20081028 NM 2008 10 28 DHL2008F00033 120040918A2612 FIRE LOOP BOEING727 7272B7 138407LNM MLG WW MALFUNCTIONED A DHLAO OTHER N FALSE WARNING CRCRUISE 1 GL05770AT 21953 IN CRUISE FLIGHT, HAD 3 INSTANCES OF MOMENTARY FIRE WARNING BELL WITH A FLICKER OF WHEEL WELL FIRE WARNING LIGHT. PERFORMED CONTINUITY TEST OF ENGINE AND WHEEL WELL FIRE LOOPS, TEST OK. INSPECTED WHEEL WELL WIRING AND FIRELOOPS, NO DEFECTS FOUND. COULD NOT DUPLICATE PROBLEM. REPLACED FIRE AND OVERHEAT ASSY UNIT AS PRECAUTIONARY IAW B727 MM 26-12-0, OPS CHECK OK. ACFT WAS GROUNDED. (K) 2L73 4F A3WE 20081028 EU 2008 10 28 VY12008F00000 120041109A6520350A33020004 GEARBOX SNIAS 350 AS350B 8680801EU TAIL ROTOR DESTROYED L VY1RK NONE O OTHER ININSP/MAINT 1 SW19655TV 1590 PERFORMED A PRELIMINARY REVIEW OF THE SERVICE HISTORY OF THE GEARBOX THAT WAS RECEIVED FOR OVERHAUL. IT WAS DETERMINED THAT THE GEARBOX WAS INVOLVED IN AN ACCIDENT. BASED ON THE ACCIDENT THAT OCCURRED ON 9 NOV 2004, MFG HAS DETERMINED THAT ALL DYNAMIC COMPONENTS INSTALLED ON THIS ACFT AT THE TIME OF THE CRASH ARE NOT TO BE RETURNED TO SERVICE FOR ANY REASON. THE LOG CARD RECEIVED WITH THE GEARBOX DID NOT INDICATE THAT IT WAS INVOLVED IN AN ACCIDENT. RECOMMENDS THAT THIS COMPONENT AND ALL INTERNAL SUBCOMPONENTS BE MULATED IN A MANNER TO PREVENT THEM FROM BEING INTRODUCED INTO SERVICE FOR INSTALLATION ON A TYPE CERTIFICATED PRODUCT. AE HAS PERMANENTLY IDENTIFIED THE GEARBOX AS SCRAP. 1G71 3U H9EU 20040809000552004080900055EU 2004 8 9 ASOA04316 120040413A5320S5367800821602 FLOOR SUPPORT AEROSPATR72 ATR72 EU FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11642AS 395 DURING A C-CHECK IN YUL, THE ZEE FLOOR SUPPORT ON THE RIGHT SIDE FROM FRAME 39 TO FRAME 41 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE ZEE FLOOR SUPPORT ON THE RT SIDE FROM FRAME 39 TO FRAME 41 IAW SRM 51-25-01. (M) 2H72 4T RT 20040219000012004021900001EA 2004 2 19 COMA0460132 120040206A3010 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM ILLUMINATED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01938CA 7046 FLIGHT 5806 WING ANTI ICE CAUTION MESSAGE. COULD NOT DUPLICATE. OPERATIONAL CHECK NORMAL. 2L72 4F RTA21EA 20040219000152004021900015NM 2004 2 19 UPS04441861 120040123A5320BAC1509100312 CHANNEL BOEING747 747123 1384873NM MAIN DECK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, M/D- BS 2320 TO 2350 LBL 40 HAT SECTION FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.040 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. HAT SECTION REPLACED PER SRM 51-10-01 PG 8 & P/N: BAC1509-100312-7075T6511. CIC APPLIED IAW CPM 53-10-17. 2L74 4F A20WE 20040219000172004021900017NM 2004 2 19 UPS04441863 120040127A5315HXC108662 FLOORBEAM BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C M/D- RT STA 2240 FLOORBEAM LOWER SECTION FOUND CORRODED IN BETWEEN RBL 6 AND RBL 40. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.050 X 1 X 2 INCH EXCEED SRM 53-10-01 LIMITS. STA 2240 RBL 30 FLOORBEAM LOWER SECTION REPAIRED AS PER SRM 51-40-04 FIG 2. CIC APPLIED IAW CPM53-10-17. 2L74 4F A20WE 20040219000292004021900029SO 2004 2 19 C2XA04SH067 120040216A531514522461011 DOUBLER EMB 135 EMB135LR 3260305SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK THE RIGHT HAND FLOORBEAM DOUBLER CAP AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040219000302004021900030SO 2004 2 19 C2XA04SH068 120040216A531514522461011 DOUBLER EMB 135 EMB135LR 3260305SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK THE RT FLOORBEAM DOUBLER CAP AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER CAP IAW EMB135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040219000372004021900037SO 2004 2 19 C2XA04SH070 120040216A531514522226003 BUTTSTRAP EMB 135 EMB135ER 3260203SO FLOORBEAM CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK THE CENTER FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED IN THE LAVATORY BETWEEN FRAMES 55 AND 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040219000382004021900038SO 2004 2 19 C2XA04SH069 120040216A532014522460015 BUTTSTRAP EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714508 145220 SHV- DURING C-CHECK THE AFT DIGITAL BUTTSTRAP AT FRAME 16 TO FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040219000422004021900042EU 2004 2 19 MALA040186 120040205A5330 SHIELD SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15361PX 340B249 DURING 4K INSPECTION IN LCQ, LT FUSELAGE AFT OF NR 2 ICE SHIELD HAS NUMEROUS DENTS. FABRICATED AND INSTALLED 2 EACH EXTERNAL DOUBLERS IAW MESABA EO NR S53009. REFER TO 409 NR 1258951 FOR FURTHER DETAIL. A/C RELEASE DATE 2/16/04. 2L72 4T RTA52EU 20040219000442004021900044EU 2004 2 19 MALA040180 120040207A2130 CIRCUIT BREAKER SAAB SF340 SF340A 7850100EU CABIN PRESS CONTMALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15106XJ 340A106 AFTER TAKEOFF, TURNED BLEED VALVES TO OPEN, AND HAD A RAPID RATE OFF DECELERATION IN CABIN RATE AND CABIN ALTITUDE. AIR RETURN TO CWA. MAINTENANCE RESET CABIN PRESSURE CONTROL CIRCUIT BREAKER. PRESSURIZATION SYSTEM OPS CHECK GOOD. VISUALLY INSPECTED WIRING BEHIND LT C/B PANEL. NO DEFECTS NOTED. 2L72 4T RTA52EU 20040219000462004021900046EU 2004 2 19 MALA040179 120040207A2612 CONNECTOR SAAB SF340 340B 7860101EU LT NACELLE CONTAMINATED A MALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL15441XJ 340B441 IN CRUISE FLT THE LT FIRE DETECT FAIL CWP CAUTION LIGHT REPEATEDLY CYCLED ON & OFF. LIGHT WOULD GO OUT FOR 3 SECONDS AND COME BACK ON, QRH COMPLETE. AIR RETURN TO MQT. MAINTENANCE FOUND CONTAMINATED CONNECTOR AT ENGINE NACELLE, CLEANED & SAFTETIED. OPS CHECK GOOD. SEE CONTINUATION CARDS NR 062320 & NR 062319 FOR FURTHER DETAIL. 2L72 4T RTA52EU 20040219000502004021900050WP 2004 2 19 04FDEA00405 120040213A5753 SKIN DOUG DC10 DC1010 3022110WP TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568053 47807 RIGHT WING OUTBOARD FLAP VANE, NR 3 FLAP VANE ATTACH HORN HAS TWO CORRODED/PITTED HOLES. REPLACED PER M/M 27-50-03-2 AND TORQUED PER M/M 20-50-20. 2L73 4F A22WE 20040219000512004021900051WP 2004 2 19 04FDEA00404 120040213A5753 SKIN DOUG DC10 DC1010 3022110WP TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568053 47807 RIGHT WING OUTBOARD FLAP VANE NR 2 FLAP VANE ATTACH HORN HAS 2 CORRODED/PITTED HOLES. REPAIRED PER EA 8-5750-68462. 2L73 4F A22WE 20040219000522004021900052WP 2004 2 19 04FDEA00403 120040213A5753 HORN DOUG DC10 DC1010 3022110WP TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568053 47807 RIGHT WING OUTBOARD FLAP VANE NR 1 FLAP VANE ATTACH HORN HAS PITTED AFT HOLE. 2L73 4F A22WE 20040219000552004021900055NM 2004 2 19 SWAA040406 120040208A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29604SW 27955 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON AFT PRESSURE BULKHEAD WEB AT BS 1016, LBL 2 TO RBL 2. REPAIRED WEB PER ACO. 2L72 4F RTA16WE 20040219000882004021900088NM 2004 2 19 PCAA0402163 120040203A3150V319 SWITCH DHAV DHC8 DHC8102 2809003NM LT CONTROL LEVERSTICKING A PCAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA13839EX 226 FLIGHT 3755 FROM SYRACUSE HAD TO RETURN TO GATE DUE TO RECEIVING THE TAKEOFF WARNING HORN WITH THE AIRCRAFT PROPERLY CONFIGURED FOR TAKEOFF. MAINTENANCE FOUND THE LT CONDITION LEVER SWITCH 3151-S3 TO BE STICKING. MAINTENANCE REPLACED SWITCH AND OPERATIONAL CHECKED SYSTEM, ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040219000962004021900096NM 2004 2 19 SWAA040362 120040204A53106546581 DOOR FRAME BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29687SW 23388 DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR FRAME CUTOUT CRACKED AT DOOR STOP. REPAIRED R1 DOOR FRAME CUTOUT PER SRM. 2L72 4F RTA16WE 20040219001012004021900101NM 2004 2 19 SWAA040342 120040203A53116546546 FRAME BOEING737 7372T4 1384492NM WINDOW BELT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29722WN 22698 DURING SCHEDULED SPV, FOUND RT SIDE OF FUSELAGE WINDOW BELT FRAMES CRACKED AT BS 842, BS 822, BS 365, BS 385. REPAIRED WINDOW BELT FRAMES PER EA. 2L72 4F A16WE 20040219001022004021900102NM 2004 2 19 SWAA040343 120040203A53126516300 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29361SW 26572 DURING SCHEDULED SPV, FOUND 2 EACH CRACKS ON WEB AT BS 178, WL 217, LBL 11 AND AT BS 178, WL 207, LBL 24. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20040219001072004021900107NM 2004 2 19 SWAA040348 120040203A53116546533 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME CRACKED AT BS 492, STRINGER 24R. REPAIRED FRAME PER ER. 2L72 4F RTA16WE 20040219001152004021900115NM 2004 2 19 SWAA040214 120040121A53116546650 FRAME BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED 1/2D CHECK, FOUND FRAME CORRODED AT BS 787, STRINGER 25R. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040219001232004021900123NM 2004 2 19 SWAA040222 120040122A53126546568 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED SERVICE CHECK, FOUND BULKHEAD WEB CORRODED AT BS 1016, BL 0. REPAIRED WEB PER ACO. 2L72 4F RTA16WE 20040219001252004021900125 2004 2 19 SWAA040224 420040122A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR DISLODGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29318SW 23339 L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM. 2L72 4F RTA16WE 20040219001342004021900134NM 2004 2 19 SWAA040233 120040122A5312 CAP BOEING737 7373A4 1384585NM BULKHEAD CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SCHEDULED C2 CHECK, FOUND AFT PRESS BULKHEAD AT BS 1016, CRACKED AT CENTER CAP. REPAIRED PER EA. 2L72 4F RTA16WE 20040219001362004021900136EA 2004 2 19 COMA0460105 120040203A5551600210617 BUSHING CNDAIRCL600 CL6002B19 1900309EA VERTICAL STAB LOOSE A COMAK NONE O OTHER ININSP/MAINT 1 SO01977CA 7157 BUSHING IN VERTICAL STABILIZER LEFT HAND LUG FOR HORIZONTAL STAB PIVOT POINT MIGRATED .029 INCHES. REMOVED AND REPLACED BUSHING. 2L72 4F RTA21EA 20040219001662004021900166 2004 2 19 SWIA200412843 420040201A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 NM07567SW8727 8727 120342 CREW REPORTS NR 1 AUTOPILOT WON'T CAPTURE HDG. REMOVED AND REPLACED NR 1 AUTOPILOT COMPUTER IAW MM 22-10-02. OPS CHECK GOOD IAW MM 22-10-00. 2L72 4T RTA31SO 20040219001852004021900185NM 2004 2 19 CALA0400079 120040122A5320 FLANGE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2734315 23366 INSPECTION FOUND THE UPPER SURFACE OF THE FORWARD FLANGE OF THE ZEE FRAME CORRODED AT STA 270, BL 0.0. THE FRAME WAS REPAIRED IAW ECRA 5321-01169. 2L72 4F RTA16WE 20040219001872004021900187CE 2004 2 19 DXTA200400235 120040130A3234 CONTROL HANDLE CESSNA750 750 2076810CE MLG MALFUNCTIONED E DXTAA UNSCHED LANDING O OTHER CLCLIMB 1 GL07953QS 7500153 AFTER TAKEOFF GEAR HANDLE STUCK IN THE DOWN POSITION, COULD NOT RETRACT GEARS, ACCOMPLISHED AIR TURNBACK. TROUBLESHOT NOSE GEAR SQUAT SWITCH, ALL WIRING CHECKED GOOD. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE, AIRCRAFT REQUIRES OCF FOR LANDING GEAR CONTROL SYSTEM. ALL WORK DONE IAW CESSNA 750 MM CHAPTER 32-30-00. 2L72 4J RTT00007WI 20040219001922004021900192NM 2004 2 19 04FDEA00317 120040205A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT WING, FOUND OUTBOARD FLAP, INBOARD FWD HINGE ACTUATOR HOLE (8) INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75243. TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBD FLAP. INBD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040219001942004021900194NM 2004 2 19 04FDEA00319 120040205A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT WING - FOUND OUTBOARD FLAP, INBOARD FWD HINGE MOUNT HOLE (7) INBOARD SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75243 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD FLAP. INBD. HINGE BRACKET REPAIR 2L73 4F RTA22WE 20040219002162004021900216NM 2004 2 19 QXEA200400107 120040127A5730 PANEL DHAV DHC8 DHC8202 2809007NM ZONE 500 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09356PH 502 PDX - LEFT WING PANEL 522AT COUNTER SINKS HAVE FRETTING FROM SCREWS AT INBOARD AND OUTBOARD ENDS. REPAIRED IAW DHC-8-200 SRM 51-20-16. 2H72 4T RTA13NM 20040219002182004021900218NM 2004 2 19 QXEA200400109 120040128A5520 FITTING DHAV DHC8 DHC8202 2809007NM ZONE 300 SCRATCHED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09356PH 502 PDX - LEFT HAND FORWARD HORIZONTAL STAB SPAR FITTING SCRATCHED. REPAIRED IAW RD 8-55-847. 2H72 4T RTA13NM 20040219002262004021900226EA 2004 2 19 QXEA200400117 120040206A26119847101505 CHIMNEY CNDAIRCL600 CL6002C10 1390015EA ZONE 200 DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09612QX 10042 FORWARD CARGO COMPARTMENT CHIMNEY IS DAMAGED. REMOVED AND REPLACED CHIMNEY. OPEATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040219002412004021900241SO 2004 2 19 C2XA04BT019 120040206A2120P1097 FILTER EMB 145 EMB145LR 3260212SO FAN FAULTY A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2716561 145610 CREW REPORTED, MELTING PLASTIC ODOR FOLLOWED BY BLEED NR 2 OVERHEAT WHILE IN ICING CONDITIONS. MAINTENANCE PERFORMED FIM TASK 36-11-00-810-803A, REMOVED AND REPLACED FAN AIR VALVE FILTER IAW EMB145 MM 36-11-03. PERFORMED OPS CHECK IAW EC3610-01062 STEPS 2.4 THROUGH 2.12. NO BURNING SMELL NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20040219002482004021900248NM 2004 2 19 CALA0400085 120040207A5320 INTERCOSTAL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND A 6 INCH CRACK IN INTERCOSTAL BETWEEN STA 344 AND 360, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040220000142004022000014EA 2004 2 20 COMA0460120 120040205A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01967CA 7134 FLIGHT 5242 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. 2L72 4F RTA21EA 20040220000162004022000016EA 2004 2 20 COMA0460122 120040203A3230555405 SELECTOR VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01964CA 7129 FLIGHT 5351 NOSE DOOR OPEN WARNING DURING GEAR RETRACTION. REPLACED THE NLG DOOR SELECTOR VALVE. 2L72 4F RTA21EA 20040220000282004022000028WP 2004 2 20 UPS04841824 120040106A53205888479 ANGLE DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE: C1, SHEARED RIVET HEAD, BULGE & CORRODED SHEAR WEB ABOVE & BELOW L21R CUSP MAIN CABIN COURIER AREA FS 25. REMOVED FRAME FITTING AND FLOOR SUPPORTS TO FOM, REMOVED CUSP ANGLES AND FABRICATED NEW ANGLE IAW DC8 SRM 53-3-3 AND DAC DWG 5888479. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW CUSP ANGLES, FRAME FITTING AND FLOOR SUPPORTS IAW DC8 SRM 51-1-20D, 51-3-0. 2L74 4F RT4A25 20040220000302004022000030WP 2004 2 20 UPS04841826 120040107A5310 SHEAR TIE DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE: C1, UPPER CARGO BETWEEN STA 1000-1020 AT LONG 13L SHEAR TIE IS CRACKED. REMOVED FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D. FABRICATED NEW SHEAR TIE IAW DC8 SRM 53-4-1 FIG 51 AND 51-1-24. HEAT TREAT TO 7075-T6 .080 IAW TPS 1003 REV A. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 20040220000472004022000047WP 2004 2 20 UPS04841851 120040205A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP EMERGENCY LIGHT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01750UP UPS2964 45950 EMERGENCY LIGHTS INOP DUE TO POWER ON AC AND LIGHT SWITCH LEFT IN ARMED POSITION. REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK. 2L74 4F RT4A25 20040220000532004022000053NM 2004 2 20 AWXA200400157 120040207A2120 ODOR AIRBUSA319 A319132 3930340NM COCKPIT/CABIN DETECTED A AWXAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 WP28820AW11483 1397 AN ELECTRICAL BURNING ODOR OBSERVED IN THE COCKPIT & CABIN NEAR SEAT ROW 4, DECLARED EMERGENCY, LANDED WITHOUT FURTHER DIFFICULTIES. MX REMOVED AFT WALL OF FWD BAG PIT & INSPECTED RECIRCULATION FANS & DUCTING FOR EVIDENCE OF OVERHEATING & ODOR, NO DEFECTS NOTED. DUE TO FAILURE HISTORY: REPLACED AVIONICS COOLING FAN (18HQ) IAW AMM 21-26-51-401, OPERATIONAL CHECK WAS GOOD. FUNCTIONAL CHECK OF AVIONICS COOLING FAN CONFIRMED FAILURE, BEARING NOISE COULD BE HEARD DURING TEST. R & R WORN BEARINGS & BALANCED ROTOR & MOTOR IMPELLER IAW CMM. RE-TEST OF UNIT GOOD. 2L72 4F RTA28NM 20040220000602004022000060NM 2004 2 20 AALA20040202 120040205A3350 WIRE BOEING757 757223 1384957NM EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21688AA 25730 DFW EMERGENCY LIGHT AT SEAT 22 INOPERATIVE. FOUND LOOSE WIRE. REINSTALLED WIRE CONNECTION FOR EMERGENCY LIGHT AT SEAT 22. SYSTEM GROUND CHECKED NORMAL OPERTION. 2L72 4F RTA2NM 20040220000682004022000068WP 2004 2 20 AALA20040199 120040206A335060030451 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21588AA 53251 DFW CEILING EMERGENCY LIGHTS AT ROWS 3 TO 7 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 3 TO 7. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040220000732004022000073NE 2004 2 20 AALA20040204 220040207A7320 FUEL CONTROL DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE ZONE 600 INOPERATIVE A AALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW219624T 53594 717857 DFW AT 10,000 FT AS POWER CAME UP THE RIGHT ENG INITIALLY CAME UP THEN DROPPED QUICKLY TO .92 EPR THEN SURGED UP TO ABOUT 1.8 EPR AND THEN IMMEDIATELY DROPPED TO .09 EPR. ENGINE WINDMILLED. RETURNED TO DFW. AIRCRAFT WAS NOT OVERWEIGHT AND LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND ENGINE FUEL PUMP AND FUEL CONTROL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA6WE E9NE 20081028 NM 2008 10 28 KNN2008F00003 120040918A5340 STRINGER CLIP BOEING737 737291 138448WNM FUSELAGE DAMAGED A KNNAO OTHER O OTHER NRNOT REPORTED 1 WP25977UA 21508 WHILE COMPLYING WITH AD 93-08-04 AND SB 737-53-1268. DURING THE CURRENT C-CHECK. WE FOUND STRINGER CLIP THAT FAILED NDT INSPECTION. THE STRINGER CLIP WAS REPLACED IAW SB-737-53-1268. ALL SUPPLEMENTAL INSPECTIONS WERE ALSO COMPLIED WITH IAW THE SB. (K) 2L72 4F A16WE 20040809000752004080900075EA 2004 8 9 COMA0470059 120040726A32406007300 SENSOR CNDAIRCL600 CL6002C10 1390015EA RT MLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01354CA 10064 FLT 5524 BRAKE OVERHEAT WARNING. REPLACED THE RT OUTBOARD BRAKE TEMP SENSOR. 2L72 4F RTA21EA 20010111041292001011104129WP 2001 1 11 SPAA0000035 120040106A2700369A7304 BRACKET HUGHES369 369D 4470706WP ALLSN 250C 250C* GL FLIGHT CONTROLS DAMAGED B EOORK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03511SB11913 1090592D FOUND BUSHINGS IN CONTROL BRACKET MOVING. UPON REMOVAL, IT WAS DISCOVERED THAT THE BUSHINGS WERE INSTALLED WITH SOME SORT OF HARD FILLER APPARENTLY TO KEEP THE BUSHINGS FROM MOVING. BUSHING HOLES ELONGATED BEYOND LIMITS. REPLACED UNIT. SEE SOR NR 300195 (K) (ALO3200411231) 1G71 3U3 U H3WE E4CE 20041109000172004110900017WP 2004 11 9 ABXA040358 120041018A55305912101501 BRACKET DOUG DC9 DC931 3022065WP VERTICAL STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 RUDDER UPPER HINGE BRACKET CRACKED AT RIGHT MOUNT HOLE. REMOVED AND REPLACED UPPER HINGE BRACKET IAW DC-9 SRM 51-30-1. 