20090422 NM 2009 4 22 SWAA092531 120090420A5315BAC1509 FLOORBEAM BOEING737 7373K2 13844BANM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 665, LBL 25, WL 208. REPAIRED BEAM PER SRM. 2L72 4F RTA16WE 20090427 SO 2009 4 27 GLBA200904221 120090422A5270 SWITCH EMB 120 EMB120ER 3260203SO FUEL DOOR OUT OF ADJUST A GLBAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM21108UX 120108 SERVICE DOOR LIGHT ILLUMINATED IN FLIGHT AND THEN EXTINGUISHED. MAINTENANCE EXAMINED THE SERVICE DOOR AND FOUND A FUEL SERVICE DOOR SCREW LOOSE. MAINTENANCE SECURED THE SCREW AND SUBSEQUENT MAINTENANCE ADJUST THE OURBOARD FUEL ACCESS DOOR SWITCH IAW MM 52-73-03. MAINTENANCE ALSO INSPECTED AND CLEANED ALL OTHER SERVICE DOOR SWITCHES AND ALL OPERATIONALLY CHECKED GOOD. 2L72 4T RTA31SO 20090605 NM 2009 6 5 USAA2009060391384120090506A532065C334192 SHEAR WEB BOEING737 7373S3 138449HNM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19313AW 23712 SAL - C21 - MAJOR REPAIR - GALVANIC CORROSION ON SHEAR WEB BETWEEN BS 1016 TO BS 1030. REPLACED SHEAR WEB BETWEEN BS 1016 TO BS 1030 IAW B737 SRM 51-40-02. 2L72 4F RTA16WE 20090609 NE 2009 6 9 UALA2009060101549220090531A7230 BLADE BOEING757 757222 1384956NM PWA 2037 PW2037 NE LT ENGINE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29577UA 26693 CREW REPORT: ON PREFLIGHT FOUND DIME SIZED DENT ON LEADING EDGE OF LEFT ENGINE NR 26 1ST STAGE BLADE. BLENDED SMALL DING ON NR 1 ENGINE, BLADE NR 26 LEADING EDGE, MARKED. 2L72 4F4 FRTA2NM E17NE 20090330 NM 2009 3 30 C8GA20090027 120090205A5312 BULKHEAD BOEING727 727230 1384080NM MLG WW CRACKED A C8GAK NONE O OTHER ININSP/MAINT 1 SO29357KP69532 20675 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE RIGHT WHEEL WELL BS 870 BULKHEAD WEB CRACKED AT LOCK FASTENER LOAD CONTROL VALVE CUTOUT RBL 10. REMOVED DAMAGE, FABRICATED FILLERS FROM 2024 T3 .063 INCH AT AFT UPPER DIM 1.425 INCH BY .580 INCH, LOWER 1.83 INCH BY 2.9, FWD UPPER 2.1 INCH BY .9 INCH LOWER 1.125 INCH BY .685 INCH. FABRICATED DOUBLERS FROM 15-5PH .050 INCH DIM UPPER 12.75 INCH BY 8.75 INCH, LOWER AFT 11 BY 12.5. INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F A3WE 20090330 SO 2009 3 30 RAIA2009032600005120090220A5210 SEAL EMB 145 EMB145LR 3260212SO CABIN DOOR LACK OF LUBE A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03832HK 145771 POST FLT 7886 - IAD - MAIN CABIN DOOR DIFFICULT TO OPEN. MAINTENANCE LUBRICATED THE DOOR SEAL. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20090330 NM 2009 3 30 SWAA091938 120090324A53156546804 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 663, LBL 24. REPAIRED BEAM PER AAR EA. 2L72 4F RTA16WE 20090330 EU 2009 3 30 IPXA09155165 120090320A5321 FLOOR PANEL AIRBUSA300 A300F4622R 3930360EU MAIN CARGO BAY DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01158UP 0847 INSPECTION TYPE:5 YR BULK CARGO FLOOR PANEL 162 HF HAS SEVERAL FIELD REPAIRS. FABBED FLOOR PANEL IAW EO A300-5320-16407-C, APPX D. 2L72 4F RTA35EU 20090330 NM 2009 3 30 IPXA09555129 120090220A5753113N300337 SKIN BOEING757 75724APF 1384969NM TE FLAP GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01455UP 25476 INSPECTION TYPE:C LEFT O/B FLAP I/B UPPER SKIN PREVIOUS REPAIR HAS A GOUGE REPAIR LOCATE 35.0 INCHES FROM I/B EDGE 25 INCHES FWD OF T/E PER EO B757-5100-30760-B APPEN 'C', CONTACT ON SITE ENGR FOR DISPO. OUT OF LIMIT SRM 57-53-01-1A (2) REMOVED PREV REPAIR SRM 51-70-10/5 /57-53-01, CLEAN PREP AREA SRM 51-70-102R4, FAB DOUBLER ALU 7075-T6 040 APL BOEGEL P/N04-002-0203 BTEN 0001489157 REPAIR SRM 51-70-10 2R4 FIG 2 SH2 APL ADHESIVE PRIMER ON REPAIR P/N 04-009-0008 BTEN 00153214 SRM 51-70-10-2R4 FIG 2 SH 2. 2L72 4F RTA2NM 20090330 NE 2009 3 30 IPXA09555156 220090224A7230723410 STRUCTURE BOEING757 75724APF 1384969NM RROYCERB211 RB211535E4 54555NE NR 2 ENGINE CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01455UP 25476 INSPECTION TYPE:C NR 2 V-BAND GROOVE HAS A CHAFED MARK AT 11 O'CLOCK POSITION. HAND BLEND CHAFE AREA IAW EO535-7230-32641 PG 4 APP A PG 1, 2 PER SP TASK70-42-11-300-001. HFEC REQRK IAW NTM51-00-19PT6 PER EO 535-7230- 32641P1 NO CRACK FOUND. APPLY CHROMATE CONVERSION PER SPM70-00-00-3 330-A01 & EO535-7230-32641. PRIMED IAW SRM 51-20-01. FINAL REPAIR ACC PER UPS 535-7230-32641-A ST 1-2 WITH NO DEVIATIONS. 2L72 4F4 FRTA2NM E12EU 20090330 NM 2009 3 30 IPXA09655133 120090318A5320146T126184 STIFFENER BOEING767 76734AF 1385212NM FUSELAGE DEFORMED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01319UP 27758 INSPECTION TYPE:C BULK CARGO - STA 1502 FLOOR PANEL SUPPORT STIFFENER DEFORMED AT RBL 9. BULK CARGO STA 1502 FLOOR PANEL SUPPORT STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43 JUST AT RBL 9. 2L72 4F RTA1NM 20090330 SO 2009 3 30 C2XA09CL032 120090323A335078241 INVERTER EMB 145 EMB145LR 3260212SO EMERGENCY LIGHTSFAULTY A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2714573 145638 DURING ROUTINE MAINTENANCE THE NR 4 & NR 5 FLOOR AISLE PATH EMERGENCY LIGHT STRIPS WERE FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 5 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20090330 NM 2009 3 30 ASAA0944891 120090219A532065479576 INTERCOSTAL BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02785AS 27628 INTERCOSTAL WEB HAS TOOLING DAMAGE AT STA 790 845. REMOVED DAMAGED WEB, INSTALLED NEW WEB IAW B737 400 SRM 51 40 02. 2L72 4F RTA16WE 20090330 NM 2009 3 30 EIAA20090042 120090222A5311 FRAME BOEING747 747273C 1384896NM BS 460 DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471 D3303 UPPER DECK FRAMES BS 460 TO 480 LEFT OF LADDER CUTOUT HAS 14 MISDRILLED HOLES. REAMED 13 HOLES AT BS 460 WITHIN LIMITS PER B747 SRM 53-10-01 FIG 1 AND REMOVED AND REPLACED LOWER CHORD AT BS 480 LT PER B747 SRM 51-30-02 PG 6-9. 2L74 4F RTA20WE 20090330 NE 2009 3 30 ASAA0954894 220090323A7220 PAINT BOEING737 737890 1384527NM CFMINTCFM56 CFM567B27 13046NE INLET CONE MISSING A ASAAK NONE O OTHER ININSP/MAINT 1 NM02558AS 35177 894148 REF T/C 78472002 STEP 6 NR 1 ENGINE FRONT SPINNER CONE IS MISSING MORE THAN 20 PERCENT OF WHITE ANTI EROSION PAINT. REPLACED FRONT SPINNER CONE IAW T/C 78472002. 2L72 4F4 FRTA16WE E00055EN 20090330 NM 2009 3 30 IPXA09655167 120090323A5754 PANEL BOEING767 76734AF 1385212NM LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01308UP 27761 INSPECTION TYPE:N/A LEADING EDGE FIBERGLASS STRIP LOWER I/B HAS CRACK NEAR WING ROOT. CLASSIFIED AS A MAJOR REPAIR. TRANSFERRED TO NRC 354826. REPAIRED LT WING I/B SLAT CLOSEOUT PANEL IAW EO B767-5730-32829A (TEMP REPAIR). PERMANENT REPAIR OR REPLACEMENT NLT 24 MONTHS. 2L72 4F RTA1NM 20090330 EA 2009 3 30 QXEA2009032600197120090322A2781 DETECTOR CNDAIRCL600 CL6002C10 1390015EA SLAT SKEW FAILED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM19611QX 10041 SEA - INTERMITTENT SLAT FAULT STATUS MSG. RETURNED TO FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. NO MX AVAILABLE IN YEG. PLACED ON MEL 27-51-4. RETURNED TO SERVICE. MEL CLEARED ON 3/25. REPLACED SKEW SENSOR ON LT INBD SLAT IAW CRJ AMM 27-81-39 PG 401-412. OPS CHECK GOOD IAW CRJ AMM 27-81-39 PG 501-504. RETURNED TO SERVICE. 2L72 4F RTA21EA 20090330 WP 2009 3 30 IPXA09855174 120090326A5730 SKIN DOUG DC8 DC871F 302199DWP RT WING MISREPAIRED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:SV SURVEY SEQ 752-W4-18 RT WING L/E UPPER REPAIR AT STA XFS 556. DOUBLER SKIN THICKNESS LESS THAN SRM CALLOUT. REPAIRED PER 57-02-01-0 FIG 38 SHT 1. 2L74 4F RT4A25 20090330 NM 2009 3 30 IPXA09M55154 120090309A5730 SKIN DOUG MD11 MD11F 3023600NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01276UP 48579 INSPECTION TYPE:4C FIXED LEADING EDGE RT ANTI-ICE DUCT CUTOUT CRACK AT TWO UPPER CORNER. REMOVED CRACK, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW MD-11 SRM 57-10-00 FIG 42. 2L73 4F RTA22WE 20090330 NM 2009 3 30 IPXA09M55171 120090325A52104224007501 CABLE DOUG MD11 MD11F 3023600NM L1 DOOR BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01289UP 48455 INSPECTION TYPE:N/A L1 DOOR INOP DUE TO OVERHEAD RETRACTABLE PANEL CABLE BROKEN. REPLACED L1 DOOR OVERHEAD PANEL CABLE IAW MM 25-23-23-5. OPS CHECKED SATISFACTORY. 2L73 4F RTA22WE 20090330 NM 2009 3 30 SWAA091940 120090324A53226543536 SHEAR TIE BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29662SW 23255 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 639, STR 17R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091941 120090324A56105717623122 WINDOW BOEING737 7373H4 1384600NM COCKPIT OVERHEATED A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW29300SW 22940 DIVERSION / DECLARED EMERGENCY. IN CRUISE LARGE AMOUNT OF SMOKE APPEARED FROM R2 SLIDING WINDOW NEAR THE HANDLE. FOUND WINDOW TERMINAL HEAR CONNECTOR SHOWED SIGNS OF OVERHEAT. REMOVED AND REPLACED WINDOW AND HEAT CONTROLLER PER MM. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091942 120090324A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29644SW 28329 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 500, STR 27R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091943 120090324A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP BROKEN AT BS 947, STR 18L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091944 120090324A3320LP1308 LIGHT BOEING737 7377H4 1384404NM CABIN OVERHEATED A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW29453WN 29847 DECLARED EMERGENCY. FLT ATTENDANT SMELLED SMOKE FROM AFT GALLEY/ENTRY AREA IN DESCENT. PULLED CIRCUIT BREAKERS IN GALLEY AND TURNED OFF GALLEY POWER IN FLT DECK. THE SMELL CEASED AT THAT TIME. CONFIRMED ELECTRICAL SMELL FROM LT AFT WORK LIGHT BULB BURNED OUT. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091945 120090324A3350417A5701 COVER BOEING737 7377H4 1384404NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29450WN 32470 DURING SCHEDULED HC2 CHECK, FOUND EEPLS LIGHT COVER WORN AT ROW 6. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091946 120090324A3350D71701100 BATTERY PACK BOEING737 7377H4 1384404NM CABIN FAILED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29450WN 32470 DURING SCHEDULED HC2 CHECK, LT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091947 120090324A3350D71701100 BATTERY PACK BOEING737 7377H4 1384404NM CABIN FAILED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29450WN 32470 DURING SCHEDULED HC2 CHECK, RT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091948 120090324A3350GMW15 FUSE BOEING737 7375H4 138449DNM CABIN BLOWN A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29506SW 24183 L1 DOOR LIGHT INOP. REMOVED AND REPLACED FUSE PER MM. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091949 120090323A3350101114 COVER BOEING737 7375H4 138449DNM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29509SW 24186 DURING SCHEDULED MV2 CHECK, FOUND RT WING EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091950 120090323A335065C27093 LIGHT BOEING737 7375H4 138449DNM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29525SW 26567 R2 DOOR EMERGENCY EXIT LIGHT MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091960 120090324A53156584176 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BETWEEN BS 706 TO BS 714, BL 0. REPAIRED BEAM PER ER. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091961 120090324A534065C27314 STRINGER CLIP BOEING737 7373K2 13844BANM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 10L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091962 120090324A53126567172 ATTACH FITTING BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED 20Y CHECK, FOUND MLG WHEEL WELL AFT BULKHEAD SUPPORT BEAM ATTACH FITTING CRACKED AT BS 728, LBL 45. REMOVED AND REPLACED FITTING PER SRM. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091963 120090324A53116546593 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091964 120090324A53116546552 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091965 120090324A53116546555 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091966 120090324A53116546552 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091967 120090324A53116546558 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 908, STR 8R. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091968 120090324A53116558280 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29603SW 27954 DURING SCHEDULED 14Y CHECK, FOUND FRAME WEB CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091969 120090324A575365C30462 WEDGE BOEING737 7373Y0 1384671NM TE FLAP DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29665WN 23497 DURING SCHEDULED 22Y CHECK, FOUND LT WING TRAILING EDGE O/B FORE FLAP TRAILING EDGE WEDGE DELAMINATED. REPAIRED FORE FLAP PER SRM. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091970 120090325A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091971 120090325A53226546529 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29307SW 22947 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091972 120090325A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED SPV CHECK, FOUND STRINGER 23R CRACKED AT BS 456, RBL 45. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091973 120090325A53226546569 SHEAR TIE BOEING737 7373K2 13844BANM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091974 120090325A53226546529 SHEAR TIE BOEING737 7373K2 13844BANM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29345SA 23786 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 480, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091975 120090325A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29349SW 24408 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 21R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091976 120090325A575465C26602 WEDGE BOEING737 7373Q8 1384670NM LE SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29685SW 23401 DURING SCHEDULED 22Y CHECK, FOUND LT WING NR 2 SLAT O/B END T/E WEDGE DELAMINATED. REPAIRED SLAT PER SRM. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091977 120090325A55116547532 RIB BOEING737 7373H4 1384600NM HORIZ STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 DURING SCHEDULED 20Y CHECK, FOUND LT HORIZONTAL STABILIZER L/E RIB 75 INCHES FROM O/B END CRACKED. REMOVED AND REPLACED RIB PER SRM. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091978 120090325A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 9L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091979 120090325A3397S417N509 WIRE BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29360SW 26571 DURING SCHEDULED 20Y CHECK, FOUND FWD GALLEY EXIT LIGHT IDENTIFIER WIRE BROKEN. REPAIRED WIRE PER WDM. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091980 120090325A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29360SW 26571 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 21R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20090330 NM 2009 3 30 SWAA091981 120090325A335010107451 SIGN BOEING737 7373H4 1384600NM CABIN OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29399WN 27693 LEFT EMERGENCY EXIT SIGN FELL OFF. INSTALLED SIGN PER MM. 2L72 4F RTA16WE 20090331 NM 2009 3 31 IPXA09655243 120090327A5610 WINDOW BOEING767 767300 1385204NM COCKPIT STIFF A IPXAK NONE O OTHER ININSP/MAINT 1 SO01307UP 27760 INSPECTION TYPE:N/A CAPT L2 SLIDING WINDOW (EMERGENCY EGRESS) EXTREMELY DIFFICULT TO OPEN/CLOSE. ADJUSTED AND TESTED IAW AMM 56-11-02-5. OPS CHECK GOOD. 2L72 4F RTA1NM 20090331 NM 2009 3 31 USAA20090330BB055120090327A335020131A BATTERY PACK BOEING767 767201 1385125NM EMERGENCY LIGHT DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19249AU 23901 LHR - THE LEFT HAND, OVER-WING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AT M736 CHARGER. 2L72 4F RTA1NM 20090331 NM 2009 3 31 ASAA0944897 120090324A572065C80736493 SUPPORT ANGLE BOEING737 7374Q8 138447QNM LT WING DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 LT WING T/E CAVITY NO STEP PANEL I/B ANGLE AFT FASTENER HOLE IS OUT OF ROUND. REPLACED SUPPORT ANGLE. 2L72 4F RTA16WE 20090331 NM 2009 3 31 ASAA0944901 120090212A5311 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02785AS 27628 FWD FRAME LOWER FLANGE STA 500C STR 28L 28R CORRODED. REMOVED CORRODED ARE, FABRICATED, TREATED AND INSTALLED REPAIR DOUBLER TRIPLER IAW ASA EA 400 53EA 00934. 2L72 4F RTA16WE 20090331 NM 2009 3 31 ASAA0944902 120090214A531165458076 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02785AS 27628 R1 DOOR UPPER FWD STUB FRAME IS CRACKED. REMOVED CRACKED STUB FRAME, INSTALLED NEW STUB FRAME IAW B737 400 SRM 51 40 0. 2L72 4F RTA16WE 20090331 NM 2009 3 31 ASAA0944909 120090213A575365C348122 FLAP TRACK BOEING737 7374Q8 138447QNM TE FLAP CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02785AS 27628 NR 1 FLAP TRACK HAS PITTING CORROSION ON ROLLER CONTACT AREA. REMOVED AND REPLACED NR 1 FLAP TRACK IAW B737 400 MM 27 51 49. 2L72 4F RTA16WE 20090331 NM 2009 3 31 ASAA0944913 120090214A531190526913 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02785AS 27628 FUSELAGE FRAME STA 727B IS CRACKED JUST BETWEEN STRINGER 8L 9L. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948. 2L72 4F RTA16WE 20090331 NM 2009 3 31 ASAA0944915 120090214A5311654655211 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02785AS 27628 FUSELAGE FRAME STA 827 IS CRACKED BETWEEN STRINGER 8L 9L. