INOPERATIVE. REPLACED SEAT HARNESS AT 19DEF FOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20050405001902005040500190NM 2005 4 5 UPS05444209 120050313A534769B620491 CARGO TRACK BOEING747 747121 1384871NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 M/DECK BS 1940 AND 1960 LBL 80 INCH TIE DOWN FTG ATT PLATE FOUND CORRODED. CORROSION BLEND OUT 0.020 INCH BY 1 INCH BY 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, M/D BS 1940 LBL 80 INCH TIE DOWN FTG REPLACED AS PER MM 20-51-01. 2L74 4F A20WE 20050405002052005040500205NE 2005 4 5 MASA200500056 220050124A73214147T70P01 FUEL CONTROL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NR 2 ENGINE CONTAMINATED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0727172137828004 7172 872268 ASH 9432 CLT TO CLT, RETURNED TO THE FIELD FOR THE NR 2 HYDRAULIC SYSTEM LOW PRESSURE AND QUANTITY. MX FOUND EVIDENCE OF HYD FLUID IN THE LT WING FUEL SYSTEM. MX TOOK FLUID SAMPLES FROM E1 AND E2 FUEL FILTER. FOUND DAMAGED LINE IN RT TANK. MX COULD NOT REPAIR REC'D TUBE ASSY FROM BOMBA. FUEL SAMPLE RESULTS WERE BEYOND ALLOWABLE LIMITS. NR 2 ENGINE FUEL CONTROL AND FUEL PUMP WERE CHANGED. FUEL PUMP P/N 6078T39P04 S/N REMOVED CGWT0595 (TT-21042 TC-17580 TSO-5546 CSO-2351 MFGR- GE). 2L72 4F4 FRTA21EA E15NE 20050406000042005040600004NM 2005 4 6 DHL2005782502 120050310A5330 SKIN BOEING727 727227 1384078NM DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 CREASE L/SIDE FUSELAGE SKIN STA 1148 STR 26L. REMOVED INTERCOSTAL IAW B727 SRM 51-30-2 CUT OUT DAMAGED AREA IAW B727 SRM 53-30-3 FIG 24. FAB FILLER SIZE 2" BY 19/16 USING 2024 T3 .100" PO NR 9001576 STRUCTURAL FILLER USING 2024 T3 .063 INCH PO NR 9002039 SIZE 13 1/2" BY 7 3/4" DOUBLER 11 1/8" BY 11 5/8" USING 2024 T3 .125" PO NR 9001673 IAW B727 SRM 53-30-3 FIG 24. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. REINSTALLED INTERCOSTAL IAW B727 SRM 53-30-2 2L73 4F A3WE 20050406000062005040600006NM 2005 4 6 DHL2005782539 120050314A5730 SKIN BOEING727 727227 1384078NM RT WING DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01782DH 21998 DENT ON RT WING L/E ABOVE NR 5 KFLAP (MARKED). CUT OUT DAMAGED AREA DIMENSIONS 1 1/2" BY 1/2" AND FABRICATED REPAIR DOUBLER MATERIAL USE 2024 T3 0.080 PO NR 9002012 DIMENSIONS 5 1/4" BY 5 1/4" IAW B727 SRM=57-30-4 FIG NR 1, PARTS TREATED AND PRIMED IAW B727 SRM=51-10-2. INSTALLED NEW DOUBLER IAW B727 SRM=57-30-4 FIG NR 1 SUBSTITUTED 2024 T3 FOR 2024 T4 IAW B727 SRM=51-20-1 FIG NR 2. 2L73 4F A3WE 20050406000132005040600013NM 2005 4 6 05FDEA00723 120050331A5320ABA7681503 SEAT TRACK DOUG MD11 MD11 3023602NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 MAIN DECK, SEAT TRACK RBL 107 CORRODED AT STA 435. REMOVED AND REPLACED IAW SRM 51-33-01 VOLUME II. 2L73 4F RTA22WE 20050406000422005040600042EA 2005 4 6 QXEA200500516 120050228A5320 FLOOR SUPPORT CNDAIRCL600 CL6002C10 1390015EA ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - FUSELAGE INTERIOR COCKPIT FLOOR SUPPORT ANGLE IS CORRODED AT FS 280. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-23-00-001-001-A01. 2L72 4F RTA21EA 20050406000482005040600048EA 2005 4 6 QXEA200500468 120050303A5230 RETAINER CNDAIRCL600 CL6002C10 1390015EA ZONE 800 GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - FORWARD CARGO DOOR SEAL RETAINER IS GOUGED AND BENT AT TWO CORNERS. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 52-35-07-400-802-A01. 