2L72 4F A6WE 20040302000022004030200002WP 2004 3 2 AALA20040241 120040215A3350 SIGN DOUG DC9 DC983 3022083WP CABIN UNSERVICEABLE A AALAK NONE O OTHER ININSP/MAINT 1 SW21436AA 49454 DFW - EMERGENCY LIGHT EXIT MARKER AT RIGHT AFT OVERWING EXIT UNREADABLE. REPLACED EMERGENCY LIGHT EXIT MARKER AT RIGHT AFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040302000132004030200013NM 2004 3 2 SWAA040427 120040210A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 277, RBL 55, WL 250 AND BS 277, RBL 55, WL 254. REMOVED AND REPLACED STRINGER CLIPS PER SRM. 2L72 4F RTA16WE 20040302000142004030200014NM 2004 3 2 SWAA040428 120040210A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29328SW 23692 DURING SCHEDULED C4 CHECK, FOUND STRINGER 18L CRACKED AT BS 750. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20040302000172004030200017NM 2004 3 2 SWAA040431 120040210A3350013071BPEGPL LIGHT BOEING737 7373A4 1384585NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29677AA 23289 DURING SCHEDULED C2 CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT BULB INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20040302000562004030200056WP 2004 3 2 AALA20040267 120040223A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21577AA 53154 DEN - CEILING EMERGENCY LIGHTS AT STATION 1209L INOPERATIVE. REPLACED BATTERY PACK AT LOCATION B5-107 FOR CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040302000702004030200070NM 2004 3 2 AALA20040250 120040219A3350 LIGHT BOEING767 767323 1385205NM EXTERIOR INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2139365 24046 SFO - RIGHT HAND EMERGENCY LIGHT ABOVE AFT WING AND EXTENDING TO BODY FAIRINGS INOPERATIVE. CLEANED CONTACTS AND RELAMPED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040302000742004030200074WP 2004 3 2 AALA20050256 120040220A3260833703 SENSOR DOUG DC9 DC982 3022082WP NLG FAULTY A AALAK NONE N FALSE WARNING CLCLIMB 1 SW21412AA 49323 ON GEAR RETRACTION AFTER TAKEOFF NOSE LANDING GEAR POSITION INDICATOR REMAINED RED. RECYCLED GEAR. NOSE LANDING GEAR POSITION LIGHT STILL REMAINED RED. NOSE LANDING GEAR INDICATOR PIN ON CENTER CONSOLE. COMPLETELY RETRACTED. ON GEAR EXTENSION, NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED. NOSE LANDING GEAR VISUAL INDICATOR PIN ON THE CENTER CONTROL PEDESTAL WAS FULLY EXTENDED INDICATING NOSE GEAR DOWN AND LOCKED. LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR SENSOR D1-32. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040302000822004030200082NM 2004 3 2 CALA0400146 120040221A5320BAC1496377X7075TCHANNEL BOEING737 737724 13844BYNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2716732 28948 INSPECTION FOUND RT FLOOR PANEL Z-CHANNEL SUPPORT RAIL CORRODED AT STA 727-767. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 53-00-53. 2L72 4F RTA16WE 20040302000922004030200092NM 2004 3 2 CALA0400141 120040220A5415313A1380114 SUPPORT FITTING BOEING737 7373T0 1384582NM NR 2 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND NR 2 ENGINE PYLON O/B MID SPAR FITTING PANEL AFT RETAINER (SUPPORT FITTING) CRACKED AT UPPER AREA, PYLON STA 279.5. THE SUPPORT FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040302000992004030200099NM 2004 3 2 CALA0400157 120040223A5510180A16122 PIN BOEING737 737824 13844BZNM HORIZ STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712218 28778 INSPECTION FOUND THE RT HORIZONTAL STABILIZER LOWER AFT PIN AND LT HORIZONTAL STABILIZER AFT MIDDLE PIN CORRODED. THE PINS WERE REPLACED IAW EA 5510-01696. 2L72 4F RTA16WE 20040302001322004030200132NM 2004 3 2 SWAA040268 120040127A53116545805 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 277, STRINGER 16 L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040220000772004022000077SO 2004 2 20 SWIA200412849 120040114A5411 FRAME EMB 120 EMB120ER 3260203SO LT NACELLE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07576SW 120345 LEFT NACELLE INBOARD HALF FRAME UNDER TAILPIPE AFT MOUNT FRAME CRACK. DISCOVERED DURING C-CHECK INSPECTION. REPLACED NACELLE HALF FRAME IAW 120 SRM 51-10-02. 2L72 4T RTA31SO 20040220000842004022000084EA 2004 2 20 SWIA200412856 120040203A274083963 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA HORIZONTAL STAB MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 NM07929SW9284 5793 7703 BOTH STAB AND MACH TRIM CAUTION LIGHTS CAME ON DURING FINAL APPROACH. UNABLE TO RESET TRIM FOR MORE THAN 10 TO 15 SEC BETWEEN DISCONNECTS. REPLACED HORIZONTAL TRIM ACTUATOR AND HORIZONTAL TRIM MOTOR CONTROL UNIT AND THE HSTCU, OPS CHECKS GOOD IAW 27-41-00-740-801. MOTOR CONTROL UNIT P/N: 9062-3, S/N ON: 961, S/N OFF: 757. HSTCU P/N: 7060-9, S/N OFF: 1364. 2L72 4F RTA21EA 20040220000882004022000088SO 2004 2 20 LR7A04004 120040124A5312 CAP LKHEED382 382G 526414USO BLKHD BEAM CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5324 FOUND FS 479 WL 200 LT INTERCOSTAL BEAM BROKEN/CRACKED THROUGH. BEAM CAP (TEE) REPLACED IAW SMP583 CHP 51-60 & 51-70, FS 479 WL 200 LBL 62. 2H74 4T A1SO 20040220000902004022000090SO 2004 2 20 LR7A04006 120040124A5330 SKIN LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5324 FOUND FWD FUSELAGE SKIN CRACKED THROUGH RIVET HEAD AT LT JACK PAD AREA FS 191 WL 180L. REPAIR CARRIED OUT IAW SMP583 FIG 51-140-12, FS 191 WL 180 LBL 61. 2H74 4T A1SO 20040220000982004022000098SO 2004 2 20 LR7A04014 120040124A5320 BRACKET LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5315 FOUND LT FS 844 WL 180 RBL 62 FOUND BRACKET CRACKED. REPAIR CARRIED OUT IAW SMP583 FIG 53-50-10, FS 844 WL 180 RBL 62. 2H74 4T A1SO 20040220001092004022000109SO 2004 2 20 LR7A04025 120040205A5310 WINDOW POST LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 768 4590 DURING SCHEDULED B3 INSPECTION PER JOB CARD HB5301 FOUND RT AFT DV WINDOW POST CRACKED. REPAIR CARRIED OUT IAW SMP583 CH 53-30-25, FS 116 WL 255 RBL 40. 2H74 4T A1SO 20040220001122004022000112WP 2004 2 20 04FDEA00366 120040208A78309152M45P004A RIB DOUG DC10 DC1010 3022110WP THRUST REVERSER DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25373FE 46611 COMPLY WITH EA 8-7830-73868 EXHAUST SYSTEM -THRUST REVERSER Z-RIB REPAIR P/N 9152M45P004A. COMPLIED WITH EA 8-7830-73868 EXHAUST SYSTEM - THRUST REVERSER Z-RIB REPAIR P/N 9152M45P004A AT BFM. 2L73 4F A22WE 20040220001202004022000120NM 2004 2 20 04FDEA00351 120040208A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 RIGHT O/B FLAP I/B HINGE (FLAP SIDE) O/B PIVOT HOLE CORRODED. RT O/B FLAP I/B HINGE (FLAP SIDE) O/B PIVOT HOLE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74310. RT O/B FLAP I/B AFT HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040220001222004022000122NM 2004 2 20 04FDEA00349 120040207A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 FOUND OUTBOARD FLAP, OUTBOARD FWD HINGE ACTUATOR HOLE (8) INBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75249. TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP OUTBD HINGE BRACKET REPAIRS. 2L73 4F RTA22WE 20040220001252004022000125NM 2004 2 20 04FDEA00346 120040207A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 FOUND OUTBOARD FLAP, INBOARD FWD HINGE MOUNT HOLE (7) OUTBOARD SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75248. TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP INBD HINGE BRACKET REPAIR. THE LOWER MOUNT SPOT FACE REMAINING IS WITHIN THE LIMITS OF DWG ARC 0502 SHEET 4. 2L73 4F RTA22WE 20040220001262004022000126NM 2004 2 20 04FDEA00344 120040207A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 FOUND OUTBOARD FLAP, INBOARD FWD HINGE ACTUATOR HOLE (8) OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75248. TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP INBD HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040220001312004022000131NM 2004 2 20 F3LA200400009 120040209A5347 MOUNT BOEING737 7373S1 138447SNM LAVATORY CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 24856 DURING C-7 CHECK, INSPECTION REPORTED FWD LAVATORY MOUNT BLOCK AT STA 303, LBL 12, CORRODED. REPLACED LAVATORY MOUNT PER SRM 53-10-15, SRM 53-10-51 AND DRAWING 65C33970. 2L72 4F RTA16WE 20040220001322004022000132NM 2004 2 20 2004UALA00007 120040104A21337207375 RELIEF VALVE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN PRESSURE FAILED A UALAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 WP29377UA 24642 AT FLIGHT LEVEL 33.0 LOST PRESSURIZATION, OXYGEN MASKS DEPLOYED INADVERTENTLY. CABIN SAFETY PRESSURE RELIEF VALVES FAILED. REPLACED INBOARD & OUTBOARD RELIEF VALVES. 2L72 4F4 FRTA16WE E2GL 20040220001372004022000137EU 2004 2 20 04019314A 120040119A5320 INTERCOSTAL JETAIRJETSTMJETSTM4101 1500501EU FUSELAGE CRACKED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27314UE 41027 DURING HEAVY INSPECTION THE INTERCOSTAL AT STATION 4 WAS FOUND CRACKED. THE INTERCOSTAL WAS REPLACED. AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF THE INSPECTION. 2L72 4T RTA41NM 20040220001422004022000142NM 2004 2 20 P5CA0401034 120040209A80123978921 START VALVE BOEING747 7472D3B 1384805NM GE CF6 CF650* 30018NE NR 4 ENGINE MALFUNCTIONED A P5CAK NONE J WARNING INDICATION ININSP/MAINT 1 WP23505MC 21251 517529 NR 4 ENG STARTER VALVE WOULD NOT CLOSE 50 PERCENT. REPLACED START VALVE, OPS CHECK OK PER MM 80-11-04. 2L74 4F4 FRTA20WE E23EA 20040220001462004022000146NM 2004 2 20 QXEA200400121 120040209A2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007NM LAVATORY FALSE ACTIVATIONA QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM09379PH 530 BOI - FLIGHT 2206 - ON CLIMBOUT THE LAVATORY SMOKE DETECTOR SOUNDED. THE AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT BUT WAS UNABLE TO DUPLICATE THE DISCREPANCY. THE AIRCRAFT WAS RETURNED TO SERVICE. NO PARTS WERE REPLACED. 2H72 4T RTA13NM 20040220001472004022000147EA 2004 2 20 04022670 120040122A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27670BR 7561 DURING INSPECTION THE EMERGENCY LIGHT ON THE GALLEY WALL WAS FOUND INOPERATIVE. THE BULBS WERE REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040220001542004022000154EA 2004 2 20 COMA0460128 120040206A7830864808 PSEU CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01488CA3165 7730 FLIGHT 5928 RIGHT THRUST REVERSER UNSAFE CAUTION. REPLACED THE PSEU. 2L72 4F RTA21EA 20040220001582004022000158NM 2004 2 20 04FDEA00375 120040209A5312 BULKHEAD BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25237FE 21331 CORROSION, AFT CARGO BAY, CORROSION ON 1183 BULKHEAD BS 1183 LBL 2 WL 153. *S/D* REMOVED BS 1183 BL 0 (I) BEAM. FABRICATED AND INSTALLED NEW (I) BEAM IAW FED EX EA 7-5310-70618 & SRM 51-30-2. 2L73 4F RTA3WE 20040220001592004022000159NM 2004 2 20 04FDEA00376 120040209A3231 CABLE BOEING727 727200 138407ENM MLG DOOR DAMAGED A FDEAA UNSCHED LANDING JS WARNING INDICATION AFFECT SYSTEMS CLCLIMB 1 SO25480FE 21462 RED DOORS WARNING LIGHT ILLUMINATED ON GEAR RETRACTION S/O'S PANEL. NOSE GEAR DOOR LIGHT ALSO ILLUMINATED AFTER FOLLOWING QRH PROCEDURES. THE LIGHTS REMAINED ILLUMINATED. RETURN TO MEM. REMOVED AND REPLACED BOTH DOOR CABLE, ADJ AND RIGGED NOSE GEAR FWD DOORS. ALSO C/W GEAR SWING. NOSE DOOR LIGHT CHECK AND MANUAL EXTENSION ON NOSE GEAR C/W. ALL WORK ACCOMPLISHED PER AMM 727-200-32-22-001-5. 2L73 4F RTA3WE 20040220001712004022000171EA 2004 2 20 04030675 120040130A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27675BR 7635 DURING INSPECTION A CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTA21EA 20040220001822004022000182NM 2004 2 20 CALA0400097 120040209A5320 WEB BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND A 2 INCH CRACK IN SHEAR WEB PANEL FORWARD OF STA 578, S17L. THE WEB WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-70-13. THE WEB WAS REINSTALLED IAW SRM 51-41-02. 2L72 4F RTA16WE 20040223000072004022300007NM 2004 2 23 G6OA04001 120040104A217018084934 COALESCER BAG DOUG MD11 MD11F 3023600NM AIR COND BAYS CONTAMINATED A G6OAAG UNSCHED LANDING O2 MASK DEPLOYED BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 EA27705GC 48412 FIFTEEN MINUTES INTO FLT, AT FLT LEVEL 310, THE LEVEL 2 (AIR SYS 1 PRESS LOW) AND (AIR SYS 2 PRESS LOW) ILLUMINATED. SMOKE WAS OBSERVED IN THE COCKPIT. AN EMERGENCY WAS DECLARED AND DIVERSION INTIATED TO KSDF. DURING DESCENT , THE LEVEL 2 AIR SYS 3 LOW PRESS LIGHT ILLUMINATED. COALESCER BAGS CONTAMINATED WITH GLYCOL. 2L73 4F RTA22WE 20040219000052004021900005WP 2004 2 19 04FDEA00335 120040206A78309059M42P019A BUMPER BLOCK DOUG DC10 DC1010 3022110WP THRUST REVERSER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25373FE 46611 NR 1 ENGINE OUTBOARD THRUST REVERSER MOST FWD UPPER BUMPER ASSY CRACKED. REMOVED AND REPLACED BUMPER ASSY IAW SRM 51-31-01 AT MAE ON N/R N01145. 2L73 4F A22WE 20040219000162004021900016NM 2004 2 19 UPS04441862 120040123A5320BAC1509100312 CHANNEL BOEING747 747123 1384873NM MAIN DECK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, M/D- BS 2315 LBL 11 TO LBL 38 HAT SECTION FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.030 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. HAT SECTION REPLACED AS PER SRM 51-10-01 PG 8. P/N: BAC1509-100312-7075T6511. CIC APPLIED IAW CPM53-10-17. 2L74 4F A20WE 20040219000332004021900033SO 2004 2 19 C2XA04SH066 120040215A532014522459003 ANGLE EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712530 145533 SHV- DURING C-CHECK THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040219000352004021900035CE 2004 2 19 57827 120040111A6123 AUTOFEATHER SYS BEECH 1900 1900D 1154162CE LT ENGINE MALFUNCTIONED A AMWAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 CE07244YV UE244 ON TAXI OUT CREW BEGAN STARTING LT ENGINE, AFTER GETTING IT STARTED PROPS WOULDN'T COME OUT. ALSO THE AUTOFEATHER WOULDN'T TEST. CREW RETURNED TO THE GATE WITH NO FURTHER INCIDENT. RAN BOTH ENGINES, ALL SYS OPS CK NORMAL. 2L72 4T RTA24CE 20040219000432004021900043EU 2004 2 19 MALA040187 120040126A5330 SHIELD SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15361PX 340B249 DURING 4K INSPECTION IN LCQ, LT ICE SHIELD IS DENTED. REMOVED DENTED ICE SHIELD, CUT OUT DAMAGED AREA, FABRICATED DOUBLER, INSTALLED DOUBLER AFTER TREATING. FABRICATED ICE SHIELD, TREATED, INSTALLED ICE SHIELD IAW EO NR S53005. REFER TO 409 NR 1258951 FOR FURTHER DETAIL. A/C RELEASE DATE 2/16/04. 2L72 4T RTA52EU 20040219000612004021900061NM 2004 2 19 SWAA040410 120040208A335090083 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29746SW 29798 DURING SCHEDULED C4 CHECK, FOUND LT EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20040219000782004021900078NM 2004 2 19 SWAA040353 120040204A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 FUSELAGE SKIN CRACKED UNDER R1 DOOR BS 319, STRINGER 17R. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040302001362004030200136NM 2004 3 2 SWAA040273 120040128A3350101114 LENS BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29353SW 24889 F/A REPORTS EXIT SIGN LENS MISSING FROM RT OVERWING DOOR. INSTALLED LENS AT RT OVERWING DOOR PER MM. 2L72 4F RTA16WE 20040302001632004030200163NM 2004 3 2 SWAA040313 120040130A53116546526 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 400, STRINGER 9L. REPAIRED FRAME SECTION PER ER. 2L72 4F RTA16WE 20040302001712004030200171 2004 3 2 SWAA040374 420040207A2565D31354 SLIDE BOEING737 7373H4 1384600NM R2 DOOR UNSERVICEABLE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29600WN 27694 R2 DOOR EVAC SLIDE PRESSURE LOW INDICATION. REMOVED AND REPLACED R2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040219000032004021900003NM 2004 2 19 04FDEA00338 120040206A5711ARB74054 SPAR DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 RT WING UPPER SURFACE IN SPAR AREA FOUND WITH MINOR CORROSION BETWEEN XORS 538 TO XORS 582. RT WING UPPER SURFACE IN SPAR AREA BETWEEN XORS 538 TO XORS 562 CORROSION REMOVED AND REPAIR CARRIED-OUT AS PER SRM 51-21-01 VOL. II. 2L73 4F RTA22WE 20040219000082004021900008NM 2004 2 19 SWAA040438 120040211A53136546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29302SW 22942 DURING SCHEDULED D CHECK, FOUND AFT CARGO COMPT SHEAR TIE CORRODED AT BS 727C, RBL 6, WL148. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040219000092004021900009 2004 2 19 SWAA040439 420040211A2565D31354 SLIDE BOEING737 7373H4 1384600NM L2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29626SW 27702 DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040219000202004021900020WP 2004 2 19 UPS04841855 120040131A534037739061 FITTING DOUG DC8 DC871F 302199DWP FLOORBEAM CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, MAIN CABIN FLOORBEAM SUPPORT FITTING IS CRACKED AT STA 798, RBL 23. REMOVED AND REPLACED FITTING IAW DWG 3773906 AND SRM 51-1-20D. 2L74 4F RT4A25 20040219000022004021900002EA 2004 2 19 COMA0460131 120040206A3010 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01938CA 7046 FLIGHT 5898 RIGHT WING ANTI ICE CAUTION. DEFERRED MAINT PER MEL. 2L72 4F RTA21EA 20040219000142004021900014NM 2004 2 19 UPS04441860 120040121A5313BAC14981477075 STRINGER BOEING747 747123 1384873NM FWD CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, FWD CARGO COMPT - RT STA 820 - STA 840 STRINGER 47 FOUND CORROSION CRACKED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.040 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. CIC APPLIED IAW EO M-5100-2780-E. 2L74 4F A20WE 20040219000192004021900019WP 2004 2 19 UPS04841854 120040201A53403758570U2 ATTACH FITTING DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, LONGERON 35R INTERCOSTAL TO FRAME ATTACH FITTING AT STA 1230 IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758570 AND SRM 51-1-20D. 2L74 4F RT4A25 20040219000272004021900027NM 2004 2 19 04036405 120040205A5311 FRAME DORNERDO32 DO328300 NM FUSELAGE CORRODED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27405FJ 3155 DURING HEAVY INSPECTION FRAME 35 WAS FOUND WITH LEVEL 2 CORROSION. THE FRAME WAS REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE UPON COMPLETION OF MAINTENANCE CHECK. 