N310SW
Registered owner: WINGS AIR HELICOPTERS LLC, NY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| WINGS AIR LLC (W1ZA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
397 reports on file, 1995-02-06 – 2012-05-01.
Part: SKIN — CRACKED (FUSELAGE) · airframe 83,704 hrs · 76,382 cycles
SKIN CRACKED AT BS 690, STR 10L. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (BS 582) · airframe 83,129 hrs · 75,935 cycles
FUSELAGE SKIN CRACKED AT BS 582, STR 10R. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (R1 DOOR) · airframe 82,859 hrs · 75,747 cycles
DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR FUSELAGE SKIN CRACKED AT UPPER AFT CORNER. REMOVED AND REPLACED DOOR IAW MM.
Part: LENS — CRACKED (CABIN) · airframe 82,859 hrs · 75,747 cycles
DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN LENS CRACKED. REMOVED AND REPLACED LENS ASSY PER MM.
Earlier reports · 1995–2011 · 393 reports
2011
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 82,177 hrs · 75,229 cycles
LEFT EMEGENCY LIGHT LENS MISSING AT ROW 20. INSTALLED LENS PER MM.
Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 81,601 hrs · 74,779 cycles
L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MM AND MT.
Part: SKIN — CRACKED (FUSELAGE) · airframe 81,170 hrs · 74,442 cycles
DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 294.5+13, STR 23R. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 81,173 hrs · 74,443 cycles
DURING SCHEDULED SPV CHECK FOUND, SKIN CRACKED AT BS 294.5+13, STR 23R. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 81,170 hrs · 74,442 cycles
DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED BS 294.5+13, STR 23R. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 80,439 hrs · 73,874 cycles
DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 735E, STR 14R. REPAIRED SKIN PER EA.
2010
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO FLOOR SUPPORT CORRODED AT BS 859, RBL 13. REPAIRED SUPPORT PER EA.
Part: BEAM — CRACKED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND LONGITUDINAL BEAM UPPER CHORD CRACKED AT BS 662, LBL 24.5. REPAIRED BEAM PER ER AND EA.
Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND CARGO FLOOR SUPPORT CORRODED AT BS 859, LBL 3. REPAIRED SUPPORT PER EA.
Part: HINGE FITTING — CRACKED (L2 DOOR) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND L2 DOOR UPPER HINGE FITTING CRACKED. REMOVED AND REPLACED FITTING PER SRM AND BAC DWG.
Part: SLAT — DELAMINATED (LT WING) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND LT WING NR 1 SLAT T/E DELAMINATED. REMOVED AND REPLACED NR 1 SLAT PER MM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 986.5, BETWEEN STR 23R TO STR 24R. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 1. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND STRINGER CORRODED AT BS 933, STR 25L. REPAIRED STRINGER PER EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER ER.
Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 25L. REMOVED AND REPLACED CLIP PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: FRAME — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND FRAME CORRODED AT BS 947, RBL 17. REPAIRED FRAME PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: SLAT — DELAMINATED (LT WING) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND LT WING NR 2 SLAT I/B TRAILING EDGE CORNER DELAMINATED. REMOVED AND REPLACED NR 2 SLAT PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 907, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.
Part: SKIN — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND SKIN CORRODED AT BS 986.5, BETWEEN STR 23R TO STR 24R. REPAIRED SKIN PER SWA EA.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.
Part: SPLICE — CRACKED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND VERTICAL BEAM SPLICE CRACKED AT BS 727, LBL 45. REMOVED AND REPLACED SPLICE PER SRM AND BAC DWG.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 887, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727C, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND STRINGER CORRODED AT BS 782, STR 26R. REPAIRED STRINGER PER SRM.
Part: FRAME — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND FRAME CORRODED AT BS 727E, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED FRAME PER SRM AND BAC DWG.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND STRINGER CORRODED AT BS 995, STR 25L. REMOVED AND REPLACED STRINGER PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727C, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: FITTING — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND TIE FITTING CORRODED AT BS 1016, STR 23L. REMOVED AND REPLACED FITTING PER SRM AND BAC DWG.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 24.8. REMOVED AND REPLACED BEAM PER SRM AND BAC DWG.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 490 TO BS 500A, STR 28R. REPAIRED STRINGER PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8R. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 12L. REMOVED AND REPLACED CLIP PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED BETWEEN BS 847 TO BS 727. REPAIRED SHEAR TIE PER SRM.
Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND RT KEEL BEAM CORRODED AT BS 807. REPAIRED BEAM PER SRM.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND LT SPLICE ANGLE CRACKED AT BS 540, BETWEEN STR 21L TO STR 22L. REMOVED AND REPLACED ANGLE PER BAC DWG.
Part: SKIN — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND SKIN CORRODED AT BS 964, STR 27R. REPAIRED SKIN PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, BETWEEN STR 27R TO STR 28R. REPAIRED SHEAR TIE PER SRM.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND STRINGER CORRODED AT BS 964, STR 27R. REPAIRED STRINGER SECTION PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 26L. REPAIRED CLIP PER SRM.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND STRINGER CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED STRINGER PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED CLIP PER SRM.
Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 79,362 hrs · 73,076 cycles
DURING SCHEDULED 26Y CHECK, FOUND RT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER MM.