2L72 4F RTA21EA 20050406000492005040600049NM 2005 4 6 SB05041 120050329A335020121 CHARGER BOEING737 7374B7 1384702NM R1 DOOR INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19780AU 24997 CLT - FOUND FORWARD SERVICE DOOR EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE CHARGER AND BATTERY. 2L72 4F RTA16WE 20050606000052005060600005 2005 6 6 UPS05144492 420050518A2565 CYLINDER AIRBUS300 A300B4622R 3930312EU PAX DOOR SLIDE DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01129UP 0813 MAIN CABIN DOOR SLIDE INOPERATIVE. SERVICED FWD DOOR EMERGENCY ACTUATOR CYLINDER PER MM 52-10-14-3. THIS CLEARS M302648. 2L72 4F RTA35EU 20050404001532005040400153NM 2005 4 4 2005UALA00262 120050324A5230 SKIN BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CARGO DOOR DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29937UA 26668 DENT ON FWD SIDE OF FWD CARGO DOOR, MEASURES 1.25 WIDE, .157 DEEP. MAJOR REPAIR ACCOMPLISHED. CAUSED BY CONTACT WITH LOADER. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20050404000222005040400022EA 2005 4 4 A6WA200540117 120050320A5743601R572100621 BUSHING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE RT MLG MIGRATED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31415AW 7593 RT MLG AFT TRUNNION BUSHING IS MIGRATED 0.15 INCH. REMOVED BUSHING, REAMED BARE AND INSTALLED 1ST OVERSIZE BUSHING IAW MFG REO. (K) 2L72 4F4 FRTA21EA E15NE 20050404001092005040400109NM 2005 4 4 USAA050352 120050203A575465C26602224 SKIN BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU NR 5 SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19436US41648 24558 PIT - C5 - SLAT, 3 INCH LONG X 2.5 INCH WIDE - 2 AREAS, DELAMINATION. NR 5 SLAT TOP SURFACE IB AND OB T/E. INSTALED NEW CORE, TOP DOUBLERS, SEAL AND REFINISH IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050404001142005040400114WP 2005 4 4 DHL2005805613 120050318A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE MISDRILLED A DHLAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01805DH80855 46125 MAIN CARGO COMPT FRAME INBOARD FLANGE (2EA) MISDRILLED HOLES STA 1320.000 L-13L L-12L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-05-05 EO AST 050205 DATED 02-21-05. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA AT STA 1320.000 L-12L IAW SRM 51-1-8B. PERFORMED DETAIL VISUAL INSPECTION NO CRACK FOUND. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLES WITH RIVETS (MS20470AD) IAW EO AST050205 SRM 51-1-21 PG 1. 2L74 4F RT4A25 20050404001672005040400167NM 2005 4 4 05FDEA00645 120050325A5347FXSEATRACK03 SEAT TRACK BOEING727 727200 138407ENM MAIN CABIN CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 SEAT TRACK STA 344-480 RBL 45 IS CORRODED AND REQUIRES REPLACEMENT PER EO 7-5340-7- 5002. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2. 2L73 4F RTA3WE 20050405000042005040500004WP 2005 4 5 ASAA0580098 120050215A53305936667501 SKIN DOUG DC9 DC983 3022083WP FUSELAGE DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02943AS 53018 OKC - DURING C-CHECK, FOUND FUSELAGE SKIN DENTED. RECONTOURED DENTED DAMAGED AREA. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050405000082005040500008WP 2005 4 5 ASAA0580115 120050226A532199365051 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - HV-CHECK, FOUND CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050405000902005040500090WP 2005 4 5 ASAA0580116 120050226A53219936651515 FLOORBOARD DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - HV-CHECK, FOUND CABIN FLOOR PANEL IS WATER DAMAGED AND HAS CORRODED FASTENERS. REPLACED FLOOR PANEL. (M) 2L72 4F RTA6WE 20050405001342005040500134EA 2005 4 5 QXEA200500460 120050310A5510 HINGE PIN CNDAIRCL600 CL6002C10 1390015EA ZONE 300 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - VERTICAL STABILIZER HINGE PIN FOR HORIZONTAL STABILIZER HAS EVIDENCE OF CORROSION COMING FROM BEARINGS. REPAIRED IAW REO 670-55-11-021 AND CRJ700 SRM 51-21-16. 