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948. 2L72 4F RTA16WE 20090331 NM 2009 3 31 ASAA0944916 120090214A5311654655514 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02785AS 27628 FUSELAGE FRAME STA 867 IS CRACKED BETWEEN STRINGER 8L 9L. CUT OUT CRACKED SECTION OF FRAME FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948. 2L72 4F RTA16WE 20090331 NM 2009 3 31 ASAA0944917 120090214A531190526913 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02785AS 27628 FUSELAGE FRAME STA 500A IS CRACKED BETWEEN STRINGER 8L 9L. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948. 2L72 4F RTA16WE 20090331 NM 2009 3 31 ASAA0944918 120090214A531190526913 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02785AS 27628 FUSELAGE FRAME STA 500C IS CRACKED BETWEEN STRINGER 8L 9L. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948. 2L72 4F RTA16WE 20090331 NM 2009 3 31 ASAA0944920 120090214A531165465292 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02785AS 27628 FUSELAGE FRAME STA 440 IS CRACKED BETWEEN STRINGER 8R 9R. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948. 2L72 4F RTA16WE 20090331 NM 2009 3 31 ASAA0944921 120090214A531190526911 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02785AS 27628 FUSELAGE FRAME STA 747 IS CRACKED BETWEEN STRINGER 8R 9R. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948. 2L72 4F RTA16WE 20090331 NM 2009 3 31 ASAA0944922 120090214A531165465252 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02785AS 27628 FUSELAGE FRAME STA 380 IS CRACKED BETWEEN STRINGER 8R 9R. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948. 2L72 4F RTA16WE 20090331 NM 2009 3 31 ASAA0944925 120090214A5311654655211 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02785AS 27628 FUSELAGE FRAME STA 827 IS CRACKED BETWEEN STRINGER 8R 9R. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948. 2L72 4F RTA16WE 20090331 NM 2009 3 31 ASAA0944926 120090214A531165526913 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02785AS 27628 FUSELAGE FRAME STA 500A IS CRACKED BETWEEN STRINGER 8R 9R. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948. 2L72 4F RTA16WE 20090331 WP 2009 3 31 IXXA090013O 120090328A2130PS1351 CONTROL VALVE DOUG DC8 DC862F 3021972WP CABIN PRESSURE DEFECTIVE A IXXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW1141CX 855732370 46129 DURING CRUISE FROM KBWI TO LPLA THE CREW WAS UNABLE TO MAINTAIN CABIN PRESSURE ON ONE PACK. THE CREW HAD TO DESCEND TO 10,000 FEET. THE CREW LANDED IN KWRI WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT FLOW CONTROL VALVE. OPERATIONAL CHECK GOOD IAW DACO MAINTENANCE MANUAL 21-31-0, AND ATI MAINTENANCE MANUAL 21-04-26. AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20090331 NM 2009 3 31 ASAA0944927 120090214A531165526913 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02785AS 27628 FUSELAGE FRAME STA 500C IS CRACKED BETWEEN STRINGER 8R 9R. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948. 2L72 4F RTA16WE 20090331 NM 2009 3 31 ASAA0944928 120090214A531190526911 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02785AS 27628 FUSELAGE FRAME STA 480 IS CRACKED BETWEEN STRINGER 8R 9R. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948. 2L72 4F RTA16WE 20090331 NM 2009 3 31 ASAA0944929 120090214A531190526913 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02785AS 27628 FUSELAGE FRAME STA 480 IS CRACKED BETWEEN STRINGER 8R 9R. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948. 2L72 4F RTA16WE 20090331 NM 2009 3 31 ASAA0944930 120090214A531190526913 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02785AS 27628 FUSELAGE FRAME STA 727D IS CRACKED BETWEEN STRINGER 8R 9R. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948. 2L72 4F RTA16WE 20090331 NM 2009 3 31 ASAA0944931 120090214A5311659465588 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02785AS 27628 FUSELAGE FRAME STA 907 IS CRACKED BETWEEN STRINGER 8R 9R. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948. 2L72 4F RTA16WE 20090331 CE 2009 3 31 GLBA200903261 120090326A3230 LANDING GEAR BEECH 1900 1900D 1154162CE MALFUNCTIONED A GLBAO OTHER J WARNING INDICATION CRCRUISE 1 NM21192GL UE192 PILOTS REPORTED THAT THE LANDING GEAR WOULD NOT COME UP. MAINTENANCE INSPECTED ALL UP AND DOWNLOCK SWITCHES AS WELL AS THE SQUAT SWITCHES. PERFORMED LANDING GEAR SWINGS AND ALL OPERATIONALLY CHECKED GOOD. COULD NOT DUPLICATE DISCREPANCY. REFERENCE B1900D MM 32-30-00. 2L72 4T RTA24CE 20090331 SO 2009 3 31 GLBA200903251 120090325A3250 UNKNOWN EMB 120 EMB120 3260201SO PWA 118 PW118 NE WARNING LIGHT UNKNOWN A GLBAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM21293UX 120293 PILOTS REPORTED THAT A PEDAL STEERING INOP LIGHT CAME ON DURING TAKEOFF ROLL. MAINTENANCE PERFORMED A NOSEWHEEL STEERING 9 DEGREE POSITION PROXIMITY SWITCH CHECK IAW MM 32-50-00. ALL CHECKS WERE GOOD. COULD NOT DUPLICATE DISCREPANCY. 2L72 4T4 TRTA31SO E20NE 20090331 SO 2009 3 31 GLBA200903252 120090325A2120 UNKNOWN EMB 120 EMB120ER 3260203SO COCKPIT ODOR A GLBAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM21299UX 120299 PILOTS REPORTED A STRONG ODOR NOTICED AFTER TURNING WINDSHIELD HEAT ON. ODOR WENT AWAY WHEN TURNED OFF. (SMELLED LIKE SOMETHING BURNING). BELIEVED TO BE CAPTAINS WINDSHIELD. MAINTENANCE INSPECTED WINDSHEILD HEAT CONNECTIONS. ALL CONNECTIONS WERE GOOD. PERFORMED WINSHILED HEAT TEST. WINDHSHIELD HEAT OPERATIONAL CHECK WAS GOOD PER MM 30-40-00. 2L72 4T RTA31SO 20090331 CE 2009 3 31 GLBA20090329A 120090329A561010138402523 WINDSHIELD BEECH 1900 1900D 1154162CE COCKPIT CRACKED A GLBAA UNSCHED LANDING O OTHER CRCRUISE 1 NM21237YV UE237 PILOTS REPORTED THAT THE CAPTAINS WINDSHIELD CRACKED ON/IN CRUISE FLIGHT. AIRCRAFT RETURNED TO "DEN". MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDOW IAW SRM 56-10-00. 2L72 4T RTA24CE 20090331 CE 2009 3 31 GLBA20090329B 120090329A3260 SWITCH BEECH 1900 1900D 1154162CE MLG DIRTY A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM21192GL UE192 PILOTS REPORTED THAT UPON GEAR RETRACTION THE HORN WAS ON WITH GEAR UNSAFE LIGHTS. MAINTENANCE INSPECTED & CLEANED LANDING GEAR UPLOCK SWITCHES & INSPECTED PRINTED CIRCUIT BOARD CONNECTOR. NO DEFECTS WERE NOTED. REFEREMCE BMM 32-60-00. OPS CHECK FLIGHT WAS PERFORMED AND WAS SATISFACTORY. 2L72 4T RTA24CE 20090331 CE 2009 3 31 GLBA20090326F 120090323A5730 SKIN BEECH 1900 1900D 1154162CE LT WING LE DENTED A GLBAK NONE O OTHER ININSP/MAINT 1 NM21257GL UE257 MAJOR REPAIR - LT OUTBOARD WING LEADING EDGE BIRDSTRIKE REPAIR AT APPROXIMATELY WS 281 TO 301. DENT APPROXIMATELY 5/8TH INCH DEEP. MAINTENANCE REPAIRED THE LT OUTBAORD LEADING EDGE AT WS 281 TO 301 IAW EO 09-UE257-01. SKIN REPAIRED OUT O F PN 118-110047-81. APPROXIMATELY 19.5 . 2L72 4T RTA24CE 20090331 NM 2009 3 31 ASAA0974936 120090321A5320 INTERCOSTAL BOEING737 737790 13844CNNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02627AS 30794 CABIN FLOOR INTERCOSTAL CRACKED AT FLOORBOARD FASTENER HOLE STA 277 TO 294.5 BL 0 LENGTH OF CRACK MEASURES .75 INCH. REMOVED FLOOR SUPPORT, LOCATED, DRILLED NEW FLOOR SUPPORT, INSTALLED NEW FLOOR SUPPORT SRM 51 40 02. 2L72 4F RTA16WE 20090331 NM 2009 3 31 ASAA0974938 120090324A5320 STRUCTURE BOEING737 737790 13844CNNM FUSELAGE CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02627AS 30794 PANEL ATTACHED T-CHORD AT BS 663 673 RBL 27 WL 155 IS CHAFED. REPLACED T-CHORD. 2L72 4F RTA16WE 20090331 EA 2009 3 31 ASOA200900329 120090323A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN BROKEN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27857AS 7411 FLT 5226, ONE OF CABIN EMERGENCY STRIP IS BROKEN. REPLACED BROKEN BROKEN CABIN EMERGENCY STRIP IAW AMM 33-51-01. 2L72 4F RTA21EA 20090331 EA 2009 3 31 ASOA200900333 120090323A5320 FINGER DOUBLER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 RIGHT FINGER DOUBLERS ON PRESSURE FLOOR FS 409+128 -559 CORRODED. BLENDED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION IAW NDTM 51-20-04. 2L72 4F RTA21EA 20090331 EA 2009 3 31 ASOA200900337 120090324A5320 PRESSURE PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 PRESSURE FLOOR SKIN HAS SEVERAL AREAS OF CORROSION BETWEEN FS 409+128 TO FS 559.00 BETWEEN LBL35 TO 45L. BLENDED AND REPAIRED IAW REO 601R-53-41-906 2L72 4F RTA21EA 20090331 EA 2009 3 31 ASOA200900338 120090324A5320 PRESSURE PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 PRESSURE FLOOR SKIN HAS SEVERAL AREAS OF CORROSION BETWEEN FS 409+128 TO FS 559.00 BETWEEN RBL 35 TO 45R. BLENDED CORROSION IAW SRM 51-21-06. 2L72 4F RTA21EA 20090331 EA 2009 3 31 ASOA200900343 120090325A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 SEAT TRACK AT FS 559+80.00 TO 559+96.00 RBL 27.00 CORRODED. 2L72 4F RTA21EA 20090331 EA 2009 3 31 ASOA200900344 120090325A2750 FLAP CNDAIRCL600 CL6002B19 1900309EA WING MALFUNCTIONED A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27981EV 7768 CLIMBING THROUGH 16,000 FT AT 290 KNOTS RECEIVED HIGH SPEED AURAL WARNING CLACKER FOLLOWED IMMEDIATELY BY FLAPS FAIL AT 0 DEGREES. RAN QRH, LANDED AT 100 FPM WITH LANDING WEIGHT OF 37,000 LBS. EMERGENCY DECLARED, EN ROUTE TO GSP. A/C DIVERTED TO ATL DUE TO MTC. 2L72 4F RTA21EA 20090331 EA 2009 3 31 ASOA200900345 120090326A5320 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 TWO INTERCOSTALS CRACKED FORWARD AND AFT OF LEFT WING TO FUSELAGE MIDDLE ATTACH FITTING. REMOVED FORWARD AND AFT MIDDLE ATTACH INTERCOSTAL FITTINGS IAW SRM 51-42-06. INSTALLED ANGLE PER SRM 51-42-21 AND 51-42-06. 2L72 4F RTA21EA 20090331 EA 2009 3 31 ASOA200900346 120090326A2560 SWITCH CNDAIRCL600 CL6002B19 1900309EA FLASHLIGHT MISSING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27977EV 7720 F/O FLASHLIGHT MISSING ON/OFF SWITCH. 2L72 4F RTA21EA 20090331 SO 2009 3 31 C2XA09RI039 120090311A521014534664401 FAIRING EMB 145 EMB145LR 3260212SO PAX DOOR LOOSE A C2XAK NONE O OTHER TXTAXI/GRND HDL 1 SW2722971 145149 FLIGHT 2788 - EWR - FLIGHT CREW REPORTED MAIN CABIN DOOR HARD TO OPEN. EWR MX RE-SECURED DOOR FAIRING, LUBRICATED MAIN DOOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20090331 SO 2009 3 31 C2XA09RI040 120090305A3350110049 BATTERY EMB 145 EMB145LR 3260212SO CABIN DEFECTIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2715910 145455 RIC - MX - DURING ROUTINE MAINTENANCE, MX FOUND LEFT FRONT WING EMERGENCY LIGHT INOPERATIVE. RIC MX REMOVED AND REPLACED NR 1 EMERGENCY BATTERY TRAY AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20090331 SO 2009 3 31 C2XA09SH106 120090330A551214532235402 SKIN EMB 145 EMB145 3260210SO HORIZ STAB CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714904 477 SHV - DURING C-CHECK HORIZONTAL STAB RT LEADING EDGE HAS CORROSION AROUND RIVET HEADS AT UPPER & LOWER SURFACE. MAINTENANCE REMOVED CORROSION AROUND RIVET HEADS AT UPPER & LOWER SURFACE ON HORIZONTAL STABILIZER RT LEADING EDGE WITH POLISHING PROCEDURE IAW EC5530-01116 REV D, 80 PERCENT MATERIAL THICKNESS REMAINS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20090331 SO 2009 3 31 C2XA09SH107 120090330A3260K0024 RELAY EMB 145 EMB145 3260210SO LANDING GEAR INOPERATIVE A C2XAO OTHER O OTHER CLCLIMB 1 SW2715980 202 SHV - AIRCRAFT N15980 WAS GIVEN A FERRY FLIGHT RELEASE PERMIT FROM DFW TO SHV BECAUSE OF AN AIR GROUND SENSOR FAIL ON T/O OUT OF OKC AND WAS UNABLE TO RETRACT THE LANDING GEAR, THEN IT WENT AWAY AND GEAR RETRACTED (CAME UP). MAINTENANCE IN SHV REMOVED AND REPLACED RELAY K0024 IAW EMB145 FIM 32-32-00-810-801-A. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20090331 SO 2009 3 31 C2XA09SH108 120090330A21318166041 VALVE EMB 145 EMB145 3260210SO CABIN PRESSURE UNKNOWN A C2XABG EMER. DESCENT O2 MASK DEPLOYED O OTHER CRCRUISE 1 SW2715980 202 SHV - AIRCRAFT N15980 WAS GIVEN A FERRY FLIGHT RELEASE PERMIT FROM DFW TO SHV BECAUSE PACK VALVE 1 CLOSED, COULD NOT RESET. CABIN ALT RAISED PASSED 8,000FT UP TO 14,000FT AT 14:00. EMERGENCY DESCENT WAS PERFORMED. ALSO, O2 MASKS DEPLOYED COMING OUT OF OKC. MAINTENANCE IN SHV PERFORMED OPERATIONAL CHECK OF PACK 1 VALVE IAW EMB145 AMM 21-31-00. OPERATIONAL CHECK GOOD. PRESSURIZATION CHECK PASSED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20090331 EU 2009 3 31 MTNA0903003 120090314A5315WASB15 FLOORBEAM AEROSPATR72 ATR72202 8680940EU FUSELAGE CRACKED A MTNAK NONE O OTHER ININSP/MAINT 1 EA68811FX 283 LONGITUDINAL FLOORBEAM CRACKED BETWEEN FRAME 28 AND 28C LEFT SIDE. REPAIRED CRACK BY ACCOMPLISHING REPAIR IAW M7 AEROSPACE LONGITUDINAL SPLICE REPAIR DRAWING NUMBER 42-7000 DATED 02/02/2007 AND LAR 0903001 DATED 03/12/2009. 2H72 4T RTA53EU 20090331 NM 2009 3 31 SWAA091984 120090325A53126516300 BULKHEAD BOEING737 7373T5 1384608NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29692SW 23062 DURING SCHEDULED 24Y CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, BETWEEN RBL 1 TO RBL 3. REPAIRED WEB PER ACO. 2L72 4F RTA16WE 20090331 NM 2009 3 31 SWAA091986 120090325A3350411A2212 LIGHT BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29754SW 29849 L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20090331 NM 2009 3 31 SWAA091988 120090325A53306562212 SKIN BOEING737 7373T0 1384582NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20090331 NM 2009 3 31 SWAA091989 120090325A52416545871132 DOOR FRAME BOEING737 7373T0 1384582NM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR LOWER FRAME AT LOWER STOP CRACKED. REMOVED AND REPLACED R1 FRAME PER MM. 2L72 4F RTA16WE 20090331 CE 2009 3 31 HYIA1361G 120090324A2450 MASTER SWITCH CESSNA402 402C 207590RCE AVIONICS FAILED E HYIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NE011361G1770 180 402C0270 CREW REPORTED BURNING ODOR IN COCKPIT. MAINTENANCE REMOVED AND REPLACED AVIONICS MASTER SWITCH. 1L72 3O A7CE 20090331 CE 2009 3 31 HYIA812AN 120090323A2450 MASTER SWITCH CESSNA402 402C 207590RCE AVIONICS UNSERVICEABLE E HYIAO OTHER S AFFECT SYSTEMS TXTAXI/GRND HDL 1 NE01812AN601 220 402C0229 CREW REPORTED AVIONICS MASTER SWITCH FAILED TO TURN OFF. MAINTENANCE REMOVED AND REPLACED SWITCH. 1L72 3O A7CE 20090331 EU 2009 3 31 USAA2009032690688120090325A33502514353 COVER AIRBUS320 A320232 3930326EU CABIN MISSING A USAAK NONE O OTHER NRNOT REPORTED 1 EA19651AW 866 FLT 654 - PHX - EEL - ROW 3 AISLE SEAT A/C LEFT MISSING EMERGENCY LIGHT COVER. INSTALLED MISSING EMERGENCY LIGHT COVER AT ROW 3 A/C LEFT IAW AIRBUS MAINTENANCE MANUAL 33-51-00. 2L72 4F RTA28NM 20090331 CE 2009 3 31 HYIA106CA 120090308A2450 MASTER SWITCH CESSNA402 402C 207590RCE AVIONICS UNSERVICEABLE E HYIAO OTHER O OTHER NRNOT REPORTED 1 NE01106CA1483 37 402C1020 DURING ROUTINE MAINTENANCE, AVIONICS SWITCH WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED SWITCH. 1L72 3O A7CE 20090331 EU 2009 3 31 USAA2009032690689120090325A3350321430 BATTERY AIRBUSA319 A319112 3930323EU CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19752US 1319 FLT 1611 - CLT-LGA - EMERGENCY LIGHTS - EMERGENCY POWER SUPPLY UNIT (ESPU) BATTERY FAULT LEFT MID CABIN. REMOVED AND REPLACED LEFT MID EMERGENCY POWER SUPPLY UNIT BATTERY. OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20090331 NM 2009 3 31 QXEA2009032300192120090317A3210AN735D6 BRACKET BOMBDRDHC8 DHC8402 1390042NM RT MLG BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM19400QX 4030 PDX - RT MLG FORWARD STAB BRACE STOP BRACKET BROKE, FOUND AT LINE CHECK. REMOVED STAB STOP BRACKET AND INSTALLED NEW BRACKET IAW SCR 026-09 ITEM 10. RETURNED TO SERVICE. 2H72 4T RTA13NM 20090331 2009 3 31 AALA2009010700152420090107A31604056510903 DISPLAY DOUG DC9 DC982 3022082WP PFD FAILED A AALAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21486AA 49679 LGA INFLIGHT - AT 15000 FEET CAPTAINS PRIMARY FLIGHT DISPLAY WENT BLANK AND SMOKE STARTED COMING INTO COCKPIT. TURNED OFF PRIMARY FLIGHT DISPLAY AND ELECTRIC SMOKE FUMES CONTINUED. RETURNED TO LGA AND LANDED WITHOUT INCIDENT. REPLACED ELECTRONIC FLIGHT INSTRUMENT SYSTEM UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20090331 NM 2009 3 31 AALA2009010900155120090109A2611 SMOKE DETECTOR BOEING767 767323 1385205NM LAVATORY FAULTY A AALAFA ACTIVATE FIRE EXT. UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW21391AA 27451 ORD INFLIGHT - CREW REPORTED FIRE ALARM SOUNDED AT LEFT MID LAVATORY WITH STRONG ELECTRICAL ODOR IN MID CABIN NEAR CEILING. CREW DISCHARGED 3 HALON BOTTLES. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. NO EVIDENCE OF FIRE. FOUND AIR INLET RESTRICTED AND FAULTY SMOKE DETECTOR. CLEANED AIR INLET AND REPLACED SMOKE DETECTOR AT LEFT MID LAVATORY. ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 20090515 NM 2009 5 15 ASAA0945515 120090507A53506548657126 FRAME BOEING737 7374Q8 138447QNM FAIRING DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02765AS 25102 RT FAIRING FORMER HAS ELONGATED HOLES FAIRING FORMER REPLACED. 