2H72 4T RTA55NM 20040219000602004021900060 2004 2 19 SWAA040236 420040123A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29633SW 27936 DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040219000632004021900063NM 2004 2 19 SWAA040238 120040126A5315BAC1505 FLOORBEAM BOEING737 7377H4 1384404NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29723SW 27855 DURING SCHEDULED 5Y CHECK, FOUND CORROSION ON FLOORBEAMS AT BS 772, LBL 17.5 TO LBL 3 AND BS 727, RBL 3 TO LBL 3. REPAIRED FLOORBEAMS PER EA. 2L72 4F RTA16WE 20040219000712004021900071NM 2004 2 19 2004UALA00096 120040202A3350 BATTERY PACK BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE EMERGENCY LIGHT INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29788UA 26942 EMERGENCY EXIT CEILING LIGHTS INOP FIRST ROW COACH TO DOOR 3L. REPLACED BATTERY PACK. 2L72 4F4 FRTT0001SE E46NE 20040219000812004021900081NM 2004 2 19 SWAA040356 120040204A53126546568 BULKHEAD BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29082SW 22731 DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CORRODED AT BS 1016, RBL 1. REPAIRED WEB PER AD. 2L72 4F A16WE 20040219000832004021900083NM 2004 2 19 UPS04441738 120040104A5347 CARGO TRACK BOEING747 747123F NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 INSPECTION TYPE: C, U/D - BS 530 - 590 LBL 66, TIE DOWN TRACK CROWN AND FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.040 X 0.5 X 2.5 INCH. U/D BS 480 TO BS 620 LBL 66 CARGO TRACK REPLACED AS PER SRM 53-10-05 FIG 1A. 2L74 4F A20WE 20040219000872004021900087SO 2004 2 19 C2XA04SH57 120040204A532014528737001 REINFORCEMENT EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711547 145563 SHV - DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19 LEFT WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040219000942004021900094NM 2004 2 19 SWAA040360 120040204A53306545774 SKIN BOEING737 737301 1384611NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727, STRINGER 24L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040219001552004021900155NM 2004 2 19 SWAA040252 120040124A53106547978 CREASE BEAM BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 617, LBL 65, WL 208. REMOVED AND REPLACED CREASE BEAM PER SRM. 2L72 4F RTA16WE 20040219001732004021900173WP 2004 2 19 DHL2004807004 120040206A2120 ODOR DOUG DC8 DC873F 302199FWP CABIN DETECTED A DHLAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO01807DH 45990 TOP OF DESCENT STRONG ODOR, INCREASE IN CABIN FLOW ODOR GOES AWAY. OPERATED LT AND RT PACKS AT VARIOUS SETTINGS IAW 21-50-0. NO ODORS NOTED. OPS GOOD. 2L74 4F RT4A25 20040219002082004021900208WP 2004 2 19 AALA20040184 120040205A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21441AA 49460 DEN - OVERHEAD EMERGENCY LIGHTS AT FIRST CLASS DIVIDER INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT FIRST CLASS DIVIDER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040219002152004021900215NM 2004 2 19 QXEA200400106 120040127A5740 ATTACH FITTING DHAV DHC8 DHC8202 2809007NM ZONE 600 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09356PH 502 PDX - RIGHT INBOARD WING FORWARD SPAR AT STATION YW138.0 BOTH UPPER AND LOWER LEADING EDGE ATTACH FITTINGS CRACKED. REPAIRED IAW DHC-8-200 SRM 51-40-00. 2H72 4T RTA13NM 20040219002212004021900221NM 2004 2 19 QXEA200400115 120040203A5420 CLIP BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - UPPER FORWARD INBOARD NACELLE CENTER STRUCTURE ATTACHMENT CLIP CRACKED AT LEFT HAND NACELLE. REPAIRED IAW HORIZON AIR EA 6-54-283. 2H72 4T RTA13NM 20040220000172004022000017EA 2004 2 20 COMA0460123 120040205A3000355523255 ELEMENT CNDAIRCL600 CL6002B19 1900309EA ANTI ICE SYSTEM FAILED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01719CA 7253 FLIGHT 5803 ANTI ICE DUCT WARNING. REPLACED BLEED LEAK SENSING ELEMENT. 2L72 4F RTA21EA 20040220000582004022000058WP 2004 2 20 AALA20040190 120040208A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21269AA 49292 STL OVERHEAD EMERGENCY LIGHTS AT L1 AND R1 COCKPIT INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT L1 AND R1 COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040220000992004022000099SO 2004 2 20 LR7A04015 120040124A5522 SKIN LKHEED382 382G 526414USO RT ELEVATOR CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5511 FOUND RT ELEVATOR (QTY 4 EA) SKIN CRACKED & DENTED AT HSS196. REPAIR CARRIED OUT IAW SMP583 FIG 51-140-12, HSS196. 2H74 4T A1SO 20040220001042004022000104SO 2004 2 20 LR7A04020 120040124A5320 CAP LKHEED382 382G 526414USO WW INTERCOSTAL CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5324 FOUND AFTER REMOVAL OF RT MLG INTERCOSTAL BRACKET FS 557 WL 198, O/B CAP BROKEN AT TIP END. REPAIR CARRIED OUT IAW SMP583 FIG 53-40-14, FS 557 WL 198 RBL 62. 2H74 4T A1SO 20040220001102004022000110SO 2004 2 20 LR7A04026 120040205A5312 BULKHEAD LKHEED382 382G 526414USO FUSELAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03403LC 768 4590 DURING SCHEDULED B3 INSPECTION PER JOB CARD HB3200 FOUND FS 617 BULKHEAD AT WL 210 EXISTING REPAIR CRACKED AT LBL 60. REPAIRED IAW SMP583 FIG 53-40-10, FS 617 WL 200 - 210 LBL 63-73. 2H74 4T A1SO 20040220001242004022000124NM 2004 2 20 04FDEA00347 120040207A5744 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 RT WING FOUND OUTBOARD FLAP, INBOARD FWD HINGE MOUNT HOLE, INBOARD SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75248 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBD FLAP INBD HINGE BRACKET REPAIR. THE LOWER MOUNT SPOT FACE REMAINING THICKNESS (0.472 INCH) IS WITHIN THE LIMITS OF DWG ARC0502 SHT 4. 2L73 4F RTA22WE 20040220001292004022000129SO 2004 2 20 C2XA04SH059 120040210A533014520553005 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE DENTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2711547 145563 SHV - DURING C-CHECK THE FUSELAGE SKIN WAS FOUND TO BE DENTED BETWEEN FRAMES 19 AND 20 AT STRINGER 7L, JUST AFT OF THE MAIN DOOR. MAINTENANCE REMOVED THE AFFECTED SECTION OF STRINGER 7L, RE-CONTOURED THE DENTED AREA OF SKIN, AND INSTALLED A NEW 7L STRINGER SECTION IAW CONTINENTAL EXPRESS EC 5330-01242. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20040220001622004022000162NM 2004 2 20 04FDEA00383 120040209A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 CABIN LEFT FRAME DENTED AT STA 1521 BETWEEN STR 12 & 13. CABIN LT FRAME DENTED AT STA 1521 BETWEEN STR 12 & 13 REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. PERFORMED NDT INSPECTION ON TRIMMED OUT AREA CRACK FREE CONDITION. FUSELAGE FRAME DAMAGE REPAIRED BY SRM. REPETITIVE INSPECTION REQUIREMENT PER SRM - DTA, EA 1-5310-74229. 2L73 4F RTA22WE 20040220001772004022000177SO 2004 2 20 C2XA04SH047 120040205A532014521725013 SILL EMB 145 EMB145 3260210SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2719966 145131 SHV-DURING C-CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED AROUND THE NUT PLATES. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040220001912004022000191 2004 2 20 AWXA200400164 420040117A256565659723 PLATE BOEING737 737277 1384570NM GIRT BAR ADAPTERCORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 LCQ - EES - DURING C-15 CHECK CORROSION WAS FOUND IN R-2 DOOR GIRT BAR FITTING ADAPTER PLATE BS 328, RBL 74. MAINTENANCE REMOVED AND REPLACED L-2 DOOR GIRT BAR FITTING ADAPTER PLATE IAW T/C C1D25006. 2L72 4F RTA16WE 20040220001942004022000194WP 2004 2 20 AALA20040207 120040209A3350 BATTERY DOUG DC9 DC982 3022082WP EMERGNEYC DISLODGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21478AA 49653 DFW AISLE EMERGENCY PATH LIGHT ASSEMBLY BETWEEN AFT LAVATORIES INOPERATIVE. FOUND BATTERY DISLODGED ON FORWARD BATTERY PACK. REINSTALLED BATTERY PACK FOR AISLE EMERGENCY PATH LIGHT ASSEMBLY BETWEEN AFT LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040223000432004022300043NE 2004 2 23 NACA20040002 220040105A8530356993 CYLINDER PWA DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 6 MAKING METAL A NACAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 AL0399330317 317 43576 P33192 NR 4 ENGINE SHUT DOWN DUE TO BACK FIRING, NR 6 CYLINDER LT AND RT LOW RESISTANCE SECONDARY. REPLACED NR 4 ENGINE DUE TO MAKING METAL. 2L74 4R4 R 6A3 5E8 20040223000692004022300069SO 2004 2 23 C2XA04BT002 120040105A2120 ODOR EMB 145 EMB145ER 3260211SO COCKPIT DETECTED A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW2715948 145056 CREW REPORTED (STRONG FUEL ODOR UPON APU START.) MAINTENANCE INSPECTED AND OPERATIONALLY CHECKED THE APU GOOD. NO DEFECTS NOTED (SUSPECT POSSIBLE TAILWIND DURING START PROCESS) AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20040223000732004022300073 2004 2 23 SWIA200412746 420040102A22106228315402 COMPUTER EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07237SW8671 8671 120314 CAPTAIN'S AP FAILS IN FLIGHT. REMOVED AND REPLACED AUTOPILOT NR 1 COMPUTER WITH SERVICEABLE UNIT. OPS CHECK GOOD IAW MM 22-10-00. 2L72 4T RTA31SO 20040223000912004022300091NM 2004 2 23 CALA0400005 120040106A80113507138040 STARTER BOEING777 777224 1385225NM GE GE90 GE9090B NE NR 1 ENGINE LEAKING A CALAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW277800417965 27580 900229 THE NR 1 ENGINE OIL QUANTITY AND PRESSURE BEGAN TO DECREASE DURING CRUISE. THE ENGINE WAS SHUTDOWN AS A PRECAUTIONARY MEASURE AND THE AIRCRAFT WAS DIVERTED WHERE IT LANDED WITHOUT INCIDENT. THE STARTER SIGHT GLASS HOUSING WAS FOUND SHEARED. THE NR 1 ENGINE STARTER WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F4 FRTT00001SEE00049EN 20040223000952004022300095EA 2004 2 23 UIA9301 120040108A324221517 BRAKE ASSY DHAV DHC8 DHC8311 1386006EA NR 1 & 4 JAMMED Z D RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 TW0015239 571 RT MLG BRAKE JAM DURING TAXI, CHK FOUND NR 1 AND NR 4 BRAKE STUCK. REPLACED NR 1 AND NR 4 BRAKE AND PERFORM BRAKE SYSTEM BLEED AND ANTI-SKID FUNCTIONAL TEST NML. 2H72 4T RTA13NM 20040223001052004022300105 2004 2 23 372PA0039 420040106A2230 SYNCRONIZER BOEING737 737306 13844BGNM AUTOTHROTTLES OUT OF ADJUST A PIDAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO05372PA 23546 AUTO THROTTLES DISENGAGED ON TAKE OFF ROLL. ADJUSTED PLA SYNCHRO. OPS NORMAL IAW MM 22-31-00. 2L72 4F RTA16NE 20040223001092004022300109NE 2004 2 23 0400076632 220040106A731470680137 PUMP BOEING747 747251B 1384892NM PWA JT9 JT9D7R4G2 52054NE FUEL SYSTEM MALFUNCTIONED A NWAAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 GL01632NW 23113 715053 AT FL380, THE CREW OBSERVED DECREASING PARAMETERS ON THE NR 4 ENGINE. THE COM PROCEDURES WERE FOLLOWED BUT THE ENGINE REMAINED AT IDLE. ALL INDICATIONS REMAINED IN THE NORMAL RANGE, SO THE ENGINE WAS LEFT AT IDLE POWER. WHEN DESCENDING THROUGH 8000 FEET ON APPROACH, THE ENGINE ROLLED BACK BELOW IDLE AND THE CREW SECURED THE ENGINE. THE FLIGHT CONTINUED TO ITS DESTINATION LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGINE DRIVEN FUEL PUMP, FUEL CONTROL, AND FUEL HEAT VALVE. AN ENGINE RUN AND LEAK CHECK WERE COMPLETED WITH NORMAL INDICATIONS. 2L74 4F4 F A20WE E3NE 20040223001102004022300110 2004 2 23 GLBA2003523 420040101A3454 DISPLAY BEECH 1900 1900D 1154162CE VOR SYSTEM DEFECTIVE A GLBAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM03208GL UE208 BOTH VOR DISPLAYS SHOWED FULL SCALE DEFECTION ON ALL VOR STATIONS, PENDING CORRECTIVE ACTION. 2L72 4T RTA24CE 20040223001152004022300115CE 2004 2 23 GLBA2003528 120040108A7712 CONNECTOR BEECH 1900 1900D 1154162CE TORQUE XDUCER INOPERATIVE A GLBAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM03255GL UE255 104 PERCENT N1 WITH 2000 LB TORQUE ON NR 2 ENG, CLEANED CONNECTOR ON TORQUE TRANSDUSER ON NR 2 ENGINE. 2L72 4T RTA24CE 20040223001192004022300119NM 2004 2 23 UPS04441702 120040109A2133 CHECK VALVE BOEING747 747200 1384847NM CABIN PRESSURE STUCK A IPXAO OTHER J WARNING INDICATION CLCLIMB 1 SO01520UP 1 DECOMP LIGHT AND ALT WARNING HORN 10000 ALT CAME ON AT ALT 22000. ACCOMPLISHED RAPID DECOMP AND EMERGENCY DESCENT. CHECK LIST BUMP PUEL ATB FOUND PNEU GROUND CONNECT CHECK VALVE INTERMITTENT, STUCK OPEN POS. REMOVED AND REPLACED PNEU GND CONNECT CHECK LEFT VALVE AND CHECKED O.K. IAW MM 36-11-14ALL DOOR SEALS AND PERFORMED EXCESSIVE CABIN PRESSURE LEAKAGE CONDITION INSP COMPLETE IAW AMM 05-51-08 P201. AND PRESS CONT SYS TEST O.K IAW AMM 21-31-00P 501 2L74 4F RTA20WE 20040223001222004022300122SO 2004 2 23 ACE010704 220040107A8530TISN712ACA CYLINDER HEAD CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO ENGINE CRACKED E YADAA UNSCHED LANDING ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CRCRUISE 1 AL039874M998 20700745 291045R PILOT REPORTED POWER LOSS AND VIBRATION - RE-ROUTED AND MADE A SAFE LANDING. MAINTENANCE DISCOVERED THE NR 2 CYLINDER HAD 100 PERCENT HEAD SEPARATION AT THE HEAD TO BARREL INTERFACE IN LINE WITH THE TOP OF THE STEEL BARREL. 1H71 3O3 O A16CE E5CE 20040223001232004022300123EA 2004 2 23 COMA0460029 120040107A5210601R31881273 CABLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR PANEL CHAFED A COMAK NONE O OTHER ININSP/MAINT 1 SO01455CA5525 7592 PAX DOOR PRESSURE PANEL CABLE (ICE BREAK) IS BROKEN AT THE END OF THE CLEAVIS DUE TO RUBBING ON THE FLAP. PAX DOOR PRESSURE PANEL CABLE WAS REPLACED WITH A SERVICEABLE CABLE. THE FLAP (DECOMPRESSION PANEL) NEEDS TO HAVE A RECESSION CUT INTO THE INTERIOR LIP TO ALLOW THE CABLE MORE ROOM AND TO PREVENT IT FROM BEING BROKEN FROM NORMAL USE. 2L72 4F RTA21EA 20040223001352004022300135WP 2004 2 23 IXXA0400002O 120040110A3231 RELEASE SYSTEM DOUG DC8 DC862 3021970WP NLG STICKING A IXXAO OTHER J WARNING INDICATION CLCLIMB 1 SW1131CX 777731799 45911318 DURING TAKE OFF, WHEN GEAR RETRACTED HAD EVIDENCE OF NOISE AND VIBRATRION COMING FROM NOSE GEAR AREA. GEAR WAS RECYCLED AND ALL INDICATIONS WERE NORMAL. MAINTENANCE FOUND LT FORWARD NOSE GEAR DOOR MANUAL RELEASE MECHANISM STICKING INTERMITTENTLY. MAINTENANCE LUBED MANUAL RELEASE MECHANISM AND MANUALLY CYCLED DOOR SEVERAL TIMES IAW ALL APPLICABLE MANUALS. NO FURTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20040223001362004022300136WP 2004 2 23 IXXA0400003O 120040110A3231510361 LINK ASSY DOUG DC8 DC862 3021970WP NLG BROKEN A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW1131CX 777741800 45911318 DURING CLIMB, 1550Z WHILE TRANSITIONING THROUGH FL 330 CREW SUSPECTED NOSE GEAR OPENED IN FLIGHT. SLOWED AIRCRAFT BELOW 230 DESCENDED AND RETURNED AIRPORT. THE CREW LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED NOSE GEAR DOOR ADJUSTMENT/TEST. FOUND LT FWD NOSE GEAR DOOR, FORWARD LINK ASSY WILL NOT LATCH - UNABLE TO ADJUST LINKAGE. MAINTENANCE REMOVED AND REPLACED LT FORWARD LINK ASSEMBLY, OPERATIONAL CHECK NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20040223001372004022300137NE 2004 2 23 IXXA0400004O 220040111A7200 ENGINE DOUG DC8 DC862 3021970WP PWA JT3D JT3D7 52039NE NR 1 MALFUNCTIONED A IXXAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 SW1131CX 777841811 45911318 DURING CLIMB, THE NR 1 ENGINE WOULD NOT GO ABOVE 1.60 EPR WHEN SETTING CLIMB POWER. CREW RETURNED AIRCRAFT TO AIRPORT AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED NR 1 ENGINE FCU MOISTURE TRAP AND INSPECTED PRBC. NO DEFECTS WERE NOTED. PERFORMED ALL OPERATIONAL CHECKS IAW ALL APPLICABLE MANUALS AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F4 F 4A25 1E8 20040219001632004021900163EA 2004 2 19 SWIA200412840 120040202A3350 BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A SWIAO OTHER L NO TEST TXTAXI/GRND HDL 1 NM07927SW 7693 FLOOR LEVEL ESCAPE PATH LIGHTING ROWS 1-5 IS ENTIRELY INOPERATIVE. REMOVED NR 1 EMERGENCY LIGHT BATTRY PACK AND INSTALLED A SERVICEABLE UNIT. OPS CHECKS GOOD. 2L72 4F RTA21EA 20040219001642004021900164 2004 2 19 SWIA200412841 420040202A22106226684006 CONTROL PANEL EMB 120 EMB120ER 3260203SO AUTOPILOT MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 NM07251YV8840 8840 120251 CAPTAIN SIDE AUTOPILOT FAILS WHEN ENGAGED EN ROUTE. FD OPERATES NORMALLY BUT AP DSC FLAG AND AP ERROR LIGHT APPEAR ON FCP AND AP CONTROL PANEL INDICATES AP DIS AND RED AP LIGHT AND AMBER FLAG ERRORS. REMOVED AND REPLACED AP CONTROL PANEL WITH NEW CONTROL PANEL IAW 24-10-04. OPS CHECK GOOD. 2L72 4T RTA31SO 20040219001762004021900176NM 2004 2 19 UPS04241816 120040122A5320 BRACKET BOEING727 72722C 138400FNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE: C, INTERGRANULAR CORROSION FOUND ON CEILING PANEL BRACKET AT BS 1130 AFT CARGO COMPT, AS MARKED. HFEC INSPECTION CARRIED OUT AROUND CUTOUT AT THE ABOVE AREA IAW B727 NDTM PT 6 51-00-00 NDF. REPAIR CARRIED OUT IAW SRM 51-40-04. 2L73 4F A3WE 20040219001912004021900191NM 2004 2 19 04FDEA00316 120040205A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT WING, FOUND OUTBOARD FLAP, INBOARD FWD HINGE ACTUATOR HOLE (8) OUTBOARD CORRODED. COMPLIED WITH FEDEX EA 1-5750-75243. TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBD FLAP. INBD. HINGE BRACKET REPAIR. 2L73 4F RTA22WE 20040219002202004021900220NM 2004 2 19 QXEA200400114 120040203A5420 CLIP BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - UPPER FORWARD INBOARD NACELLE CENTER STRUCTURE ATTACH CLIP CRACKED ON RIGHT HAND NACELLE. REPAIRED IAW HORIZON AIR EA 6-54-283. 2H72 4T RTA13NM 20040219002232004021900223NM 2004 2 19 QXEA200400105 120040130A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09356PH 502 PDX - RIGHT HAND INBOARD SEAT TRACK HAS PITTING CORROSION ON TOP END FROM FS 220.00 TO FS 246.00. REPAIRED IAW DHC-8-200 SRM 51-40-11. 2H72 4T RTA13NM 20040219002312004021900231SO 2004 2 19 C2XA04TY033 120040206A532014522459003 ANGLE EMB 145 EMB145LR 3260212SO FRAME 20 CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713550 145575 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER RAMP ANGLE AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20040219002472004021900247NM 2004 2 19 CALA0400084 120040206A5320 WEB BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND SHEAR WEB PANEL CRACKED IN TWO PLACES AT LT FUSELAGE FORWARD OF STA 639 AT S17L. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040220000372004022000037WP 2004 2 20 UPS04841833 120040114A5340 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE: C1, CABIN STA 680 LONGERON 11 RIGHT SIDE FITTING CRACKED. REMOVED FITTING IAW DC8 SRM 51-3-5. LOCATED NEW FITTING, DRILLED EXISTING FASTENER HOLES, DEBURRED IAW DC8 SRM 51-3-2 AND INSTALLED IAW DC8 SRM 51-3-0. 2L74 4F RT4A25 20040220000462004022000046WP 2004 2 20 UPS04841849 120040130A57515764617U51 PANEL DOUG DC8 DC871F 302199DWP LT OB.AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, LT WING OUTBOARD AILERON WEIGHT PANEL IS CORRODED BEYOND LIMITS BETWEEN XA 614 TO XA 638. REMOVED, FABRICATED AND REPLACED WEIGHTED PANEL IAW DWG 5764617 AND DOUBLER IAW DWG 5763133 AND SRM 51-1-21, 51-3-0. 2L74 4F RT4A25 20040220000632004022000063NM 2004 2 20 AALA20040189 120040208A3350 LIGHT BOEING757 757223 1384957NM R1 DOOR BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21174AA 31308 ORD EMERGENCY EXIT LIGHT AT R1 DOOR HAS BROKEN BASE PLATE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040220000662004022000066NM 2004 2 20 AALA20040196 120040206A3397 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21690AA 25696 DFW SEAT MOUNTED ESCAPE PATH LIGHTING AT SEAT 23D INOPERATIVE. RESECURED CONNECTOR FOR SEAT MOUNTED ESCAPE PATH LIGHTING AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040219000822004021900082NE 2004 2 19 DXTA200400242 220040212A7200 ENGINE BRAERO1000 HAWKER1000 7450005EU PWA 306 PW306B NE NR 1 SHUTDOWN E DXTAF ACTIVATE FIRE EXT. J WARNING INDICATION LDLANDING 1 GL07548QS 259048 PCE305072 ON LANDING WHILE PULLING BACK ON THE THRUST REVERSER LEVERS, NR 1 ENGINE WENT TO SHUTDOWN AND NR 1 ENGINE FIRE LIGHT ILLUMINATED. PULLED NR 1 ENGINE FIRE BOTTLE, AIRCRAFT ARRIVED AT GATE WITHOUT FURTHER INCIDENTS. ITEM IS UNDER INVESTIGATION. 