2L72 4F RTA21EA 20050405001692005040500169WP 2005 4 5 AALA20050224 120050328A323039567851 LINK DOUG DC9 DC982 3022082WP MLG INOPERATIVE A AALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SW21203AA 49145 STL INFLIGHT T1245/28MAR - AFTER TAKEOFF AND GEAR HANDLE RAISED AIRCRAFT BEGAN VIBRATING TOWARD NOSE AND BELOW OUR FEET. CYCLED GEAR DOWN. VIBRATION REDUCED BUT CONTINUED. RETURNED TO STL AND LANDED WITHOUT INCIDENT. REPLACED RIGHT NOSE GEAR DOOR ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20050405001962005040500196EU 2005 4 5 05FDEA00740 120050331A5410A5451526850600 GUSSET AIRBUS310 A310 EU ZONE 400 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 NR 1 PYLON OUTBD SIDE AT RIB 15 ANGLE HAS 3 SQ INCHES OF CORROSION. REMOVED AND REPLACED GUSSET IAW A310200 SRM 51-72-10. 2L72 4F RTA35EU 20050406000152005040600015NM 2005 4 6 UPS05444213 120050311A5311 FRAME BOEING747 747121 1384871NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 BS 2180 STR 25R FRAME FOUND CRACKED, CRACK LENGTH 1 INCH. FRAME REPAIRED AT BS 2180 STR 25R AREA AS PER HX RS R-53-62-35275 AND UPS EO B747-5310-21972A. 2L74 4F A20WE 20050406000512005040600051NM 2005 4 6 72300071 120050117A5322 ANGLE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 3 INCH AREA OF CORROSION ON REINFORCEMENT ANGLE. 2L73 4F4 FRTA3WE E2EA 20050406000622005040600062NM 2005 4 6 72300072 120050131A5311 FRAME BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 APPROX 2 INCH BY 3 INCH AREA OF CORROSION ON FRAME. 2L73 4F4 FRTA3WE E2EA 20050406000542005040600054NM 2005 4 6 05FDEA00713 120050330A5347 CARGO TRACK DOUG MD11 MD11 3023602NM ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25583FE 48421 MAIN DECK CARGO COMPARTMENT FLOOR TRACK AT STA 635, WL 8.5, FOUND CRACKED APPROXIMATELY 3 INCHES LONG. REPAIR TRACK AND SPLICE FABRICATED AS PER SRM 53-70-00 VOL I, FIG 1 & INSTALLED PER SRM 51-31-01 VOL II. 2L73 4F RTA22WE 20050406000562005040600056NM 2005 4 6 QXEA200500523 120050330A27207G773 SWITCH DHAV DHC8 DHC8202 2809007NM ZONE 200 INOPERATIVE A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09357PH150 504 FLT NUMBER 2118, RETURNED TO FIELD. RUDDER FULL PRESSURE CAUTION ON TAKEOFF, NO OTHER CAUTION LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED RUD FULL PRESS SWITCHES. PERFORMED OPERATIONAL CHECK AND LEAK CHECK, ALL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20050406000592005040600059NM 2005 4 6 05FDEA00818 120050404A5512 SKIN DOUG MD11 MD11 3023602NM ZONE 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25616FE 48747 CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER AFT SKIN PLANK NR 28L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82941. 2L73 4F RTA22WE 20050406000822005040600082SW 2005 4 6 ALGA098989 120050112A6710406310405101 PITCH LINK BELL 407 407 1182206SW MAIN ROTOR WORN B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03404AL140 53479 SEVERE BINDING AND AXIAL PLAY BEYOND MAX. REPLACED BY FIELD MAINTENANCE. 