2L72 4F RTA16WE 20090331 NM 2009 3 31 AALA2009011800170120090118A7712855692 STATOR BOEING767 767323 1385205NM GE CF6 CF680C2* GL NR 1 RPM FAILED A AALAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21386AA 27060 690373 JFK INFLIGHT ORD TO MAN - CREW REPORTED NR 1 ENGINE HIGH PRESSURE ROTOR SPEED INDICATION FAILURE ACCOMPANIED BY LEFT CENTER FUEL PUMP PRESSURE LIGHT. IN DESCENT AT IDLE THRUST LEFT OIL PRESSURE INDICATION TURNED AMBER WITH 33 PSI. LANDED JFK WITHOUT INCIDENT. SUSPECT THE HIGH PRESSURE ROTOR SPEED TACH CONTROL ALTERNATOR STATOR FAILED. REPLACED NR 1 ENGINE ROTOR AND STATOR. ALSO, REPLACED NR 1 ENGINE HIGH PRESSURE ROTOR SPEED CARD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 FRTA1NM E23EA 20090331 NM 2009 3 31 HALA2009032600107120090326A3150 WARNING MESSAGE BOEING767 76733A 1385209NM PWA 4060 PW4060 52119NE FALSE ACTIVATIONA HALAO OTHER N FALSE WARNING CLCLIMB 1 WP35582HA 28139 ETOPS SIGNIFICANT SYSTEM, MX LEVEL EICAS MSG 'IDG OUT TEMP' DISPLAYED, AT TOP OF CLIMB IDG OUT- L63 DEGRESS, R95 DEGREES. IDG RISE- L9, R9. PERFORMED FIM 24-20-00 FIG 103. BITE CHECK NO FAULTS NOTED. OK FOR SERVICE. 2L72 4F4 FRTA1NM E24NE 20090331 NM 2009 3 31 HALA2009032500108120090325A4990 O-RING BOEING767 767332 1382001NM APU OIL CAP DEFORMED A HALAK NONE K FLUID LOSS ININSP/MAINT 1 WP35598HA 23278 ETOPS SIGNIFICANT SYSTEM, ON WALKAROUND FOUND EVIDENCE OF OIL LEAKING FROM APU COMPARTMENT. UPON FURTHER INVESTICATION FOUND APU OIL CAP O-RING STRETCHED OUT OF SHAPE. REPLACED O-RING ON APU OIL CAP. SERVICED APU PER MM 12-13-04. LEAK CHECKED OK. NO FURTHER DEFECTS NOTED. 2L72 4F RTA1NM 20090331 EA 2009 3 31 QXEA2009032400193120090320A2120 AIR DUCT CNDAIRCL600 CL6002C10 1390015EA CONTAMINATED A QXEAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 NM19612QX 10042 PDX - SMOKE AFT LAVATORY MESSAGE, MASTER WARNING, AFTER TAKEOFF. PERFORMED CHECKLIST AND PULLED APPLICABLE CB'S. RETURNED TO FIELD, NO FURTHER PROBLEMS NOTED. INSPECTED A/C, NOTICED STRONG ODOR OF SOAP IN CABIN BLEED SYS GROUND RAN IAW TASK 72-00-00-100-801 PAR H STEP 25. OP CHECK GOOD, NO DEFECTS NOTED. NOTE: ACFT ENGINES NR 1 AND NR 2 HAD PRESSURE WASH THE NIGHT BEFORE. RETURNED TO SERVICE. NO PARTS REPLACED. 2L72 4F RTA21EA 20090331 NM 2009 3 31 QXEA2009032400194120090320A3230465161 SPRING BOMBDRDHC8 DHC8402 1390042NM MLG UPLOCK BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM19424QX 4006 PDX - DURING WALK AROUND FOUND RT MLG UPLOCK SPRING BROKEN. REMOVED AND REPLACED SPRING IAW GOODRICH CMM 32-31-03 STEP 31, OK FOR CONTINUED SERVICE. 2H72 4T RTA13NM 20090331 2009 3 31 AALA2009010700153420090107A2210403239901 ACCELEROMETER DOUG DC9 DC983 3022083WP AUTOPILOT FAILED A AALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW21599AA 53289 ORD INFLIGHT - AFTER TAKEOFF CREW REPORTED AUTO THROTTLE AND AUTO PILOT WERE INOPERATIVE. CAPTAIN ELECTED TO RETURN TO ORD. LANDED ORD WITHOUT INCIDENT. REPLACED BOTH ACCELEROMETERS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA6WE 20090331 NM 2009 3 31 QXEA2009032400195120090320A243511521062 STARTER GEN BOMBDRDHC8 DHC8402 1390042NM NR 2 ENGINE FAILED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM19400QX8904 1196 4030 ALW - NR 2 ENGINE WILL NOT START. NO ROTATION SMOKE COMING FROM STARTER EXHAUST. REMOVED AND REPLACED THE NR 2 STARTER/GENERATOR IAW MTC 6243101. GROUND RAN A/C OPS TEST IS GOOD IAW Q400 AMM TASK 24-31-00-710-802. A/C IS OK FOR CONTINUED SERVICE. 2H72 4T RTA13NM 20090331 NM 2009 3 31 QXEA2009032500196120090321A5270 WARNING SYSTEM BOMBDRDHC8 DHC8402 1390042NM DOORS FALSE ACTIVATIONA QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM19436QX 4236 GEG - "FUSELAGE DOORS" WARNING SYSTEMS PAGE DISPLAYS AND SHOWS AFT CABIN DOOR UNSAFE. RETURNED TO FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. INSPECTED AND FOUND HANDLE PROTRUDING AFTER LANDING AT GATE. PERFORMED FUNCTIONAL CK IAW AMM 51-12-00-720-801. NO DEFECTS NOTED. NO PARTS REPLACED. COULD NOT DUPLICATE. RETURNED TO SERVICE. 2H72 4T RTA13NM 20090331 NM 2009 3 31 C8GA20090034 120090205A5344 HINGE BOEING727 727230 1384080NM L1 DOOR MISREPAIRED A C8GAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO29357KP69532 20675 WHILE IN HEAVY MAINTENANCE PERFORMING DTA EVALUATION IT WAS NOTED THAT THE L1 DOOR LOWER HINGE REPAIR FASTENERS DID NOT COMPLY WITH SB 727-53A0198. FASTENERS WERE REMOVED, HOLES NDT AND OVER SIZED. INSTALLED NEW FASTENERS IAW 727-53A0198. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F A3WE 20090331 NM 2009 3 31 C8GA20090035 120090205A5754 RIB BOEING727 727230 1384080NM NR 3 SLAT CRACKED A C8GAK NONE O OTHER ININSP/MAINT 1 SO29357KP69532 20675 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE NR 3 SLAT HAS AN INTERNAL ATTACH FITTING CRACKED. THE SLAT ACTUATOR INBD AND OTBD RIBS WERE REMOVED AND REPLACED. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F A3WE 20090331 2009 3 31 USAA2009032790699420090326A2565D5227917520200 PIN AIRBUSA319 A319132 3930340NM ZONE 200 DIRTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19810AW 1116 FLT 431- LEFT OVERWING SLIDE DOES NOT SHOW ARMED ON ECAM. CLEANED LEFT OVERWING DOOR ARM PIN, REINSTALLED DOOR, MESS DISAPPEARED. 2L72 4F RTA28NM 20090331 NM 2009 3 31 USAA2009032690694120090321A53306545765100 SKIN BOEING737 7373B7 138447FNM ZONE 200 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19505AU 23380 CLT - MAJOR REPAIR - 5 CRACKS AT THE LOWER EDGE OF THE CHEM-MILLED POCKETS JUST ABOVE S-10R BETWEEN BS 500D TO BS 530 WHILE PERFORMING LAP JOINT INSPECTION. REPAIRED FUSELAGE SKIN PANEL IAW SRM 51-40-02. 2L72 4F RTA16WE 20090331 NM 2009 3 31 USAA2009032690696120090321A53306545766 SKIN BOEING737 7373B7 138447FNM BS 435 S14R CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19505AU 23380 CLT - MAJOR REPAIR - CRACK INDICATION AT LOWER AFT CORNER FASTENER HOLE OF THE 5TH WINDOW FRAME AFT OF THE R1 DOOR, STA 435 RT SIDE. REPAIRED LOWER AFT CORNER FASTENER HOLE OF THE 5TH WINDOW FRAME AFT OF THE R1 DOOR, STA 435 RT SIDE IAW EA 130249. 2L72 4F RTA16WE 20090331 EU 2009 3 31 USAA2009032790704120090323A5347D53112815200 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19655AW 1075 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON SEAT TRACK AT FR 16, +Y1292. REPLACED SEAT TRACK AT FR 12 - FR 24, +Y1292 IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20090331 NM 2009 3 31 USAA2009032790708120090327A53206546568519 CHANNEL BOEING737 7373B7 138447FNM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19529AU 24411 CLT - MAJOR REPAIR - C1 CHECK - CORROSION ON STIFFENER CHANNEL AT BS 1016, BL 0. REPAIRED STIFFENER CHANNEL AT BS 1016, BL 0 IAW B737 SRM 53-80-01. 2L72 4F RTA16WE 20090331 NM 2009 3 31 USAA20090327BB054120090326A3397 WIRE BOEING757 7572S7 1384962NM CABIN LOOSE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19906AW 23568 PHX - THE L1 DOOR OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE SECURED WIRE DISCONNECTS BEHIND THE LIGHT ASSEMBLY. 2L72 4F RTA2NM 20090331 NM 2009 3 31 DU4R2009328 120090323A5300 FLOORBEAM BOEING737 7373T0 1384582NM BS 1016 CORRODED B DU4RK NONE O OTHER ININSP/MAINT 1 SO15732VA 23366 DURING SCHEDULED INSP, FOUND CORROSION ON FLOORBEAM AT BS 1016 BL 0 TO RBL 36. 2L72 4F RTA16WE 20090331 EA 2009 3 31 ASOA200900335 120090324A5260 STEP CNDAIRCL600 CL6002C10 1390015EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27753EV 10169 BOTTOM STEP ON PAX DOOR CRACKED NEAR ANCHOR FITTING. 2L72 4F RTA21EA 20090331 NM 2009 3 31 CALA2009032900166120090327A5311146N871172 FRAME BOEING757 757224 1384958NM FUSELAGE WORN A CALAK NONE O OTHER ININSP/MAINT 1 SW2729129 28969 FRAME AT STA 1640 BETWEEN STR 5RT & AMP; 6RT CHAFED INTO ON I/B FLANGE. REPAIRED DAMAGED FRAME FLANGE REF ECRA 5310-04921. INSTALLATION OF REPAIR ANGLE STEPS 1-12 AND ISSUED DIP FOR PERMANENT REPAIR REF STEP 13. ACCOMPLISH PERM REPAIR WITHIN 12 MONTHS FROM 3/24/2009. PLANNING TO CONTACT ENGR AFTER 10 MONTHS BUT BEFORE 11 MONTHS FOR A PER REPAIR. 2L72 4F RTA2NM 20090331 NM 2009 3 31 CALA2009032900167120090327A5311146N871171 FRAME BOEING757 757224 1384958NM FUSELAGE WORN A CALAK NONE O OTHER ININSP/MAINT 1 SW2729129 28969 FRAME AT STA 1640 BETWEEN STR 5LT & AMP; 6LT CHAFED INTO ON I/B FLANGE. REPAIRED DAMAGED FLANGE REF ECRA 5310-04920. INSTALLATION OF REPAIR ANGLE STEPS 1-12 AND ISSUED DIP FOR PERMANENT REPAIR REF ST EP 13. ACCOMPLISH PERM REPAIR WITHIN 12 MONTHS FROM 3/24/2009. PLANNING TO CONTACT ENGR AFTER 10 MONTHS BUT BEFORE 11 MONTHS FOR A PER REPAIR. 2L72 4F RTA2NM 20090331 NM 2009 3 31 CALA2009032900169120090328A5230143A6112 SKIN BOEING737 737724 13844BYNM FWD CARGO DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713750 28941 FWD BAG BIN DOOR EXT SKIN HAS DENT AT TOP CENTER ABOUT 2 INCH FROM SKIN EDGE. INSTALLED INTERIM REPAIR DOUBLER REF ECRA 5230-01816, PART 1, STEPS 1 THRU 22. DIP TO ACCOMPLISH PERMANENT REPAIR WITHIN 24 MONTHS FROM 03/27/2009 CONTACT ENGINEERING AFTER 22 MONTHS BUT BEFORE 23 MONTHS FOR A PERMANENT REPAIR. 2L72 4F RTA16WE 20090331 NM 2009 3 31 CALA2009033000170120090330A3260655579716 UPLOCK SENSOR BOEING737 737524 1384721NM RT MLG INOPERATIVE A CALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2714605 27318 RT MAIN GEAR RED UNSAFE AFTER TAKEOFF, EXTENDED TO NORMAL 3 GREEN. JACKED A/C PERFORMED SEVERAL GEAR SWINGS, ALL INDICATIONS NORMAL. AS PRECAUTIONARY REMOVED AND REPLACED RT GEAR UPLOCK SENSOR REF AMM 32-61-21, FUNCTIONAL CHECKS GOOD. 2L72 4F RTA16WE 20090331 NM 2009 3 31 CALA2009033000172120090330A5311143A1111 FRAME BOEING737 737724 13844BYNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713750 28941 CABIN FRAME CRACKED AT PSU SUPPORT BRACKET STA 400 STR 8L. INSTALLED INTERIM REPAIR PART B, STEPS 1 THRU 13 AND ISSUED DIP REF PART C, STEP 4, OF ECRA 5310-04919. ISSUED DIP ON LOG PAGE 9879503. 2L72 4F RTA16WE 20090331 NM 2009 3 31 CALA2009033000173120090330A5311146A1111 FRAME BOEING737 737724 13844BYNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713750 28941 CABIN FRAME CRACKED AT PSU SUPPORT BRACKET STA 727D STR 8L. INSTALLED INTERIM REPAIR PART B, STEPS 1 THRU 13 AND ISSUED DIP REF PART C, STEP 4 OF ECRA 5310-04919. ISSUED DIP ON LOG PAGE 9879503. 2L72 4F RTA16WE 20090331 EA 2009 3 31 COMA2009033050105120090324A531210531102555 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAO OTHER O OTHER ININSP/MAINT 1 SO27819CA21780 7415 FWD PRESSURE BULKHEAD CRACKED AROUND PARKING BRAKE CABLE HOLE. REPAIRED PER EA 10-5311-02555. 2L72 4F RTA21EA 20090331 NM 2009 3 31 HNAA2009033000100120090329A3350OL3071BPEGPL LIGHT DHAV DHC8 DHC8102 2809003NM CABIN INOPERATIVE A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07812EX4271642716 312 FOUND FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE DURING ROUTINE LINE CHECK AT MAINTENANCE FACILITY. REMOVED AND REPLACED BULB, OPERATIONAL CHECK GOOD. 2H72 4T RTA13NM 20090401 NM 2009 4 1 DU4R2009329 120090325A5320 WEB BOEING737 737300 1384610NM FUSELAGE CORRODED B DU4RK NONE O OTHER ININSP/MAINT 1 SO15732VA 23366 DURING SCHEDULED INSP, FOUND CORROSION ON WEB AT S-23R W/L 208. 2L72 4F RTA16WE 20090401 EA 2009 4 1 A6WA200940155 120090322A5315 FLOORBEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31416AW 7603 RT PILOT BULKHEAD CROSSBEAM INBD CLIP FOUND CRACKED .500 INCH . RT PILOT BULKHEAD CROSSBEAM INBD CLIP REPAIRED IAW REO 601R-53-11-171, REV D. SCHEME B. (K) 2L72 4F RTA21EA 20090330 NM 2009 3 30 ASAA0944899 120090325A5315654680474 FLOORBEAM BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 FLOORBEAM WHERE SEAT TRACK ATTACHES AFT FASTENER HOLE IS A DOUBLE HOLE. REPAIRED FLOORBEAM AT BS 727D. 2L72 4F RTA16WE 20090330 NE 2009 3 30 ASAA0954895 220090323A72203402523070 SHIM BOEING737 737890 1384527NM CFMINTCFM56 CFM567B27 13046NE NR 1 ENGINE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02558AS 35177 894148 NR 1 ENG REF T/C 78472002 FOUND BLADE SHIMS MISSING MORE THAN 25 PERCENT OF MOLYDAG COATING REF MM 72-21-02-200-801-F00. SHIMS NIS SEA DEFERRED FOR 250 CYCLES IAW MM 72-21-02-200-801 SEAMC NOTIFIED. 2L72 4F4 FRTA16WE E00055EN 20090330 NM 2009 3 30 IPXA09655175 120090318A5712111T20058 STIFFENER BOEING767 76734AF 1385212NM CENTER WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01319UP 27758 INSPECTION TYPE:C WING CENTER SECTION FWD BULKHEAD VERTICAL STIFFENER FOUND CRACKED JUST AT RBL 10, WL 195. CRACK 3.75 INCH LENGTH. WING CTR SECTION FWD BULKHEAD STA 785.9 WL 195 RBL 10 VERTICAL STIFFENER REPAIRED AS PER HX RS R57-11-36287 REV B AND UPS EO B767-5710-32138-B THIS REPAIR CLASSIFIED AS MAJOR REPAIR WITH MAT'L 2024T351-0250 IN AND 2024T3-0100 IN FOR REPAIR LENGTH 19.25 APPROX. 2L72 4F RTA1NM 20090330 NM 2009 3 30 EIAA20090045 120090228A5315 FLOORBEAM BOEING747 747273C 1384896NM BS 420 DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09471 D3303 HOLE IN FLOORBEAM BS 420 UPPER DECK CENTER HAS NO EDGE DISTANCE. FABBED AND INSTALLED REPAIR FLOORBEAM LWR CHORD STA 4020 CENTER PER B747 SRM 51-30-02 PG 8-9. 2L74 4F RTA20WE 20090331 NM 2009 3 31 ASAA0944911 120090214A531190526911 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02785AS 27628 FUSELAGE FRAME STA 747 IS CRACKED JUST BELOW STRINGER 8R. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00946. 2L72 4F RTA16WE 20090331 NM 2009 3 31 ASAA0944912 120090214A531190526911 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02785AS 27628 FUSELAGE FRAME STA 787 IS CRACKED JUST BELOW STRINGER 8R. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00946. 2L72 4F RTA16WE 20090331 NM 2009 3 31 ASAA0944933 120090214A531165465588 FRAME BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02785AS 27628 FUSELAGE FRAME STA 907L IS CRACKED BETWEEN STRINGER 8L 9L. CUT OUT CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR ANGLES IAW ASA EA 400 53EA 00948. 2L72 4F RTA16WE 20090331 EA 2009 3 31 ASOA200900328 120090323A5260 STEP CNDAIRCL600 CL6002B19 1900309EA ASD CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27846AS 7328 ASD BOTTOM STEP CRACKED. 2L72 4F RTA21EA 20090331 EA 2009 3 31 ASOA200900332 120090323A5320 FINGER DOUBLER CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 LEFT FINGER DOUBLERS ON PRESSURE FLOOR FS 409+128 -559 CORRODED. BLENDED CORROSION IAW SRM 51-21-06. 2L72 4F RTA21EA 20090331 EA 2009 3 31 ASOA200900339 120090324A5320 SUPPORT CNDAIRCL600 CL6002B19 1900309EA CARGO BAY CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 AFT CARGO DOOR SUPPORT STRUCTURE TO 621 BULKHEAD CLIP APPEARS CRACKED. 2L72 4F RTA21EA 20090331 SO 2009 3 31 C2XARI041 120090306A335078241 INVERTER EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE L NO TEST TXTAXI/GRND HDL 1 SW2716911 145446 FLIGHT 2521 - EWR - FLIGHT CREW REPORTED LAST 3 FLOOR PROXIMITY LIGHT STRIPS NOT WORKING. EWR MX REMOVED AND REPLACED INVERTER NR 6 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20090331 2009 3 31 NOCA01509 420090325A2565101656305 SLIDE BOEING767 767324 1385203NM CABIN DEPLOYED A NOCAK NONE O OTHER ININSP/MAINT 1 EA15767NA 27569 BOTH THE LT & RT OVERWING SLIDES WERE DEPLOYED DURING THE A-8-CHECK AT AA HANGER 10 WHILE CHECKING SLIDE S/N'S. REMOVED AND REPLACED BOTH LT AND RT OVERWING SLIDE PER JOBCARD 25-020-01 AS REQUIRED. 2L72 4F RTA1NM 20090331 2009 3 31 USAA2009032090643420090318A2565720129101 HOSE BOEING767 767201 1385125NM EVAC SLIDE DEFECTIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19246AY 23898 BFM - C4 - EES - LEFT OFF-WING INFLATION HOSE FAILED INSPECTION (HAS SOFT SPOT AREA NEAR MOST FORWARD RUBBER CLAMP). REPLACED LEFT OFF-WING INFLATION HOSE IAW B767 AMM 20-10-10. 2L72 4F RTA1NM 20090331 NM 2009 3 31 USAA2009032690690120090321A53306545766 SKIN BOEING737 7373B7 138447FNM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19505AU 23380 CLT - MAJOR REPAIR - CRACK INDICATION AT UPPER FWD CORNER FASTENER HOLE OF 12TH WINDOW FRAME AFT OF R1 DOOR STA 500C RT. REPAIRED UPPER FWD CORNER FASTENER HOLE OF 12TH WINDOW FRAME AFT OF R1 DOOR STA 500C RT IAW EA 130249. 2L72 4F RTA16WE 20090331 NM 2009 3 31 USAA2009032690695120090321A53116546529 FRAME BOEING737 7373B7 138447FNM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19505AU 23380 CLT - MAJOR REPAIR - FRAME CRACKED, BS 440, S-9R. REPAIRED FRAME AT BS 440, S9R IAW EA 130232. 2L72 4F RTA16WE 20090331 EU 2009 3 31 USAA2009032790703120090317A5210FE240004 DAMPENER AIRBUS320 A320232 3930326EU L2 DOOR LOW PRESSURE A USAAK NONE O OTHER ININSP/MAINT 1 EA19655AW3523635227 1075 SAL - EES - C7 CHECK - L2 DOOR DAMPER HAS LOW PRESSURE. SERVICED THE L2 DOOR DAMPER IAW A320 AMM 52-10-00-614-001. 2L72 4F RTA28NM 20090331 EU 2009 3 31 USAA2009032790705120090324A5315D53472197200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19655AW 1075 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON FLOORBEAM HARD-POINT, FR 68 - FR 70, -Y160. REPLACED FLOORBEAM, FR 68 - FR 70, -Y160 IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20090331 EA 2009 3 31 ASOA200900331 120090323A5210 INTERCOSTAL CNDAIRCL600 CL6002B19 1900309EA ASD CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 ASD TOP FWD INTERCOSTAL -9 CRACKED. 2L72 4F RTA21EA 20090331 NM 2009 3 31 CALA2009032900168120090328A5210147A61663 SKIN BOEING737 737724 13844BYNM L2 DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713750 28941 SMALL DENT ON LOWER AFT SIDE OF L-2 DOOR, L= 3.25", W=2.4", Y=0.122". INSTALLED REPAIR DOUBLER ON L-2 LOWER AFT SIDE, RESTORED AIRCRAFT EXTERIOR IN REPAIRED AREA REF SRM 52-00-01. 