2L72 4F4 FRTA3EU E35NE 20040219000922004021900092NM 2004 2 19 SWAA040358 120040204A555265C25798 FITTING BOEING737 7373H4 1384600NM LT ELEVATOR WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 DURING SCHEDULED C3 CHECK, LT ELEVATOR TAB FAILED FREE PLAY INSPECTION. REMOVED AND REPLACED LT ELEVATOR TAB NR 1 HINGE FITTING PER SRM. 2L72 4F RTA16WE 20040219000972004021900097EU 2004 2 19 F3LA200400005 120040204A5610NP1653116 WINDSHIELD AIRBUSA318 A318111 3940019EU COCKPIT CRACKED A F3LAA UNSCHED LANDING O OTHER CLCLIMB 1 NM03801FR 1939 AIR TURNBACK, FLIGHT CREW REPORTED FIRST OFFICER'S WINDSHIELD CRACKED. DECLARED AN EMERGENCY, AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED FIRST OFFICER'S WINDSHIELD PER 56-11-11-000-001 AND 56-11-11-400-001. PERFORMED TEST OF WINDOW HEAT AND DEFOGGING PER 30-42-00-710-001 AND CHECKED OKAY. 2L72 4F RT 20040219000992004021900099NM 2004 2 19 SWAA040340 120040203A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29314SW 23336 DURING SCHEDULED PM CHECK, FOUND SKIN CRACKED AT BS 980, STRINGER 23 L. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20040219001042004021900104 2004 2 19 SWAA040345 420040203A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29759GS 30544 DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM. 2L72 4F RTA16WE 20040219001052004021900105NM 2004 2 19 SWAA040346 120040203A53116546550 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 787, STRINGER 9L. REPAIRED FRAME SECTION PER ER. 2L72 4F RTA16WE 20040219001092004021900109NM 2004 2 19 SWAA040350 120040203A3350D717011000 BATTERY BOEING737 7377H4 1384404NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29716SW 27850 DURING SCHEDULED SPV, FOUND L1 DOOR AND RT BULLNOSE AT ROW 1 TO ROW 4, EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER MM. 2L72 4F RTA16WE 20040219001122004021900112NM 2004 2 19 SWAA040211 120040121A53106546546 SHEAR TIE BOEING737 7373Y0 1384671NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D-CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 767, LBL 2. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20040219001132004021900113NM 2004 2 19 SWAA040212 120040121A53116516301 FRAME BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 188, STRINGER 17 L. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20040219001222004021900122NM 2004 2 19 SWAA040221 120040122A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29363SW 26574 DURING SCHEDULED C2 CHECK, FOUND SKIN CRACKED AT BS 518, STRINGER 10R. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20040219001272004021900127NM 2004 2 19 SWAA040226 120040122A53106545857 DOOR FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29363SW 26574 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR LOWER FRAME HINGE CUTOUT RADIUS CRACKED. REPAIRED FRAME PER EA. 2L72 4F RTA16WE 20040219001322004021900132NM 2004 2 19 SWAA040231 120040122A575465C26603 WEDGE BOEING737 7373A4 1384585NM LT WING SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29680AA 23505 DURING SCHEDULED C2 CHECK, FOUND NR 3 SLAT T/E WEDGE INBOARD END DELAMINATED. REMOVED AND REPLACED NR 3 SLAT PER MM. 2L72 4F RTA16WE 20040219001392004021900139EA 2004 2 19 COMA0460116 120040103A5320601R35031241 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01812CA 7381 CARGO FLOOR ANGLE AT FS 621.00 BULKHEAD, LEFT AND RIGH SUPPORT, CRACKED. COMPLIED WTIH BOMBARDIER REO 601R-53-61-004. PAINTED REPAIR IN ACCORDANCE WITH CRJ SRM 51-25-00. 2L72 4F RTA21EA 20040219001412004021900141NM 2004 2 19 C1HA200483001 120040202A3297 CONNECTOR BOEING727 7272S7 138407ZNM MLG DIRTY A C1HAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 GL15683CA 22490 WHEN GEAR HANDLE PLACED TO DOWN POSTION, GEAR DID NOT CYCLE NORMALLY. NOSE GEAR STAYED INTO UP & LOCKED POSITION. AFTER GO-AROUND GEAR OPS NORMAL. VISUAL CHECK, CLEAN PLUG PER MC 32-61-01. 2L73 4F A3WE 20040219001812004021900181NM 2004 2 19 CALA0400075 120040205A5320 ANGLE BOEING737 737724 13844BYNM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2739726 28796 INSPECTION FOUND RT SIDE ZEE ANGLE CORRODED AT STA 727-797. A NEW ZEE ANGLE WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040220000752004022000075CE 2004 2 20 58598 120040205A5210MS166241075 HANDLE BEECH 1900 1900D 1154162CE PAX DOOR SEPARATED A AMWAO OTHER O OTHER TXTAXI/GRND HDL 1 CE07142YV UE142 WHEN PREPARING TO BOARD, DOOR HANDLE CAME OFF IN THE PILOTS HAND. MX VERIFIED INDOOR HANDLE. PLANE WAS FERRIED TO LIT FOR REPAIR. REMOVED OUTSIDE DOOR HANDLE RETAINER. REINSTALLED HANDLE AND NEW SNAP RING. ALSO, REINSTALLED HANDLE ASSY, OPS CHECK NORMAL. 2L72 4T RTA24CE 20040220000762004022000076SO 2004 2 20 SWIA200412848 120040114A5210 CHANNEL EMB 120 EMB120ER 3260203SO PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07576SW 120345 PAX DOOR MID SECTION OF DOOR AFT CHANNEL CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CHANNEL TO PAX DOOR MID SECTION AFT AREA OF DOOR IAW SRM 120 51-10-02 PG 3 SEC 3A. 2L72 4T RTA31SO 20040220000912004022000091SO 2004 2 20 LR7A04007 120040124A5312 CAP LKHEED382 382G 526414USO RT MLG WW CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND HAIRLINE CRACK RT MWW INTERCOSTAL BEAM O/B CAP AT FS 479 WL 200. BEAM CAP REPLACED IAW SMP583 CHP 51-60 & 51-70, FS 479 WL 200 RBL 62. 2H74 4T A1SO 20040220000972004022000097SO 2004 2 20 LR7A04013 120040124A5330 SKIN LKHEED382 382G 526414USO FUSLEAGE CRACKED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND AFT FUSELAGE LT SKIN CRACKED AT FS 860 WL 200 BL 82L. REPAIR CARRIED OUT IAW SMP583 FIG 51-140-10, FS 860 WL 200 LBL 82. 2H74 4T A1SO 20040220001132004022000113WP 2004 2 20 04FDEA00365 120040208A78309152M45P004A RIB DOUG DC10 DC1010 3022110WP THRUST REVERSER DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25373FE 46611 COMPLY WITH EA 8-7830-73868 EXHAUST SYSTEM -THRUST REVERSER Z-RIB REPAIR P/N 9152M45P004A. COMPLIED WITH EA 8-7830-73868 EXHAUST SYSTEM - THRUST REVERSER Z-RIB REPAIR P/N 9152M45P004A AT BFM. 2L73 4F A22WE 20040220001142004022000114NM 2004 2 20 04FDEA00357 120040208A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 LEFT I/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT HOLE & LUG CORRODED. LT I/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT HOLE & LUG SURFACE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74312. LT I/B TE FLAP HINGE BRACKET CORRODED. 2L73 4F RTA22WE 20040220001152004022000115NM 2004 2 20 04FDEA00356 120040208A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 LEFT I/B FLAP O/B HINGE (FLAP SIDE) O/B PIVOT HOLE AND LUG CORRODED. LT I/B FLAP O/B HINGE (FLAP SIDE) O/B PIVOT HOLE & LUG SURFACE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74312. LT I/B TE FLAP HINGE BRACKET CORRODED. 2L73 4F RTA22WE 20040220001332004022000133 2004 2 20 2004UALA00026 420040109A2210MR22176 COUPLER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE YAW DAMPER MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29331UA 24192 YAW DAMPER TRIPPED OFF. *S/D* REPLACED YAW DAMPER COUPLER. 2L72 4F4 FRTA16WE E2GL 20040220001432004022000143NM 2004 2 20 QXEA200400120 120040209A2133 SEAL BOMBDRDHC8 DHC8401 1390041NM OUTFLOW VALVE FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09415QX 4081 SMF - FLIGHT 2438 - AIRCRAFT FAILED TO PRESSURIZE ON CLIMBOUT AND THE CREW RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE SYSTEM ON MEL. MAINTENANCE REPLACED THE SEAL ON THE AFT PASSENGER DOOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 20040220001642004022000164NM 2004 2 20 04FDEA00385 120040209A5311 FRAME DOUG MD11 MD11 3023602NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 CABIN RT FRAME DENTED AT STA 1661 BETWEEN STR 12 & 13. CABIN RT FRAME DENTED AT STA 1661 BETWEEN STR 12 & 13 REPAIR CARRIED OUT AS PER MD11 SRM 53-30-00 FIG 1 VOL 1. PERFORMED NDT INSPECTION ON TRIMMED OUT AREA CRACK FREE CONDITION. FRAME DAMAGE REPAIRED BY SRM. REPETITIVE INSPECTION REQUIREMENT PER SRM - DTA, EA 1-5310-74229. 2L73 4F RTA22WE 20040220001802004022000180NM 2004 2 20 CALA0400095 120040209A5730 SKIN BOEING757 757224 1384958NM LT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717126 27566 INSPECTION FOUND MULTIPLE CRACKS IN LT WING L/E SKIN AT O/B END OF NR 4 SLAT, OSS 430. THE LONGEST CRACK WAS SIX INCHES. THE SKIN WAS REPAIRED IAW EA 5731-01010, REV D, SEQ 399. 2L72 4F RTA2NM 20040223000202004022300020EU 2004 2 23 06041 120040105A26131734362 DETECTOR SAAB SF340 340B 7860101EU TAILPIPE INOPERATIVE A NSVAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 EA27252CJ 340B252 TAIL PIPE HOT ANNUNCIATION FOR LT ENGINE DURING CLIMBOUT. REDUCED POWER IAW CHECKLIST, LIGHT REMAINED ILLUMINATED, EXECUTED PRECAUTIONARY IN-FLIGHT ENGINE SHUTDOWN. REMOVED AND REPLACED THREE ENGINE DETECTORS IAW MM. ENGINE RUN, NO DISCREPANCIES NOTED. 2L72 4T RTA52EU 20040223000802004022300080EA 2004 2 23 COMA0460026 120040107A5320601R35031239 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01815CA9312 7397 THE UNDER FLOOR SUPPORT ANGLE P/N 601R35031-239 IS CRACKED AT FS 621.9 WL 73, LBL 41.5 AND RBL 41.5. REMOVED THE CRACKED AREAS AND INSTALLED REPAIR PARTS IAW REO 601R-53-61.117 REV.B. 2L72 4F4 FRTA21EA E15NE 20040223001342004022300134WP 2004 2 23 IXXA0400001O 120040109A3231 DOOR DOUG DC8 DC862 3021970WP NLG UNLATCHED A IXXAO OTHER E VIBRATION/BUFFET CLCLIMB 1 SW1131CX 777661793 45911318 AFTER TAKE OFF AND GEAR RETRACTION, CREW NOTICED A VIBRATION AND NOISE. CREW RECYCLED LANDING GEAR, DID NOT CORRECT PROBLEM. SUSPECT NOSE GEAR DOOR NOT CLOSE PROPERLY. CREW CONTINUED FLIGHT TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENACE PERFORMED FUNCTIONAL CHECK OF LOCKING MECHANISM OF LT AND RT NOSE LANDING GEAR. OPERATIONAL CHECK GOOD ON GROUND IAW ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20040223001442004022300144NM 2004 2 23 2004UALA00015 120040107A5320 SPLICE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29385UA 24660 STR SPLICE IS CRACKED BETWEEN 2 RIVETS AT BS 907 S4L. MAJOR REPAIR ACCOMPLISHED. INSTALLED SHEAR CLIP AND STRINGER SPLICE. 2L72 4F4 FRTA16WE E2GL 20040223001452004022300145NM 2004 2 23 2004UALA00021 120040109A5320 DOUBLER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE WEB GOUGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29392UA 24667 WEB DOUBLER GOUGED AT BS 187 WL 207 RBL 28. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA16WE E2GL 20040223001692004022300169SW 2004 2 23 2004F00037 120040113A243651509002B GCU SWRNGNSA227 SA227AC 8780603SW LT GENERATOR FAILED E C ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL27371PH AC576 WHILE ON THE TAKEOFF ROLL, THE LT GENERATOR FAIL WARNING LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND MAINTENANCE WAS NOTIFIED. UPON INVESTIGATION, IT WAS DETERMINED THAT THE GENERATOR CONTROL UNIT FAILED. 2L72 4T RTA8SW 20040223001952004022300195EU 2004 2 23 AALA20040064 120040113A3350 BATTERY PACK FOKKERF28 F28MK0100 4990807EU EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW211443A 11446 ORD CEILING EMERGENCY LIGHTS AT LT AND RT HATCH EXIT ABOVE 17D AND 12D AND UPPER RT FUSELAGE INOPERATIVE. REPLACED BATTERY PACK FOR LT AND RT HATCH EXIT ABOVE 17D AND 12D AND UPPER RIGHT FUSELAGE. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED-- 2L72 4F RT 20040223001992004022300199EA 2004 2 23 MASA200400006 120040104A32304622 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA MLG LEAKING A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0775987529 5987 ASH NR 2705) DURING THE RETRACTION OF THE GEAR HANDLE, THE NOSE GEAR UNSAFE LIGHT CAME ON. A/C RETURNED TO FIELD. MECHANIC REPLACED THE NLG PRIORITY VALVE. OP CHECKS GOOD. 2L72 4F RTA21EA 20040223002002004022300200EA 2004 2 23 MASA200400007 120040104A2751 WARNING LIGHT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS ILLUMINATED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0717231 7231 DURING CLIMB OUT, A FLAP FAIL CAUTION MSG OCCURED. AIRCRAFT RETURNED TO FIELD WHERE MECHANIC COMPLIED WITH PART "A" OF FLAP FAIL PROCEDURES AND AN OVER WEIGHT LANDING INSPECTION. NO DEFECTS WERE NOTED. A/C WAS RETURNED TO SERVICE. NO PARTS USED 2L72 4F RTA21EA 20040223002062004022300206NM 2004 2 23 COOSDR030036 120040101A5755 SKIN BOEING727 72731 1384010NM RT WING SPOILER DELAMINATED A EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23220NE TO85 18905 RT WING, TE SECTION SPOILER NR 9, UPPER SURFACE, DELAMINATED. 2L73 4F A3WE 20040223002102004022300210NM 2004 2 23 COOSDR030039 120040101A5511 RIB BOEING727 72731 1384010NM HORIZONTAL STAB CRACKED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23220NE 18905 LT HORIZONTAL STABILIZER, ELEV. STA 17.20 ELEVATOR HINGE, OB AFT END, SUPPORT RIB, CRACKED. 2L73 4F A3WE 20040223002142004022300214NM 2004 2 23 COOSDR030044 120040101A571265479342 RIB BOEING737 737200 1384453NM RT WING CRACKED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23767TW 20258 RT WING, FSS 263 LEADING EDGE RIB CRACKED. 2L72 4F A16WE 20040223002152004022300215NM 2004 2 23 COOSDR030045 120040101A571265479352 RIB BOEING737 737200 1384453NM RT WING CRACKED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23767TW 20258 RT WING, FSS 266 LEADING EDGE RIB CRACKED. 2L72 4F A16WE 20040223002172004022300217NM 2004 2 23 COOSDR030047 120040101A5320 CHANNEL BOEING737 737200 1384453NM MLG CRACKED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23767TW 20258 RT MAIN LANDING GEAR CHANNEL. 2L72 4F A16WE 20040224000042004022400004NM 2004 2 24 COOSDR030051 120040101A5753656715616 FLAP TRACK BOEING737 737200 1384453NM LT WING CORRODED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23767TW 20258 LT WING, FLAP TRACK NR 2 CORRODED. 2L72 4F A16WE 20040224000072004022400007NM 2004 2 24 N770AN 120040116A5753113W93391 HINGE BOEING777 777223 1385213NM TE FLAP MISSING D AALAO OTHER O OTHER NRNOT REPORTED 1 GL13770AN 29578 HINGE BROKEN, SEAL AND BRACKET ASSY DEPARTS THE AIRCRAFT. 2L72 4F RTT00001SE 20040224000082004022400008 2004 2 24 GLBA20030532 420040115A34006226137201 RECEIVER BEECH 1900 1900D 1154162CE NR1 NAV FAILED A GLBAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 NM03208GL2379 UE208 NR 1 NAV FAILED, REMOVED AND REPLACED NR 1 NAV RECEIVER PN 622-6137-201. 2L72 4T RTA24CE 20040224000092004022400009EA 2004 2 24 ASOA04009 120040105A2750860D10018 CONTROL UNIT CNDAIRCL600 CL6002B19 1900309EA TE FLAPS OUT OF RIG A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11846AS10982 7328 DURING TAKEOFF, THE CREW RECEIVED A FLAPS FAIL MESSAGE WHEN SELECTING THE FLAPS TO ZERO DEGREES. QRH PROCEDURES WERE COMPLIED WITH AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO ICT AND LANDED SAFELY. MAINTENANCE INSPECTED THE FLAPS AND RESET THE FLAPS ELECTRONIC CONTROL UNIT USING THE BREAKERS IAW ASA EO 600-27-0004A. (M) 2L72 4F RTA21EA 20040224000132004022400013EA 2004 2 24 ASOA04015 120040106A5320 CLIP CNDAIRCL600 CL6002B19 1900309EA FLOORBEAM CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11852AS 7369 DURING A C-CHECK IN MCN, THE FLOOR SUPPORT CLIPS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR FRAME CLIPS AT FS 280, LBL 9 AND RBL 9 IAW SRM 51-00. (M) 2L72 4F RTA21EA 20040224000142004022400014EA 2004 2 24 ASOA04014 120040106A5260601R3198055 STEP CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11852AS 7369 DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE TOP STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040224000152004022400015EA 2004 2 24 ASOA04013 120040106A5320601R3501163 PLATE CNDAIRCL600 CL6002B19 1900309EA SILL CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11852AS 7369 DURING A C-CHECK, THE CARGO SILL PLATE UNDER THE FORWARD ATTACH BRACKET AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO SILL PLATE UNDER THE FORWARD ATTACH BRACKET AT FS 562.72-589. (M) 2L72 4F RTA21EA 20040224000202004022400020EA 2004 2 24 A6WA200440005 120040110A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY FALSE ACTIVATIONA O OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL31443AW 7781 SMOKE TOILET CAS MESSAGE ON TAXI, COMPLIED WITH QRH. FIRE DEPARTMENT INSPECTED LAV, NO EVIDENCE OF SMOKE OR FIRE. INSTALLED SMOKE DETECTOR AFT LAV, TESTED OK. REMOVED FROM MEL. (M) 2L72 4F RTA21EA 20040224000282004022400028EU 2004 2 24 A6WA200460001 120040105A492038000864 APU BAC 146 146200A 1500266EU APU BAY INOPERATIVE A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL31607AW E2052 SMOKE IN CABIN WHEN APU IS SUPPLYING AIR TO PACKS. MAINTENANCE PERFORMED PACK BURNOUT AND REMOVED AND REPLACED APU. (M) 2H74 4F A49EU 20040224000292004022400029EA 2004 2 24 A6WA200440004 120040109A5210 LATCH CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE PAX DOOR INOPERATIVE A A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31401AW 7280 DURING CLIMB-OUT, AMBER DOOR LATCH CAS MESSAGE, FOLLOWED QRH. AT APPROXIMATELY FL20.0 RED PASSENGER DOOR MESSAGE ILLUMINATED FOLLOWED QRH DIVERTED. INSPECTED DOOR ALIGNMENT PINS AND INTERROGATED PSEU. FOUND 3 FAULTS ON PSEU. DOOR CLOSES AND LOCKS NORMALLY. PRESSURIZED CABIN TO 5 PSID. ADJUSTED PASSENGER DOOR OUTER HANDLE IAW 52-11-03. OPS CHECK GOOD. (M) 2L72 4F4 FRTA21EA E15NE 20040224000402004022400040EU 2004 2 24 USAASA04006 120040117A335032145410 POWER SUPPLY AIRBUS320 A320214 3930316EU EMERGENCY LIGHT FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19110UW 1112 DCA - FOUND INTERNAL FAULT ON LEFT EPSU. MAINTENANCE REPLACED THE EPSU. (M) 2L72 4F RTA28NM 20040224000412004022400041EU 2004 2 24 USAASA04009 120040128A335032145410 POWER SUPPLY AIRBUSA319 A319112 3930323EU EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19714US 1046 DCA - THE EMERGENCY LIGHTS WOULD NOT PASS THE SELF TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT AT THE MID CABIN, RIGHT HAND POSITION. OPS CHECKED OK. (M) 2L72 4F RTA28NM 20040224000432004022400043EA 2004 2 24 A6WA200440014 120040131A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31406AW 7402 FOUND SKIN DAMAGED, LEFT SIDE OF AIRCRAFT AT FS 682 TO FS 718 BETWEEN STRINGERS 16L AND 18L. (M) 2L72 4F RTA21EA 20040224000472004022400047 2004 2 24 USAASA04010 420040129A2565 SLIDE AIRBUSA319 A319112 3930323EU PAX DOOR DEPLOYED A K NONE W INADEQUATE Q C ININSP/MAINT 1 EA19740UW 1265 PRIOR TO DEPARTURE, THE MAIN ENTRY DOOR WAS OPENED WHILE THE SLIDE WAS ARMED. THE SLIDE DID NOT INFLATE. MAINTENANCE REMOVED THE SLIDE AND DEPLETED THE AIR PRESSURE FROM THE CYLINDER. AIRCRAFT FERRIED FOR MAINTENANCE TO PIT. THE SLIDE WAS REPLACED. IN THE SHOP, THE SLIDE TIME CONTINUATION TASK WAS PERFORMED. OK FOR SERVICE. 