1G71 3U O H2SW 20050406000902005040600090NM 2005 4 6 P9RA20050072 120050315A3350S417N50918MI LIGHT BOEING757 757236 1384971NM AFT CABIN BURNED OUT A P9RAK NONE L NO TEST ININSP/MAINT 1 SO11958PG 24118 AIRCRAFT IN MAINTENANCE FLOOR EMERGENCY TRACK LIGHTS AFT CABIN INOPERATIVE. REPLACED FLOOR TRACK LIGHT ASSY PER MM. 2L72 4F RTA2NM 20050406001092005040600109EU 2005 4 6 05FDEA00568 120050315A5410 RIB AIRBUS310 A310 EU NR 2 PYLON CORRODED A FDEAO OTHER O OTHER NRNOT REPORTED 1 SO25419FE 345 NR 2 PYLON OTBD SIDE RIB 16A UPPER AREA BRACKET LWR AREA HAS AN AREA OF CORROSION EXTENDING UNDER FASTENERS. REMOVED AND REPLACED BRACKET IAW A310-200 SRM 51-72-10. REINSTALLED 3 NUTPLATES IAW A310 SRM 51-40-21. (SEE JPF) 2L72 4F RTA35EU 20050406001122005040600112EU 2005 4 6 ALGA099803 120050307A6230C622A1003102 SWASHPLATE UROCOPEC120 EC120B 8680987EU MAIN ROTOR DEBONDED B ALGAO OTHER O OTHER NRNOT REPORTED 1 SW03512AL255 1148 DEBONDED, REPLACED WITH NEW PART IN FIELD. 1G72 3U NCR0001RD 20050406001242005040600124NM 2005 4 6 ASAA0540130 120050211A53206551629U501 SEAL DEPRESSOR BOEING737 737490 1384715NM CFMINTCFM56 CFM563C1 13802EU FWD GALLEY DOOR CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02713AS 28896 PAE - FWD GALLEY DOOR CUTOUT FWD SIDE SEAL DEPRESSOR CRACKED ABOVE UPPER HINGE CUTOUT. REMOVED AND REPLACED. (K) 2L72 4F4 FRTA16WE E21EU 20050411001842005041100184CE 2005 4 11 2003788 120050207A5511 SPAR BEECH 1900 1900D 1154162CE HORIZONTAL STAB CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM03100UX UE100 DURING ROUTINE STRUCTURAL "I" INSPECTION, FOUR CRACKS WERE IDENTIFIED EMANATING FROM THE DE-ICE HOLE ON THE HORIZONTAL CENTER MAIN SPAR CENTER WEB SKIN APPROX 1 INCH LONG EACH UNDER PANEL 332 ATC. REPAIR WAS MADE AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 20050411002052005041100205EA 2005 4 11 QXEA200500471 120050302A5753 SKIN CNDAIRCL600 CL6002C10 1390015EA ZONE 500 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - LEFT HAND INBOARD FLAP LOWER SURFACE HAS GRAVEL DAMAGE. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, SRM 51-25-01-001-001-A01, AND SRM 57-52-01-101-001-A01. 2L72 4F RTA21EA 20050412002342005041200234WP 2005 4 12 GTIA050055 120050227A5753 SKIN DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE FLAP VANE DENTED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23804NK 49104 LT WING FLAP VANE NR 4 HAS DENT TOP SIDE. REMOVED DAMAGED SKIN AND CORE. FABRICATED NEW CORE AND DOUBLER, TREATED DOUBLER AND BONDED CORE IAW 57-50. (K) 2L72 4F4 F A6WE E9NE 20050412002702005041200270NM 2005 4 12 ASAA054069 120050130A5320654147327 WEB BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - FOUND DAMAGED FLOOR SUPPORT SHEAR WEB AT BS 500E-500F RBL 36 WL 152. REMOVED, FABRICATED AND INSTALLED NEW SHEAR WEB. (M) 2L72 4F RTA16WE 20050412002832005041200283WP 2005 4 12 ASAA080137 120050227A52305910141129 SKIN DOUG DC9 DC983 3022083WP MID CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02965AS 53079 OKC - FOUND HV CHECK, MID CARGO BAY DOOR IS DENTED. INSTALLED REPAIR DOUBLER. (M) 2L72 4F RTA6WE 20050412002962005041200296NM 2005 4 12 ASAA0540058 120050125A5320654795134 RETAINER BOEING737 7374Q8 138447QNM AFT CARGO BAY GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02772AS 25105 PAE - AFT CARGO BAY FLOOR RETAINER STRIP GOUGED. GOUGED OUT OF LIMITS. FABRICATED NEW AFT CARGO BAY FLOOR RETAINER STRIP IAW BOEING DWG 65-47951, AMM 51-40-02 PAGE 1 STEP 2. (M) 2L72 4F RTA16WE 20050412003102005041200310NM 2005 4 12 ASAA0540155 