2L72 4F RTA16WE 20090331 NM 2009 3 31 CALA2009033000171120090330A5311143A1113 FRAME BOEING737 737724 13844BYNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2713750 28941 CABIN FRAME CRACKED AT PSU SUPPORT BRACKET STA 440 STR 8L. INSTALLED INTERIM REPAIR PART B, STEPS 1 THRU 13, AND ISSUED DIP REF PART C, STEP 4, OF ECRA 5310-04919, ISSUED DIP ON LOG PAGE 9879503. 2L72 4F RTA16WE 20090331 NM 2009 3 31 HNAA2009032800099120090327A3350OL3O718PEGPL LIGHT DHAV DHC8 DHC8102 2809003NM CABIN INOPERATIVE A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07934HA5208852088 139 UPON INSPECTION AT SBY, IT WAS NOTICED THAT AN EMERGENCY LIGHT AT ROW 1 WAS INOPERATIONAL. REPLACED THE LIGHT BULB AND THE OPERATIONAL CHECK WAS GOOD. 2H72 4T RTA13NM 20090401 WP 2009 4 1 NWAA09939875 120090322A3350 SOCKET DOUG DC9 DC951 3022051WP EMERGENCY LIGHT INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL31784NC 48109 DURING LINE CHECK, MX FOUND THAT THE RT OVERWING EMERGENCY EXIT SIGNS WAS INOPERATIVE. MX REPLACED THE LIGHT SOCKET ASSY AND FUNCTIONALLY CHECKED IT. (K) 2L72 4F RTA6WE 20090401 WP 2009 4 1 NWAA09889957 120090324A3350 BATTERY PACK DOUG DC9 DC931 3022065WP EMERGENCY LIGHT INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL31915RW 47139 DURING LINE CHECK, MX FOUND THAT THE LT SIDE EXTERIOR EMERGENCY OVERWING EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHT RETURNED TO AN OPERATIONAL CONDITION. (K) 2L72 4F A6WE 20090401 NM 2009 4 1 ASAA0944947 120090325A532069414556 SUPPORT ANGLE BOEING737 7374Q8 138447QNM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 SUPPORT ANGLE ABOVE ANTI COLLISION LIGHT CORRODED. REPLACED SUPPORT ANGLE PER SRM 51-40-02 AND DWG 65-45866. 2L72 4F RTA16WE 20090401 NM 2009 4 1 ASAA0944949 120090326A524565458962 SKIN BOEING737 7374Q8 138447QNM AC BAY DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 GROUND AIR CONDITIONING ACCESS DOOR EXTERNAL SKIN PILLOWING AND INTERNAL SKIN CORRODED. REPLACED GROUND AIR CONDITIONING ACCESS DOOR PER SRM 51 40 02. 2L72 4F RTA16WE 20090401 NM 2009 4 1 ASAA0944950 120090327A532065C2614312 SUPPORT CHANNEL BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02762AS 25099 WX RADAR R/T UNIT LT SUPPORT CHANNEL CRACKED. REMOVED AND REPLACED CHANNEL PER SRM 51-40-02. 2L72 4F RTA16WE 20090401 NM 2009 4 1 ASAA0944952 120090324A532069434023 CHANNEL BOEING737 7374Q8 138447QNM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02763AS 25100 DURING BS 794 RT FRAME REPLACEMENT FOUND WEB MECHANICAL DAMAGE BS 794 STR 16R. REPLACED WEB PER SRM 53 60 15 DETAIL VI SRM 51 40 05 AND DWG 65 47962. 2L72 4F RTA16WE 20090401 NM 2009 4 1 ASAA0944961 120090328A532069735633 SUPPORT ANGLE BOEING737 7374Q8 138447QNM E&E BAY CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02763AS 25100 E1 2 EQUIPMENT SHELF RT SUPPORT ANGLE CRACKED. REMOVED AND REPLACED PER ER 09 2053 ASA EA 400 25EA 00939. 2L72 4F RTA16WE 20090401 NM 2009 4 1 ASAA0944962 120090329A5320 FASTENER BOEING737 7374Q8 138447QNM CARGO BAY LOOSE A ASAAK NONE O OTHER ININSP/MAINT 1 NM02763AS 25100 FWD CARGO PIT BLOW OUT PANEL NOT SECURED. REPLACED BUTTON HEAD FASTENERS WITH FLUSH RIVETS AND STRAP PER ASA EA 400 53EA 00501 AND ASA EA 400 53A 00973. 2L72 4F RTA16WE 20090401 NM 2009 4 1 ASAA0954939 120090327A5313148A337017 STRINGER BOEING737 737890 1384527NM FUSELAGE DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02563AS 35180 STR 25R HAS THREE OVERSIZED HOLES. REMOVED & REPLACED DAMAGED SECTION OF STR PER SRM 53 00 03 REPAIR 1. 2L72 4F RTA16WE 20090401 NM 2009 4 1 ASAA0974940 120090320A5320146A7502 TRANS PANEL BOEING737 737790 13844CNNM CARGO BAY CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02627AS 30794 AFT PIT TRANSITION PANEL CORRODED STA 887 927. REMOVED CORRODED TRANSITION PANEL, FABRICATED AND INSTALLED NEW TRANSITION PANEL IAW 737 700 SRM 51 40 02. 2L72 4F RTA16WE 20090401 NM 2009 4 1 ASAA0974943 120090321A5321141A5810175 FLOORBOARD BOEING737 737790 13844CNNM CABIN BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02627AS 30794 CABIN FLOORBOARD BROKEN STA 270 312 LBL 11 LBL 56. REPAIRED IAW B737 700 SRM 53 00 50 REPAIR 4. 2L72 4F RTA16WE 20090401 NM 2009 4 1 ASAA0974945 120090326A5320143A7510 INTERCOSTAL BOEING737 737790 13844CNNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02627AS 30794 INTERCOSTAL CRACKED STA 500B STR 25. REMOVED CRACKED INTERCOSTAL (BAFFLE) FABRICATED AND INSTALLED NEW BAFFLE IAW 737 700 SRM 53 30 53 FIG 2. 2L72 4F RTA16WE 20090401 NM 2009 4 1 ASAA0974946 120090326A5320143A7510 INTERCOSTAL BOEING737 737790 13844CNNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02627AS 30794 INTERCOSTAL CRACKED STA 500 STR 25L. REMOVED CRACKED INTERCOSTAL, FABRICATED AND INSTALLED NEW INTERCOSTAL IAW 737 700 SRM 51 40 02 FIG 8. 2L72 4F RTA16WE 20090401 EA 2009 4 1 ASOA200900348 120090327A5312 VERTICAL BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 PRESSURE FLOOR FWD BULKHEAD FS 409.00+128 HAS CRACKED VERTICAL BEAM AT LBL 18.0 OUTBOARD SIDE LOWER AFT RADIUS. REPAIRED CRACK ON VERTICAL BEAM ON BULKHEAD IAW REO 601R-53-41-056. COMPLIED WITH EC/TC REO 601R-53-41-056 STEPS 4 & 5. 2L72 4F RTA21EA 20090401 EA 2009 4 1 ASOA200900349 120090327A5312 VERTICAL BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 PRESSURE FLOOR FWD BULKHEAD FS 409.00+128 HAS CRACKED VERTICAL BEAM AT RBL 9.0 INBOARD SIDE FWD LOWER RADIUS. REPAIRED DAMAGED AREA PER REO 601R-53-41-910 REFER TO EC/TC REO 601R-53-41-910. 2L72 4F RTA21EA 20090401 EA 2009 4 1 ASOA200900350 120090327A5312 VERTICAL BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 PRESSURE FLOOR FWD BULKHEAD FS 409.00+128 HAS CRACKED VERTICAL BEAM AT RBL 18.0 OUTBOARD SIDE AFT LOWER RADIUS. REPAIRED BULKHEAD VERTICAL BEAM IAW REO 601R-53-41-056. 2L72 4F RTA21EA 20090401 EA 2009 4 1 ASOA200900351 120090327A5312 VERTICAL BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27821AS 7194 PRESSURE FLOOR AFT BULKHEAD FS 559.00 HAS CRACKED VERTICAL BEAM AT LBL 9.0 OUTBOARD SIDE FWD LOWER RADIUS. REPAIRED IAW EC/TC REO 601R-53-41-057. 2L72 4F RTA21EA 20090401 CE 2009 4 1 GUUA93355032709A 120090327A55201016200131 HINGE BRACKET BEECH 1900 1900D 1154162CE LT ELEVATOR CORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO2981533 UE137 DURING SCHEDULED ROUTINE INSP DISCOVERED LT ELEVATOR CENTER HINGE BRACKET CORRODED. REPLACED LT ELEVATOR CTR HINGE BRACKET. 2L72 4T RTA24CE 20090401 SO 2009 4 1 GLBA20090327H 120090325A3097 TERMINAL EMB 120 EMB120ER 3260203SO WINDSHIELD HEAT LOOSE A GLBAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM21299UX 120299 PILOTS REPORTED THAT WITH THE CAPTAINS WINDSHIELD HEAT ON ONLY, A NOTICEABLE BURNING ODOR IN THE COCKPIT OCCURRED AFTER 3 MINUTES. MX INSPECTED THE LT WINDSHIELD HEAT CONNECTIONS AND FOUND A LT GROUND TERMINAL TO WINDSHIELD HEAT LOOSE. MX TIGHTENED CONNECTION AND PERFOMRED AN OPS TEST OF THE CAPTAINS WINDSHIELD HEAT SYS. NO ODOR OR BURNING WAS NOTICED. OPS CHECK WAS GOOD IAW MM 30-40-00. 2L72 4T RTA31SO 20090401 SO 2009 4 1 GLBA20090327J 120090325A3097W11056696 WIRE HARNESS EMB 120 EMB120ER 3260203SO WINDSHIELD HEAT BURNED A GLBAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM21299UX 120299 PILOTS REPORTED THAT IT APPEARED TO THEM THAT THE WINDSHIELD HEAT ON BOTH SIDES PRODUCED AND ELECTRICAL ODOR. MX REMOVED AND REPLACED WIRE SECTION W110-5669-6 P1 TERMINAL IAW 20-00 AND TESTED GOOD IAW MM 30-40-00. 2L72 4T RTA31SO 20090401 NM 2009 4 1 NWAA09895814 120090324A3350 POWER SUPPLY BOEING757 757351 1384991NM EMERGENCY LIGHTSINOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL31594NW 32994 DURING AN OVERNIGHT LINE CHECK THE EMERGENCY LIGHT AT DOOR 4R WAS INOPERATIVE. MX FOUND THE ASSOCIATED POWER SUPPLY, M736, TO BE DEFECTIVE AND REPLACED IT. SYSTEM OPERATION WAS NORMAL AFTER THE POWER SUPPLY WAS REPLACED. (K) 2L72 4F RTA2NM 20090401 CE 2009 4 1 FFSA200900003 120090324A3097 TERMINAL PPG BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA HARTZLHCB4M HCB4MP3 GL WINDSHIELD HEAT MELTED A FFSAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 AL01575F 4901 04044R5697 UC99 SHORTLY AFTER TAKE OFF, SMOKE WAS OBSERVED COMING OUT OF FIRST OFFICER’S GLARE SHIELD. AIRCRAFT RETURNED FOR LANDING. FOUND TERMINAL BLOCK AND RING TERMINAL INSULATION FOR CO-PILOT WINDSHIELD LOW HEAT POWER LEAD MELTED AND CRACKED. THE TERMINAL APPEARED TO BE LOOSE CAUSING A HIGH RESISTANCE CONNECTION LEADING TO THE OVERHEATING AND SUBSEQUENT DAMAGE. REPLACED WINDSHIELD AND POWER LEAD RING TERMINAL, ALL OPERATIONAL CHECKS OF HEATING SYSTEM SATISFACTORY. 2L72 4T4 TRTA24CE E4EA 6 CP56GL 20090401 WP 2009 4 1 NWAA09879926 120090324A3350 BATTERY DOUG DC9 DC932 3022066WP EMERGENCY LIGHTSINOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL31926NW 47425 DURING LINE CHECK, BOT OF THE AFT OVERWIN EMERGENCY EXIT SIGNS WERE FOUND TO BE INOPEATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. (K) 2L72 4F A6WE 20090401 EA 2009 4 1 COMA2009033150106120090330A5312601R53412515 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO27819CA21780 7415 LEFT FS 559 SEMI PRESSURE BULKHEAD CAP ANGLE CRACKED AT LBL 18. CUT OUT CRACKED SECTION OF CAP ANGLE, INSTALLED NEW CAP ANGLE SECTION WITH SPLICE PLATES AND DOUBLERS PER REO 601R-53-41-260 REV C. 2L72 4F RTA21EA 20090401 EU 2009 4 1 IPXA09155189 120090329A5330A53778737208 SKIN AIRBUSA300 A300F4622R 3930360EU FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01163UP 0852 INSPECTION TYPE:N/A RT FUSELAGE SKIN BETWEEN FRAME 34 AND 35 STRINGER 41R AND 42R DAMAGED. CUT OUT 10.3 X 8.9 INCHES, REPAIRED PER EO A300-5330-32881-A. 2L72 4F RTA35EU 20090401 EU 2009 4 1 IPXA09155190 120090329A5330A53778737208 SKIN AIRBUSA300 A300F4622R 3930360EU FUSELAGE DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01163UP 0852 INSPECTION TYPE:N/A RT FUSE SKIN DENTED AT FRAMES 31R AND 32R AT STR 44R. CUT OUT 13.0 X 10.150 INCHES. REPAIRED PER EO A300-5330-32792-A. 2L72 4F RTA35EU 20090401 EU 2009 4 1 IPXA09155191 120090329A5313A53778557230217 STRINGER AIRBUSA300 A300F4622R 3930360EU FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01163UP 0852 INSPECTION TYPE:N/A RT STR 44R AND 45R DAMAGED BETWEEN FRAMES 31R AND 32R. REPAIRED PER EO A300-5310-32795A. 2L72 4F RTA35EU 20090401 EA 2009 4 1 A6WA200940145 120090305A5242 RETAINER CNDAIRCL600 CL6002B19 1900309EA E/E DOOR SEAL CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31413AW 7585 MAIN AVIONICS DOOR SEAL RETAINERS (4EA) FOUND CORRODED. MAIN AVIONICS DOOR SEAL RETAINERS (4 EA) REPLACED IAW SRM 51-42-06. (K) 2L72 4F RTA21EA 20090401 SO 2009 4 1 GLBA20090326B 120090326A3230 LANDING GEAR EMB 120 EMB120ER 3260203SO MALFUNCTIONED A GLBAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 NM2171GL 120071 PILOTS REPORTED THAT AFTER TAKEOFF THE GEAR LEVER SELECTOR WAS SELECTED UP, THEY HEARD THE GEAR IN TRANSIT AND SAW IN TRANSIT LIGHTS. ALL IN TRANSIT LIGHTS EXTINGUISHED EXCEPT THE LT MLG A SYS LIGHT. FOLLOWING CHECKLIST PROCEDURES GEAR LEVER SELECTOR CYCLED WITH NO CHANGE. QRH REFERENCED TO EMERGENCY FREEFALL EXTENSION CHECKLIST UPON COMPLETION OF CHECKLIST, 6 GREEN LIGHTS WERE OBSERVED AND LANDED WITHOUT INCIDENT. -SUP- REFERENCE MM 32-30-00, RETRACTED GEAR 10 TIMES NO DEFECTS NOTED. 2L72 4T RTA31SO 20090401 EA 2009 4 1 A6WA200940149 120090304A5210 STIFFENER CNDAIRCL600 CL6002B19 1900309EA PAX DOOR DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31413AW 7585 PASSENGER DOOR AFT WEB + AFT TEE STIFFENER FOUND BUCKLED AND BENT. NEW PASSENGER AFT WEB + AFT TEE STIFFENERS INSTALLED IAW SRM 51-42-06. (K) 2L72 4F RTA21EA 20090401 EU 2009 4 1 IPXA09155247 120090328A3350 LIGHT AIRBUSA300 A300F4622R 3930360EU LAVATORY INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01162UP 0851 INSPECTION TYPE:N/A LAVATORY AUXILIARY LIGHT OUT. RELAMPED AND OPS CHECKED GOOD PER AMM 33-51-21-04. 2L72 4F RTA35EU 20090401 EU 2009 4 1 COEA2009032601912120090323A5315 FLOORBEAM AEROSPATR42 ATR42300 8680920EU ZONE 100 CORRODED A COEAK NONE O OTHER ININSP/MAINT 1 NM13912FX 047 CORROSION FOUND ON LT FLOORBEAM AT FRAME 25L UNDER LT OTBD SEAT TRACK. BLEND OUT BEYOND SRM LIMIT. ATR STRUCTURAL REPAIR INSTRUCTION DO/TS-1351/09-11496 ISSUED FOR THIS DISCREPANCY. BLEND OUT CORROSION IAW ATR INSTRUCTIONS AND LEAVE "AS IS". 2H72 4T RTA53EU 20090401 CE 2009 4 1 COEA2009032601728120090326A541226530351 FITTING CESSNA208 208B 2073701CE ENGINE FIREWALL CRACKED A COEAK NONE O OTHER ININSP/MAINT 1 NM13729FE5692 5692 C208B0471 HAIRLINE CRACK .4375 INCH IN LENGTH FOUND ON ENGINE FIREWALL SUPPORT FITTING JUST ABOVE NOSE GEAR SPRING BEARING SUPPORT. REMOVED AND REPLACED SUPPORT STRUCTURE FITTING. 1H71 3T A37CE 20090401 WP 2009 4 1 IPXA09855173 120090326A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING MISREPAIRED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE:SV SURVEY SEQUENCE 752-W3-2 MINIMUM EDGE DISTANCE LESS THAN 1.5 ON REPAIR LT AUX FUEL TANK LOWER EDGE AT XFS 154. *SDR FILED OPEN* 2L74 4F RT4A25 20090401 CE 2009 4 1 GLBA20090331A 120090331A32971123640211 CIRCUIT BOARD BEECH 1900 1900D 1154162CE E/E BAY WORN A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM21192GL UE192 AIR RETURN- A/C N192GL - FLIGHT 5028 PILOTS REPORT THAT LANDING GEAR UNSAFE LIGHT WILL NOT GO OUT ON GEAR RETRACTION ON TAKEOFF AND HORN CAME ON. MAINTENANCE REMOVED AND REPLACED THE A119 PRINTED CIRCUIT BOARD PER MM 32-60-00. OPERATIONAL CHECK FLIGHT WAS PERFORMED AND WAS SATISFACTORY. 2L72 4T RTA24CE 20090401 WP 2009 4 1 IPXA09855181 120090327A5730 SKIN DOUG DC8 DC871F 302199DWP LT WING MISREPAIRED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:SV SEQ SURVEY 752-W3-11 REPAIR ON LT WING O/B LEADING EDGE LOWER EXTERIOR SURFACE, XFS 618 FAILS APPX H. REPAIRED PER TIMCO REO-G12589 AND UPS EO DC8-5720-32216-A. 2L74 4F RT4A25 20090401 WP 2009 4 1 IPXA09855182 120090327A5730 SKIN DOUG DC8 DC871F 302199DWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:SV SURVEY SEQ 752-W4-05 REPAIR RT WING LEADING LOWER SURFACE AT STA XFS 310 HAS FASTENER SPACING LESS THAN 4D & TRACK EXTENDS THROUGH PREVIOUS STOP DRILLED HOLE. REPAIRED PER TIMCO REO-G12591 AND EO DC8-5720-32212. 2L74 4F RT4A25 20090401 WP 2009 4 1 IPXA09855183 120090328A5320975044885 SUPPORT ANGLE DOUG DC8 DC873F 302199FWP FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01852UP 46052 INSPECTION TYPE:SV CUSP SUPPORT ANGLE BETWEEN STA 1600 TO 1620 RBL 60 HAS DRILL DAMAGE ON SUB FLOOR LEG. INSTALL REPAIR PER DAC DWG 9750448. 2L74 4F RT4A25 20090401 WP 2009 4 1 IPXA09855184 120090328A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE MISREPAIRED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE:SV SURVEY SEQ 814-F1-46 DOUBLER STA 1282-1293 L33L-L34L. DOES NOT CORRELATE TO A SRM REPAIR. INSTALLED REPAIR PER DC8 SRM 53-2-1 FIG 7 SHT 13 TR 53-203 REV 78. 2L74 4F RT4A25 20090401 WP 2009 4 1 IPXA09855185 120090328A5730 DOUBLER DOUG DC8 DC873F 302199FWP RT WING GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 INSPECTION TYPE:SV RT WING L/E STA XFS 284 REPAIR DOUBLER GOUGED SURVEY 814-W4-18. INSTALLED REPAIR PER DC8 SRM 52-02-01-0 FIG 38 SHT 1. 2L74 4F RT4A25 20090401 WP 2009 4 1 IPXA09855186 120090119A5730 SKIN DOUG DC8 DC871F 302199DWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:SV RT WING L/E SECTION LOWER INTERIOR SKIN CRACKED ON O/B END AFT OF SPAR NEXT TO FWD SCREW ATTACH HOLE XS 526. REPAIRED PER TIMCO REO-G12594 REV A, AND UPS EO DC8-5720-32213A. 2L74 4F RT4A25 20090401 WP 2009 4 1 IPXA09855187 120090112A5753 DOUBLER DOUG DC8 DC871F 302199DWP TE FLAP GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 INSPECTION TYPE:SV LT OUTBOARD FLAP UPPER SKIN DOUBLER HAS DENT AND SMALL GOUGE XF 345, 9 INCHES FWD OF FLAP FRONT SPAR SS 752-W3-19. REPAIRED PER TIMCO REO-G12585 REV B, AND UPS EO DC8-5720-32341-A. 2L74 4F RT4A25 20090401 NM 2009 4 1 IPXA09B55213 120090321A71602242101573 INLET BOEING747 74744AF 13848B2NM NR 3 ENGINE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01571UP 35668 INSPECTION TYPE:N/A NR 3 ENGINE NACELLE DAMAGED BY DE-ICE TRUCK DURING DE-ICE. INLET COWL NR 3 ENG NACELLE REMOVED AND INSTALLED PER MM 71-11-01-4. 2L74 4F RTA20WE 20090401 NM 2009 4 1 IPXA09B55240 120090328A3310 LIGHT BOEING747 74744AF 13848B2NM COCKPIT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01570UP 35667 COCKPIT CEILING DOME LIGHT INOP. RELAMP DOME LIGHT, NO HELP. RELAMPED, OPS CHECK NORMAL. 2L74 4F RTA20WE 20090401 NM 2009 4 1 ANCF2009032500038120090325A3240 WARNING LIGHT AIRBUSA319 A319114 3930350NM BRAKES FALSE ACTIVATIONW ANCFC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO23691AV 3691 DURING T/O ROLL BRAKES HOT ECAM COME ON , REJECTED T/O WAS EXECUTED AT 40 KTS, AUTO BRAKE ACTIVATED. CORRECTIVE ACTION PERFORMED, TASK 32-00-810-924 NO FAULTS DETECTED ALSO PERFORMED BITE TEST OF THE BSCU IAW AMM 32-46-00-740-00, NO FAULTS. 2L72 4F RTA28NM 20090401 EU 2009 4 1 COEA2009032502912120090325A5310 CREASE BEAM AEROSPATR42 ATR42300 8680920EU FUSELAGE DAMAGED A COEAK NONE O OTHER ININSP/MAINT 1 NM13912FX 047 IN HEAVY CHECK: FOUND FR27 LT SIDE AT CREASE BEAM DAMAGED. DAMAGED AREAS EXCEED OUT OF DAMAGE TOLERANCE. 