2L72 4F RTA28NM 20040223000392004022300039SO 2004 2 23 RAIA00401001 120040104A3230 CONNECTOR EMB 145 EMB145LR 3260212SO MLGEU DIRTY A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03827HK 145021 5621-STL- LANDING GEAR AIR GROUND FAIL MESSAGE. MAINTENANCE CLEANED ELECTRICAL CONNECTOR ON LANDING GEAR ELECTRONIC UNIT. 2L72 4T RTT00011AT 20040223000872004022300087EU 2004 2 23 AWXA200400020 120040106A3510MXP801 STOWAGE BOX AIRBUS320 A320232 3930326EU ZONE 212 STICKING A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28650AW 856 MCI - DIVERSION - FLT 0688 - EN ROUTE, 2 HOURS AND 20 MINUTES INTO FLIGHT, CREW OXYGEN PRESSURE INDICATED 20 PSI, DIVERTED. MAINTENANCE FOUND FIRST OFFICERS MASK TEST BUTTON STUCK KEEPING VALVE PARTIALLY OPEN, AFTER TAPPING ON BUTTON THE VALVE RESET, OPERATIONAL TEST WAS PERFORMED SEVERAL TIMES WITH NO DISCREPANCIES NOTED. REMOVED AND REPLACED CREW OXYGEN BOTTLE, LEAK CHECK WAS GOOD. WHEN AIRCRAFT ARRIVED, MAINTENANCE REPLACED THE FIRST OFFICERS OXYGEN MASK STOWAGE BOX IAW AMM 35-12-41-401, OPERATIONAL AND LEAK CHECK WAS GOOD. 2L72 4F RTA28NM 20040223001142004022300114CE 2004 2 23 GLBA2003527 120040107A2750 FLAP BEECH 1900 1900D 1154162CE WING STUCK A GLBAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM03154GL UE154 FLAPS STUCK AT 17 DEG, PENDING CORRECTIVE ACTION 2L72 4T RTA24CE 20040223002012004022300201NM 2004 2 23 COOSDR030029 120040101A531165163008687 FRAME BOEING737 737300 1384610NM BULKHEAD CRACKED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23318FL 26293 BS 178, RBL 28 AND LBL 28, SIDE CHORDS CRACKED. 2L72 4F RTA16WE 20040223002072004022300207NM 2004 2 23 COOSDR030037 120040101A5755651734748 SKIN BOEING727 72731 1384010NM RT WING SPOILER DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23220NE 18905 RT WING, SPOILER NR 14, LOWER SURFACE DELAMINATED. 2L73 4F A3WE 20040223002082004022300208NM 2004 2 23 COOSDR030038 120040101A5755 SKIN BOEING727 72731 1384010NM SPOILER DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SW23220NE 502 18905 RT WING, SPOILER NR 11, LOWER SURFACE DELAMINATED. 2L73 4F A3WE 20040223002162004022300216NM 2004 2 23 COOSDR030046 120040101A5755 SKIN BOEING737 737200 1384453NM SPOILER DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23767TW BN073 20258 RT WING, FLIGHT SPOILER NR 7 UPPER SURFACE DELAMINATED. 2L72 4F A16WE 20040219001882004021900188CE 2004 2 19 DXTA200400233 120040128A3240 RELAY CESSNA500 560CESSNA 2076750CE BRAKE SYSTEM MALFUNCTIONED E DXTAO OTHER JS WARNING INDICATION AFFECT SYSTEMS LDLANDING 1 GL07392QS 5600429 ON FINAL APPROACH THE POWER BRAKE LOW PRESSURE AND ANTISKID INOP ANNUNCIATOR ILLUMINATED. FOLLOWED ABNORMAL PROCEDURES CHECKLIST AND PLACED THE ANTISKID SWITCH IN THE OFF POSITION. BRAKES FAILED NEAR THE END OF LANDING ROLLOUT, BRAKE PEDALS WENT TO THE FLOOR DURING EMERGENCY BRAKE APPLICATION. GAINED ACCESS TO BRAKE ACCUMULATOR, POWER BRAKE VALVE & ANTISKID SERVO, HYDRAULIC BRAKE RESERVOIR, INSPECTED AREA AND NO HYDRAULIC FLUID LEAKING NOTED. TROUBLESHOT BRAKE SYSTEM AND CHECKED CONNECTORS, ALL SECURED, CHECKED ANTISKID BITE INDICATOR, NO BITE SHOWING, REMOVED GROUND WIRES FROM GROUNDING STUBS, INSPECTED AND REINSTALLED. REPLACED BRAKE RELAY, BLED SYSTEM IAW CESSNA 560 MM CHAPTER 32-40-00. 2L72 4F RTA22CE 20040219001892004021900189CE 2004 2 19 DXTA200400236 120040202A3240 BRAKE ASSY CESSNA500 560CESSNA 2076750CE MLG MALFUNCTIONED E DXTAO OTHER S AFFECT SYSTEMS LDLANDING 1 GL07395QS 5600496 UPON TOUCH DOWN AND INITIAL APPLICATION OF BRAKES, CAPTAIN’S SIDE HAD POSITIVE BRAKE PRESSURE BUT AIRCRAFT WOULD NOT SLOW DOWN. AFTER APPLICATION OF EXCESSIVE BRAKE PRESSURE A/C BRAKES GRABBED AND AIRCRAFT SLOWED RAPIDLY. BLED BRAKE SYSTEM, OPS CHECK OF BRAKES GOOD AT THIS TIME IAW CESSNA 560 MM CHAPTER 32-42-00. 2L72 4F RTA22CE 20040219001902004021900190CE 2004 2 19 DXTA200400238 120040205A21202724128714 CONTROL VALVE CESSNA560 560XL 2076702CE AIR DISTRIBUTIONFAILED E DXTAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL07688QS2443 5605188 AIR DUCT OVERHEAT COCKPIT LIGHT ILLUMINATED 30 SECONDS AFTER TAKEOFF, PASSENGERS SAW SMOKE IN THE CABIN. SELECTED MANUAL TEMPERATURE CONTROL TO COLD FOR 30 SECONDS WITHOUT A CHANGE, THE SOURCE TEMP REACHED 325 DEGREES, EMERGENCY DECLARED, AIRCRAFT DIVERTED TO CHS AND LANDED SAFELY. COMPLIED WITH GROUND RUN CHECKS OF THE TEMP CONTROL SYSTEM, NO DISCREPANCIES NOTED, CHECKED ELECTRICAL CONNECTORS ON CONTROLLER & COCKPIT TEMP CONTROL VALVE. REMOVED & REPLACED VALVE DUE TO CESSNA RECOMMENDATION. SYSTEM OPS CHECK & LEAK CHECK GOOD ON GROUND RUN. ALL WORK DONE IAW CESSNA 560XL MM CHAPTER 21-61-00. 2L72 4F RTA22CE 20040219001952004021900195NM 2004 2 19 04FDEA00320 120040205A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25589FE 48491 LT WING - FOUND OUTBOARD FLAP, INBOARD FWD HINGE MOUNTING HOLE (7) INBOARD SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75243 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBD. FLAP INBD HINGE BRACKET REPAIR 2L73 4F RTA22WE 20040219002042004021900204NM 2004 2 19 04FDEA00329 120040205A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 RIGHT I/B FLAP O/B HINGE FWD UPPER ATTACH FITTING FOUND CRACKED. RT I/B FLAP O/B AFT HINGE ASSY REMOVED & REPLACED AS PER DRAWING NR NRC6060. 2L73 4F RTA22WE 20040219002192004021900219NM 2004 2 19 QXEA200400113 120040203A5420 CLIP BOMBDRDHC8 DHC8401 1390041NM ZONE 400 CRACKED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09409QX 4051 PDX - UPPER FORWARD OUTBOARD NACELLE CENTER STRUCTURE ATTACH CLIP CRACKED ON RIGHT HAND NACELLE. REPAIRED IAW HORIZON AIR EA 6-54-283. 2H72 4T RTA13NM 20040219002222004021900222NM 2004 2 19 QXEA200400102 120040129A5347 SEAT TRACK DHAV DHC8 DHC8202 2809007NM ZONE 100 CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09356PH 502 PDX - RIGHT OUTBOARD SEAT TRACK NR 11 CORROSION TOP AND BOTTOM SEAT ATTACH AREA APPROXIMATELY X438.00. REPAIRED IAW DASH 8-200 SRM 51-40-11, SRM 51-40-00. 2H72 4T RTA13NM 20040219002282004021900228EU 2004 2 19 027751 120040207A3210 LANDING GEAR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE MAINS MALFUNCTIONED A UHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL1719XS 340A019 DURING CLIMBOUT FROM PIT THE AIRCREW RAISED THE GEAR HANDLE, THE TRANSIENT LIGHT REMAINED ON AND THE HYDRAULIC PUMP CONTINUED TO RUN. THE CREW ATTEMPTED ANOTHER GEAR CYCLE AND HAD THE SAME RESULTS. A/C RETURNED TO PIT. 2L72 4T4 TRTA52EU E8NE6 20040219002322004021900232SO 2004 2 19 C2XA04TY034 120040207A531514522460013 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713550 145575 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER FLOORBEAM AT FRAME 20. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMB SRM 53-21-10, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20040219002342004021900234SO 2004 2 19 C2XA04CL009 120040206A3397 WIRE EMB 145 EMB145ER 3260211SO EMERGENCY LIGHT LOOSE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714943 145040 DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT ON THE THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE REPAIRED WIRE SPLICE SP3676, OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20040219002442004021900244NM 2004 2 19 CALA0400081 120040206A5320 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND A 2 INCH CRACK IN AFT CABIN L-ANGLE AT TOP OF INTERCOSTAL WEB AT FASTENER HOLES (4 EACH), STA 927-947, BL 0, WL 209. A SHEAR WEB ANGLE WAS INSTALLED IAW SRM 51-40-02 AND BOEING DRAWING 69-36656. 2L72 4F RTA16WE 20040219002522004021900252NM 2004 2 19 CALA0400089 120040208A5320 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND R-1 DOOR CUTOUT ZEE ANGLE CORRODED FROM STA 290-360. THE ZEE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040220000012004022000001EU 2004 2 20 118161 120040206A7720 WARNING LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE RT ENGINE ILLUMINATED A UHLACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL1743SZ 340A043 406 ON 02-06-04, APPROX 16450 (UTC), FLT 4591 PIT-TOL. ON TAKEOFF ROLL, RT ENGINE OVERTEMP LIGHT ILLUMINATED. LP BLEEDS IN AUTO, HP BLEEDS OFF AND ANTI-ICE ON. 2L72 4T4 TRTA52EU E8NE6 20040220000132004022000013EA 2004 2 20 COMA0460119 120040103A5313 STRINGER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01812CA 7381 CARGO ENTRY WAY FORWARD FRAME AT FS 574.00 APPROXIMATELY STRINGER 15L HAS DAMAGE. COMPLIED WITH REO 601R-53-61-690 TO FACILITATE CARGO ENTRY WAY FORWARD FRAME FS 574.00 REPAIR. PARTIALLY REMOVED FRAME AT FS 574.00 IN ACCORDANCE WITH CRJ SRM 51-40-06. LOCATED FRAME, SPLICE DOUBLER AND FRAME ANGLE AND COMPLETED INSTALLATION OF FRAME REPAIR AT FS 574.00 IN ACCORDANCE WITH BOMBARDIER REO 601R-53-61-901. APPLIED TOPCOAT TO FS 574.00 REPAIR IN ACCORDANCE WITH CRJ SRM 51-25-16. 2L72 4F RTA21EA 20040220000212004022000021NM 2004 2 20 UPS04441841 120040126A5310 SHEAR TIE BOEING747 747123 1384873NM AFT CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, AFT CARGO BILGE AREA - FX 1820, STR 44R - 46R SHEAR TIES CORRODED. BS 1820 TO 1820, STR R44-R46 CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.040 INCH X 0.5 INCH X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. FLANGE REPAIRED REFER SRM 53-10-04 FIG 3 AND CIC APPLIED IAW EO M-5100-2780-E. 2L74 4F A20WE 20040224000182004022400018EA 2004 2 24 ASOA04012 120040106A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11852AS 7369 DURING A C-CHECK, THE CARGO COMPARTMENT AFT FLOOR SUPPORT ANGLES ON THE LT AND RT SIDES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT AFT FLOOR SUPPORT ANGLES ON THE LT AND RT SIDES AT FS 621 IAW ASA EO 600-53-0105. (M) 2L72 4F RTA21EA 20040224000342004022400034EU 2004 2 24 USAASA04008 120040126A335032145410 POWER SUPPLY AIRBUSA319 A319112 3930323EU GE CFM56 CFM56* 13802NE EMERGENCY LIGHT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19751UW5599 1317 MAINTENANCE FOUND THE MID RIGHT EMERGENCY POWER SUPPLY UNIT INOPERATIVE. MAINTENANCE REPLACED MID RIGHT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M) 2L72 4F4 FRTA28NM E2GL 20040224000372004022400037EA 2004 2 24 ASOA04057 120040121A33501317 LAMP CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE EMERGENCY LIGHT BURNED OUT A ASOAK NONE O OTHER ININSP/MAINT 1 SO11867AS 7463 DURING A GROUND INSPECTION, THE EMERGENCY CEILING LIGHT AT ROW TEN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW TEN. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA21EA E15NE 20040224000382004022400038EA 2004 2 24 ASOA04056 120040121A33974871907191 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCONNECTED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11825AS 7207 DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY FLOOR LIGHTS BETWEEN ROWS 1 TO 5 WERE FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE EMERGENCY FLOOR LIGHTS BETWEEN ROWS 1 TO 5. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040224000642004022400064EA 2004 2 24 040038662 120040207A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27662BR 7526 DURING INSPECTION THE RIGHT HAND FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040224000762004022400076EA 2004 2 24 COMA0460133 120040211A53116003603032 DOUBLER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01982CA16547 7168 RIGHT FS 718 BETWEEN STRINGERS 10R AND 12R P/N 600-36030-32 IS CRACKED. PERFORMED A MAJOR REPAIR TO FS 718 BETWEEN STRINGERS 10R AND 12R BY REMOVING AND REPLACING DOUBLER P/N 600-36030-32 IAW CRJ 200 SRM 51-42-00 AND 51-42-21. 2L72 4F RTA21EA 20040224000792004022400079NM 2004 2 24 QXEA200400126 120040208A335082520977001 LIGHT DHAV DHC8 DHC8202 2809007NM ZONE 100 BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09362PH 518 PDX - ON FLIGHT 2243 FLOOR EMERGENCY LIGHT SEGMENT IS INOPERATIVE AT FORWARD RIGHT SIDE. REMOVED AND REPLACED EMERGENCY FLOOR PATH LIGHT SEGMENT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040224000802004022400080EA 2004 2 24 COMA0460135 120040211A5330601R53211801 DOUBLER CNDAIRCL600 CL6002B19 1900309EA BENT A COMAK NONE O OTHER ININSP/MAINT 1 SO01982CA 7168 PREVIOUS REPAIR TO LEFT SIDE FUSELAGE SKIN HAS SUBSTAINED FURTHER DAMAGE ON FUSELAGE SKIN EXTERNAL DOUBLER. PERFORMED A MAJOR REPAIR TO FUSELAGE SKIN AT FS 310 BETWEEN STRINGER 15R AND 16R BY REMOVING DAMAGED TOP REPAIR DOUBLER. NO DAMAGE FOUND ON BOTTOM DOUBLER AND FILLER. FABRICATING NEW REPAIR DOUBLER FROM 2024T3.063 (WVAC PO 32572/1) AND INSTALLING IAW BOMBARDIER INC REO 601R-53-21-180 REV NC. 2L72 4F RTA21EA 20040224000852004022400085EA 2004 2 24 COMA0470016 120040209A3610GG670950103 CONTROL VALVE CNDAIRCL600 CL6002C10 1390015EA BLEED AIR MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01379CA2158 10102 FLIGHT 5073 LEFT COWL ANTI ICE AND LEFT BLEED CAUTION MESSAGE. REPLACED THE TEMP CONTROL VALVE. 2L72 4F RTA21EA 20040224000872004022400087EA 2004 2 24 COMA0460141 120040210A2760278003 PCU CNDAIRCL600 CL6002B19 1900309EA GROUND SPOILER BROKEN A COMAL ABORTED APPROACH JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 SO01941CA22443 7050 FLIGHT 5110 GROUND SPOILER DEPLOY MESSAGE DURING APPROACH. LEFT OUTBOARD SPOILER PCU BROKEN. REPLACED PCU. 2L72 4F RTA21EA 20040224001032004022400103WP 2004 2 24 04FDEA00394 120040211A5753ARC03291 SUPPORT DOUG DC10 DC1010 3022110WP ZONE 500 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25373FE 46611 COMPLY WITH EA 8-5750-73880 WINGS - INBOARD FLAP ACTUATOR SUPPORT ASSY BARREL NUT HOLE GOUGED. REPAIR P/N ARC0329-1. COMPLIED WITH EA 8-5750-73880. 2L73 4F A22WE 20040224001062004022400106NM 2004 2 24 AWXA200400169 120040210A2560P4010021 BATTERY BOEING737 73733A 1384673NM ZONE 900 - LAVATDISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 LAS - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED CABIN EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20040224001102004022400110WP 2004 2 24 AALA20040214 120040210A3397 WIRE DOUG DC9 DC983 3022083WP EMERGENCY LIGHT LOOSE A AALAK NONE O OTHER ININSP/MAINT 1 SW21964TW 53614 MIA EMERGENCY LIGHT AT SEAT 8D INOPERATIVE. FOUND LOOSE WIRING. SECURED WIRING FOR EMERGENCY LIGHT AT SEAT 8D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040224001172004022400117NM 2004 2 24 QXEA200400128 120040209A2751 WARNING LIGHT BOMBDRDHC8 DHC8401 1390041NM ZONE 100 ILLUMINATED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09405QX 4047 SEA - ON FLT NR 9850, WHEN SELECTING APPROACH FLAPS, FLAP POWER CAUTION LIGHT ILLUMINATED. PER CHECKLIST, THE FLAP CONTROL CIRCUIT BREAKER WAS CYCLED. CYCLED SHIPS POWER. OPERATED FLAPS. FLAP POWER CAUTION REMAINS EXTINGUSHED. CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20040224001182004022400118SO 2004 2 24 C2XA04TY036 120040210A531514521700007 FLOORBEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717513 145292 TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND OMEGA BEAM AT FRAME 19. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMB SRM 53-21-10, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4F RTT00011AT 20040224001192004022400119NM 2004 2 24 0400206302 120040208A3350 LIGHT BOEING747 747451 1384940NM CABIN INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01662US 23720 DURING LINE CHECK, FOUND LEFT AND RIGHT SIDE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPAIRED LIGHTS. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040224001272004022400127EA 2004 2 24 COMA0470019 120040205A2750766389G CONTROL UNIT CNDAIRCL600 CL6002C10 1390015EA TE FLAPS MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01331CA3 10061 FLIGHT 5476 FLAPS HALF SPEED MESSAGE. REPLACED THE SFECU. 2L72 4F RTA21EA 20040224001332004022400133SO 2004 2 24 C2XA04SH061 120040212A531014522226003 BUTTSTRAP EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712530 145533 SHV-DURING C-CHECK THE CENTER BUTTSTRAP AT FRAME 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040224001352004022400135SO 2004 2 24 C2XA04SH063 120040212A531514521713005 FLOORBEAM EMB 135 EMB135LR 3260305SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2712530 145533 SHV-DURING C-CHECK THE CENTER FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20040224001442004022400144NM 2004 2 24 CALA0400104 120040211A5311146N1014 FRAME BOEING757 757224 1384958NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2717126 27566 INSPECTION FOUND FRAME DENTED AT BS 1460, S27L. THE FRAME WAS REPAIRED IAW SRM 53-00-07, FIGURE 201. 2L72 4F RTA2NM 20040224001462004022400146NM 2004 2 24 CALA0400106 120040212A532065524572 WEB BOEING737 7373T0 1384582NM FUSLAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND AFT WEB RT SIDE ADJACENT TO RUBBER MEMBRANE AT APB, STA 1016, RBL 0 TO RBL 48, CORRODED. A NEW WEB WAS INSTALLED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040224001472004022400147NM 2004 2 24 CALA0400107 120040212A532069353593 INTERCOSTAL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND A 4 INCH CRACK IN AFT BAGGAGE BIN INTERCOSTAL UNDER TRANSITION PANEL AT STA 928, RBL 26. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040224001532004022400153NM 2004 2 24 UPS04241872 120040130A5350 BRACKET BOEING727 72722C 138400FNM WING-BDY FAIRINGDAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE: C, LATCH FITTING ON W/BODY FAIRING BRACKET FOR AFT CARGO DOOR FAIRING LATCH IS DAMAGED. BRACKET REPLACED IAW SRM 51-20-01. 2L73 4F A3WE 20040224001592004022400159NM 2004 2 24 UPS04441871 120040127A532065B0434527 STIFFENER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, AFT OF BULK CARGO COMPT- LT STA 2160 STRINGER 40 STIFFENER ANGLE FOUND CRACKED. AFT OF BULK CARGO LT STA 2160 FRAME AT STRINGER 40 STIFFENER ANGLE REPLACED AS PER SRM 51-10-01 PG 8. 2L74 4F A20WE 20040224001612004022400161NM 2004 2 24 UPS04441893 120040127A5311 FRAME BOEING747 747123 1384873NM SECTION 41 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, SECTION 41, FS 250 BETWEEN STR 40L - 41L, FRAME WEB CRACKED BS 260 CANTED BULKHEAD WEB SEGMENT BETWEEN STR 38L AND STR 41L. REPLACED AS PER HX RS R-53-13-35101 AND UPS ENGINEERING FILE NUMBER 747-53-20167. 2L74 4F A20WE 20040224001642004022400164WP 2004 2 24 UPS04841868 120040204A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, FUSELAGE SKIN IS CRACKED AT FASTENER HOLE AT STATION 1342 LONG 31R. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER, DOUBLER AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7. 2L74 4F RT4A25 20040224001652004022400165WP 2004 2 24 UPS04841869 120040128A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE:C3 FUSELAGE SKIN IS CORRODED BEYOND LIMITS STATION 1690-1700 LONG 35L-35R. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER, DOUBLER AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7. 2L74 4F RT4A25 20040224001662004022400166WP 2004 2 24 UPS04841877 120040129A5313 LONGERON DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, STATION 1735 LONGERON 13R IS CRACKED. REMOVED DAMAGED LONGERON SECTION BETWEEN STATION 1716-1742, FABRICATED AND INSTALLED LONGERON SECTION, STRAPS AND INSTALLED SPLICE FITTING IAW SRM 53-2-2 FIG 10. 