120050303A53206552878102 SILL BOEING737 737490 1384715NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02791AS 28886 PAE - FOUND CORROSION ON AFT ENTRY DOOR MOPSILL. REPLACED MOPSILL. (M) 2L72 4F RTA16WE 20050406000112005040600011NM 2005 4 6 05FDEA00736 120050331A5322 SUPPORT BOEING727 727233 138408ANM SKIN CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25272FE 22037 LWR FUSELAGE, BS 740 R A/C BAY RBL 10, CORROSION EMANATING FROM LWR CHORD AND BULKHEAD. REPAIRED BS470 LOWER CHORD PER FED-EX EA 7-5310-86268. 2L73 4F RTA3WE 20050406000272005040600027NM 2005 4 6 72300068 120050114A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 GOUGED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 .1875 INCH DIAMETER GOUGE ON LOWER FLANGE OF SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050406000282005040600028NM 2005 4 6 72300069 120050205A5322 SHEAR TIE BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 1 INCH BY 4 INCH AREA OF CORROSION ON SHEAR TIE. 2L73 4F4 FRTA3WE E2EA 20050406000442005040600044EA 2005 4 6 QXEA200500478 120050306A5730 ACCESS PANEL CNDAIRCL600 CL6002C10 1390015EA ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09605QX 10022 YYC - LEFT HAND, FUEL PANEL 55100 REBATE IS CORRODED. REPAIRED IAW REO 670-57-00-010, CRJ700 SRM 51-24-11-001-001-A01, AND HORIZON AIR EA R-57-96. 2L72 4F RTA21EA 20050406000572005040600057EU 2005 4 6 05FDEA00737 120050331A5414 ACCESS PANEL AIRBUS310 A310 EU ZONE 400 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25402FE 201 NR 2 PYLON ACCESS PANEL NR 423EL HAS MODERATE CORROSION AROUND INTERIOR SIDE OF ALL FASTENER HOLES. REMOVED CORROSION IAW A310-200 SRM 51-74-10, VERIFIED THREE AREAS OUT OF LIMITS. VERIFIED REPAIR MATERIAL, FABBED THREE EA. REPAIR DOUBLERS AND FILLERS IAW A310-200 SRM 54- 52-51. CUT OUT DAMAGED AREAS IAW A310-200 SRM 54-52-51. APPLIED PROTECTIVE TREATMENT TO FABBED PARTS AND ACCESS PANEL IAW A310-200 SRM 51-21-10. INSTALLED THREE EACH REPAIR DOUBLER AND FILLERS IAW A310-200 SRM 54-52-51. 2L72 4F RTA35EU 20050406000612005040600061CE 2005 4 6 4519203142005 120050314A21306621000000073 VALVE LEAR 45 45LEAR 5170805CE CABIN PRESSURE MALFUNCTIONED E J7SAA UNSCHED LANDING BMJSMOKE/FUMES/ODORS/SPARKS OVER TEMP WARNING INDICATION CLCLIMB 1 SW05433FX 192 SMOKE IN CABIN AND COCKPIT WITH HIGH HEAT ALSO AN AMBER CABIN DUCT OVERHEAT CAS MESSAGE ILLUMINATED. CREW REPORTED IN A CLIMB AMBER ICAS (CAB DUCT OVHT) CAME UP. CREW REPORTED CABIN TEMP WAS SHOWING 91F. CREW SELECTED MANUAL TEMP CONTROL AND NO CHANGE. THE CABIN TEMP CONT CARROT RED X'ED. CREW REPORTED SMOKE STARTED TO COME INTO CABIN. AIRCRAFT RETURNED TO THE AIRPORT. CREW NOTICED NOW THE COCKPIT CONT CARROT RED X'ED AND CABIN CARROT WAS BACK NOW ON THE ICAS. FIRE DEPARTMENT MEASURED CABIN TEMP AND FOUND 114F AFTER THE DOOR HAD BEEN OPEN FOR SOME TIME. EMERGENCY PRESSURIZATION VALVES ARE NOT OPENING. REPLACED LT HIGH PRESSURE VALVE AND ECS CONTROLLER AND CABIN TEMP CONTROL VALVE. OPS CHECK NORMAL 2L72 4F RTT00008WI 20050406000982005040600098NM 2005 4 6 05010 120050204A3600 DUCT BOEING747 7472B4B 138481BNM PWA JT9 JT9D7J 52054NE 8TH STAGE LOOSE A KCSAO OTHER MJ OVER TEMP WARNING INDICATION CRCRUISE 1 GL23713CK 21099 662450 AT FL 34.0, NR 2 ENG START VALVE LIGHT ILLUMINATED; FOLLOWED CHECKLIST. NR 2 THROTTLE SEIZED; RAN SEVERE DAMAGE CHECKLIST. ALL ENGINE INDICATIONS NORMAL. PERFORMED VISUAL INSPECTION TO ENGINE. FOUND 8TH STAGE BLEED DUCTS LOOSE AND START VALVE DAMAGED. INSTALLED SERVICEABLE 8TH STAGE DUCTS AND STARTER LEAK AND OP'S CHECK GOOD IAW B747 MM 71-00-00. 