2H72 4T RTA53EU 20090401 SO 2009 4 1 C2XA09SH102 120090325A5340 SUPPORT EMB 145 EMB145EP 3260221SO ZONE 100 CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713929 145009 DURING C-CHECK, TOILET WASTE DRAIN VALVE SUPPORT CORRODED. REPAIRED TOILET WASTE DRAIN SUPPORT IAW SRM 53-31-02. ACFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20090401 SO 2009 4 1 C2XA09SH103 120090325A531314525771011 STRINGER EMB 145 EMB145EP 3260221SO ZONE 100 CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713929 145009 DURING C-CHECK, STR 21L CORRODED BTW FR 65-66. REPAIRED STR 21L IAW IC 2009-145/01544. ACFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20090401 SO 2009 4 1 C2XA09SH104 120090325A531114521809401 FRAME EMB 145 EMB145EP 3260221SO ZONE 200 CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713929 145009 DURING C-CHECK. FR 75 SHOWS SIGNS OF CORROSION BTW STR 2L-2R. REPAIRED FR 75 IAW EC 5310-01317. ACFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20090401 NE 2009 4 1 22AA20090303 220090326A7261 OIL SYSTEM DOUG DC10 DC1030F 3023504WP GE CF6 CF650C2 30018NE NR 2 ENGINE LEAKING A 22AAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO19526MD8390240661 46998 455278 LOG PAGE NR 126111. NR 2 ENGINE STARTED LOOSING OIL RAPIDLY. ACCOMPLISHED ENGINE FAILURE SHUTDOWN IN FLIGHT CHECK LIST. SHUTDOWN ENGINE AT 05:52Z AND REST OF FLIGHT UNEVENTFULL. REMOVED AND INSTALLED ENGINE IAW W/C 142R7101M. OPERATION TEST ON ENGINE RUN UP CHECKED NORMAL IAW MM 71-00-00. 2L73 4F4 FRTA22WE E23EA 20090401 EA 2009 4 1 A6WA200940146 120090303A5320 SILL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31413AW 7585 SERVICE DOOR LOWER SILL, STEP PLATE CORRODED. CORROSION ON SERVICE DOOR LOWER SILL, STEP PLATE REMOVED IAW SRM 51-21-06 AND FOUND OUT OF LIMITS IAW SRM 53-21-23, SERVICE DOOR LWR SILL STEP PLATE REPLACED IAW SRM 51-41-04. (K) 2L72 4F RTA21EA 20090401 EA 2009 4 1 A6WA200940148 120090225A5312 PRESSURE BLKHD CNDAIRCL600 CL6002B19 1900309EA BS 202 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31413AW 7585 CRACK FOUND ON FWD PRESSURE BULKHEAD FS 202.75, LBL 23.71 AROUND PARKING BRAKE CABLE (CRACK LENGTH 1.000) CRACK ON FWD PRESSURE BULKHEAD FS 202.75, LBL 23.71. REPAIRED IAW CRJ 200 601R-53-11-563. (K) 2L72 4F RTA21EA 20090401 CE 2009 4 1 DXTA2009033003571120090329A2840 INDICATOR CESSNA560 560XL 2076702CE FUEL SYSTEM UNKNOWN E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07627QS 5605227 AT BEGINNING OF TAKEOFF ROLL THE RT FUEL QUANTITY INDICATOR DROPPED TO ZERO AND THE RT FUEL GAUGE ANNUNCIATOR AND MASTER CAUTION ILLUMINATED. STARTED APU AND WAITED 15 MIN. CHECKED SIGNAL CONDITIONER LED'S NO FAULTS DISPLAYED. STARTED ENGINES & TAXIED ACFT. MONITORED RT FUEL GAUGE, NO FAULTS, ALL INDICATIONS NORMAL. SUMPED FUEL FROM TANKS, FUEL REMOVED CONTAINED A SMALL AMOUNT OF WATER. RAN ENGINES & TAXIED AGAIN. DURING TAXIING EXECUTED SEVERAL AGGRESSIVE STEERING MANEUVERS. NO FAULTS FOUND OR DISPLAYED. PERFORMED AN ADDITIONAL COMPLETE SHUTDOWN FOLLOWED BY ANOTHER FULL START OF ENGINES. NO FAULTS FOUND OR DISPLAYED ON SIGNAL CONDITIONER. REINSTALLED ACCESS PANELS. 2L72 4F RTA22CE 20090401 EA 2009 4 1 N6WA20090307 120090330A5210 DOOR CNDAIRCL600 CL6002C10 1390015EA MAIN PAX STIFF A N6WAK NONE O OTHER ININSP/MAINT 1 CE03155GJ 10225 PAX DOOR HARD TO OPEN. PAX DOOR OPS CHECK NORMAL AT THIS TIME. 2L72 4F RTA21EA 20090401 EA 2009 4 1 A6WA200940152 120090310A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31453AW 7838 CRACK FOUND ON AFT ANGLE OF PILOT BULKHEAD FS 280, LBL 9 CRACK LENGTH IS .500. REPAIR ON ANGLE OF PILOT BULKHEAD FS 28000, LBL 9 C/O IAW REO 601R-53-11-138. (K) 2L72 4F RTA21EA 20090401 EU 2009 4 1 RMXA032520097195 120090224A5302 DOUBLER BOLKMS117 BK117B2 5626013EU TAILBOOM CRACKED E RMXAK NONE O OTHER ININSP/MAINT 1 SW05217MC 7195 DURING A DAILY INSP A CRACK WAS DISCOVERED IN A DOUBLER LOCATED ON THE LT SIDE OF THE TAILBOOM. 1G72 3U NCH13EU 20090401 EA 2009 4 1 A6WA200940153 120090319A531060034017739 CROSSBEAM CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31416AW 7603 RT SIDE PILOTS BULKHEAD CROSSBEAM FS 280.00, RBL 9.0 IS CRACKED. RT SIDE PILOTS BULKHEAD CROSSBEAM FS 280.00, RBL 9 REPAIRED IAW REO 601R-53-11-171, REV D. (K) 2L72 4F RTA21EA 20090401 EA 2009 4 1 REXA2009F00029 120090225A3222 STRUT CNDAIRCL600 CL6002B19 1900309EA NLG UNDERSERVICED A REXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE218444F 7444 RECEIVED "GEAR DISAGREE" MESSAGE ON CLIMBOUT WHEN GEAR SELECTED UP. QRH FOLLOWED AND RETURNED TO AIRPORT. MX INSPECTED AIRCRAFT AND FOUND NOSE STRUT REQUIRED SERVICE. SERVICED NOSE STRUT IAW MM AND PERFORMED OPS CHECK. (K) 2L72 4F RTA21EA 20090401 NM 2009 4 1 NOCA01909 120090325A3411 PITOT LINE BOEING767 767328 1385290NM PITOT/STATIC SYSCONTAMINATED A NOCAA UNSCHED LANDING I FLT. ATTITUDE INST. CRCRUISE 1 EA15764NA 27135 ALTIMETERS ACTS LIKE A VSI INDICATION FO/CAPT DIFFERENT BETWEEN RT AND LT WAS 180’ FLUCTUATED TO 220 AND EICAS MSG ALT DISCREPANCY. T/S SYSTEM CAPT/FO ALTIMETER FOUND WATER IN CAPTS PRIMARY STATIC SYSTEM PLUMBING ACCOMPLISHED PITOT/STATIC SYSTEM FLUSH AS PER AMM 34-11-00. REMOVED MOISTURE SYSTEM A/C SYSTEM CHECKS OK. REMOVED AND REPLACED LT AND RT ADC P/N 4040800-906, SERIAL NUMBER 82110355 IAW 34-12-01 BITE CK OPS OK. ACMP MCDP TEST 30 AS PER AMM 22-00-02. REFM EICAS BITE. NO FAULTS NOTED. REMOVED DISPLAY AND CLEANED COOLING AIR SCREEN. REINSTALLED DISPLAY UNIT DISPLAY OK. FIM 34-41-00 AMM 31-41-01. 2L72 4F RTA1NM 20090401 2009 4 1 NOCA02009 420090327A3431285T05532 TEST PANEL BOEING767 767328 1385290NM ILS SYSTEM MALFUNCTIONED A NOCAA UNSCHED LANDING O OTHER CRCRUISE 1 EA15764NA 27135 ILS INDICATION COMES ON & OFF, ON F/O ADI WITHOUT AN ILS FREQUENCY SELECTED AT FL290 & FL 350 F/O AND CAPTAINS ALTIMETERS EXCEEDED RVSM LIMITATIONS. NO ILS INDICATIONS ON F/O AND CAPT SIDE ON ILS FREQ SELECTED FOR APPROACH (ON ID HEARD VOICE - NO MORSE CODE). T/S PER FIM 34-31-00 FIG 104, FOUND ILS TEST PANEL AT FAULT R & R ILS TEST PANEL PER MM 34-31-02 ALL OPS OK, ACCOMPLISHED FLUSH OF S1 LT UPPER, RT LOWER & S1 RT UPPER, LT LOWER PITOT STATIC SYS TO ADC1 & ADC2 PER MM 34-11-00. R & R F/O PITOT PROBE (RT TOP) PER MM 34-11-01. R & R CAPT'S PITOT PROB (LT TOP) PER CAPT'S AOA PRBE AS PER MM 34-12-03 UPON COMPLETION OF ALL WORK PERFORMED FULL TEST RANGE LEAK TEST IAW 34-11-00. NO LEAKS NOTED. 2L72 4F RTA1NM 20090401 SO 2009 4 1 RAIA2009032700001120090318A5210 MECHANISM EMB 145 EMB145LR 3260212SO PAX DOOR LACK OF LUBE A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03812HK 145373 POST FLIGHT 8003 - IAD - PASSENGER DOOR DIFFICULT TO OPEN. MAINTENANCE CLEANED AND LUBED THE DOOR MECHANISMS. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20090401 SO 2009 4 1 RAIA2009032700002120090318A5210 SEAL EMB 145 EMB145LR 3260212SO PAX DOOR LACK OF LUBE A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03812HK 145373 POST FLIGHT 7956 - IAD - PASSENGER DOOR DIFFICULT TO OPEN. MAINTENANCE CLEANED AND LUBED THE DOOR AND DOOR SEAL. OPS CHECKED GOOD. 2L72 4T RTT00011AT 20090401 SO 2009 4 1 RAIA2009032700003120090326A3040 MODULE EMB 145 EMB145EP 3260221SO WINDSHIELD WIPERMALFUNCTIONED A RAIAA UNSCHED LANDING O OTHER CRCRUISE 1 CE03807HK 145119 FLT 7986 - BTV - FIRST OFFICER'S WINDSHIELD WIPER WILL NOT PARK. MAINTENANCE DEFERRED THE FIRST OFFICER'S WINDSHIELD WIPER PARK MODE IN ACCORDANCE WITH THE MEL. 2L72 4F RTT00011AT 20090401 SW 2009 4 1 EVCA 2009/03/30 120090329A6210206015001115 BLADE BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL MAIN ROTOR CRACKED E EVCAK NONE O OTHER ININSP/MAINT 1 CE03708M 1534 38 51186 CAE895257 DURING POST FLIGHT INSPECTION, PILOT DISCOVERED A CRACK IN A MAIN ROTOR BLADE STARTING AT THE TRAILING EDGE AND CONTINUING FORWARD TO THE SPAR. 1G71 3U3 U H2SW E1GL 20090401 EU 2009 4 1 P4YA2009032500001120090325A5320369A75058 SUPPORT BRACKET HUGHES369 369FF 4470709EU ALLSN 250C 250C30 03013GL ZONE 100 CRACKED E P4YAK NONE O OTHER ININSP/MAINT 1 EA39971BW 066FF CAE890296 WHILE PERFORMING A FLIGHT CONTROL CHECK, PILOT PUSHED ON BOTH RUDDER PEDALS FIRMLY AND THE PEDAL BRACKET SUPPORT BROKE. 1G71 3U3 U H3WE E1GL 20090401 WP 2009 4 1 NWAA09859948 120090323A3350 POWER SUPPLY DOUG DC9 DC931 3022065WP EMERGENCY LIGHTSINOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL318929E 45866 DURING LINE CHECK, MX FOUND THAT THE RT SIDE EXTERIOR EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MX REPLACED THE POWER SUPPLY AND THE LIGHT RETURNED TO AN OPERATIONAL CONDITION. (K) 2L72 4F A6WE 20090401 SW 2009 4 1 ALGR0325009457AL 120090325A6230 BEARING BELL 407 407 1182206SW ANTI-DRIVE LINK UNSECURE E ALGAK NONE O OTHER ININSP/MAINT 1 SW03457AL8 53151 DURING DAILY SERVICE CHECK, MECHANIC NOTICED THAT THE ANTI-DRIVE LINK UPPER BEARING HAD UNSEATED. 1G71 3U O H2SW 20090401 NE 2009 4 1 REXA2009F00028 220090228A7200 ENGINE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 30070NE RIGHT FLAMED OUT A REXAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION APAPPROACH 1 CE218665A 7665 872960 ON APPROACH, ATC ISSUED DESCENT CLEARANCE TO 9000. BOTH THRUST LEVERS WERE REDUCED TO IDLE AT WHICH POINT THE FLIGHT CREW NOTICED A SEVERE YAW IN THE ACFT AND RT ENG OIL PRESSURE MASTER WARNING. ECIAS INDICATED A FLAMEOUT OF THE RT ENGINE. THE FLIGHT CREW DECLARED AN EMERGENCY, PERFORMED THE QRH FOR SINGLE ENGINE APPROACH. AN OTHER WISE NORMAL APPROACH AND LANDING WAS MADE. CFR MET THE ACFT AND SOC CLEARED IT TO THE GATE. MX INSPECTED THE ENGINE AND PERFORMED A GROUND RUN WITH ACCELERATION AND DECELERATION CHECKS. NO REPEAT OF THE FLAMEOUT OCCURRED AND THE ACFT WAS RELEASED FOR SERVICE. NO FURTHER PROBLEMS OCCURRED UNTIL MARCH 2, 2009. ON THAT DATE THE ACFT WAS TAXIING TO THE GATE AND THE RT ENGINE FLA2L72 4F4 FRTA21EA E15NE 20090401 WP 2009 4 1 22AA20090302 120090324A5230 STRUCTURE DOUG DC10 DC1030F 3023504WP CARGO DOOR DAMAGED A 22AAO OTHER O OTHER NRNOT REPORTED 1 SO19526MD 46998 LOADER DAMAGED FAIRING AT THE FWD EDGE OF LWR CARGO DOOR (CTR). RED BORDER NR 025212 ACCOMPLISH TEMPORARY REPAIR OF CTR DOOR FAIRING DAMAGE IAW FLIGHT VRHICLES CONSULTING EO 53-03242009. REFERENCE F/V CONSULTING EO 53-03242009 PART 2 REPEAT INSP. PERFORMED TEMPORARY REPAIR AT LWR CTR CARGO DOOR IAW F/V CONS. EO 53-03242009 PART 1 WORK INSTRUCTIONS FAIRING DAMAGE. ACCOMPLISHED RED BORDER NR 025212 TEMPORARY REPAIR AT LWR CENTER CARGO DOOR IAW F/V CONS. EO NR 53-03242009 PART 1 INSTRUCTIONS. TRANSFERRED TO CARRY OVER NR 22529. REPEAT THE ALL VISUAL INSPECTIONS AT EVERY 5 CYCLES AFTER PART 2. 2L73 4F RTA22WE 20090401 CE 2009 4 1 DXTA2009032603563120090325A2120 CONVERTER CESSNA750 750 2076810CE CABIN ODOR E DXTAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07921QS 7500241 A VISIBLE HAZE WITH AN OILY ODOR FORMED IN THE COCKPIT AND CABIN WHEN IN THE T/O DETENT. WENT TO THE RUN UP PAD AND RAN IT UP WITH BOTH PACS ON AND IT HAPPENED AGAIN. REMOVED LT AND RT COALESCER SOCKS (PN 746451-3), INSTALLED NEW SOCKS (PN 746451-3). REMOVED LT AND RT OZONE CONVERTERS, CLEANED AND INSTALLED OZONE CONVERTERS. REMOVED COCKPIT ACM (PN 738384-33 SN EC22E), INSTALLED REPAIRED ACM (PN 738384-33 SN 960220A), OPS AND LEAK CHECK GOOD. WORK PERFORMED REF THE MM 21-51-00. 2L72 4J RTT00007WI 20090401 CE 2009 4 1 DXTA2009032603564120090325A3260 SQUAT SWITCH CESSNA750 750 2076810CE MLG MALFUNCTIONED E DXTAA UNSCHED LANDING O OTHER CLCLIMB 1 GL07984QS 7500084 AFTER TAKEOFF, GEAR HANDLE WOULD NOT MOVE TO RETRACT POSITION. TROUBLE TO NOSE STRUT UNDERSERVICED AND NOSE SQUAT SWITCH ON EDGE OF SPEC. SERVICED STRUT IAW MM CH 12-10-38. ADJUSTED NOSE SQUAT SWITCH IAW MM, CHAP 32-60-00. GEAR SWING OPS CK GOOD. 2L72 4J RTT00007WI 20090401 NM 2009 4 1 DU4R20090331 120090220A5754 WEDGE BOEING757 757* NM NR 1 SLAT CORRODED B DU4RK NONE O OTHER ININSP/MAINT 1 SO15868AN 24868 DURING SCHEDULED INSP, FOUND L/E SLAT NR1 HAS HEAVY CORROSION IN L/E AND IN T/E WEDGE. 2L72 4F RTA2NM 20090401 NE 2009 4 1 HEEA123994 120090326A26129231004802104 FIRE DETECTOR SKRSKYS92 S92A NE NR 2 NACELLE INOPERATIVE E HEEAO OTHER N FALSE WARNING CLCLIMB 1 SW03592PH 920027 NR 2 ENGINE FIRE LIGHT AND AUDIBLE WARNING ON DURING INITIAL TAKEOFF. LANDING UNEVENTFUL. REPLACED OTBD NR 2 ENGINE FIRE DETECTOR. 2G72 4U R00024BO 20090401 CE 2009 4 1 DXTA2009032703565120090326A2720 ANGLE CESSNA560 560XL 2076702CE BENT E DXTAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL07600QS 5605664 ON TAKEOFF ROLL, THE RUDDER PEDALS FELT VERY STIFF. AFTER TAKEOFF WITH THE YAW DAMPER OFF, IT WAS VERY DIFFICULT TO DEPRESS THE RT RUDDER. ON FINAL APPROACH WITH THE YAW DAMPER OFF, THE RUDDER PEDALS FELT LIKE THEY WERE RUBBING SOMETHING WHEN DEPRESSED. FOUND AUX GEAR CALE CLAMP BRACKET ANGLE BENT CAUSING CABLE TO RUB RUDDER PEDAL. REPOSITIONED ANGLE AND CLAMP. TAXI CHECK GOOD. IAW MM 27-20-00 AND 27-20-05. 2L72 4F RTA22CE 20090401 CE 2009 4 1 DXTA2009032703566120090326A2910545353911 LINE RAYTHNDH125 HAWKER800XP 7150012CE HYD SYSTEM LEAKING E DXTAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 GL07832QS 258683 AFTER LANDING, (REVERSER) LIGHT ON, (FLAP FAULT) LIGHT ON AND HYD PRESSURE AT 2200 PSI. ON POST FLIGHT DISCOVERED LT TR DEPLOYED AND LT/REAR FUSELAGE COVERED IN HYD FLUID. REMOVED AND REPLACED LT TR HYD HOSE ASSY AND CHANGE MAIN HYD FILTER. RAN ACFT AND OPS CHECK NORMAL. ALL WORK COMPLIED IAW AMM 29-10-00 AND 79-32-00 FILTER CHANGED (PN MFHA189/1A). 2L72 4F RTA3EU 20090401 CE 2009 4 1 DXTA2009032703567120090326A3260 SQUAT SWITCH CESSNA750 750 2076810CE MLG OUT OF POSITION E DXTAO OTHER S AFFECT SYSTEMS CLCLIMB 1 GL07944QS 7500144 AFTER TAKEOFF, LDG GEAR HANDLE COULD NOT BE MOVED TO UP POSITION. INSTALLED SPACER AND ADJUSTED SQUAT SWITCH IAW MM 32-20-02 AND 32-60-00. OPS CHECKED GOOD. 2L72 4J RTT00007WI 20090401 CE 2009 4 1 DXTA2009032703568120090326A7830 SWITCH CESSNA560 560XL 2076702CE THRUST REVERSER LOOSE E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07687QS 5605187 UPON APPLYING T/O POWER THE LT ENGINE TR HAD AN UNCOMMANDED DEPLOYMENT, THIS HAPPEN MULTIPLE TIMES. EACH TIME WE USED EMER STOW. DID NOT BEGIN TAKEOFF ROLL. TROUBLESHOT SYS AND FOUND THE STOW AND DEPLOY SWITCHES LOOSE IN THE PEDESTAL. TIGHTENED AND ADJUSTED THE LT STOW AND DEPLOY SWITCHES IAW MM 78-31-00. GROUND RAN ACFT AND OPS CHECK OF THE SYS WAS GOOD. 2L72 4F RTA22CE 20090401 NM 2009 4 1 DXTA2009032703569120090325A760345AS4201039 THROTTLE CABLE RAYTHN400 400ARAYTHEON NM LEFT FROZEN E DXTAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL07151QS 1136 RK422 LT THROTTLE FROZE AT FL 350. UNFROZE AT FL 240. REPLACED LT ENG AFT THROTTLE CONTROL CABLE WITH NEW. OPS CHECKED GOOD IAW MM 76-10-00 AND MM 71-20-00-201 FOR LOOSENING REAR ENG MOUNT. 2H72 4F RTA16SW 20090401 WP 2009 4 1 NWAA09869926 120090324A3350 POWER SUPPLY DOUG DC9 DC932 3022066WP EMERGENCY LIGHTSINOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL31926NW 47425 DURING CHECK, MX FOUND THA THE EMERGENCY PATHWAY LIGHTING IN ROWS 18-21 OF THE CABIN WERE INOPERATIVE. MX FOUND THE POWER SUPPLY INOPERATIVE, REPLACED IT, AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. (K) 2L72 4F A6WE 20090401 NM 2009 4 1 SWAA092007 120090326A3297BACC45FN CONNECTOR BOEING737 7373H4 1384600NM RT MLG BROKEN A SWAAK NONE N FALSE WARNING CLCLIMB 1 SW29604SW 27955 AT APPROXIMATELY 20,000 FT ON CLIMBOUT, RECEIVED RIGHT RED & GREEN LIGHT. CYCLED GEAR, LIGHTS EXTINGUISHED. REMOVED AND REPLACED CONNECTOR D4536P PER MM. 2L72 4F RTA16WE 20090401 CE 2009 4 1 GUUA93355032609A 120090326A55101016200111 HINGE BRACKET BEECH 1900 1900D 1154162CE RT ELEVATOR CORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO2981533 UE137 DURING SCHEDULED ROUTINE INSP, DISCOVERED RT ELEVATOR OTBD HINGE BRACKET CORRODED. REPLACED RT ELEVATOR OTBD HINGE BRACKET. 2L72 4T RTA24CE 20090401 CE 2009 4 1 GUUA93357032709A 120090327A5730 SKIN BEECH 1900 1900D 1154162CE RT WING CORRODED A GUUAK NONE O OTHER ININSP/MAINT 1 SO2981533 UE137 DURING FURTHER INSP OF RT WING UPPER SKIN SURFACE CORROSION DISCOVERED DEBOND BETWEEN WS 146.00 THROUGH 171.00. REMOVED DAMAGED OF RIGHT WING UPPER SKIN FROM WS 126.50 TO 196.06 AND INSTALLED EXTERNAL DOUBLER REPAIR. 2L72 4T RTA24CE 20090401 CE 2009 4 1 GUUA94132032809A 120090328A3297 CIRCUIT BREAKER BEECH 1900 1900D 1154162CE LANDING GEAR TRIPPED A GUUAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO2917541 UE203 DURING APPROACH LANDING GEAR INDICATION CIRCUIT BREAKER POPPED AFTER SELECTING GEAR DOWN. RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. OPS CHECK FOUND TO BE WORKING OK. INSPECTED LANDING GEAR SYSTEMS UNABLE TO FIND ANY PROBLEM OPERATIONAL CHECK OK. 2L72 4T RTA24CE 20090401 EA 2009 4 1 NWAA200940110 120090303A323317008111 ACTUATOR CNDAIRCL600 CL6002B19 1900309EA MLG MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL01407AW23642 7424 REQUEST INSP OF LANDING GEAR DUE TO YEAR DISAGREE MESSAGE INFLIGHT. REMOVED AND REPLACED RT SIDESTAY ACTUATOR. (K) 2L72 4F RTA21EA 20090401 NM 2009 4 1 SWAA091990 120090325A273165C26384 TAB BOEING737 7373T0 1384582NM ELEVATOR FAILED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29697SW 23838 DURING SCHEDULED HC2 CHECK, FOUND RT ELEVATOR TAB FAILED FREE PLAY CHECK. REPAIRED TAB PER SWA EA. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092008 120090327A3350417A5701 COVER BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29227WN 34450 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 11. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20090401 EA 2009 4 1 N6WA20090305 120090320A2560 GLOWSTRIP CNDAIRCL600 CL6002C10 1390015EA CABIN LOOSE A N6WAK NONE O OTHER ININSP/MAINT 1 CE03164GJ 10256 GLOW STRIP FLOOR LIGHTING AT SEAT 1C IS COMING UP. RESECURED GLOW STRIP FLOOR LIGHTING AT SEAT 1C IAW AMM 33-51-00. 2L72 4F RTA21EA 20090401 NM 2009 4 1 SWAA092009 120090327A3350207377 LENS BOEING737 7377H4 1384404NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29227WN 34450 DURING SCHEDULED HC1 CHECK, FOUND FWD EEPLS LENS MISSING AT ROW 1. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092010 120090327A335081000 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29259WN 35554 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LIGHT INOP AT ROW 19. REMOVED AND REPLACED LIGHT PER MM. 2L72 4F RTA16WE 20090401 EA 2009 4 1 N6WA20090306 120090323A3260 WARNING LIGHT CNDAIRCL600 CL6002C10 1390015EA MLG ILLUMINATED A N6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03151GJ 10216 GEAR DISAGREE WARNING UPON RETRACTION. DEFERRED GEAR DOWN IN COMPLIANCE WITH MEL 32-30-01 CAT A DMI NR 10170. 2L72 4F RTA21EA 20090401 NM 2009 4 1 SWAA092011 120090329A3350207377 LENS BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29264LV 32521 FWD EEPLS LENS LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20090401 2009 4 1 SWAA092012 420090326A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29287WN 32537 R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092013 120090327A335065C27093 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092014 120090328A335010107451 SIGN BOEING737 7373K2 13844BANM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29340LV 23738 L1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092015 120090330A53306545768 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29344SW 24152 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 304, WL 261L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092016 120090326A3350101331 LENS BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29398SW 27692 DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED LENS PER MM. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092017 120090330A53156546804 FLOORBEAM BOEING737 7377H4 1384404NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29400WN 27891 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 55 TO RBL 5. REMOVED AND REPLACED BEAM PER SRM. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092018 120090330A5315BAC1509100146 FLOORBEAM BOEING737 7377H4 1384404NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29400WN 27891 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, RBL 8. REPAIRED BEAM PER AAR EA. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092019 120090326A33508210248801 LENS BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29409WN 27896 RT OVERWING EEPLS LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092020 120090326A3350D71701100 BATTERY PACK BOEING737 7377H4 1384404NM CABIN DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29411WN 29821 DURING SCHEDULED HC2 CHECK, LT EMERGENCY LIGHT BATTERY PACK FAILED FUNCTIONAL TEST. CHARGED BATTERY PER MM. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092021 120090326A5753113A37007 FLAP BOEING737 7377H4 1384404NM LT WING DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29411WN 29821 DURING SCHEDULED HC2 CHECK, FOUND LT WING O/B TRAILING EDGE FLAP I/B AFT END DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092022 120090326A3350D71701100 BATTERY BOEING737 7377H4 1384404NM CABIN FAILED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29411WN 29821 DURING SCHEDULED HC2 CHECK, FWD LT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092023 120090326A335081000 TRACK BOEING737 7377H4 1384404NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29436WN 32456 DURING SCHEDULED HC1 CHECK, FOUND EEPLS TRACK WORN AT ROW 1. REMOVED AND REPLACED EEPLS PER MM. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092024 120090328A5754114A50104 SLAT BOEING737 7377H4 1384404NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29436WN 32456 DURING SCHEDULED HC1 CHECK, FOUND RT WING NR 8 SLAT CRACKED AT LOWER L/E. REMOVED AND REPLACED SLAT PER MM. 2L72 4F RTA16WE 20090401 2009 4 1 SWAA092025 420090327A256510613232003 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29447WN 33720 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. REMOVED AND REPLACED SLIDE PER MT. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092026 120090327A335081000 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29448WN 33721 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LIGHT INOP AT ROW 11. REMOVED AND REPLACED EEPLS PER MM. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092027 120090327A3350417A5701 LENS BOEING737 7377H4 1384404NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29448WN 33721 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LIGHT LENS MISSING AT ROW 10. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092028 120090326A335065C28060 BALLAST BOEING737 7375H4 138449DNM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29507SW 24184 DURING SCHEDULED MV1 CHECK, FOUND LT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092029 120090326A3350BR2013 LIGHT BOEING737 7373H4 1384600NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29609SW 27929 DURING SCHEDULED CV CHECK, FOUND EEPLS WORN AT ROW 8. REMOVED AND REPLACED EEPLS PER MM. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092030 120090326A3350101073 LENS BOEING737 7373H4 1384600NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29624SW 27934 DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092031 120090327A3350300432 LIGHT BOEING737 7373H4 1384600NM EXTERIOR INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29637SW 27710 DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY LIGHT PER MM. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092032 120090327A25606556685 BRACKET BOEING737 7377H4 1384404NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29724SW 27856 R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOLDER LOOSE. SECURED BRACKET PER MM. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092033 120090326A3350101073 LENS BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29774SW 27882 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092034 120090326A3350417A5701 COVER BOEING737 7377H4 1384404NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29916WN 36623 EEPLS LIGHT COVER MISSING. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092035 120090328A335081000 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29919WN 36625 DURING SCHEDULED MV2 CHECK, FOUND FWD EEPLS LIGHT INOP. REPAIRED EEPLS PER MM. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092036 120090330A53306545776 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29644SW 28329 DURING SCHEDULED 12Y CHECK, FOUND SKIN CRACKED BETWEEN BS 951 TO BS 960, BETWEEN STR 7L TO STR 20L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20090401 NM 2009 4 1 SWAA092037 120090330A53116546560 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29644SW 28329 DURING SCHEDULED 12Y CHECK, FOUND LT LOWER STUB FRAME CRACKED AT BS 951 L2 DOOR LOWER FWD CUTOUT. REPAIRED STUB FRAME PER SRM. 2L72 4F RTA16WE 20090401 2009 4 1 ASAA0954973 420090329A2310 HF COMM BOEING737 737890 1384527NM COCKPIT MALFUNCTIONED A ASAAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 NM02518AS 35693 UNABLE TO TRANSMIT ON HF RADIOS. HF NR 1 AND NR 2 RADIO'S RECEIVE AND TRANSMIT NORMAL REF MM TASK 24 22 00 860 812. VERIFICATION FLIGHT SATISFACTORY HF RADIO CHECK GOOD. SEAMC NOTIFIED A/C IS NOW QUALIFIED. 2L72 4F RTA16WE 20090401 NM 2009 4 1 QXEA2009033100215120090327A3260 PROXIMITY SENSOR BOMBDRDHC8 DHC8402 1390042NM MLG FAILED A QXEAO OTHER N FALSE WARNING APAPPROACH 1 NM19404QX 4046 LAX - WHEN GEAR CYCLED ON APPROACH THE RIGHT MAIN LANDING GEAR DID NOT INDICATE DOWN, AND GEAR DOORS REMAINED OPEN. AFTER LANDING GEAR LIGHT (RIGHT MAIN) CAME ON, AND DOOR RETRACTED. LANDING GEAR ALTERNATE EXTENSION SHOW ALL THREE GREEN FROM THE TIME GEAR WAS EXTENDED. LANDING UNEVENTFUL. FERRIED TO PDX FOR REPAIRS. INTERROGATED PSEU, FOUND IN HISTORY FAULT RGDLK1 SENSOR UNREASONABLY FAR. PERFORMED INDUCTANCE VALUE CHECK OF RGDLK1 IAW Q400 AMM TASK 32-61-00-280-801, AND FOUND SENSOR AT 8.10 REMOVED, AND REPLACED PROX SENSOR RGDLK1 IAW Q400 AMM 32-61-06-000-802, AND TASK 32-61-06-400-802. PERFORMED OPERATIONAL TEST OF THE LANDING GEAR PRIMARY EXTENSION, AND RETRACTION SYSTEM IAW Q400 AMM TASK 32-31-00-7102H72 4T RTA13NM 20090402 SO 2009 4 2 SIMA200908502 120090324A2120 DUCT EMB 145 EMB145 3260210SO AC BAY MELTED A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21612AE 145079 ON FLIGHT 9800 CREW REPORTED ON CRUISE A SLIGHT BURNING SMELL IN COCKPIT. SMELL WAS NOT NOTICED IN CABIN. CREW SELECTED A COOLER TEMP ON LEFT PACK SMELL DISSIPATED. SELECTED WARMER ON LEFT PACK SMELL RETURNED. TURNED LEFT PACK OFF SMELL WENT AWAY. KEPT PACK OFF. AIRCRAFT REMOVED FROM SERVICE. INSPECTED AND FOUND NR 1 PACK DUCT MELTED. REMOVED AND REPLACED DUCT, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20090402 NE 2009 4 2 SWIA200921258 220090131A7200 SPHERICAL BEARIN CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 30070NE RT ENGINE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07927SW 7693 RIGHT ENGINE AFT THRUST FITTING SPHERICAL BEARING CORRODED (C CHECK). REPLACED PER AMM. 2L72 4F4 FRTA21EA E15NE 20090402 WP 2009 4 2 NWAA091029956 120090328A2130 SEAL DOUG DC9 DC931 3022065WP RELIEF VALVE LOOSE A NWAABG EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 GL01923RW 47183 ACFT WAS IN A DESCENT FROM FL330 TO FL310 WHEN THE CABIN ALT LIGHT CAME ON. FLIGHT CREW DONNED OXYGEN MASKS PERFORMED THE RED BORDERED CABIN PRESSURE LOSS PROCEDURE. THE CABIN WAS STILL AT 11000 FT AND DESCENT TO FL240 WAS INITIATED. AT FL270 THE CABIN CLIMB RATE INCREASED TO 1500 FT PER MIN; AN EMERGENCY WAS DECLARED WAS DECLARED, THE CREW WAS CLEARED MANUALLY ACTIVATED DEPLOYMENT. THE ACFT LEVELED OFF AT 10,000 FT ANT THE CABIN STABILIZED AROUND 8000 FT. DISPATCH RECOMMENDED THE FLIGHT CONTINUE TO DESTINATION. MX FOUND THE LT NEGATIVE RELIEF VALVE SEALS LOOSE AND RESECURED THEM AND ALSO REPLACED BOTH WATER SEPARATORS TEMPERATURE CONTROL VALVES. (K) 2L72 4F A6WE 20090402 EA 2009 4 2 SWIA200921262 120090201A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07926SW 7687 BRACKET CRACKED AT FS 484 LEFT SIDE (C CHECK). REPAIRED PER REO. 2L72 4F RTA21EA 20090402 EA 2009 4 2 SWIA200921263 120090201A5346 BEAM CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07926SW 7687 A .75 INCH CRACK ON ENGINE BEAM AFT OF UPPER SKIN DOUBLER CUTOUT (C CHECK). REPAIRED PER MODSUM 603. 2L72 4F RTA21EA 20090402 EA 2009 4 2 SWIA200921267 120090203A5320 FITTING CNDAIRCL600 CL6002B19 1900309EA CARGO BAY CRACKED A SWIAK NONE O OTHER UKUNKNOWN 1 NM07930SW 7713 CARGO BAY LEFT LINTEL FITTING CRACKED (C CHECK). REPAIRED PER REO. 2L72 4F RTA21EA 20090402 EA 2009 4 2 SWIA200921269 120090325A2910 CAP CNDAIRCL600 CL6002B19 1900309EA HYDRAULIC SYS LEAKING A SWIAA UNSCHED LANDING O OTHER CLCLIMB 1 NM07930SW 7713 HYDRAULIC SYSTEM 3 LOST ALL FLUID ON CLIMB (FLT 6398). REPLACED HYDRAULIC LINE END CAP PER SB 601R-29-031. 2L72 4F RTA21EA 20090402 EA 2009 4 2 SWIA200921270 120090324A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAK NONE O OTHER UKUNKNOWN 1 NM07496CA 7791 CEILING EMERGENCY LIGHT INOP (FLT 2621). RELAMPED EMERGENCY LIGHT. 2L72 4F RTA21EA 20090402 EA 2009 4 2 SWIA200921271 120090323A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAK NONE O OTHER UKUNKNOWN 1 NM07957SW 7829 NR 3 CEILING MOUNTED EMERGENCY FLOOD LIGHT INOP (FLT 5933). RELAMPED EMERGENCY LIGHT. 2L72 4F RTA21EA 20090402 EA 2009 4 2 SWIA200921272 120090327A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A SWIAK NONE O OTHER NRNOT REPORTED 1 NM07471CA 7655 BIRD STRIKE ON LEFT SIDE OF NOSE AND ACROSS LEFT PITOT TUBE (FLT 2768). DENT WITHIN LIMITS PER SRM, DOWNGRADED FROM RVSM DUE TO LOCATION OF DENT. 2L72 4F RTA21EA 20090402 EA 2009 4 2 SWIA200921273 120090325A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAK NONE O OTHER UKUNKNOWN 1 NM07926SW 7687 EMERGENCY LIGHT BY LAV IS INOP (FLT 6025). RELAMPED EMERGENCY LIGHT. 2L72 4F RTA21EA 20090402 NM 2009 4 2 UALA2009032500884120090324A7120310W30302 CLEVIS BOEING777 777222 1385219NM PWA PW4090PW40903 51538NE NR 2 ENGINE WORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29218UA46020 30222 NR 2 ENGINE AFT ENGINE MOUNT OUTBOARD CLEVIS HAS A WORN AREA ON INNER, AFT SURFACE. CONTINUED INSTALLATION OF AFT ENGINE MOUNT. NEED TO COMPLETE TORQUE AND SAFETY OF ALL MOUNT BOLTS. 2L72 4F4 FRTT00001SEE46NE 20090402 NM 2009 4 2 UALA2009032500888120090325A3350362624 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29121UA 29167 EMERGENCY EXIT LIGHT AT ROW 17 INOP. RELAMPED EMERGENCY LIGHT, OPS CHECKS NORMAL. 2L74 4F4 FRTA20WE E24NE 20090402 NM 2009 4 2 UALA2009032500889120090325A33509F19948501 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN DEFECTIVE A UALAK NONE O OTHER ININSP/MAINT 1 WP29121UA 29167 EMERGENCY LIGHT AT DOOR 4 RIGHT DIM. REPLACED LIGHT ASSY, OPS CHECKS NORMAL. 2L74 4F4 FRTA20WE E24NE 20090402 NM 2009 4 2 UALA2009032500890120090325A3350362624 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29121UA 29167 EMERGENCY EXIT EEL LIGHT INOP SEAT ROW 21 LEFT. REPLACED LIGHT ASSY, OPS CHECKS NORMAL. 2L74 4F4 FRTA20WE E24NE 20090402 NM 2009 4 2 NWAA09836312 120090320A3397 CONNECTOR BOEING747 747451 1384940NM EMERGENCY LIGHTSDAMAGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01672US 30267 MX FOUND THE EMERGENCY LIGHTS FOR THE LT OVERWING EXIT INOPERATIVE DURING AN OVERNIGHT LINE CHECK. MX FOUND THE CONNECTOR FOR THE ASSOC PWR SUPPLY TO BE DAMAGED AND REPAIRED THE CONNECTOR PLUG. SYS OPERATION WAS NORMAL AFTER THE CONNECTOR PLUG WAS REPAIRED. (K) 2L74 4F RTA20WE 20090402 NM 2009 4 2 NWAA09845635 120090322A3350 BATTERY PACK BOEING757 757251 1384970NM EMERGENCY LIGHT DEFECTIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01535US 26482 DURING AN OVERNIGHT LINE CHECK THE BATTERY PACK THAT POWERS THE LT OVERHEAD EXIT SIGN WAS INOPERATIVE. MX FOUND POWER SUPPLY M10567 TO BE DEFECTIVE AND REPLACED IT. SYS OPS WAS NORMAL AFTER THE BATTERY PACK WAS REPLACED. (K) 2L72 4F RTA2NM 20090402 NM 2009 4 2 UALA2009032500891120090325A335080541 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29121UA 29167 EMERGENCY EXIT EEL LIGHT INOP LOWER WALL EEL ACROSS DOOR 1 LEFT. REPLACED LIGHT ASSY, OPS CHECKS NORMAL. 2L74 4F4 FRTA20WE E24NE 20090402 NM 2009 4 2 NWAA09795816 120090318A2530 OVEN BOEING757 757351 1384991NM GALLEY SMOKE A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01596NW 32996 ENROUTE, OVEN NR 3 IN GALLEY 2B (AT DOOR 2R) BEGAN TO EMIT SMOKE. THE OVEN WAS TURNED OFF AND THE CIRCUIT BREAKER WAS PULLED. THE FLIGHT CONTINUED TO DESTINATION AND LANDED UNEVENTFULLY. MX DEFERRED THE OVEN TO MEL FOR FUTURE REPLACEMENT. (K) 2L72 4F RTA2NM 20090402 EU 2009 4 2 NWAA09693304 120090227A2530 CONNECTOR AIRBUS330 A330323 3940030EU OVEN DAMAGED A NWAAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL01804NW 5009 0549 IAW SHOP REPORT, OVEN TEARDOWN FOUND SMOKE AND ELECTRICAL ARCHING DAMAGE ON AN INTERNAL CONNECTOR. (K) 2L72 4F RTA46NM 20090402 NM 2009 4 2 UALA2009032500892120090325A335080541 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29121UA 29167 EMERGENCY LIGHT AT DOOR 2 GALLEY AREA CENTER AND RIGHT LOWER WALL INOP. RELAMPED EMERGENCY LIGHT. 