2L74 4F RT4A25 20040224001692004022400169WP 2004 2 24 UPS04841880 120040130A5712 RIB DOUG DC8 DC871F 302199DWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE:C3 LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 372.75, XFS 379. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040224001702004022400170WP 2004 2 24 UPS04841881 120040130A5712 RIB DOUG DC8 DC871F 302199DWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 766.250. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040224001782004022400178WP 2004 2 24 UPS04841889 120040201A5712 RIB DOUG DC8 DC871F 302199DWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT XS 478.897. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040224001792004022400179WP 2004 2 24 UPS04841890 120040201A5712 RIB DOUG DC8 DC871F 302199DWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, RIGHT WING L/E UPPER RIBS ARE CRACKED AT XFS 410.25, XFS 347.75, XFS 354. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040224001812004022400181WP 2004 2 24 ABXA040063 120040214A5320 PLATE DOUG DC8 DC861 3021952WP FUSELAGE MISREPAIRED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23847AX 46031 FOUND MAIN ENTRY DOOR SCUFF PLATE DID NOT MEET REQUIREMENTS OF SERVICE REWORK DRAWING SRO8530021. TEMPORARY REPAIRED MAIN ENTRY DOOR SCUFF PLATE IAW REA D853-49056MR. PLACED ON CARRY OVER NR COI 46070. PROPER FASTENERS TO BE INSTALLED ON OR BEFORE 9-6-2005. 2L74 4F 4A25 20040224001822004022400182WP 2004 2 24 ABXA040062 120040210A5210 DOOR DOUG DC9 DC931 3022065WP MAIN PAX OBSTRUCTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 PASSENGER ENTRY DOOR WOULD NOT OPEN FROM INSIDE, WORKED OKAY FROM OUTSIDE. FOUND DOUBLER PLATE INTERFERING WITH MOVEMENT OF OUTER DOOR HANDLE. FAIRED DOUBLER IAW DC-9 SRM 52-01. OPERATED DOOR SEVERAL TIMES. OPS CHECKED GOOD. 2L72 4F A6WE 20040224001852004022400185NM 2004 2 24 CALA0400112 120040213A53106552863507 HINGE BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND A 1 INCH CRACK IN R-2 DOOR HINGE HOUSING AT LOWER SURFACE, STA 954, RBL 55, WL 230. THE HOUSING WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040224001872004022400187NM 2004 2 24 CALA0400114 120040213A533065C33756 SKIN BOEING737 7373T0 1384582NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND FUSELAGE SKIN DENTED AT BS 324 JUST BENEATH S20R. THE DENTED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 202. 2L72 4F RTA16WE 20040224001882004022400188NM 2004 2 24 CALA0400115 120040214A5320654580148 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND ANGLE ATTACHED TO FORWARD WALL OF NOSE WHEEL WELL CORRODED AT STA 227, RBL 14. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2L72 4F RTA16WE 20040224001902004022400190NM 2004 2 24 CALA0400117 120040214A5320BMS569 WEB BOEING737 737724 13844BYNM RT MLG WW CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713720 28939 INSPECTION FOUND A 4 INCH CRACK IN RT MAIN WHEEL WELL AFT WEB. THE WEB WAS REMOVED AND REPLACED IAW SRM 53-40-71 AND 51-10-2. 2L72 4F RTA16WE 20040224001972004022400197NM 2004 2 24 UPS04241898 120040123A5320 WEB BOEING727 72722C 138400FNM RT TORQUE BOX CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE: C, AFT STAIRWELL RT TORQUE BOX VERTICAL WEB HAS CRACKING BEYOND PREVIOUS REPAIR AT BS 1273. REPAIR CARRIED OUT IAW EO B727-5310-1239-E & MM 20-10-05. 2L73 4F A3WE 20040224001992004022400199NM 2004 2 24 UPS04441899 120040125A5340 FITTING BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C BS 1241 RT CANTED PRESSURE DECK FITTING AFT HOLE FOUND CRACK APPROX 0.030 INCH RUNNING DOWN. BS 1241 RT CANTED P/D FITTING AFT BOLT HOLE REPAIRED PER RS R53-41-35107 & ENG'R FILE 747-53-20170, REPAIR IS CONSIDERED A TIME-LIMITED REPAIR 2 YEARS/1500 FLT CYCLES WHICHEVER COMES FIRST, AT WHICH TIME CANTED FITTING SHOULD BE REPLACED. SPLICE STRAP SHOULD BE REPLACED WITHIN 2 YEARS OF CRACK DISCOVERY, DUE TO CRACK WAS DISCOVERY DURING PRESENT MAINTENANCE. 2L74 4F A20WE 20040225000012004022500001WP 2004 2 25 COOSDR030064 120040101A53203936595513 SUPPORT BRACKET DOUG DC9 DC982 3022082WP FUSLEAGE CORRODED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23135NJ 49440 AFT CARGO COMPARTMENT, SUPPORT BRACKETS CORRODED AT Y:STA 1250 AND Y:STA 1271 BETWEEN LONG 27L AND 28L. 2L72 4F A6WE 20040225000022004022500002WP 2004 2 25 COOSDR030065 120040101A5320 FLOOR SUPPORT DOUG DC9 DC914 3022034WP FUSELAGE CRACKED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23600ME 45725 AFT AND FORWARD CARGO COMPARTMENT, FLOOR SUPPORT LATERAL ANGLES AT B/S Y:STA 351, 427, 465, AND 737 BETWEEN LONG 28L AND 28R, WITH CRACKS. 2L72 4F A6WE 20040225000042004022500004NM 2004 2 25 COOSDR030067 120040101A5320656097130 FLOOR SUPPORT BOEING727 727224 1384076NM PAX CABIN CORRODED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2379745 22448 PAX CABIN, BS 1034 FLOOR SUPPORT PN 65-60971-30 CORRODED. 2L73 4F A3WE 20040225000112004022500011NM 2004 2 25 COOSDR030074 120040101A57306519281158 PANEL BOEING727 727224 1384076NM RT WING CORRODED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO2379745 22448 RT WING, LOWER SURFACE FIXED PANEL PN 65-19281-158, OUTER SKIN, CORRODED. 2L73 4F A3WE 20040225000262004022500026EU 2004 2 25 2004F00044 120040104A769730709341 WIRE HARNESS BRAERODH125 HS125700A 4230170EU RT ENGINE DETERIORATED E A UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 CE03120JC6970 NA0247 WHILE ENROUTE, NOTED RT ENGINE AMBER WARNING LAMP BECAME ANNUNCIATED. ALSO NOTED INDICATED LOSS OF POWER RT ENGINE. CONSULTED OPERATORS MANUAL AND COMPLIED WITH EMERGENCY PROCEDURES WHICH INCLUDED TO SWITCH TO MANUAL CONTROL AND MONITOR ALL ENGINE PARAMETERS. IMMEDIATE NOTIFICATION TO ATC AND REQUESTED TO DIVERT FOR INSPECTION. INSPECTION WAS PERFORMED AND FOLLOWING TROUBLESHOOTING AND INSPECTION THAT THE SOURCE OF THE DEFECTS WAS THE RT ENGINE PT2 HARNESS. PARTS WERE REPLACED AND PN 3070934-1 HARNESS. SYSTEM WAS OPERATIONALLY TESTED WITH NO FURTHER DEFECTS NOTED. 2L72 4F A3EU 20040225000312004022500031GL 2004 2 25 JIKA200400001 320040116A61147503503AF PACKING SWRNGNSA227 SA227AT 8780610SW ROTOL R321 R321482F8 GL LEFT PROPELLER CUT E JIKAEA ENGINE SHUTDOWN UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 WP01246DH AT625B DGIDRG160280 AFTER TAKE-OFF AT APPROXIMATELY 6000 FT AGL, PILOT NOTED LT ENGINE R.P.M. DROPPED FROM 100 PERCENT TO 97 PERCENT WITH SPEED LEVER FULL FORWARD. SHORTLY AFTER, COCKPIT FILLED UP WITH BLUE SMOKE AND LT ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. PILOT SHUT DOWN THE LT ENGINE, DECLARED AN EMERGENCY, RETURNED TO CVG AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LT ENGINE AND FOUND OIL LEVEL ABOUT 6 QUARTS LOW. OIL WAS LEAKING FROM PROPELLER HUB. INSPECTION OF THE PROPELLER HUB REVEALED PROPELLER PISTON O-RING P/N 7503503AF CUT IN HALF CAUSING THE OIL LEAK. THIS MASSIVE OIL LEAK FROM THE PROPELLER HUB INTO THE ENGINE INLET WAS THE CAUSE OF THE SMOKE IN THE COCKPIT. 2L72 4T RTA5SW 6 CP61GL 20040225000422004022500042 2004 2 25 MEX2004007 420040105A3416 INDICATOR DOUG MD80 MD83 3023681NM ALTIMETER MALFUNCTIONED W ASMFD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23491SH 49150 AIRCRAFT RETURNED TO PLATFORM AFTER ENGINES STARTING THE PO ALTIMETER FLAG CAME ON. CADC NR 2 WAS RESEATED AND TESTED IAW MM, ALL TESTED CORRECT. THE FLAG DISAPPEARED BUT IT HAD 130 FEET INDICATION BETWEEN ALTIMETERS. PNEUMATIC CONNECTIONS OF CADC NR 2 AND ALTIMETER WERE DRAINED AND CLEANED, ALL CORRECT. 2L72 4F RT 20040225000452004022500045NM 2004 2 25 MEX2004012 120040108A3213920629515 PISTON DOUG MD88 MD88 3023688NM NLG STRUT DAMAGED W ASMFC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 SW23169PL 53175 AIRCRAFT RETURN OF FLIGHT, DURING TAKEOFF ROLL, THE NLG HIT A BIG BUMP ON THE RUNWAY AND IT DID NOT RETRACT. DURING REVISION WAS DETECTED THE NLG SHOCK STRUT LOW. AIRCRAFT WAS SENT TO HANGAR, WHERE THE PISTON AXLE ASSEMBLY CYLINDER ASSY AND SHOCK STRUT SEALS WERE REPLACED IAW MM. OVERWEIGHT LANDING INSPECTION WAS PERFORMED IAW MM, ALL CORRECT. 2L72 4F RTA6WE 20040225000522004022500052CE 2004 2 25 DWH2004F00000 120040102A3297 WIRE HARNESS BEECH 200 B200 1152922CE PWA PT6 PT6* 52043EA MLG INDICATOR BROKEN E DWHAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 WP014QL 7891 BB942 PILOT REPORTED LT MLG DOWN AND LOCKED INDICATOR WAS NOT ILLUMINATED AFTER LANDING GEAR EXTENSION AND DECLARED AN EMERGENCY. THE AIRCRAFT WAS LANDED ANT VNY WITHOUT INCIDENT. UPON INVESTIGATION, A TY-WRAP WAS MISSING FROM THE LT MLG DRAG ACTUATING ROLLER HAD CAUGHT THE WIRE BUNDLE AND BROKEN THE DOWN AND LOCKED CIRCUIT WIRE UPON GEAR RETRACTION. THE WIRE WAS REPAIRED, THE WIRE BUNDLE WAS RESECURED, AND THE LANDING GEAR WAS OPERATIONALLY TESTED WITH NO FURTHER DISCREPANCIES NOTED. 1L72 4T3 T A24CE E2NE 20040225000532004022500053EA 2004 2 25 JRP2004F00000 120040112A5711C6WM10271 FITTING DHAV DHC6 DHC6 2802606EA PWA PT6 PT6* 52043EA SPAR CAP CRACKED A JRPRO OTHER O OTHER NRNOT REPORTED 1 WP21885EA22197 454 LATERAL CRACK BETWEEN RIVETS IN VERTICAL LEG OF FITTING AT WS 40 AND AT WS 47.5 FITTING IS PART OF FORWARD WING ATTACHMENT ASSEMBLY. NOTE: PART NAME IS FRONT SPAR CAP ADAPTOR FITTING. 1H72 3T3 TRTA9EA E2NE 20040223000642004022300064CE 2004 2 23 DXTA200400212 120040105A3260G2387 BULB CESSNA560 560XL 2076702CE MLG INDICATOR INOPERATIVE E DXTAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL07639QS 5605139 AFTER EXTENDING LANDING GEAR, LT MAIN GEAR GREEN LIGHT DOES NOT ILLUMINATE, BLOW-DOWN OF GEAR. FOUND BOTH LT GEAR INDICATOR BULBS TO BE INOPERATIVE. REMOVED BULBS AND REPLACED WITH 2 NEW BULBS, OPS CHECK GOOD IAW CESSNA 560XL MM CHAPTER 33-10-06. 2L72 4F RTA22CE 20040223000882004022300088EU 2004 2 23 AWXA200400022 120040104A335032145410 EPSU AIRBUS320 A320231 3930325EU ZONE 221 DEFECTIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28645AW111099031 238 MCN - EEL - DURING C-02 CHECK FOUND EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 1, 2, & 4 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT (10WL) ABOVE THE L-1 DOOR, OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM WAS GOOD. 2L72 4F RTA28NM 20040223000892004022300089NM 2004 2 23 AWXA200400023 120040104A575165C2591118A SPAR BOEING737 73733A 1384673NM AILERON DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW 23633 MCN - MINOR REPAIR - DURING C-18 CHECK THE RT AILERON FORWARD SPAR LOWER FLANGE WAS FOUND DELAMINATED AT ACCESS PANEL ATTACHMENT WS 430. MAINTENANCE TRIMMED OUT DAMAGE ON RT AILERON FORWARD SPAR, LOWER FLANGE; CLEANED AND PREPARED SURFACE; PERFORMED BOND REPAIR IAW AWA E.R. 03-5751-00159-SS2. 2L72 4F RTA16WE 20040223001022004022300102WP 2004 2 23 DHL2004801001 120040108A5210 DOOR DOUG DC8 DC873F 302199FWP MAIN CABIN LACK OF LUBE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01801DH 46033 MAIN CABIN DOOR WAS VERY DIFFICULT TO OPEN. LUBRICATED MAIN CABIN DOOR IAW DC-8 M/M 52-11-1. OPERATES NORMAL AT THIS TIME. 2L74 4F RT4A25 20040223001292004022300129EA 2004 2 23 UIA9302 120040110A2910DSC252B40124 LINE DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE HYD SYSTEM LEAKING Z B EMER. DESCENT KS FLUID LOSS AFFECT SYSTEMS DEDESCENT 1 TW0015237 467 AE0001 IN FLT NR 2 HYD SYSTEM QTY LOW. A/C MANUAL DOWN LANDING GEAR. PFM INSP FOUND HYD FLUID LEAK FORM NOSE GEAR UPLOCK HYD TUBE(PIN-HOLE). IAW AMM29-10-00 REPLACED NR 2 EDPAND CASE DRAIN FILTER AND HYD TUBE . LDG SWING CHK COND NML . ENG RUNUP CHK NR 2 EDP FUNCTION NML. 2H72 4T4 TRTA13NM E20NE 20040223001512004022300151WP 2004 2 23 IXXA0400005O 120040112A5320 CURTAIN DOUG DC8 DC871 302199AWP NLG WW UNSECURE A IXXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SW11829BX87071210 45994 DURING TAKEOFF AND UPON GEAR RETRACTION, A NOISE WAS HEARD FROM NOSE GEAR AREA. CREW RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED GEAR DOOR BRACKETS AND HINGES FOR DEFECTS AND NONE WERE NOTED. CHECKED DOOR LINKAGES, SEALS AND MECHIANISM AND NO DEFECTS WERE NOTED. LT NOSE WHEEL WELL INSPECTION FOUND CURTAIN WAS UNSNAPPED. RESECURED NOSE WHEEL WELL CURTAIN, THEN INSPECTED GEAR DOOR. PERFORMED GENERAL INSPECTION OF NOSE GEAR, NOSE WHEELS, WHEEL WELL AND RETRACTION SYSTEM IAW ALL APPLICABLE MANUALS. NO DEFECTS NOTED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20040223001522004022300152WP 2004 2 23 IXXA0400006O 120040109A3241 WARNING LIGHT DOUG DC8 DC873F 302199FWP ANTI SKID SYSTEMILLUMINATED A IXXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW11606AL903722124 46044 WHEN LANDING GEAR WAS EXTENDED THE ANTI-SKID INOP LIGHT AND LAO AND LAI LIGHTS ILLUMINATED. LAO AND LAI LIGHT REMAINED ILLUMINATED IN MANUAL ON THE SKID MONITOR PANEL. RECYCLED MAIN LANDING GEAR, ANTI-SKID CONTROL SWITCH AND RESET CIRCUIT BREAKER, NO HELP. CREW HAD TO OVER FLY KEWR FOR ANTI-SKID INOP, AND LANDED AIRCRAFT AT KBDL WITHOUT INCIDENT. MAINTENANCE AT KBDL DEFERRED ANTI-SKID AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20040223001712004022300171WP 2004 2 23 ZW0A0400101 120040112A33507732 LAMP DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139402W 53138 THE EGRESS LIGHTS WERE INOPERATIVE AT ROW 20 TO 26. REPLACED THE LAMPS. CHECK-C 7-16-03 STL. CLOSED 2L72 4F RTA6WE 20040223001722004022300172WP 2004 2 23 ZW0A0400102 120040112A33507732 LAMP DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A ZW0AK NONE O OTHER ININSP/MAINT 1 CE139402W 53138 THE AFT OVERWING EMERGENCY EXIT SIGNS WERE INOPERATIVE. REPLACED THE LAMPS. CHECK-C 7-16-03 STL. CLOSED 2L72 4F RTA6WE 20040223001792004022300179EU 2004 2 23 03009305 120040109A3220 LANDING GEAR JETAIRJETSTMJETSTM4101 1500501EU NOSE INOPERATIVE A VTZAL ABORTED APPROACH J WARNING INDICATION LDLANDING 1 EA27305UE 41019 DURING LANDING OF FLIGHT 7768 TO IAD NOSE GEAR NOT LOCKED INDICATION. CREW PERFORMED MISSED APPROACH, DECLARED EMERGENCY, AND VERFIED WITH TOWER THAT GEAR WAS NOT DOWN. CREW PERFORMED AN EMERGENCY NO NOSE GEAR LANDING AND PASSENGERS DEPLANED THROUGH EMERGENCY EXIT DOOR ON RUNWAY WITH NO INJURIES. 2L72 4T RTA41NM 20040224000442004022400044EA 2004 2 24 A6WA200440012 120040130A5210 LATCH CNDAIRCL600 CL6002B19 1900309EA PAX DOOR OUT OF ADJUST A A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31401AW 7280 ON CLIMB-OUT, PASSENGER DOOR LATCH CAUTION MESSAGE FOLLOWED BY PASSENGER DOOR WARNING. FLIGHT ATTENDANT STATED THE TWO TOP ALIGNMENT MARKS WERE OFF. REMOVED AND REPLACED AFT UPPER PASSENGER DOOR BEARING ROD. ADJUSTED DOOR LATCH MECHANISM. PERFORMED OPS AND FUNCTINAL TEST OF PASSENGER DOOR, OPS CHECK GOOD AT THIS TIME. (M) 2L72 4F RTA21EA 20040224000602004022400060EA 2004 2 24 ASOA04025 120040108A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA CABIN DETECTED A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11906EV 7642 FLT 4561 - DURING TAKEOFF AND CLIMB-OUT FROM ATL-MOB, THE CREW NOTICED A STRONG OIL ODOR WHICH WAS MOST NOTICEABLE AFTER TRANSFER OF BLEED AIR TO THE ENGINES. THE ODOR WENT AWAY AFTER FOUR TO FIVE MINUTES. THE AIRCRAFT LANDED SAFELY IN MOB. MAINTENANCE INSPECTED THE PACKS AND GROUND RAN THE ENGINES WHILE CYCLING THE PACKS. NO OIL ODOR OR DEFECTS WERE NOTED. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040224000612004022400061EA 2004 2 24 ASOA04024 120040108A21707536893 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA CABIN AIR CONTAMINATED A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11906EV 7642 FLT 4156 - DURING CLIMB-OUT FROM EVV-ATL, THE CREW NOTICED A STRONG OIL ODOR IN THE CABIN AND COCKPIT. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE COALESCER BAGS TO THE AIR CYCLE MACHINE. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20040224000652004022400065 2004 2 24 04038638 420040207A34183995100208 COMPUTER CNDAIRCL600 CL6002B19 1900309EA STALL WARNING FAULTY A VTZAO OTHER S AFFECT SYSTEMS APAPPROACH 1 EA27638BR 7311 DURING APPROACH CREW REPORTED A STALL SYSTEM FAILURE WHEN FLAPS WERE SELECTED TO 8 DEGREES. THE STALL COMPUTER WAS FOUND FAULTY AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040224000692004022400069EA 2004 2 24 04040651 120040209A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27651BR 7426 DURING INSPECTION THE LEFT FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND FAULTY AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 20040224000772004022400077EA 2004 2 24 COMA0460134 120040211A53306003301039 SKIN PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01982CA16547 7168 RIGHT AND LEFT SIDE LOWER FUSELAGE SKINS ARE CRACKED AT NOSE LANDING GEAR CUTOUT AT FS 235 STRINGERS 26R AND 26L. CRACKS ARE 1.0 INCH LONG. PERFORMED A MAJOR REPAIR FUSELAGE SKIN AT FS 235 STRINGER 26R AND 26L BY CUTTING OUT DAMAGED AREAS, FABRICATING REPAIR FILLERS AND DOUBLERS FROM 2024T3.050 (WVAC PO 33196/1) AND 2024T3.063 (WVAC PO 32572/1). PERFORMING LP1 TO ENSURE CUTOUT AREAS ARE CRACK FREE AND INSTALLING REPAIR PARTS IAW BOMBARDIER, INC REO 601R-53-11-010 REV C AND REO 601R-53-11-014 REV NC. 2L72 4F RTA21EA 20040224001042004022400104GL 2004 2 24 04FDEA00395 220040211A7210 HOUSING DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL NR 2 ENG GEARBOXGOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25373FE 46611 COMPLY WITH EA 8-7260-75573. ENGINE DRAIN - TRANSFER GEARBOX HOUSING DAMAGE INTERIM REPAIR. COMPLIED WITH EA 8-7260-75573. 2L73 4F4 F A22WE E23EA 20040224001212004022400121NM 2004 2 24 0400216637 120040205A3097CWC011210 TERMINAL BOEING747 747251B 1384892NM 1L WINDOW BURNED A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01637US 23548 DURING CLIMB, A STRONG BURNING ODOR EMITTED FROM THE CAPTAIN'S L1 LOWER LEFT WINDOW HEAT ELECTRICAL CONNECTIONS. PLACED L1 IN OVERRIDE AND ODOR DISSIPATED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT LOWER AND UPPER WINDOW HEAT TERMINALS ON L1 WINDOW AND REPLACED THE WINDOW HEAT CONTROLLER. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20040224001222004022400122NM 2004 2 24 0400236309 120040207A3350 LIGHT BOEING747 747451 1384940NM ROWS 21-31 INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01669US 24224 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21 TO 31. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 20040224001382004022400138CE 2004 2 24 DXTA200400241 120040212A2120 ODOR CESSNA500 560CESSNA 2076750CE GALLEY DETECTED E DXTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07341QS 5600341 HOT ELECTRICAL ODOR COMING FROM THE CABIN. ODOR STARTED AT FL100 AND CONTINUED TO GET WORSE. CREW TURNED DOWN THE HEATER CLOSED FOOT WARMERS, PULLED COFFEE POT OUT OF SLOT. ODOR DID NOT STOP. AT FL180 TO FL200 CREW MADE DECISION TO RETURN TO CLT ON DESCENT BEGAN TO QUIT AT FL100. ODOR WAS GONE ON THE GROUND. 2L72 4F RTA22CE 20040224001452004022400145NM 2004 2 24 CALA0400105 120040211A5414311A1400 SKIN BOEING737 7373T0 1384582NM NR2 PYLON STRUT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714335 23573 INSPECTION FOUND A 0.75 INCH CRACK IN NR 2 PYLON STRUT SKIN AT ACCESS DOOR 5824R CUTOUT, TOP FORWARD CORNER. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER AND FILLERS WERE INSTALLED IAW ECRA 5430-01204. 2L72 4F RTA16WE 20040224001542004022400154NM 2004 2 24 UPS04241873 120040123A5280 HINGE BOEING727 72722C 138400FNM MLG DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 INSPECTION TYPE: C, LEFT WING GEAR DOOR AFT HINGE, INNER HINGE HALF CRACKED. REPLACED HINGE IAW SRM 51-30-02. 2L73 4F A3WE 20040224001602004022400160NM 2004 2 24 UPS04441892 120040121A5320 WEB BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, M/D - BS 270 LT STR 26L VERTICAL SUPPORT WEB FOUND CRACKED. REPAIRED VERTICAL SUPPORT WEB PER SRM 51-40-02 FIG 1. 2L74 4F A20WE 20040224001752004022400175WP 2004 2 24 UPS04841886 120040201A5712 RIB DOUG DC8 DC871F 302199DWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 641.25. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040224001802004022400180WP 2004 2 24 UPS04841891 120040212A3510 REGULATOR DOUG DC8 DC873F 302199FWP OXYGEN SYSTEM LEAKING A IPXAK NONE O OTHER ININSP/MAINT 1 SO01808UP 46008 F/O OXYGEN REGULATOR LEAKING. REMOVED AND REPLACED 02 BOTTLE IAW MM 12-70-01-3, NO LEAKS NOTED. 2L74 4F RT4A25 20040224001962004022400196NM 2004 2 24 CALA0400124 120040216A532065479571 WEB BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND A .25 INCH CRACK IN C-2 DOOR OPENING LOWER FORWARD SILL WEB AT STA 787. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040225000472004022500047CE 2004 2 25 2004F00045 120040113A2612 FIRE LOOP LEAR 25 25B 5170511CE GE CJ610 CJ6108 30006NE NACELLE DIRTY E O OTHER N FALSE WARNING CRCRUISE 1 GL257810W 117 249044A FALSE FIRE WARNING DURING FLIGHT. AFTER A/C LANDED, PILOT REPORTED INDICATION WAS INTERMITTENT. COWL WAS REMOVED, ENGINE INSPECTED, NO INDICATION OF FIRE/OVERHEAT. DETECTION LOOP INTACT/NO DAMAGE. WIRING CONNECTIONS AT FIREWALL DISCONNECTED, APPEARED TO BE MORE THAN NORMAL BUILD UP OF GRIME/CARBON. CLEANED TERMINALS/CONTACTS, RECONNECTED. GROUND RUN, UNABLE TO DUPLICATE FIRE INDICATION. 2L72 4J4 J A10CE 1E16 20040225000892004022500089CE 2004 2 25 GLBA20030533 120040115A2100 ANNUNCIATOR BEECH 1900 1900D 1154162CE ENVIR SYS ACTIVATED A GLBAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM03170GL UE170 RT ENVIRO FAIL ANNC ILLUM ON TAKEOFF, PERFORMED GROUND PERFORMANCE RUN. OPS CK GOOD. 2L72 4T RTA24CE 20040225000932004022500093 2004 2 25 BAQA092100 420040116A3416066305401 ALTIMETER AEROSPAS355 AS355F1 8680810EU ALLSN 250C 250C20 03013GL RADAR STICKING B BAQAO OTHER O OTHER NRNOT REPORTED 1 EA03652PM 5179 RADAR ALTIMETER UNIT INOPERATIVE, STICKING. FAILED OUT OF BOX. REPLACED WITH SERVICABLE UNIT. 01/20/2004 1G72 3U3 U H11EU E4CE 20040225000982004022500098EU 2004 2 25 CX7A194J0405 120040125A3260 BULB SAAB SF340 340B 7860101EU MLG INDICATOR BURNED OUT A CX7AO OTHER P NO WARNING INDICATION APAPPROACH 1 GL03300CE 340B184 ON APPROACH WHEN GEAR IS SELECTED DOWN, LT GEAR LIGHT (MAIN) DID NOT ILLUMINATE, HOWEVER INTRANSIT LIGHT WAS OUT. GEAR CONFIRMED DOWN. 2L72 4T RTA52EU 20040225001002004022500100EU 2004 2 25 MALA040131 120040109A5347 SEAT TRACK SAAB SF340 340B 7860101EU FUSELAGE CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15436XJ 340B436 DURING 4K INSPECTION IN LCQ, RT IB SEAT TRACK HAS HEAVY CORROSION. MAINTENANCE REMOVED AND REPLACED CORRODED SEAT TRACK IAW MESABA EO NR S53060 DATED 3 NOV 2003. 2L72 4T RTA52EU 20040225001012004022500101EU 2004 2 25 MALA040129 120040109A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15436XJ 340B436 DURING 4K INSPECTION IN LCQ, EXTERIOR FUSELAGE HAS DENTS AT FS 350. MAINTENANCE FABRICATED AND INSTALLED 2 EACH EXTERNAL DOUBLER REPAIRS IAW MESABA EO NR S53009 DATED 21 SEPT 2001. 2L72 4T RTA52EU 20040225001052004022500105EU 2004 2 25 MALA040132 120040119A21507769106 ACM SAAB SF340 340B 7860101EU LEFT SEIZED A MALAO OTHER O OTHER NRNOT REPORTED 1 GL15365PX 340B265 POST FLIGHT OF NR 3084, LT ACM BURNING ODOR. SECONDARY INDICATION OF INMINENT LT ACM FAILURE, BURNING ODOR GRINGING NOSIES LT SIDE MIDSECTION. MAINTENANCE FOUND BURNING ODOR FROM RT ACM, FOUND RT ACM SEIZED. REPLACED RT ACM PN 776910-6 SEE 409 NR 071530 FOR DETAILS. OPS CHECKS OF BOTH ACMS GOOD. RT AUTO TEMP CONTROL INOPERATIVE REPLACED AIR CONDITIONING PANEL PN 7739019-505 OPS CHECK GOOD. 2L72 4T RTA52EU 20040225001082004022500108EA 2004 2 25 AKG2004F00000 220040116A732132447452 FUEL CONTROL BEECH 90 C90A 1152911CE PWA PT6 PT6A21 52043EA LT ENGINE MALFUNCTIONED B AKGRA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 CE05475JA 2193 LJ1147 PCE25421 AFTER TAKEOFF AND SHORTLY INTO FLIGHT THE LT ENGINE ROLLED BACK TO IDLE WITH THE POWER LEVER NOT BEING MOVED. MAKING A GROUND RUNUP, FOUND THAT THE FCU WAS VERY UNSTABLE AND NOT RESPONSIVE TO POWER LEVER CONTROL INPUTS. 1L72 3T4 TRT3A20 E4EA 20040225001142004022500114WP 2004 2 25 MEX2004017 120040114A27601474253 SELECTOR VALVE DOUG DC9 DC983 3022083WP PWA JT8 JT8D* NE SPOILER LEAKING W ASMZO OTHER K FLUID LOSS NRNOT REPORTED 1 SW23838AM1242612426 49397 DURING TRANSIT CHECK IT WAS DETECTED A HYDRAULIC LEAKAGE IN THE RT MAIN LANDING GEAR COMPARTMENT. THE SPOILER SELECTOR VALVE WAS FOUND DAMAGED. IT WAS REPLACED AND THE SYSTEM WAS TESTED IAW MM. AT OVERNIGHT SERVICE, THE SYSTEM WAS TESTED IAW MM, ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20040225001152004022500115NM 2004 2 25 MEX2004018 120040115A2913 PUMP DOUG MD88 MD88 3023688NM PWA JT8 JT8D* NE HYD SYSTEM FAILED W ASMZO OTHER O OTHER NRNOT REPORTED 1 SW23158PL8120 3019 49761 DURING TRANSIT SERVICE THE ELECTRICAL HYDRAULIC PUMP DOES NOT WORK. THE PUMP WAS CHECKED AND A PUMP BREAKER WAS DAMAGED. THE PUMP WAS REPLACED AND TEST WAS CORRECT. 2L72 4F4 FRTA6WE E2EA 20040225001162004022500116NM 2004 2 25 MEX2004019 120040115A7830 THRUST REVERSER BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE LEFT FAILED W ASMZO OTHER J WARNING INDICATION NRNOT REPORTED 1 SW23805AM 26272 DURING TRANSIT REVISION, THE LT REVERSER WAS OPEN AND LIGHT AND MESSAGE WAS IN DISPLAY. THE REVERSER WAS REVISED AND ICE AND SNOW WAS DETECTED INTO THE REVERSE. THE REVERSER WAS NOT CLOSED COMPLETELY BECAUSE A GAP OF 2 INCHES IS BETWEEN COVERS. THE CABLE BETWEEN ACTUATORS WAS REMOVED AND REVERSER WAS RETRACTED. THE AIRCRAFT WAS DISPATCHED BY MEL. DURING OVERNIGHT SERVICE THE REVERSER ACTUATOR WAS TRIMMED IAW MM, TEST CORRECT. 2L72 4F4 FRTA2NM E17NE 20040225001172004022500117WP 2004 2 25 MEX2004020 120040116A30007914644501 DUCT DOUG DC9 DC987 3022087WP PWA JT8 JT8D* NE TAIL CONE BROKEN W ASMZA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW23214AM 49585 AIRCRAFT RETURNED DUE TO LIGHT OF TAIL CONE HIGH TEMPERATURE CAME ON, AFTER 3 MINUTES THAT THE ANTI-ICE PROTECTION WAS USED. AIRCRAFT WAS CARRIED TO THE HANGAR TO ATTEND REPORT. AT OVERNIGHT SERVICE, THE ANTI-ICE DUCT ASSY WAS REPLACED AND SYSTEM WAS TESTED IAW MM. HARD LANDING INSPECTION WAS PERFORMED IAW MM, DETECTING A FUEL LEAKAGE IN THE CENTRAL LOWER SECTION OF THE FUEL TANK FRONT SPAR. THE FUEL TANK WAS SEALED IAW SRM, ALL CORRECT. 2L72 4F4 FRTA6WE E2EA 20040225001182004022500118NE 2004 2 25 MEX2004021 220040117A7412103538754 IGNITER BOX DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE RT ENGINE FAILED W ASMZD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW23753RA519 49587 725439 AIRCRAFT RETURNED TO PLATFORM, THE RT ENGINE DID NOT START WHEN THE FUEL CONTROL WAS PUT ON, SHUTTING DOWN THE IGNITION AND THE START VALVE. THE IGNITION BOX WAS REPLACED AND SYSTEM TESTED IAW MM, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20040225001192004022500119NM 2004 2 25 MEX2004026 120040118A5754 SKIN BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE NR 5 DAMAGED W ASMZK NONE O OTHER ININSP/MAINT 1 SW23802AM AL0644 26270 DURING OVERNIGHT SERVICE, IT WAS DETECTED THAT THE SLAT NR 5 HAD DAMAGES AND MATERIAL LOST IN A 20 X 10 INCH AREA, AND THE WING LEADING EDGE HAD DAMAGES TOO. SLAT NR 5 WAS REPLACED AND THE WING LEADING EDGE WAS REPAIRED IAW MM, ALL CORRECT. 2L72 4F4 FRTA2NM E17NE 20040220000232004022000023WP 2004 2 20 UPS04841819 120040114A5320 INTERCOSTAL DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE: C1, AFT PIT STA 1540 RBL 30 INTERCOSTAL ON AFT BULKHEAD CRACKED AT NUT PLATE. FABRICATED REPAIR ANGLE IAW DC8 SRM 53-2-0. ALODINE AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED ANGLE IAW DC8 SRM 51-1-21. 2L74 4F RT4A25 20040220000352004022000035WP 2004 2 20 UPS04841831 120040110A5340 SUPPORT FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE: C1, AFT PIT STA 1140 L35L SUPPORT FITTING CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. LOCATED NEW FITTING AND DRILLED EXISTING FASTENER HOLES IAW DC8 SRM 51-3-2 AND 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D. 2L74 4F RT4A25 20040220000482004022000048NM 2004 2 20 UPS04M41837 120040120A5347 SEAT TRACK DOUG MD11 MD11 3023602NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, CABIN - CORROSION ON SEAT TRACK AT STA 805-919 X=8.5. CORROSION REMOVED ON SEAT TRACK PER SRM 51-21-01 VOL II REV 34, MAT REMOVED 0.036 INCH, ORIGINAL THICK 0.112 INCH FOUND EXCEED LIMIT PER SRM 53-70-00 FIG 3 VOL I REV 34. NEW SEAT TRACK AND SPLICE INSTALLED AT STA 800-929 X =8.5 AS PER SRM 53-70-00 FIG 1 VOL I REV 34. 2L73 4F RTA22WE 20040220000512004022000051NM 2004 2 20 UPS04M41840 120040119A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, CABIN - CORROSION ON SEAT TRACK AT STA 775-899 X=-75.0. CORROSION REMOVED ON SEAT TRACK AT STA 775-815 MAT REMOVED 0.007 INCH, ORIGINAL THK 0.112 INCH FOUND WITHIN LIMIT PER SRM 53-70-00 VOL I REV 34. NEW SEAT TRACK AND SPLICE INSTALLED AT STA 815-909 X=-75.0 AS PER SRM 53-70-00 FIG 1 VOL I REV 34. 2L73 4F RTA22WE 20040220000542004022000054EU 2004 2 20 AWXA200400158 120040207A2120 ODOR AIRBUS320 A320231 3930325EU GALLEY DETECTED A AWXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP28625AW 064 MSP - DIVERSION - FLT 0232 - APPROXIMATELY 45 MINUTES AFTER TAKEOFF FROM DTW, EN ROUTE FOR LAS, THE FLIGHT ATTENDANTS REPORTED A STRONG ODOR OF GAS OR SULFUR IN THE AFT GALLEY, DIVERTED TO MSP. WHEN MAINTENANCE ARRIVED, FOUND NO ODOR IN AFT GALLEY. THE MSP FIRE DEPARTMENT GAS ANALYZER WAS USED TO DETECT ANY EVIDENCE OF GAS, ANALYZER READ -0-. AFT GALLEY OVENS AND COFFEEMAKERS WERE OPERATED, NO SULFUR ODOR WAS NOTED, RAN BOTH ENGINES AND OPERATED AIR CONDITIONING PACKS, NO ODOR WAS NOTED. 2L72 4F RTA28NM 20040220000612004022000061NM 2004 2 20 AALA20040195 120040206A3397 CONNECTOR BOEING757 757223 1384957NM EMERGENCY LIGHT DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21690AA 25696 DFW SEAT MOUNTED EMERGENCY PATH LIGHT AT SEAT 31D INOPERATIVE. RESECURED CONNECTOR FOR SEAT MOUNTED EMERGENCY PATH LIGHT AT SEAT 31D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20040220000622004022000062NM 2004 2 20 AALA20040201 120040206A3350 LIGHT BOEING767 767323 1385205NM 4L DOOR INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21354AA 24035 MIA EMERGENCY EXIT INDICATOR LENS AT LOWER AFT DOOR 4L IS DAMAGED. REPLACED EMERGENCY EXIT INDICATOR AT LOWER AFT 4L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040220000652004022000065WP 2004 2 20 AALA20040194 120040207A3350 BATTERY DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21269AA 49292 STL CEILING EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY FOR FIRST CLASS CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040220000692004022000069WP 2004 2 20 AALA20040192 120040208A33506011770 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21584AA 53247 ORD LEFT HAND AND RIGHT HAND OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACKS FOR LEFT AND RIGHT HAND OVERWING EMERGENCY EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20040220000822004022000082EA 2004 2 20 SWIA200412854 120040201A2752852D10019 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED DEDESCENT 1 NM07918SW 7645 FLAPS FAIL CAUTION MESSAGE ON WHEN FLAPS SELECTED AT APPROXIMATELY 13,000 FT. REMOVED AND REPLACED RIGHT NR 1 AND LEFT NR 1 ACTUATOR (FLAP), IAW 27-53-01, 27-53-05, AND RII 27-412. OPS CHECKS GOOD. S/N OFF RIGHT: 3392. 2L72 4F RTA21EA 20040220000922004022000092SO 2004 2 20 LR7A04008 120040124A5230 SKIN LKHEED382 382G 526414USO CARGO DOOR DENTED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND RAMP DOOR BOTTOM SKIN DENT & PITTING CORROSION AT FS 820 BL 18R. REPAIR CARRIED OUT IAW SMP583 FIG 51-140-12, FS 820 RBL 18. 2H74 4T A1SO 20040220001162004022000116NM 2004 2 20 04FDEA00355 120040208A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 LEFT I/B FLAP O/B HINGE I/B STRAP PIVOT HOLE CORRODED. LT I/B FLAP O/B HINGE I/B STRAP PIVOT HOLE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74312. LT I/B TE FLAP HINGE BRACKET CORRODED. 2L73 4F RTA22WE 20040220001192004022000119NM 2004 2 20 04FDEA00352 120040208A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 RIGHT O/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT HOLE AND LUG CORRODED. RT O/B FLAP O/B HINGE (FLAP SIDE) I/B PIVOT HOLE & LUG SURFACE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74311. RT O/B FLAP O/B AFT HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040220001212004022000121NM 2004 2 20 04FDEA00350 120040208A5753 HINGE DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 RIGHT O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT HOLE AND LUG CORRODED. RT O/B FLAP I/B HINGE (FLAP SIDE) I/B PIVOT HOLE & LUG SURFACE CORROSION REMOVED & REPAIRED AS PER FEDEX EA 1-5750-74310. WINGS - RT O/B FLAP I/B AFT HINGE BRACKET BORE CORRODED. 2L73 4F RTA22WE 20040220001342004022000134NE 2004 2 20 2004UALA00086 220040130A7320 WARNING LIGHT AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE FUEL CONTROL ILLUMINATED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29827UA 1022 RETURN TO FIELD DUE TO ECAM NR 2 FUEL CONTROL FAULT. DEBRIS FLOWING THROUGH FMU CAUSED TORQUEMOTOR FAULT. THE DEBRIS WAS SUBSEQUENTLY FLUSHED OUT. THIS IS AN ISOLATED INCIDENT AND ENGINEEING WILL CONTINUE TO MONITOR THE FMU. 2L72 4F4 FRTA28NM E40NE 20040220001352004022000135NM 2004 2 20 2004UALA00087 120040130A2910 VALVE AIRBUSA319 A319131 3930317NM IAE V2527 V2527A5 NE HYDRAULIC SYSTEMFAILED A UALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29822UA 948 FLIGHT EXPERIENCED A GREEN HYDRAULIC SYSTEM FAILURE. REPLACED THE HYDRAULIC SAFETY VALVE. 2L72 4F4 FRTA28NM E40NE 20040225001242004022500124EA 2004 2 25 X6PA200400002 220040127A7414SS1001 BOOSTER PIPER PA32 PA32260 7103206SO LYC O540 IO540* 41532EA MAGNETO INOPERATIVE E X6PAO OTHER R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 SO334817 15 321277 L2001540A DURING RUNUP THE PILOT FOUND LT MAGNETO WAS INOPERATIVE. A MECHANIC INSPECTED THE AIRCRAFT AND FOUND THE SLICK START MAGNETO START BOOST BOX STC NR SA593CH MALFUNCTIONED AND GROUNDED THE LEFT MAGNETO OUT. THE MECHANIC REPLACED THE SLICK START BOX; THIS FIXED THE PROBLEM. 1L71 3O3 O A3SO 1E4 20040225001272004022500127NM 2004 2 25 DHL2004750003 120040128A33501000677 LIGHT BOEING727 7272M7 138407SNM EMERGENCY EXIT INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01750DH 21951 ON P/F MAIN EXIT DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT IAW 33-50-101. OPS CHECKED GOOD. (P/N ON: 10-0067-7, S/N ON: 23781) 2L73 4F A3WE 20040225001322004022500132NM 2004 2 25 UPS04441903 120040202A5330 SKIN BOEING747 747123 1384873NM FUSELAGE MISREPAIRED A IPXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, DURING WORK ACCOMPLISH FOR RAP, ITEM N672-46-28 AT BS 1960-1975 STR 45R-47R EXISTING PATCH FOUND NOT MATCH WITH SRM 53-30-03 FIG 19 AS PROVIDED BY CUSTOMER RE-DO THE REPAIR REQUIRE. EXPANDED DOUBLER REPAIRED AS PER SRM 53-30-03 FIG 48 AT FX STA 1960 TO STA 1980 BETWEEN STR 45R AND STR 47R AREA SUBSEQUENT INSPECTION REQUIRE AS PER SRM 53-30-03 FIG 48 SHT 9 TABLE II & SHT 13 TABLE III. THIS REINSPECTION WILL BE CONTROLLED BY EO B747-5330-13494-H. 2L74 4F A20WE 20040225001332004022500133NM 2004 2 25 UPS04441904 120040122A53302024T30071IN SKIN BOEING747 747123 1384873NM EMPENNAGE CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C EMP- LT AFT FUSELAGE UPPER EXTERNAL SKIN SURFACE FOUND CHAFING MARK AT STA 2280 TO STA 2360 STR 2L TO STR 3L VERTICAL STABILIZER SEAL INTERFACE AREA (AS MARK). BS 2280-2360 STR 2L-4L AREA SKIN SMOOTHED OUT & REPROTECTED AS PER SRM 51-10-01 & 51-10-02 WITHIN EO 5330-18431 APP-A ITEM 8 LIMITS. HFEC INSPECTED, NO CRACK FOUND EXCEPT BS 2290-2310 STR 2L-3L & BS 2330-2360 STR 2L-4L. SKIN REPAIRED AS PER SRM 53-30-03 FIG 1 (UPS MPI ASSIGNED FOR REPEAT INSPECTION). 2L74 4F A20WE 20040225001342004022500134NM 2004 2 25 UPS04441905 120040127A5330 SKIN BOEING747 747123 1384873NM FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C DURING REPAIR ASSESSMENT PROGRAM ACCOMPLISH, ITEM N672-41-08 AT BS 447-463 STR 42R-44R 2 LAYERS REPAIR DOUBLER FOUND SINCE THE OUTER DOUBLER IS ONLY 0.040 INCH THK WHICH WILL CREATE KNIFE-EDGE CONDITION, RE-DO THE REPAIR REQUIRE. EXISTING DOUBLER REMOVED & DISCARDED AS PER SRM 53-30-03 FIG 1. HFEC INSPECTED AT THE REPAIR AREA FASTENER HOLES, NO CRACK REVEALED. NEW EXTENDED DOUBLER REPAIRED AS PER SRM 53-30-03 FIG 1. SUBSEQUENCE INSPECTION REQUIRE AS PER SRM 53-30-03 FIG 1 TABLE IV (REPEAT INSPECTION PER EO B747-5330-13494H). 2L74 4F A20WE 20040225001412004022500141NM 2004 2 25 UPS04441912 120040127A5310 SHEAR TIE BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, AFT OF BULK CARGO COMPT- RT STA 2220 IN BETWEEN STR 40 AND STR 44 SHEAR TIE ATTACH ANGLE FOUND CORROSION CRACKED. CORROSION BLEND OUT 0.071 X 1 X 3 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. ANGLE REPAIRED PER SRM 51-40-03 FIG 2. CIC APPLIED IAW EO M-5100-2780-1. 2L74 4F A20WE 20040225001422004022500142NM 2004 2 25 UPS04441913 120040121A5313 STRINGER BOEING747 747123 1384873NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C FWD CARGO COMPT- RT STA 790- STA 810 STRINGER 46 FOUND CORROSION CRACKED. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.050 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. STRINGER REPAIRED PER HX RS R53-21-35100 & UPS ENGINEERING FILE 747-53-20168. CIC APPLIED IAW EO M-5100-2780-E. 2L74 4F A20WE 20040225001432004022500143NM 2004 2 25 UPS04441914 120040124A532065B065691 FLOOR SUPPORT BOEING747 747123 1384873NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C M/D- BS 2240 TP 2270 LBL 80 FLOOR SUPPORT FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.030 X 1 X 1 EXCEED SRM 53-10-01 FIG 1 LIMITS. FLOOR SUPPORT REPLACED PER SRM 51-10-01 PG 8. CIC APPLIED IAW CPM53-10-17. 2L74 4F A20WE 20040225001452004022500145NM 2004 2 25 UPS04541896 120040206A5320 WEB BOEING757 75724APF 1384969NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01405UP 23727 INSPECTION TYPE:C-CHECK, CORROSION ON FLOOR SHEAR WEB IN SEVERAL AREAS BETWEEN BS 365 TO 395 LBL 46 TO LBL 62 WL 208. BS 368 LBL 46 OUT OF LIMITS. FABRICATED DOUBLER AND FILLER AND INSTALLED REPAIR PARTS ALL WORK DONE IAW SRM 53-00-51 FIG 101, 51-70-13, 51-40-08, 51-40-02 AND SOPM 20-41-02. 