2L74 4F4 FRTA20WE E20EA 20050406001002005040600100NM 2005 4 6 72300001 120050202A5340 STRINGER CLIP BOEING727 7272H3 138368NNM PWA JT8 JT8D9A 52048NE ZONE 100 CORRODED A K11AK NONE O OTHER ININSP/MAINT 1 GL23723CK 20545 APPROX 1 INCH BY 2 INCH AREA OF CORROSION ON STRINGER SLIP. 2L73 4F4 FRTA3WE E2EA 20050406001192005040600119NM 2005 4 6 ASAA0540031 120050118A5350654865790 FRAME BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU RT FAIRING DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02755AS 25096 PAE - RT AFT WING -TO-BODY FAIRING FORMER HOLES ELONGATED. REMOVED AND INSTALLED NEW T-ANGLE IAW SRM. (K) 2L72 4F4 FRTA16WE E21EU 20050406001392005040600139NM 2005 4 6 ASAA0510001 120050128A29106544510 HYDRAULIC LINE BOEING737 737290C 138448VNM PWA JT8 JT8D17 52049NE HYDRAULIC SYS CRACKED A ASAAK NONE J WARNING INDICATION APAPPROACH 1 NM02730AS 22577 SEA - WHILE EXTENDING FLAPS TO NR5 POSITION, HYDRAULIC LOW-PRESSURE LIGHTS ILLUMINATED. QUANTITY WENT TO ZERO. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED (A) SYSTEM HYDRAULIC PRESSURE LINE. ACCOMPLISHED CONDITIONAL INSPECTIONS. RETURNED TO SERVICE. (K) 2L72 4F4 F A16WE E2EA 20050406001402005040600140NM 2005 4 6 ASAA0540142 120050223A2424948F4583 GCU BOEING737 7374Q8 138447QNM CFMINTCFM56 CFM563C1 13802EU E/E BAY MALFUNCTIONED A ASAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM02774AS4385 385 25107 SEA - ATB SMOKE IN FLIGHT DECK THROUGH 1000 FT. COMING FROM G4 AND G5 AREA, BEHIND F/O AREA. TROUBLESHOT NR 2 ENG GCU. INSPECTED AREA NEAR P-6 C/B PANELS, EE COMPARTMENT, AND NR 2 ENGINE GENERATOR. REPLACED NR 2 GCU. ENGINE RUN, OPS CHECK NORMAL. GCU RECEIVED UNSERVICEABLE. INSP SHOWED INTERNAL PWR SUPPLY CIRCUIT OVERHEATED AND TRANSFORMER T901 AND DIODE CR909 HAD OVERHEATED AND BURNED. TRANSFORMER AND DIODES TO BE REPLACED. UNIT REQUIRES COMPLETE CLEANING TO REMOVE BURNED COMPONENTS AND RESIDUE. (K) 2L72 4F4 FRTA16WE E21EU 20050411001812005041100181EU 2005 4 11 F3LA200500003 120050120A2150 DUCT AIRBUSA318 A318111 3940019EU WATER EXTRACTOR MISINSTALLED A F3LAO OTHER WB INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM03804FR 2051 ON ARRIVAL, CREW REPORTED FUMES IN COCKPIT. F/A REPORTED SMELL IN AFT CABIN. A/C RETURNED TO MDW & LANDED W/O INCIDENT. REMOVED BELLY FAIRINGS FOR ACCESS TO LT PACK. INSPECTED PACK DUCTING & FOUND VASELINE ON DUCT SEALS & JOINTS. REMOVED WATER EXTRACTOR SEALS & JOINTS, REMOVED VASELINE, & RENSTALLED WATER EXTRACTOR. REMOVED DUCT BETWEEN MAIN HEAT EXCHANGER & ACM. CLEANED SEALS & JOINTS & REMOVED VASELINE. REINSTALLED DUCT. REMOVED ANTI-ICE VALVE/PRIMARY HEAT EXCHANGER BYPASS DUCT. CLEANED VASELINE FROM SEALS & JOINTS. REINSTALLED DUCT. REMOVED REHEATER DUCTING. CLEANED RESIDUE FROM SEALS & DUCTS. REINSTALLED REHEATER DUCTING. PERFORMED OPS CHECK OF LT PACK USING APU BLEED. OPS TEST NORMAL. 2L72 4F RT 20050411001972005041100197SO 2005 4 11 C2XA05IA050 120050322A5610163500111 WINDSHIELD EMB 145 EMB145XR 3260214SO COCKPIT BURNED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW27171385004 5004 145727 IAH - FLIGHT 3229, THE CREW REPORTED THE NUMBER TWO PACK CAUSED A BURNING SMELL DURING DESCENT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NUMBER TWO PACK TO BE OPERATING NORMALLY, FURTHER INSPECTION REVEALED THE CAPTAINS WINDSHIELD TERMINAL BLOCK WAS BURNT. THE CAPTAINS WINDSHIELD WAS REMOVED AND REPLACED, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20050412002242005041200224WP 2005 4 12 05FDEA00320 120050228A2550 PANEL DOUG DC10 DC1010F 3022111WP CARGO BAY CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568053 47807 COMPLY WITH EA8-2550-55440, EQUIP/FURNISHINGS LWR CARGO, REPAIR OF STA 1841 CENTER/AFT PARTITION. COMPLIED WITH EA8-2550-55440. 