2L74 4F4 FRTA20WE E24NE 20090402 WP 2009 4 2 NWAA09959928 120090326A3350 POWER SUPPLY DOUG DC9 DC931 3022065WP EMERGENCY LIGHTSINOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL018921E 45836 DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WAS INOPERATIVE. MX REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND OPERATIONALLY CHECKED THE SYSTEM. (K) 2L72 4F A6WE 20090402 EA 2009 4 2 A6WA200940140 120090319A2170 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA LT A/C PACK ODOR A A6WAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL31430AW 7719 AT FL230, TURNED TEMP UP ON LT PACK AND GOT A STRONG BURNED OIL ODOR IN COCKPIT DESCENDED AND TURNED LT PACK OFF, ODOR WENT AWAY. INSP ACM, OK COLOR NORMAL. OPERATED SYS AND OIL ODOR COMES BACK SOON AS LT PACK IS TURNED ON. REMOVED AND REPLACED LT PACK COALESCER IAW AMM 21-51-13. OPS CHECK GOOD, REMOVED. (K) 2L72 4F RTA21EA 20090402 2009 4 2 A6WA200940141 420090320A3432S414222 ANTENNA CNDAIRCL600 CL6002B19 1900309EA GLIDE SLOPE ERRATIC A A6WAA UNSCHED LANDING N FALSE WARNING APAPPROACH 1 GL31404AW24443 7294 NAV 1 AND NAV 2 INDICATED ERRATIC GLIDE SLOPE INDICATIONS FOLLOWED BY ERRONEOUS INDICATION AND GLIDE SLOPE FLAG WHILE OTHER ACFT RECEIVED NAV-AID RECEPTION. REMOVED AND REPLACED GLIDE SLOPE ANTENNA IAW AMM 34-51-11. OPS CHECK GOOD. (K) 2L72 4F RTA21EA 20090402 CE 2009 4 2 S8A2009F00000 120090321A2721720303 INDICATOR BEECH MU300 400A 1155402CE PWC JT15 JT15D5D 52192NE TRIM MALFUNCTIONED E S8AAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA39400CT3522 RK179 DEPARTED, ON CLIMB OUT CREW ENGAGED AUTO PILOT, A/P MIS-TRIM WARNING, DISENGAGED A/P TRIED TO TRIM THE RUDDER MANUALLY BUT WERE UNSUCCESSFUL. FLIGHT CREW RETURNED TO DEPARTURE, NO PASSENGERS, 2 CREW, NO EMERGENCY WAS DECLARED AND LANDING WAS UNEVENTFUL. MFG WAS CONTACTED FOR INSP AND REPAIR. INSPECTED AND FOUND RUDDER TRIM INDICATOR DEFECTIVE, REPLACED RUDDER TRIM INDICATOR WITH NEW UNIT IAW AMM 27-20-00. OPS CHECK AND TEST FLIGHT WILL BE PERFORMED 3-25 BEFORE RELEASE TO SERVICE. (K) 2H72 4F4 FRTA16SW E45NE 20090402 EU 2009 4 2 UALA2009032600894120090325A2530 OVEN AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE GALLEY DEFECTIVE A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29422UA 503 DIVERTED TO DEN DUE TO CIRCUIT BREAKER FOR AFT GALLEY TRIPPING OFF. AFT GALLEY TRIPPING OFF. FLIGHT DIVERTED. FOUND ON INSPECTION BRACKET THAT HOLDS BUS PLUG 9025ML4 PULLED OUT FROM WALL. SUSPECT IT IS THE CAUSE OF TRIPPED BREAKER. REPAIRED BRACKET FOR OVEN RECEPTICLE. STILL NEEDS OVEN REPLACEMENT. REPLACED OVEN ASSY, RAN OVEN FOR 30 MIN, BREAKER DID NOT TRIP. 2L72 4F4 FRTA28NM E40NE 20090402 EU 2009 4 2 FDEA200903210981 120090321A7997224W9922501 WIRE HARNESS AIRBUS300 A300F4605R 3930327EU GE CF6 CF680C2A5 NE NR 2 ENGINE FAILED A FDEAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 CE21655FE13211 742 705279 AT TOP OF DESCENT NR 2 ENG OIL PRESS INDICATED 0 PSI ON ECAM AND MECHANICAL GAUGE. SHUT DOWN ENGINE. WINDMILLED FOR 33 MINUTES INDICATING 0 OIL PRESSURE OIL TEMPS MATCHED PRIOR TO SHUTDOWN. REMOVED AND REPLACED NR 2 ENG OIL PRESSURE HARNESS (224W9722) IAW MM 71-52-01-4. OPS CHECKS GOOD ON ENG RUN IAW JRH. BOTH NR 1 AND NR 2 ENG OIL PARAMETERS WERE 30 PSI AT IDLE. OK FOR SERVICE. 2L72 4F4 FRTA35EU E13NE 20090402 NM 2009 4 2 UALA2009032700895120090325A335078941 LIGHT BOEING777 777222 1385219NM PWA PW4077PW4077 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29768UA 26919 EMERGENCY EXIT LIGHT ON SEAT 3E, AFT LIGHT IS INOP. RPL LAMP ASSY, OPS CHECK OKAY. 2L72 4F4 FRTT00001SEE46NE 20090402 NM 2009 4 2 FDEA200903220996 120090322A2810 FUEL TANK DOUG MD11 MD11F 3023600NM RIGHT VENTING A FDEAJA DUMP FUEL UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 CE21617FE 48748 "TANK WING OVERFILL" AMBER LEVEL 2. COMPLIED WITH RED TABS. VISUALLY CONFIRMED FUEL VENTING FROM CARGO BAY WINDOW. FUEL VENTING FROM OVER TOP OF LT AILERON. RTB WITH FUEL DUMP OF APPROX 90,000 LBS. UNEVENTFUL LDG. NO FUEL VENTING AFTER FUEL DUMP. CREW ADVISED THAT AT TOP OF CLIMB FUEL APPROX 2000 LBS LESS THAN COMPUTED. COMPUTED FUEL BURN 7000 LBS EVERY 20 MIN & USING 10000 LBS IN 10 MIN. AT THE TIME THE TANK WING OVER FILL MESSAGE CAME ON NONE OF FILL VALVE ON. FUEL STILL COMING OUT OF VENT AFTER FUEL LEVEL DOWN TO 39000 LBS IN RT TANK. PER FIM 28-14 PAGE 172 PRESSURIZED MANIFOLD FOR APPROX 30 MIN NO FUEL MIGRATED BETWEEN TANKS. FILLED BOTH TANK 1 & TANK 3 TANK 1 AUTO SHUT OFF AT 39800 LBS & TANK 2L73 4F RTA22WE 20090402 EU 2009 4 2 UALA2009032700896120090325A3350BR964421 LIGHT AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29475UA 1495 SEAT MOUNTED EEL LIGHT OUT AT 1C, 5C, 11C. RELAMPED. 2L72 4F4 FRTA28NM E40NE 20090402 NM 2009 4 2 FDEA200903220997 120090322A5330 SKIN BOEING757 757236 1384971NM ZONE 200 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21910FD 50523 25054 DENT AT FUSE EXT UPPER SURFACE APPROX STA 1542, S2R. COMPLIED WITH EA 757-5361-16-F1907, REV A AT FUSE STA 1542, S2R. THIS IS A CATEGORY A REPAIR. THIS REPAIR IS CLASSIFIED AS A CAT. "A" MAJOR REPAIR. 2L72 4F RTA2NM 20090402 EU 2009 4 2 FDEA200903220999 120090322A7933662285002 SIGNAL COND UNIT AIRBUS310 A310222 3930315EU PWA JT9 JT9D7 52054NE ENGINE OIL PRESSMALFUNCTIONED A FDEAC ABORTED TAKEOFF JN WARNING INDICATION FALSE WARNING TOTAKEOFF 1 CE21454FE 278 715411 REJECTED TAKEOFF. NR 1 ENGINE HIGH OIL PRESSURE WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL APPROXIMATELY 85KTS. INDICATION DEFERRED PER MEL 79-33-01-02. REMOVED AND REPLACED NR 1 ENG OIL SIGNAL CONDITIONER P ER MM 79-33-31-4, PERFORMED OPERATIONAL TEST OF THE OIL PRESSURE AND LOP WARNING SYS SATI. 2L72 4F4 FRTA35EU E20EA 20090402 EU 2009 4 2 FDEA200903231014 120090323A5320A5397426300000 FLOOR SUPPORT AIRBUS300 A300B4622R 3930312EU ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21726FD 41435 575 BULK CARGO COMPARTMENT FLOOR SUPPORT BETWEEN FRAME 68 AND FRAME 69 AT STRINGER 48R HAS CORROSION AROUND FASTENER HOLE. BLENDED CORROSION IAW SRM 51-74-10 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. INSTALLED NEW FLOOR SUPPORT P/N A5397426300000 IAW SRM 51-40-21; PARA 6; SHEET 1. 2L72 4F RTA35EU 20090402 EU 2009 4 2 FDEA200903231015 120090323A5321FXSRZ25005242HK FLOOR PANEL AIRBUS300 A300B4622R 3930312EU ZONE 200 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21726FD 41435 575 FLOOR PANEL 242 HK IS CRACKED. FABRICATED NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE. MATERIAL ID; LOCATED AND COUNTERSUNK HOLES; POTTED INSERTS; POTTED EDGES; COMPLETED CURE; SANDED; APPLIED ANTI-SKID AND PART MARKED IAW DWG SRZ 25-005; REV "H". 2L72 4F RTA35EU 20090402 NM 2009 4 2 UALA2009032700899120090325A3350Z010H000520A DIRECTOR AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE NR 1 MALFUNCTIONED A UALAK NONE O OTHER ININSP/MAINT 1 WP29822UA 948 REF LOG NR 3 ON EMERGENCY LIGHTS REMAIN ON WITH POWER OFF. ACCP TEST OF EMERGENCY LIGHT SYSTEM FROM FWD PANEL. FAULT SHOWS EMERGENCY LIGHT L INTERNAL LOAD FAULT AND NO COMM FAULTS WITH FWD, MID & AFT EPSU'S. REPLACED NR 1 CIDS DIRECTOR, LIGHTS CHK OK. 2L72 4F4 FRTA28NM E40NE 20090402 NM 2009 4 2 UALA2009032700900120090326A335020131A POWER SUPPLY BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29177UA 24384 LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP. TWO MOST FORWARD LIGHT ASSY'S. REPLACED POWER SUPPLY. 2L74 4F4 FRTA20WE E24NE 20090402 NM 2009 4 2 UALA2009032700901120090326A335078961 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29177UA 24384 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 3A AFT LIGHT ASSY. RELAMPED 2L74 4F4 FRTA20WE E24NE 20090402 NM 2009 4 2 UALA2009032700902120090326A335078941 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29177UA 24384 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 5J AFT LIGHT ASSY. RELAMPED 2L74 4F4 FRTA20WE E24NE 20090402 EU 2009 4 2 UALA2009032700903120090326A3397 WIRE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE CABIN BROKEN A UALAK NONE L NO TEST ININSP/MAINT 1 WP29415UA 475 EMERGENCY EXIT LIGHT TEST FAULTS L FWD EPSU WITH EXT LOAD FWD L FAULT. FOUND DOOR 1L SLIDE LIGHTS INOP. SUSPECT WIRE HARNESS BETWEEN SLIDE AND DOOR. REPAIRED BROKEN WIRE, SYSTEM TESTS OKAY. 2L72 4F4 FRTA28NM E40NE 20090402 NM 2009 4 2 2ARF 20090301 120090322A2421976J2528 GENERATOR DOUG MD80 MD83 3023681NM PWA JT8 JT8D219 52053NE LEFT FAILED W 2ARFA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 SW23838AM151413572 49397 27733C AIRCRAFT RETURNED DUE TO APU GENERATOR FAILED AT FL 270 AND LT GENERATOR WAS DEFERRED. MX PERFORMED APU GENERATOR RESET AND TESTED IAW 49-00-00 AND LT GENERATOR WAS REPLACED AND TESTED IAW AMM 24-20-02, ALL CORRECT. 2L72 4F4 FRT E9NE 20090402 NM 2009 4 2 ASMF 20090304 120090322A2120 UNKNOWN BOEING737 73776Q 13845AANM CFMINTCFM567CFM567B22 13802NE CABIN SMOKE W ASMFC ABORTED TAKEOFF BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TOTAKEOFF 1 SW23855AM1425714257 33792 890977 ACFT REJECTED TAKEOFF AT 80 KNOTS DUE TO SMOKE IN THE CABIN. THE ACFT WAS SENT TO THE HANGAR AND MX PERFORMED SMOKE IN THE CABIN SOURCE UNKNOWN PROCEDURE IAW FIM 21-00 TASK 806 AND WATER SEPARATOR PACK LT AND RT WERE REPLACED IAW AMM 21-51-05, ALL CORRECT. A HIGH ENERGY STOP INSPECTION WAS NOT NECESSARY, LIMITS WERE NOT EXCEEDED IAW MM 05-51-07. 2L72 4F4 FRTA16WE E00055EN 20090402 EU 2009 4 2 FDEA200903180948 120090318A5321SRZ25005REVG132QFLOOR PANEL AIRBUS300 A300B4622R 3930312EU ZONE 100 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21726FD 575 FWD CARGO PIT FLOOR PANEL 132QF IS BROKE IN HALF. FABRICATED FWD PIT FLOOR PANEL 132QF PER A300-600 DRW SRZ-25-005 REV G. 2L72 4F RTA35EU 20090402 EU 2009 4 2 FDEA200903180949 120090318A5313A53833366206 STRINGER AIRBUS300 A300B4622R 3930312EU ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21750FD 555 FOUND CORROSION ON STRINGER P 37LT, C 39/40 REPAIR PERFORMED BY BLEND OUT THE CORROSION, NDT FOR CRACK FREE CONDITION IAW RAS 70517791/007/2008 ISS A, APPROVED BY EA 6-5310-120190. 2L72 4F RTA35EU 20090402 EU 2009 4 2 FDEA200903180950 120090318A5312 BULKHEAD AIRBUS300 A300B4622R 3930312EU ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21750FD 555 FOUND TOOLING MARK AT AFT PRESSURE BULKHEAD RIM BETWEEN ME1-ME2 REPAIR PERFORMED BY BLEND OUT AND FASTENER CHANGE IAW RAS/DAHAM/4026750/2008 ISS B, APPROVED BY EA 6-5310-120178. 2L72 4F RTA35EU 20090402 EU 2009 4 2 FDEA200903180951 120090318A5330A53970399200 BUTTSTRAP AIRBUS300 A300B4622R 3930312EU ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21750FD 555 FOUND DAMAGED HOLES IN STRUCTURE AT FRAME C 58, P 4-5 RT REPAIR PERFORMED BY CUT THE BUTT STRAP, INSTALL A COUPLING SHEET AND BUSHS IAW RAS/EFW/9000140/2008 ISS A, APPROVED BY EA 6-5310-120212. 2L72 4F RTA35EU 20090402 EU 2009 4 2 FDEA200903180952 120090318A5220A53970875201 PANEL AIRBUS300 A300B4622R 3930312EU EMERGENCY DOOR CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21750FD 555 FOUND CHAFING MARKS ON EMERGENCY EXIT CROSS SHEET PANEL C 56-56A, P 14-15A REPAIR PERFORMED BY BLEND OUT THE AREA IAW RAS/EFW/9000141/2008 ISS C, APPROVED BY EA 6-5310-120165. 2L72 4F RTA35EU 20090402 EU 2009 4 2 FDEA200903180953 120090318A5210A53611513 FAILSAFE AIRBUS300 A300B4622R 3930312EU PAX DOOR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21750FD 555 FOUND CORROSION IN RT FWD PAX DOOR FAIL SAFE RING. REPAIR PERFORMED BY REPLACEMENT OF FAILSAFE RING IAW RAS 70517390/041/2009 ISS A, APPROVED BY EA 6-5310-120177. 2L72 4F RTA35EU 20090402 NM 2009 4 2 FDEA200903180955 120090318A5315652083844 FLOORBEAM BOEING727 7272D4 138407UNM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21288FE 21850 MAIN CARGO DECK FLOORBEAM UPPER "T " BS 1130 HAS CORROSION BETWEEN LBL25 AND LBL46. CUTOUT CORRODED SECTION IAW SRM 53-10-8 FIG 10 (SHEET 9). HFEC INSPECTED IAW NTM 51-00-19 PT.6, NO CRACK INDICATION NOTED. FABRICATED FILLER FROM 7075-T6 .156. FABRICATED DOUBLER ON MAE TRAVELER NR T9/784510 TREATED AND PRIMED IAW SRM 51-20-2. INSTALLED BOUBLER AND FILLER IAW SRM 51-30-2. CLASSIFIED MAJOR REPAIR. 2L73 4F A3WE 20090402 WP 2009 4 2 FDEA200903180956 120090318A5730ARB2912502 SKIN DOUG DC10 DC1030F 3023504WP ZONE 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21317FE 46835 RT WING LEADING EDGE FOUND CRACK ON SKIN L/E LOWER SIDE. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 SHT 2 VOL I. 2L73 4F RTA22WE 20090402 WP 2009 4 2 FDEA200903180957 120090318A5753ANB73942 SUPPORT FITTING DOUG DC10 DC1010F 3022111WP RT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE2168053 47807 RT WING INBD FLAP SUPPORT STRUCTURE FOUND FITTING P/N ANB7394-502 WITH GOUGE AND 4 ATTACHMENT HOLES (FOR ANB7118-502 FITTING) WITH CORROSION ON BORES AND ON LUG FACES. REPAIRED AREA IAW EA 8-5340-128544. 2L73 4F A22WE 20090402 NM 2009 4 2 BQVA2009031600001120090316A793030506031 REGULATOR AMD FALC50FALCON2000 2730170NM CFE CFE73811B NE OIL PRESSURE MALFUNCTIONED E BQVAO OTHER J WARNING INDICATION CRCRUISE 1 EA01797CM4308 4308 51 P105218 NR 2 ENGINE OIL PRESSURE AT BOTTOM OF GREEN ARC ON GAUGE, 60 PSI. 2L72 4F4 FRTA50NM E44NE 20090402 NM 2009 4 2 UALA2009032700905120090326A2150762A000004 ACTUATOR AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE LT AC PACK FAULTY A UALAK NONE O OTHER UKUNKNOWN 1 WP29802UA 690 CREW REPORTS LEFT PACK IS OVERHEATING AND HAVING MULTIPLE PROBLEMS. REPLACED LEFT PACK AIR OUTLET FLAP ACTUATOR REPLACED RT PACK INLET DOOR ACTUATOR BECAUSE RT INLET DOOR ACTUATOR WAS CYCLING BACK AND FORTH. INSTALLED NEW AIR INLET DOOR (FLAP) ACTUATOR, OPS CK OK. 2L72 4F4 FRTA28NM E40NE 20090402 NM 2009 4 2 FDEA200903180958 120090318A5347 SEAT TRACK BOEING757 75723A 1384967NM ZONE 200 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21917FD 24291 STA 418-440 RBL 45 SEAT TRACK GOUGED. REMOVED SEAT TRACK AT STA 418-440 RBL 45 FOUND TO BE DAMAGED AND SEVERAL DOUBLE HOLES (6) EACH IAW SRM 51-40-2. FABRICATED NEW SEAT TRACK IAW SRM 53-00-52 FIG 201. INSTALLED NEW SEAT TRACK IAW SRM 51-40-2 AND SRM 53-00-52 FIG 201 AT STA 418-440 RBL 45. THIS REPAIR IS A CATEGORY "A" MAJOR REPAIR. 2L72 4F RTA2NM 20090402 EU 2009 4 2 UALA2009032700906120090326A2720 CONTROL CABLE AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE RUDDER OUT OF RIG A UALAK NONE O OTHER ININSP/MAINT 1 WP29424UA 506 FOUND RUDDER CABLES OUT OF RIG. WITH RUDDER TRIM ZERO AND RIG PINS IN AFT CABLE QUADRANT AND MIXER OF FEEL AND CENTERING UNIT FREE FIT CANNOT INSERT RIG PIN IN FWD CABLE QUADRANT-CABLE TENSION REGULATOR. STARTED CABLE ADJUSTMENT. CABLE THAT NEEDS TO BE SHORTENED MARKED WITH TAPE. RIGGED RUDDER CONTROL CABLES. WORK COMPLETE. 2L72 4F4 FRTA28NM E40NE 20090402 NM 2009 4 2 FDEA200903180959 120090318A5347 SEAT TRACK BOEING757 75723A 1384967NM ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21917FD 24291 STA 377.0-440 LBL 45 SEAT TRACK REQUIRES REPLACEMENT PER CUSTOMER REQUEST. REMOVED SEAT TRACK AT STA 377-440 LBL 45 IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK IAW SRM 53-10-52. INSTALLED NEW SEAT TRACK AT STA 377-440 LBL 45 IAW SRM 51-40-02. THIS REPAIR IS A CATEGORY "A" MAJOR REPAIR. 2L72 4F RTA2NM 20090402 NM 2009 4 2 FDEA200903210982 120090321A5347AEA732523 SEAT TRACK DOUG MD11 MD11F 3023600NM BS 1401 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21588FE 48490 CABIN, LT STA 1401 TO STA 1461, X= 8 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107. 2L73 4F RTA22WE 20090402 NM 2009 4 2 FDEA200903210983 120090321A5347AEA732523 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21588FE 48490 CABIN, RT STA 1401 TO STA 1426, X= -8 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107. 2L73 4F RTA22WE 20090402 NM 2009 4 2 FDEA200903210984 120090321A5744ARC050311 BRACKET DOUG MD11 MD11F 3023600NM LT WING TE FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21588FE 48490 LT WING OTBD FLAP OTBD FWD HINGE SIDE LINK BARREL NUT HOLE FOUND CORRODED. COMPLIED WITH EA 1-5750-127792. CLASSIFIED AS A MAJOR REPAIR AS PER GMM 6-2-100 REV. 107. 2L73 4F RTA22WE 20090402 NM 2009 4 2 FDEA200903210985 120090321A5347AEA732516 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21588FE 48490 CABIN, LT STA 1299 TO STA 1309, X= 75 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107. 2L73 4F RTA22WE 20090402 NM 2009 4 2 UALA2009032700907120090325A3397 CONNECTOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN LOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29178UA 24385 EMERGENCY EXIT GREEN STRIP LIGHT SEAT 42KJH INOP. EEL LIGHT PLUG LOOSE SO RECONNECTED THE PLUG AND THEN OPERATIONAL CHECKED GOOD. 2L74 4F4 FRTA20WE E24NE 20090402 NM 2009 4 2 FDEA200903210986 120090321A5347AEA732523 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21588FE 48490 CABIN, RT STA 1279 TO STA 1299, X= -8.5 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107. 2L73 4F RTA22WE 20090402 NM 2009 4 2 FDEA200903210987 120090321A5347AEA732523 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21588FE 48490 CABIN, RT STA 1305 X= -8.5 SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107. 2L73 4F RTA22WE 20090402 NM 2009 4 2 FDEA200903210988 120090321A5347AEA732523 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21588FE 48490 CABIN, LT STA 1325 TO STA 1381, X= 8.5 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107 2L73 4F RTA22WE 20090402 NM 2009 4 2 FDEA200903210989 120090321A5347AEA732516 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21588FE 48490 CABIN, LT STA 1331 X= 75 SEAT TRACK FOUND CORRODED. SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107. 2L73 4F RTA22WE 20090402 NM 2009 4 2 UALA2009032700908120090327A33501317 LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29178UA 24385 RT OVERWING EMERGENCY EXIT LIGHT INOP, 3RD FROM FWD END. RELAMPED, OPS CHECK OKAY. 2L74 4F4 FRTA20WE E24NE 20090402 NM 2009 4 2 FDEA200903220990 120090322A5320AJC71662 VERTICAL SUPPORT DOUG MD11 MD11F 3023600NM ZONE 300 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21588FE 48490 AFT FUSELAGE LOWER COMPARTMENT RT VERTICAL STIFFENER AT APPROX STA 2007 UPPER EDGE FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 53-00-01 FIG. 9 VOL. I REV. 40. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 107. 2L73 4F RTA22WE 20090402 NM 2009 4 2 FDEA200903220991 120090322A5347AEA732516 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21588FE 48490 CABIN, LT STA 1341 TO STA 1361 X= 75, SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIG. I VOL. I REV. 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107. 