2L72 4F RTA2NM 20040225001462004022500146NM 2004 2 25 04FDEA00412 120040216A5330 SKIN BOEING727 727200 138407ENM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25288FE 21850 FUSELAGE EXTERNAL SKIN HAS GOUGES AT BS 1149 BETWEEN STRINGER 6 & 7 LT. SKIN AT BS 1149 BETWEEN STR 6 & 7 LT WAS FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE & REPAIRED SKIN PER FED EX EA 7-5330-55232. 2L73 4F RTA3WE 20040225001512004022500151NM 2004 2 25 2004UALA00118 120040210A2150 JACKSCREW BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE LT PACK FAILED A UALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP29643UA 25093 FLIGHT DIVERTED DUE TO LEFT PACK TEMPERATURE CONTROL MESSAGE AND LIGHT. THE LEFT PACK INLET ACTUATOR WAS FOUND MECHANICALLY FROZEN. THE JACK SCREW ASSEMBLY FAILED. THE ACTUATOR WAS REPLACED AND NO FURTHER PROBLEMS WERE REPORTED. 2L72 4F4 FRTA1NM E24NE 20040223001582004022300158SO 2004 2 23 ENHA2004P3101 120040108A5280 HINGE PIPER PA31 PA31350 7103110SO RT MLG DOOR BROKEN E ENHAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL034105D 318252027 AT TAKEOFF INITIAL CLIMB GEAR UP SELECTED (IN TRANSIT) LIGHT WOULD NOT EXTINGUISH. SELECT GEAR DOWN ALL GEAR GREEN. LANDED WITH OUT INCIDENT. FOUND RT MLG IB DOOR FWD HINGE BROKEN. LANDING GEAR LAST INSPECTED IAW AD 2000-25-01 AT 10754.9. REPLACED FWD HINGE WITH NEW P/N 47529-32. C/W SB 682. REINSPECTED AFT HINGE IAW AD 00-25-01 NO DEFECTS. 1L72 3O A20SO 20040223001932004022300193WP 2004 2 23 AALA20040065 120040113A80109794104 START VALVE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE LT ENGINE FAILED A AALAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW219628W 53598 728182 DURING CLIMBOUT LT ENGINE FIRE WARNING CAME ON 5-10 SECONDS THEN WENT OUT. STAYED OUT 5-10 SECONDS THEN BACK ON FOR 2-3 SECONDS AND STAYED OFF FOR REMAINDER OF FLIGHT. ENGINE WAS SHUT DOWN USING FIRE HANDLE. ENGINE WINDMILLED 3 OR 4 MINUTES WITH NORMAL OIL PRESSURE. NO OTHER WARNING LIGHTS OR INDICATIONS. RETURNED AND LANDED WITHOUT INCIDENT. FOUND LT ENGINE STARTER DISINTEGRATED AND FOUND 2 BY 3 INCH HOLE IN OUTSIDE SURFACE OF FAN BYPASS DUCT WITH ONE INCH HOLE PENETRATING THROUGH INTO FAN DUCT. REPLACED STARTER AND START VALVE. MADE INTERIM REPAIR TO ENGINE CASE. AIRCRAFT WILL BE FERRIED OR ENGINE CHANGE. SYSTEM GROUND CHECKED NORMAL OPERATION. --CLOSED-- 2L72 4F4 FRTA6WE E9NE 20040223001982004022300198EU 2004 2 23 RAIA00401004 120040104A3350 LAMP AEROSPATR72 ATR72202 8680940EU EMERGENCY LIGHT BLOWN A RAIAK NONE O OTHER ININSP/MAINT 1 CE03723TE 283 ENTRY DOOR STEP EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LIGHT BULB. 2H72 4T RTA53EU 20040224000052004022400005NM 2004 2 24 COOSDR030054 120040101A575165464542 SKIN BOEING737 737200 1384453NM RT WING AILERON DELAMINATED W EE4YO OTHER O OTHER NRNOT REPORTED 1 SO23767TW 20258 RT WING, AILERON (PN-65-46454-2) SN 305, SKIN DELAMINATED. 2L72 4F A16WE 20040220001412004022000141EA 2004 2 20 04016633 120040116A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27633BR 7274 DURING INSPECTION THE RIGHT HAND FUSELAGE EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040220001482004022000148EA 2004 2 20 04024620 120040124A7830 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA THRUST REVERSER OUT OF RIG A VTZAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27620BR 7179 DURING CRUISE OF FLIGHT 9950 THE CREW REPORTED THE THRUST REVERSER UNLOCKED DURING FLIGHT. THE THRUST REVERSER WAS RIGGED AND ADJUSTED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040220001492004022000149EA 2004 2 20 04025676 120040125A3350 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27676BR 7644 DURING INSPECTION THE LEFT HAND MID WING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040220001602004022000160NM 2004 2 20 04FDEA00380 120040209A5753 FAIRING DOUG MD11 MD11 3023602NM ZONE 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25623FE 48794 LEFT WING O/B FLAP I/B HINGE FAIRING FOUND O/B BRACKET CRACKED. LT WING O/B FLAP I/B HINGE FAIRING FWD OUTER CRACKED BRACKET REMOVED, FABRICATED, AS PER DRWG ARC7717 & COMPLIED AS PER EA 1-5750-74228. TE FLAP O/B TE FLAP AFT HINGE BRACKET AERODYNAMIC FAIRINGS FWD SUPPORT BRACKET. FABRICATION, AND INSTALLED AS PER SRM 51-31-01 VOL 2. 2L73 4F RTA22WE 20040220001662004022000166EU 2004 2 20 04FDEA00389 120040210A2170 COALESCER BAG AIRBUS310 A310 EU CABIN AIR DIRTY A FDEAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO25412FE 360 ON TAKEOFF ROLL STRONG ODOR OF OIL OR AIR CONDITIONING SMOKE IN COCKPIT, REJECTED TAKEOFF. NO SIGN OF SMOKE COMING FROM VENTS, NO SMOKE WARNINGS, ALL INDICATIONS APPEAR NORMAL, RETURNED TO RAMP. FOUND NR 1 AND NR 2 PACK WATER SEPARATOR BAGS VERY DIRTY. REMOVED AND REPLACED WATER SEPARATOR BAGS IAW MM 21-51-16-4, OPS CHECK NORMAL. NO SIGN OF SMOKE OR OTHER SIGN OF ABNORMAL ODORS, OK FOR SERVICE. 2L72 4F RTA35EU 20040220001672004022000167EA 2004 2 20 COMA0460127 120040207A2750860D10018ABCD FCU CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01981CA 7163 FLIGHT 5131 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU. 2L72 4F RTA21EA 20040220001762004022000176NM 2004 2 20 04031420 120040131A33508GH00247308 BULB DORNERDO32 DO328300 NM EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27420FJ 3178 DURING INSPECTION AN OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20040220001832004022000183NM 2004 2 20 CALA0400098 120040209A5320 WEB BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714347 23585 INSPECTION FOUND SHEAR WEB IN RT AFT LAV AREA CORRODED AT FS 1019, RBL 28. THE SHEAR WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040220001852004022000185NM 2004 2 20 0400186740 120040102A5312 BULKHEAD BOEING747 747251F 1384898NM FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01640US 23888 DURING H-CHECK FOUND CORROSION ON LOWER BULKHEAD CHORD AT BS 1000 S 41L. REPAIRED PER EA 67-165093. 2L74 4F A20WE 20040220001952004022000195WP 2004 2 20 AALA20040206 120040209A3350 BATTERY PACK DOUG DC9 DC983 3022083WP EMERGENCY LIGHT INOPERATIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW21975TW 53625 SEA OVERHEAD EMERGENCY EXIT LIGHT AT LIFE RAFT STORAGE COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK B5-101 FOR EMERGENCY EXIT LIGHT AT LIFE RAFT STORAGE COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20040220001992004022000199NM 2004 2 20 QXEA200400124 120040204A5330 SKIN DHAV DHC8 DHC8202 2809007NM ZONE 200 DENTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09356PH 502 PDX - DENT IN FUSELAGE SKIN - LEFT HAND SIDE UNDER ICE SHIELD 10.5 INCHES ABOVE NR 2 WINDOW. REPAIRED IAW HORIZON AIR EA 2-53-541 AND RD 8-53-7768. 2H72 4T RTA13NM 20040219000132004021900013NM 2004 2 19 UPS04441859 120040123A5313BAC14981427075 STRINGER BOEING747 747123 1384873NM FWD CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE: C, FWD CARGO COMPT- LT STA 720 - STA 740 STRINGER 47 FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.030 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. CIC APPLIED IAW EO M-5100-2780-E. 2L74 4F A20WE 20040219000342004021900034NM 2004 2 19 SWAA040443 120040211A53126546568 BULKHEAD BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29675AA 23253 DURING SCHEDULED C1 CHECK, FOUND BULKHEAD WEB CRACKED AT BS 1016, BETWEEN STRINGER 3R AND STRINGER 5R. REPAIRED WEB PER EA. 2L72 4F RTA16WE 20040219000662004021900066NM 2004 2 19 2004UALA00091 120040131A3397 TERMINAL BLOCK BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHT MISSING A UALAK NONE L NO TEST ININSP/MAINT 1 WP29197UA 26901 EMERGENCY LIGHT ON DOOR NR 2 LEFT, STAYS ON ALL THE TIME. FOUND GROUND MISSING AT TERMINAL BLOCK. SECURED GROUND TERMINAL. LIGHT ASSY OPS CHECKS OK FOR ALL FUNCTIONS. 2L74 4F4 FRTA20WE E24NE 20040219000802004021900080NM 2004 2 19 SWAA040355 120040204A57536549508 FLAP TRACK BOEING737 7373Q8 1384670NM LT WING WORN A SWAAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 SW29689SW 23387 AIRFRAME VIBRATION WHEN FLAPS SELECTED TO 5 DEGREES. REPAIRED LT WING T/E INBOARD MIDFLAP TRACK PER EA. 2L72 4F RTA16WE 20040219000892004021900089CE 2004 2 19 58604 120040205A5270 ANNUNCIATOR BEECH 1900 1900D 1154162CE PAX DOOR FALSE INDICATIONA AMWAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CE07182YV UE182 WHILE ON FLIGHT, PASSENGER DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. THE CAPTAIN FOLLOWED PROCEDURES TO LAND AT AN ALTERNATE FIELD TRI. CREW INSPECTED DOOR AND FOUND ANNUNCIATOR GAVE FALSE ILLUMINATION. THIS ITEM WAS DEFERRED. THEN PROCEEDED TO FINAL DESTINATION. STILL AWAITING MORE INFORMATION TO COME AT A LATER DATE. 2L72 4T RTA24CE 20040219001062004021900106NM 2004 2 19 SWAA040347 120040203A5315BAC1509 FLOORBEAM BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CRACKED AT BS 986, RBL 55 TO LBL 14, WL 208. REPAIRED FLOORBEAM PER ER. 2L72 4F RTA16WE 20040219001212004021900121 2004 2 19 SWAA040220 420040122A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29626SW 27702 R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20040219001422004021900142NM 2004 2 19 SWAA040239 120040123A2560PH22300L STRIP BOEING737 7373L9 1384470NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29658SW 23332 DURING SCHEDULED SPV, FOUND EEPLS PHOTO LUMINESCENT STRIP CRACKED AT RT, BS 833.45 TO BS 847.45. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20040219001572004021900157NM 2004 2 19 SWAA040254 120040126A335007912 LIGHT BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29346SW 24153 EEPLS FLOOR TRACK LOOSE AT ROW 8. REMOVED AND REPLACED EEPLS FLOOR STRIP PER MM. 2L72 4F RTA16WE 20040219001582004021900158NM 2004 2 19 SWAA040255 120040126A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29309SW 22948 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STRINGER 5L. REMOVED AND REPLACED CRACKED CLIP PER SRM. 2L72 4F RTA16WE 20040219001672004021900167SO 2004 2 19 SWIA200412844 120040107A5720 BRACKET EMB 120 EMB120ER 3260203SO LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07232SW 120306 LEFT INBOARD WING, BRACKET CRACKED AT RIB STATION 8 AFT LOWER OUTBOARD ACCESS PANEL, MARKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED BRACKET AT RIB STATION NR 8 AFT OF OUTBOARD FUEL ACCESS PANEL PER SRM 51-40-02. NO LEAKS AT THIS TIME. 2L72 4T RTA31SO 20040219001752004021900175EU 2004 2 19 AWXA200400156 120040205A33501013081 LIGHT AIRBUS320 A320232 3930326EU SEAT ROW 11 RT DEFECTIVE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28605AW 543 EWR - EEL - DURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH SIDEWALL LIGHT AT SEAT ROW 11 RT INOPERATIVE, BULB REPLACEMENT DID NOT HELP. MAINTENANCE REPLACED THE EMERGENCY ESCAPE PATH SIDEWALL LIGHT ASSEMBLY AT SEAT ROW 11 RT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20040219001862004021900186NM 2004 2 19 CALA0400080 120040128A5230 SKIN BOEING737 7373T0 1384582NM CARGO DOOR DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW2734315 23366 IN PREPARATION FOR INSTALLING A PERMANENT REPAIR, A TEMPORARY REPAIR DOUBLER ON THE INNER SKIN OF THE AFT CARGO DOOR ABOVE THE DOOR HANDLE CUTOUT WAS REMOVED AND A SMALL AREA OF DAMAGE TO THE INNER SKIN WAS DISCOVERED. A REPAIR DOUBLER WAS INSTALLED AS A PERMANENT REPAIR IAW ECRA 5232-01044. 2L72 4F RTA16WE 20040219002052004021900205WP 2004 2 19 04FDEA00333 120040206A3000 PRESSURE SWITCH DOUG DC10 DC1010 3022110WP ANTI ICE SYSTEM MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25388FE 46622 DURING CLIMBOUT WITH WING & ENGINE ANTI ICE ON GOT A NR 1 MANFOLD FAIL ALERT. COMPLIED WITH QRH AND RTB. TROUBLESHOT PER FIM CH 36-23 FOUND MANIFOLD FAULT INDICATOR SET (LEFT WING PRESSURE SW SHOWN) SWITCH WOULD NOT RESET. REMOVED AND REPLACED PRESS SWITCH IAW MM CH 36-23-03-4. OPS CHECK NORMAL. 2L73 4F A22WE 20040219002122004021900212NM 2004 2 19 AALA20040188 120040129A5753 SUPPORT FITTING BOEING777 777223 1385213NM FLAPERON GROOVED A AALAK NONE O OTHER ININSP/MAINT 1 SW21790AN 30251 AFW - RT WING FIXED TRAILING EDGE FLAPERON OUTBOARD SUPPORT FITTING HAS 0.7 X 2.0 AND 0.092 DEPTH GROOVE WORN ON UPPER SURFACE. BLENDED OUT DAMAGE AND PERFORMED HFEC FOR CRACKS. ROTO PEENED BLENDED AREA. ALODINE AND APPLIED TWO COATS OF PRIMER TO REWORKED AREA. 2L72 4F RTT00001SE 20040219002302004021900230SO 2004 2 19 C2XA04TY032 120040206A532014524131009 BRACKET EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713550 145575 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE PASSENGER DOOR SILL PLATE ATTACH BRACKET. MAINTENANCE REMOVED AND REPLACED THE ATTACH BRACKET IAW EMB SRM 51-40-02 AND CPM 51-21-05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20040219002332004021900233SO 2004 2 19 C2XA04TY035 120040207A531514522460013 FLOORBEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713550 145575 TYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM TOP CAP AT FRAME 15. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION. 2L72 4T RTT00011AT 20040219002352004021900235NM 2004 2 19 F3LA200400006 120040205A5313 STRINGER BOEING737 7373S1 138447SNM FUSELAGE CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03311FL 1937 24856 DURING C-7 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR STRINGER AND NUT PLATE CORRODED AT STA 727B, STR 2L. REPLACED FLOOR BEAM STRINGER PER SRM 53-00-53 FIG 201. 2L72 4F RTA16WE 20040219002382004021900238SO 2004 2 19 C2XA04BT017 120040206A3210 LANDING GEAR EMB 145 EMB145LR 3260212SO MAINS MALFUNCTIONED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2729906 145472 CREW REPORTED, AIR RETURNED, GEAR WOULD NOT RETRACT. MAINTENANCE OPERATIONALLY CHECKED LANDING GEAR EXTENSION AND RETRACTION, FOUND NORMAL OPERATION IAW EMB145 AMM 32-30-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20040219002422004021900242SO 2004 2 19 C2XA04CL010 120040202A33501317 LAMP EMB 145 EMB145LR 3260212SO EMERGENCY LIGHT INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714907 145468 IAH FLIGHT 2636, THE CREW REPORTED THE EMERGENCY LIGHT OVER 12A WAS INOPERATIVE. MAINTENANCE RELAMPED THE EMERGENCY LIGHT OVER 12A. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20040219002542004021900254NM 2004 2 19 CALA0400091 120040208A5320 STRAP BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW2714335 23573 INSPECTION FOUND STRAP UNDER BEAM AT C-2 DOOR CUTOUT I/B SILL STRUCTURE CORRODED AT STA 800. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-40-02. 2L72 4F RTA16WE 20040220000062004022000006EU 2004 2 20 MALA040175 120040123A5330 SKIN SAAB SF340 SF340A 7850100EU FUSELAGE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL1527XJ 340A027 LEFT UPPER FUSELAGE HAS NUMEROUS DENTS AT FS 339-345 STRINGER 1505-1206. MAINTENANCE FABRICATED DOUBLER FOR FUSELAGE SKIN AT FS 339-345, STRINGER 1505-1506, TREATED AND PRIMED, INSTALLED DOUBLER, TOP COATED IAW SAAB 340 SRM 53-70-10-2. A/C RELEASE DATE 2/5/04. 2L72 4T RTA52EU 20040220000182004022000018EA 2004 2 20 COMA0460124 120040203A55516002100617 BUSHING CNDAIRCL600 CL6002B19 1900309EA VERTICAL STAB LOOSE A COMAK NONE O OTHER ININSP/MAINT 1 SO01977CA 7157 BUSHING IN VERTICAL STABILIZER LEFT HAND LUG FOR HORIZONTAL STAB PIVOT POINT MIGRATED .029 INCHES. THE BUSHING IN THE RIGHT VERTICAL STABILIZER IS IMPROPERLY REAMED CAUSING MISALIGNMENT AND BINDING. REMOVED THE LT AND RT VERTICAL STABILIZER LUG BUSHINGS. MACHINED AND CADMIUM PLATED OVERSIZED BUSHINGS IAW WVAC EO 601R-55-4669. INSTALLED BUSHINGS IAW CRJ AMM 20-26-00-910-803. LINE REAMED BUSHING IAW DRAWING 600-21029. 2L72 4F RTA21EA 20040220000222004022000022NM 2004 2 20 UPS04441842 120040123A5310 FORGING BOEING747 747123 1384873NM WINDOW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 INSPECTION TYPE:C M/D- BS 1560-1580 LT WINDOW FORGING AFT EDGE ATT SKIN FOUND CORROSION REVEALED. BS 1560-1580, STR L19-L22 CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.030 INCH X 1 INCH X 1 INCH EXCEED SRM 53-30-01 FIG 1 LIMIT. WINDOW FORGING REPAIRED PER RS R-53-61-35104 & UPS ENGINEERING FILE 747-53-20164, CIC APPLIED IAW CPM 53-10-47. 2L74 4F A20WE 20040220000252004022000025WP 2004 2 20 UPS04841821 120040104A534336410042 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE: C1, RIGHT MLG WW L24R AT STA 879 VERT BATHTUB FITTING HAS CORROSION ON FWD SIDE. REMOVED CORROSION & FOUND TO BE BEYOND ALLOWABLE LIMITS IAW DC8 SRM 53 -2-0 FIG 1F. REMOVED FITTING, FABRICATED REPAIR SPLICES AND INSTALLED NEW FITTING AND SPLICES IAW DC8 SRM 53-2-0 FIG 8. 2L74 4F RT4A25 20040220000452004022000045WP 2004 2 20 UPS04841848 120040203A5712 RIB DOUG DC8 DC871F 302199DWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 INSPECTION TYPE: C3, RIGHT WING CENTER L/E LOWER RIB HAS A HOLE WORN THRU AT XFS 416. REMOVED DAMAGE, NDT VERIFIED NO CRACKS AT DAMAGE REMOVAL. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2. 2L74 4F RT4A25 20040220000502004022000050NM 2004 2 20 UPS04M41839 120040120A5347 SEAT TRACK DOUG MD11 MD11F 3023600NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01274UP INSPECTION TYPE: C, CABIN - CORROSION ON SEAT TRACK AT STA 805-899 X=-27.5. CORROSION REMOVED ON SEAT TRACK PER SRM 51-21-01 VOL II REV 34, MAT REMOVED 0.030 INCH, ORIGINAL THK 0.112 INCH EXCEED LIMIT OF SRM 53-70-00 FIG 3 VOL I REV 34. NEW SEAT TRACK AND SPLICE INSTALLED AT STA 800-909 X=-27.5 AS PER SRM 53-70-00 FIG 1 VOL I REV 34. 2L73 4F RTA22WE 20040220000712004022000071NM 2004 2 20 AALA20040200 120040206A3350 LIGHT BOEING767 767323 1385205NM SEAT 2G BROKEN A AALAK NONE O OTHER ININSP/MAINT 1 SW21354AA 24035 MIA EMERGENCY LIGHT DIRECTIONAL ARROW IN FRONT OF SEAT 2G IS BROKEN. REPLACED DIRECTION ARROW EMERGENCY LIGHT IN FRONT OF SEAT 2G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20040220000932004022000093SO 2004 2 20 LR7A04009 120040124A5230339119 FAIRING LKHEED382 382G 526414USO CARGO DOOR DENTED A LR7AK NONE O OTHER ININSP/MAINT 1 AL03402LC 2434 4698 DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND RAMP DOOR BOTTOM PEDESTAL FWD FAIRING AND LT & RT FAIRINGS WARPED. FAIRINGS REPLACED IAW SMP583 CHP51-60 & 51-70, FS 845 BL 18R. 2H74 4T A1SO 20040220001442004022000144EA 2004 2 20 04019626 120040119A2611PU90421R3 SMOKE DETECTOR CNDAIRCL600 CL6002B19 1900309EA LAVATORY FAULTY A VTZAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA27626BR 7225 DURING FLIGHT THE CREW REPORTED A LAVATORY SMOKE INDICATION. FLIGHT LANDED WITHOUT INCIDENT. UPON MAINTENANCE THE SMOKE DETECTOR WAS FOUND TO GIVE FALSE INDICATIONS. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20040220001502004022000150EA 2004 2 20 04027308 120040127A33506040751 POWER SUPPLY CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DISCHARGED A VTZAK NONE O OTHER ININSP/MAINT 1 EA27308UE 41023 DURING INSPECTION THE EMERGENCY TRACK LIGHTING FROM ROW