2L73 4F A22WE 20050412002262005041200226WP 2005 4 12 05FDEA00322 120050301A5753ARC1953 SKIN DOUG MD10 MD1010F 3022112WP T/E FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25361FE 48260 RIGHT OUTBOARD FLAP WEDGE TOP SKIN STATION XFO 560 TO 575 HAS 3 EACH PREVIOUS REPAIRS WITH TEMPORARY FASTENERS. REMOVED DAMAGED SKIN IAW DC10 SRM 51-35-01 VOL II, FABRICATED NEW SKIN IAW DAC DWG NR ARC1953. INSTALLED SKIN IAW DC 10 SRM 51-35-01 VIL II AND FEDEX EA 8-5710-83982, WINGS RIGHT OUTBOARD FLAP WEDGE, TOP SKIN REPAIR. REFERENCE NON-ROUTINE N00341. 2L73 4F RTA22WE 20050412002532005041200253WP 2005 4 12 GTIA050076 120050326A2797 WIRE DOUG DC9 DC983 3022083WP PWA JT8 JT8D217A 52053NE RUDDER CONTROL BROKEN A GTIAK NONE P NO WARNING INDICATION ININSP/MAINT 1 GL23808NK 49504 UPON PREFLIGHT (COCKPIT SETUP) COULD NOT GET RUDDER CONTROL MANUAL LIGHT DURING TEST, AIRCRAFT TAIL SWAP TO 817NK. TROUBLESHOT DOWN TO BROKEN WIRE AT CANT. STA 1485, REPAIRED BROKEN WIRE IAW SRM. OPS CHECK, OK. (K) 2L72 4F4 FRTA6WE E9NE 20050412002552005041200255WP 2005 4 12 GTIA050047 120050118A5315 FLOORBEAM DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE FUSELAGE CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23800NK 49144 AFT PIT FS 1338 APB FWD SIDE LOTER T-CHORD CORRODED L28L TO L28R. REMOVED CORROSION OUT OF LIMITS, REMOVED T-CAP (CHORD) STA 1338, L28L TO L29L, DRILLED AND LOCATED NEW T-CAP STA 1338. OK TO TOP COAT AND INSTALL NEW T-CAP. (K) 2L72 4F4 F A6WE E9NE 20050412002792005041200279NM 2005 4 12 ASAA0540145 120050224A1430654587523 NUT BOEING737 7374Q8 138447QNM R1 DOOR MISSING A ASAAK NONE O OTHER ININSP/MAINT 1 NM02756AS 25097 PDX- FOUND R1 DOOR WOULD NOT OPEN. FOUND UPPER GEAR CONTROL ROD RETAINING NUT MISSING AND BOLT FELL OUT. SECURED UPPER CONTROL ROD BOLT AND RETAINING NUT. ALL RIG AND OPS CHECKS GOOD. 2L72 4F RTA16WE 20050413000022005041300002EU 2005 4 13 ASOA05185 120050204A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE SEAT TRACKS BETWEEN FRAME 36 AND 39 LEFT/RIGHT WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS BETWEEN FRAME 36 AND 39 LT/RT IAW SRM 51-25-04. (M) 2H72 4T RTA53EU 20050413000032005041300003EU 2005 4 13 ASOA05184 120050204A5320S53371293201 SUPPORT AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE SUPPORT PLATE BETWEEN FRAME 13-17 LEFT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SUPPORT PLATE BETWEEN FRAM 13-17 LEFT IAW SRM 53-31-00, 51-21-42 AND 51-25-01. (M) 2H72 4T RTA53EU 20050413000062005041300006EU 2005 4 13 ASOA05177 120050202A5714 ANGLE AEROSPATR72 ATR72212 8680945EU WINGBOX CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE ANGLE IN THE WING BOX AT FS 28 RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE ANGLE IN THE WING BOX AT FS 28 RT IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20050413000212005041300021EU 2005 4 13 ASOA05187 120050204A5315 FLOORBEAM AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE FLOORBEAMS AT FRAME 38/40 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANANCE REMOVED AND REPLACED THE FLOORBEAMS AT FRAME 38/40 IAW SRM 51-25-01. (M) 