2L73 4F RTA22WE 20090402 2009 4 2 UALA2009032700909420090327A3418285T110423 CIRCUIT CARD BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE STALL WARNING FAULTY A UALAK NONE N FALSE WARNING UKUNKNOWN 1 WP29673UA 29241 STATUS MESSAGE WARN ELEX . TRIED NEW PWR SUPPLY, NO HELP. SWAPPED LEFT AND RIGHT PWR SUPPLY, NO HELP. SWAP LEFT AND RIGHT STALL WARNING CARDS, NO HELP. LEFT FAULT CODE D9, RIGHT FAULT CODE C1, F/O STICK SHAKER INOP DURING RIGHT STALL WARNING TEST. REPLACED RIGHT STALL WARNING CARD AND TESTED. ALSO REPLACED RIGHT STICK SHAKER. OPS NORMAL. 2L72 4F4 FRTA1NM E24NE 20090402 2009 4 2 UALA2009032700915420090326A3120 UNKNOWN BOEING737 737322 1384676NM CFMINTCFM56 CFM563C1 13802EU COCKPIT FAILED A UALAA UNSCHED LANDING O OTHER UKUNKNOWN 1 WP29328UA 24148 F/O'S INSTRUMENTS FAILED INFLIGHT WITH SEVERAL OTHER FAILURES OF SYSTEMS. AC DIVERTED TO PIT. 2L72 4F4 FRTA16WE E21EU 20090402 NM 2009 4 2 UIEA200900022 120090325A575365B08548604 SUPPORT FITTING BOEING747 74747UF 1384812NM TE FLAP FAILED A UIEAK NONE E VIBRATION/BUFFET ININSP/MAINT 1 EA15499MC 29260 DENT ON OUTBOARD AFT FLAP NOSE AND MID FLAP DUE TO OUTBOARD FLAP FITTING FAILURE. REPAIRED PER SRM 51-70-17. REPLACED SUPPORT ARM. 2L74 4F RTA20WE 20090402 NM 2009 4 2 UIEA200900023 120090328A8012 START VALVE BOEING747 74747UF 1384812NM NR 3 ENGINE MALFUNCTIONED A UIEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15408MC 29261 DIVERSION: AFTER TAKEOFF EICAS MESSAGE "START CUTOUT 3" DISPLAYED AT APPROX 11,000 FEET, ALSO STATUS MESSAGE "ENG-3 START VALVE". TRANSFERRED TO DMI M09-016 PER MEL 80-11-1. START VALVE TO BE OPERATED MANUALLY UNTIL FINAL REPAIR IS PERFORMED. 2L74 4F RTA20WE 20090402 EU 2009 4 2 USAA2009033090711120090327A3350F100066000 LENS AIRBUS320 A320232 3930326EU CABIN MISSING A USAAK NONE O OTHER ININSP/MAINT 1 EA19668AW 1764 FLT 456 - SLC - EEL - EMERGENCY LIGHT LENS COVER R1 LOWER FORWARD OFF. MAINTENANCE REPLACED THE R1 EMERGENCY LIGHT LENS. 2L72 4F RTA28NM 20090402 EU 2009 4 2 USAA2009033090712120090328A5210FE277000 CYLINDER AIRBUSA321 A321211 3930370EU SERVICE DOOR LOW PRESSURE A USAAK NONE O OTHER ININSP/MAINT 1 EA19171US27206505 1465 FLT 1546-CLT - AFT RIGHT SERVICE DOOR EMERGENCY ASSIST CYLINDER BELOW WEEKLY LIMITS. SERVICED AFT RIGHT DOOR EMERGENCY ASSIST CYLINDER PER AIRBUS MAINTENANCE MANUAL 52-10-00. 2L72 4F RTA28NM 20090402 EU 2009 4 2 USAA2009033090713120090328A5210FE174004 CYLINDER AIRBUS320 A320231 3930325EU L2 DOOR LOW PRESSURE A USAAK NONE O OTHER ININSP/MAINT 1 EA19629AW538705379 76 FLT 350 - LAS - EMERGENCY EQUIPMENT - L2 DOOR EMERGENCY CYLINDER / ACCUMULATOR PRESSURE LOW. SERVICED L2 DOOR EMERGENCY CYLINDER PER AIRBUS MAINTENANCE MANUAL 52-10-00-614-001. 2L72 4F RTA28NM 20090402 EU 2009 4 2 USAA2009033090714120090329A5210FE240004 CYLINDER AIRBUSA321 A321211 3930370EU DOOR LOW PRESSURE A USAAK NONE J WARNING INDICATION NRNOT REPORTED 1 EA19169UW288785008 1455 FLT 752 - SEA - EMERGENCY EQUIPMENT - RED CAUTION LIGHTS ILLUMINATED ON CIDS PANEL FOR MID-R DOOR LOW PRESSURE. MAINTENANCE SERVICED DOOR ASSIST DAMPER IAW AIRBUS MAINTENANCE MANUAL 52-10-00. 2L72 4F RTA28NM 20090402 NM 2009 4 2 USAA2009033090715120090328A53136545776 STRINGER BOEING737 7373B7 138447FNM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19529AU 24411 CLT - C4 - MAJOR REPAIR - CORROSION ON STRINGER 27L AT BS 1016. REPAIRED STRINGER 27L AT BS 1016 IAW B737 SRM 53-00-03. 2L72 4F RTA16WE 20090402 EU 2009 4 2 USAA2009033090716120090328A33502514355 LENS AIRBUSA319 A319112 3930323EU CABIN MISSING A USAAK NONE O OTHER ININSP/MAINT 1 EA19725UW 1135 FLT 1181 - DTW-CLT - EMERGENCY LIGHTS - EMERGENCY EXIT LIGHT COVER MISSING ON SEAT 10C. BULBS ARE OPERATING NORMAL. REMOVED AND REPLACED LENS ON EMERGENCY LIGHT ON ROW 10C. 2L72 4F RTA28NM 20090402 EU 2009 4 2 USAA2009033090717120090314A5320D5347112420300 SHEAR PLATE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19655AW 1075 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, -Y1732. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, -Y1732 IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20090402 EU 2009 4 2 USAA2009033090718120090314A5315D53472193200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19655AW 1075 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR70, -Y765 IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20090402 EU 2009 4 2 USAA2009033090719120090314A5315D53472190203 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19655AW 1075 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66 + 5 INCHES, -Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66 + 5 INCHES, -Y765 IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20090402 EU 2009 4 2 USAA2009033190723120090314A5320D53480020342 COVER AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19655AW 1075 SAL - C7 - MAJOR REPAIR - CRACK ON COVER SHEET TRAY BETWEEN FR68 TO FR69, Y1732. REPLACED COVER SHEET TRAY BETWEEN FR68 TO FR69, Y1732 IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20090402 NM 2009 4 2 USAA2009033190724120090324A5320 INTERCOSTAL BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19246AY 23898 BFM - C4 - MAJOR REPAIR - LEVEL 2 CORROSION ON INTERCOSTAL BETWEEN BS 1241 TO BS 1263, S29L. REPLACED INTERCOSTAL BETWEEN BS 1241 TO BS 1263, S29L IAW B767 SRM 51-40-02, 51-10-00, 51-40-05, & 51-20-01. 2L72 4F RTA1NM 20090402 NM 2009 4 2 USAA2009033190725120090323A5313146T3003 STRINGER BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19246AY 23898 BFM - C4 - MAJOR REPAIR - LEVEL 2 CORROSION ON STRINGER BETWEEN BS 1535 TO BS 1562, S38L. REPLACED STRINGER BETWEEN BS 1535 TO BS 1562, S38L IAW B767 SRM 53-00-03. 2L72 4F RTA1NM 20090402 NM 2009 4 2 USAA2009033190726120090328A5313146T3002 STRINGER BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19246AY 23898 BFM - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON STRINGER AT BS 1540, S34L. REPLACED STRINGER AT BS 1540, S34L IAW B767 SRM 53-00-03. 2L72 4F RTA1NM 20090402 NM 2009 4 2 USAA2009033190727120090328A5322 SHEAR TIE BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19246AY 23898 BFM - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON SHEAR TIE AT BS 1562 BETWEEN S38L TO S39R. REPLACED SHEAR TIE AT BS 1562 BETWEEN S38L TO S39R IAW B767 SRM 53-00-07 & 51-40-02. 2L72 4F RTA1NM 20090402 NM 2009 4 2 USAA2009033190728120090328A5320 STRUCTURE BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19246AY 23898 BFM - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON T-CHORD AT BS 1562 BETWEEN S38L TO S39R. REPLACED T-CHORD AT BS 1562 BETWEEN S38L TO S39R IAW B767 SRM 53-00-07 & 51-40-02. 2L72 4F RTA1NM 20090402 EU 2009 4 2 USAA2009033190729120090324A5330 SKIN AIRBUS330 A330323 3940030EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19271AY 323 BFM - MAJOR REPAIR - C1 CHECK - CORROSION ON FUSELAGE SKIN AND BELLY FAIRING SUPPORT STRUCTURE AT FRAME 40 BOTTOM FLANGE RT SIDE. REPLACED FUSELAGE SKIN AND BELLY FAIRING SUPPORT STRUCTURE AT FRAME 40 BOTTOM FLANGE RT SIDE IAW A330 SRM 51-42-11. 2L72 4F RTA46NM 20090402 NM 2009 4 2 USAA2009033190730120090329A5322 SHEAR TIE BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19246AY 23898 BFM - C4 - MAJOR REPAIR - LEVEL 2 CORROSION ON SHEAR TIE AT BS 1540 BETWEEN S38L TO S39L. REPLACED SHEAR TIE AT BS 1540 BETWEEN S38L TO S39L IAW B767 SRM 53-00-07 & 51-40-02. 2L72 4F RTA1NM 20090402 NM 2009 4 2 USAA2009033190731120090328A5322 SHEAR TIE BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19246AY 23898 BFM - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON SHEAR TIE AT BS 1540 BETWEEN S37L TO S38L. REPLACED SHEAR TIE AT BS 1540 BETWEEN S37L TO S38L IAW B767 SRM 51-40-02. 2L72 4F RTA1NM 20090402 NM 2009 4 2 USAA2009033190732120090328A5322 SHEAR TIE BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19246AY 23898 BFM - C4 - MAJOR REPAIR - LEVEL 2 CORROSION ON SHEAR TIE AT BS 1540 BETWEEN S39L TO S39R. REPLACED SHEAR TIE AT BS 1540 BETWEEN S39L TO S39R IAW B767 SRM 51-40-02 & 53-00-07. 2L72 4F RTA1NM 20090402 NM 2009 4 2 USAA2009033190733120090323A5347145T5213 SEAT TRACK BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19246AY 23898 BFM - C4 - MAJOR REPAIR - LEVEL 2 CORROSION ON SEAT TRACK BETWEEN BS 1043 TO BS 1087 AT RBL 88.5. REPLACED SEAT TRACK BETWEEN BS 1043 TO BS 1087 AT RBL 88.5 IAW B767 SRM 53-00-52, 51-40-05, & 53-00-52. 2L72 4F RTA1NM 20090402 NM 2009 4 2 USAA2009033190734120090320A5322 SHEAR TIE BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19246AY 23898 BFM - C4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SHEAR TIE AT BS 1540 BETWEEN S36L TO S37L. REPLACED SHEAR TIE AT BS 1540 BETWEEN S36L TO S37L IAW B767 SRM 51-40-02 & 51-10-02. 2L72 4F RTA1NM 20090402 NM 2009 4 2 USAA2009033190735120090320A5322 SHEAR TIE BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19246AY 23898 BFM - C4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SHEAR TIE AT BS 1540 BETWEEN S38R TO S39R. REPLACED SHEAR TIE AT BS 1540 BETWEEN S38R TO S39R IAW B767 SRM 51-40-02 & 51-10-02. 2L72 4F RTA1NM 20090402 NM 2009 4 2 USAA2009033190736120090327A531314673003 STRINGER BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19246AY 23898 BFM - C4 - MAJOR REPAIR - LEVEL 2 CORROSION ON STRINGER BETWEEN BS 1510 TO BS 1540, S39R. REPAIRED STRINGER BETWEEN BS 1510 TO BS 1540, S39R IAW B767 SRM 51-10-02, 53-00-03 & 51-40-02. 2L72 4F RTA1NM 20090402 NM 2009 4 2 USAA2009033190737120090327A5313146T3003 STRINGER BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19246AY 23898 BFM - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON STRINGER BETWEEN BS 1510 TO BS 1540, S39L. REPAIRED STRINGER BETWEEN BS 1510 TO BS 1540, S39L IAW B767 SRM 53-00-03. 2L72 4F RTA1NM 20090402 NM 2009 4 2 USAA2009033190738120090329A5340 STRINGER CLIP BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19246AY 23898 BFM - C4 - MAJOR REPAIR - LEVEL 2 CORROSION ON STRINGER CLIP AT BS 1540, S39L. REPLACED STRINGER CLIP AT BS 1540, S39L IAW B767 SRM 51-40-02. 2L72 4F RTA1NM 20090402 NM 2009 4 2 USAA2009033190739120090329A5340 STRINGER CLIP BOEING767 767201 1385125NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19246AY 23898 BFM - C4 - MAJOR REPAIR - LEVEL 2 CORROSION ON STRINGER CLIP AT BS 1540, S38L. REPLACED STRINGER CLIP AT BS 1540, S38L IAW B767 SRM 51-40-02. 2L72 4F RTA1NM 20090402 NM 2009 4 2 USAA2009033190740120090328A5753113N380083 FLAP BOEING757 757225 1384959NM LT WING DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19923UW 22203 CLT - C1 - MAJOR REPAIR - DELAMINATION ON LEFT OUTBOARD AFT FLAP AT INBOARD END. REPAIRED LEFT OUTBOARD AFT FLAP AT INBOARD END IAW B757 SRM 51-70-17. 2L72 4F RTA2NM 20090402 NM 2009 4 2 USAA2009033190741120090319A5320 INTERCOSTAL BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19923UW 22203 CLT - C1 - MAJOR REPAIR - CRACK ON INTERCOSTAL AT BS 660, S15L. REPAIRED INTERCOSTAL AT BS 660, S15L IAW BOEING DRAWING 143N8385 & US AIRWAYS EO 5304R143. 2L72 4F RTA2NM 20090402 NM 2009 4 2 USAA2009033190742120090319A5320 INTERCOSTAL BOEING757 757225 1384959NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19923UW 22203 CLT - C1 - MAJOR REPAIR - CRACK ON INTERCOSTAL AT BS 660, S15R. REPAIRED INTERCOSTAL AT BS 660, S15R IAW BOEING DRAWING 143N8385 & US AIRWAYS EO 5304R143. 2L72 4F RTA2NM 20090402 NM 2009 4 2 WRLA2009088 120090328A5420 ANGLE DOUG MD11 MD11 3023602NM NR 3 PYLON CRACKED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277WA 48743 DURING C3 CHECK IN TPE INSPECTION FOUND: CRACK ON NR 3 ENG PYLON INTERNAL ANGLE AT STA 180 (REF GET N/R U05032). REPLACED THE INTERNAL ANGLE PER MD-11 SRM 51-35-01 VOL 2 REV 40. JOB COMPLETED AND CONDITION CHECK NORMAL. 2L73 4F RTA22WE 20090402 NM 2009 4 2 WRLA2009090 120090330A5720 DOUBLER DOUG MD11 MD11 3023602NM LT WING CRACKED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11277WA 48743 DURING C3 CHECK IN TPE INSPECTION FOUND: CRACK ON THE DB DOUBLER FASTENER AREA OF THE LEFT WING OUTBOARD FIXED CAVITY AT STA XOS627 (REF EGAT N/R U05035). REPAIR THIS CRACKED AREA B PER MD-11 SRM 57-00-01 VOL 1 FIG 10 REV 40. PERFORM ET INSPECTION FOR CUTOUT AREA AND ANGLE PARTS HEAT TREAT. REFER TO JOB CARD ATTACHING SHEET NR 079580. JOB COMPLETED AND CONDITION CHECK NORMAL. 2L73 4F RTA22WE 20090402 NM 2009 4 2 YENA20090331030 120090330A2120 DUCT EMB ERJ190ERJ190100IGW3260408NM CONDITIONED AIR DISCONNECTED A YENAA UNSCHED LANDING O OTHER CRCRUISE 1 EA15279JB 190000090 FLT 1263, BOS-AUS, DIVERTED TO IAD, COCKPIT AIR TO COLD CABIN AIR TOO HOT AND UNBEARABLE. FOUND CONDITIONED AIR SUPPLY DUCT TO FORWARD CABIN DISCONNECTED AT H DUCT. RE-SECURED SAME IAW AMM 21-20-03-400. PERFORMED PAX CABIN TEMP CONTROL TEST IAW AMM 21-62-00-710. OPS CHECK OK. PERFORMED COCKPIT TEMP CONTROL TEST IAW AMM 21-61-00-710. OPS CHECK OK. 2L72 4F RTA57NM 20090402 2009 4 2 YENA20090331031 420090328A25651040051 LIGHT EMB ERJ190ERJ190100IGW3260408NM EVAC SLIDE INOPERATIVE A YENAK NONE L NO TEST ININSP/MAINT 1 EA15203JB3101 190000023 ON EMERGENCY EVAC SLIDE ASSY SCHEDULED T/C E190-25-65-01-720-801 AFT LT FUNCTIONAL TEST EVAC SLIDE PASSED INFLATION TEST BUT SLIDE LAMPS DID NOT ILLUMINATE. REMOVED AND REPLACED LEFT PAX DOOR EMERGENCY EVAC SLIDE IAW T/C E190-25-65-01-400-801-ALH. ALL CHECKS GOOD. 2L72 4F RTA57NM 20090402 NM 2009 4 2 ZZDA2009102 120090323A5220 RELEASE MECH BOEING717 717200 1383700NM TAILCONE MISINSTALLED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO37991AT 55135 FOUND TAIL CONE RELEASE CAM ASSEMBLY AND LANYARD IMPROPERLY STOWED. PERFORMED T/C 414A, 415, 417, 418 & 419 FOR TAIL CONE OPERATIONAL CHECK & PROPER ROUTING OF TAIL CONE LANYARD. OK TO RETURN TO SERVICE. 2L72 4F TRA6WE 20090402 NM 2009 4 2 ABXA200904010018 120090329A2120 UNKNOWN BOEING767 767232 1385132NM CARGO BAY ODOR A ABXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL23745AX 22222 AFTER T/O, LOADMASTER REPORTED UNUSUAL SMELL IN THE CARGO AREA. RETURNED FOR LANDING. FIRE DEPT TESTED AIR AND FOUND OK. LOADMASTER INSPECTED THE FREIGHT AND FOUND NO DAMAGE. UPPER CARGO COMPARTMENT IS CLEAR AT THIS TIME. NO FREIGHT WAS IN BELLY. 2L72 4F RTA1NM 20090402 EA 2009 4 2 ASOA200900352 120090228A2400 UNKNOWN CNDAIRCL600 CL6002B19 1900309EA FIRE A ASOAH DEACTIVATE SYST/CIRCUITS AB FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27830AS 7236 WITH AC EXTERNAL SELECTED ON BATT BUS, CAPT AND F/O ON BOARD PERFORMING PRE FLT DUTIES, OBSERVED A RUSHING AIR SOUND, COCKPIT AND FED CABIN QUICKLY FILLED WITH SMOKE. EXTERNAL AC WAS DE-SELECTED AND BATT TURNED OFF. WHILE EXITING A/C, FIRE WAS OBSERVED PENETRATING A/C SKIN AFT OF CAPT SIDE WINDOW. 2L72 4F RTA21EA 20090402 EU 2009 4 2 DATA200900001 120090331A2910SD3730749XA HYDRAULIC LINE STBROSSD3 SD330 8100602EU HYDRAULIC SYS RUPTURED E DATAO OTHER J WARNING INDICATION TOTAKEOFF 1 GL132629P SH3079 IMMEDIATELY AFTER THE GEAR WAS SELECTED UP, BOTH THE HYDRAULIC LIGHTS CAME ON THE CENTRAL WARNING PANEL. THE GEAR WAS SELECTED DOWN. THREE RED WAS SHOWN ON THE GEAR INDICATION. AN EMERGENCY WAS DECLARED. THE EMERGENCY GEAR HANDLE WAS PULLED PER THE CHECK LIST. THE CREW MADE A 45 DEGREE BANK AND HEARD THE GEAR LOCK. THE AIRCRAFT WAS LANDED AT DTW ON 21L WITHOUT INCIDENT. THE GEAR WAS PINNED AND TOWED OFF THE RUNWAY BACK TO RAMP. 2H72 4T A41EU 20090402 NM 2009 4 2 HNAA2009033100102120090327A3310F18T5WWRS LIGHT DHAV DHC8 DHC8102 2809003NM CABIN SPARKS A HNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA07937HA50965 148 FLIGHT ATTENDANT REPORTS SPARKS COMING FROM SIDEWALL OVERHEAD LIGHT SWITCH AT FLIGHT ATTENDANT POSITION. HAPPENED ONCE. MAINT INSPECTED AND FOUND 3 BULBS OUT. NO OTHER DEFECTS NOTED. RELAMPED, OPS CHECK GOOD. 2H72 4T RTA13NM 20090402 NM 2009 4 2 HNAA2009033100103120090330A335082410162007 CONTROL BOX DHAV DHC8 DHC8102 2809003NM CABIN FAULTY A HNAAO OTHER O OTHER CLCLIMB 1 EA07329EN35326 290 EMERGENCY LIGHTS FLICKER WHEN SELECTING GEAR UP OR DOWN. REMOVED AND REPLACED EMERGENCY LIGHTS CONTROL BOX IN ACCORDANCE WITH 33-51-00. AIRCRAFT RELEASED FOR EVALUATION FLIGHT DUE TO EMERGENCY LIGHTS FLICKER DURING GEAR EXTENSION AND RETRACTION. MAINTENANCE ACTION COMPLETE, EVALUATION SATISFACTORY. 2H72 4T RTA13NM 20090402 EA 2009 4 2 HNAA2009040200104120090327A2497MS3459L2222P CONNECTOR DHAV DHC8 DHC8311 1386006EA NR 2 GENERATOR SHORTED A HNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA07336EN37764 336 NR 2 AC GENERATOR CAUTION LIGHT ILLUMINATED DURING TAKEOFF ROLL. REJECTED TAKEOFF. CYCLED GENERATOR SWITCH IN ACCORDANCE WITH ABNORMAL EMERGENCY CHECKLIST, LIGHT RESET AND GENERATOR OPERATES NORMAL. REMOVED AND REPLACED CONNECTOR 2421-P2 IN ACCORDANCE WITH MAINTENANCE MANUAL 20-45-06, OPS CHECK GOOD. 2H72 4T RTA13NM 20090402 EU 2009 4 2 IPXA09155249 120090328A5753A57960000007 SKIN AIRBUSA300 A300F4622R 3930360EU TE FLAP DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01144UP 0827 INSPECTION TYPE:N/A RT INBOARD FLAP LOWER SURFACE HAS SEVERAL DENTS. DAMAGE LOCATION BETWEEN RIB 9A THRU 10A AND RIB 14 THRU 15A. REPAIRED PER EO A300-5750-32921-A. 2L72 4F RTA35EU 20090402 EU 2009 4 2 IPXA09155251 120090325A5610 MECHANISM AIRBUSA300 A300F4622R 3930360EU SLIDING WINDOW LACK OF LUBE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01124UP 0808 INSPECTION TYPE:4C F/O'S SLIDING WINDOW DOES NOT OPEN F