2H72 4T RTA53EU 20050413000222005041300022EU 2005 4 13 ASOA05186 120050204A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27633AS 344 DURING A C-CHECK IN YUL, THE SEAT TRACK BETWEEN FRAME 39 AND 40 RIGHT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK BETWEEN FRAME 39 AND 40 RT IAW SRM 51-25-04. (M) 2H72 4T RTA53EU 20050413000322005041300032EA 2005 4 13 ASOA05233 120050314A3350 LIGHT CNDAIRCL600 CL6002C10 1390015EA CABIN MALFUNCTIONED A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27718EV 10095 FLT 4911 - DURING A GROUND INSPECTION IN SLC, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE RESET CIRCUIT BREAKER P2U3. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20050413000702005041300070SO 2005 4 13 SIMA200507508 120050306A531314533888001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21655AE 145452 ABI - DURING INSPECTION OF AIRCRAFT, STRINGER 19R WAS FOUND CHAFED. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/1147 PARA 8 DATED MARCH 3, 2005. (M) 2L72 4T RTT00011AT 20050413000722005041300072SO 2005 4 13 SIMA200507509 120050304A532014522178005 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21655AE 145452 ABI - DURING INSPECTION OF THE AIRCRAFT, FOUND THE SERVICE DOOR CENTER SILL CORRODED. BLENDED THE CENTER SILL TO REMOVED THE CORROSION AND PERFORMED NDT INSPECTION. FABRICATED THREE REPAIR DOUBLERS, REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 28, CHAPTERS 53-21-02. (M) 2L72 4T RTT00011AT 20050413000902005041300090SO 2005 4 13 SIMA200507519 120050308A532013500469401 ANGLE EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21705AE 145184 SAW - DURING CPCP INSPECTION, FOUND Z-ANGLE AT FRAME 22A CORRODED. RAI'D ANGLE AT FRAME 22A IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTT00011AT 20050413000962005041300096EU 2005 4 13 USAA050012 120050101A5347 SEAT TRACK AIRBUS330 A330323 3930335EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19670UW 0315 BFM - FOUND SEAT TRACK CORRODED .640 INCH LONG BY .125 INCH WIDE BY .038 INCH DEEP AREA, Y+450. CORROSION LEVEL 2, TASK NR J7-200-2580C. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-15, 53-00-10, 51-42-11, 51-21-11, 51-42-11. (M) 2L72 4F RTA46NM 20050414000162005041400016WP 2005 4 14 UPS05844251 120050321A5531 RIB DOUG DC8 DC873F 302199FWP VERTICAL STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C2, VERTICAL FIN L/E HAS CRACKED RIB .75 INCH AT ACCESS PNL 51F. REPAIRED VERTICAL FIN RIB IAW DC-8 SRM 55-02-00 FIG 002 AND SRM 51-1-20D. 2L74 4F RT4A25 20050414000172005041400017WP 2005 4 14 UPS05844252 120050318A5712 RIB DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 INSPECTION TYPE: C2, RIGHT WING L/E UPPER RIB CRACKED .5 INCH LONG AT STA XRS 727, VIEW FROM PANEL 518A. REPAIRED RIGHT WING L/E UPPER RIB AT STA XRS 727 IAW DC-8 SRM 57-2-0. 2L74 4F RT4A25 20050404001452005040400145NM 2005 4 4 2005UALA00256 120050318A5330147W4350 SKIN BOEING777 777222 1385219NM PWA PW4077PW4077 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29778UA35305 26940 FUSELAGE SKIN IS DENTED JUST FWD OF FUSELAGE STA 2108 AT STR 24R. *S/D* EXISTING DENT RE-EVALUATED AND REPAIRED AT BS 2108, STR 24R. REPAIR WAS ACCOMPLISHED BY UA-EVA-50137. 2L72 4F4 FRTT0001SE E46NE 20050405000552005040500055WP 2005 4 5 ASAA0580063 120050131A5320993053857 WEB DOUG DC9 DC983 3022083WP FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02948AS 53021 OKC - DURING C-CHECK, LONGERON CUSP WEB CRACKED IN FORW