Part: SIGN — INOPERATIVE (CABIN) · airframe 78,998 hrs · 72,779 cycles
L1 DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED SIGN PER MM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 78,389 hrs · 72,319 cycles
DURING SCHEDULED MV2 CHECK, FOUND FRAME CRACKED AT BS 767, BETWEEN STR 23L TO STR 23R. REPAIRED FRAME PER EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 78,199 hrs · 72,186 cycles
DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 287, STR 15L. REPAIRED SKIN PER SRM.
Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 78,188 hrs · 72,176 cycles
L1 DOOR EVACUATION SLIDE FEEL OUT OF CONTAINER. DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.
Part: SKIN — CRACKED (FUSELAGE) · airframe 77,543 hrs · 71,720 cycles
DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 740.5B TO BS 745.5, STR 2R. REPAIRED SKIN PER AAR EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 77,543 hrs · 71,720 cycles
DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 728D TO BS 734D, STR 2R. REPAIRED SKIN PER AAR EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 77,543 hrs · 71,720 cycles
DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 743C TO BS 744C, STR 2R. REPAIRED SKIN PER AAR EA.
Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 77,543 hrs · 71,720 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED SPLICE PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 77,543 hrs · 71,720 cycles
DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 905, STR 5R. REPAIRED SKIN PER AAR EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 77,543 hrs · 71,720 cycles
DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 905, BETWEEN STR 3L TO STR 4L. REPAIRED SKIN PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 77,400 hrs · 71,612 cycles
DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500B, STR 1. REPAIRED FRAME PER AAR EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 77,400 hrs · 71,612 cycles
DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500D, STR 20L. REPAIRED FRAME PER AAR EA.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 77,400 hrs · 71,612 cycles
DURING SCHEDULED SPV CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP CRACKED AT BS 1016, STR 7R. REPAIRED DOME CAP PER AAR EA.
Part: BATTERY — DISCHARGED (CABIN) · airframe 77,400 hrs · 71,612 cycles
DURING SCHEDULED SPV CHECK, FOUND EMERGENCY EXIT LIGHTS INOP. CHARGED BATTERY PER MM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 77,400 hrs · 71,612 cycles
DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 520, STR 20L. REPAIRED FRAME PER AAR EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 77,400 hrs · 71,612 cycles
DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500D, STR 20R. REPAIRED FRAME PER AAR EA.
2009
Part: TRIM TAB — DELAMINATED (AILERON) · airframe 77,273 hrs · 71,511 cycles
DURING SCHEDULED MV3 CHECK, FOUND RT WING AILERON TRIM TAB DELAMINATED. REMOVED AND REPLACED TRIM TAB PER MM.
Part: TAB — CRACKED (AILERON) · airframe 76,913 hrs · 71,225 cycles
DURING SCHEDULED HC2 CHECK, FOUND RT WING AILERON TAB CRACKED. REMOVED AND REPLACED TAB PER MM.
Part: FLAP — DELAMINATED (RT WING) · airframe 76,799 hrs · 71,132 cycles
DURING SCHEDULED MV1 CHECK, FOUND RT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,698 hrs · 71,052 cycles
DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 76,698 hrs · 71,052 cycles
DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 15. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,438 hrs · 70,132 cycles
DURING SCHEDULED MV2 CHECK, FOUND RT AFT WING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 75,438 hrs · 70,132 cycles
DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 867, STR 2R. REPAIRED SKIN PER SWA EA.
2008
Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,935 hrs · 69,074 cycles
DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.
Part: COVER — MISSING (CABIN) · airframe 73,832 hrs · 69,006 cycles
FOUND EMERGENCY EXIT LIGHT ON BULLNOSE MISSING COVER AT ROW 15 DEF. REPLACED COVER PER MM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 73,757 hrs · 68,956 cycles
DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, BETWEEN RBL 44 TO LBL 43, WL 208. REPAIRED BEAM PER PAE ER.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 73,757 hrs · 68,956 cycles
DURING SCHEDULED 24Y CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED AT BS 1016, BETWEEN STR 6L TO 7L. REPAIRED WEB PER PAE ER.
Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND LT KEEL BEAM CORRODED AT BS 733. REMOVED AND REPLACED BEAM PER PAE ER.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND ANGLE CORRODED BETWEEN BS 219 TO BS 203, LBL 14, WL 156. REMOVED AND REPLACED ANGLE PER SRM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 5R. REPAIRED WEB PER PAE ER.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1014, STR 7L. REMOVED AND REPLACED CLIP PER SRM.
Part: WIRE — OUT OF POSITION (CABIN) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND LT AFT EMERGENCY EXIT LIGHT IDENTIFIER WIRES PULLED OUT OF SPLICES. RESPLICED WIRES PER WDM.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 729A TO BS 733A, STR 26R. REPAIRED STRINGER PER SRM.
Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND BULKHEAD CHORD CORRODED AT BS 270, LBL 8 TO LBL 10, WL 208. REMOVED AND REPLACED CHORD PER SRM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CRACKED AT BS 328, RBL 11, WL 206. REPAIRED BEAM PER PAE ER.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 2, WL 208. REPAIRED BEAM PER PAE ER.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 787 + 4, STR 27R. REPAIRED STRINGER PER PAE ER.
Part: SKIN — CRACKED (FUSELAGE) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 500D + 16, STR 7R. REPAIRED SKIN PER PAE ER.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 344, RBL 17. REMOVED AND REPLACED TIE PER SRM.
Part: STINGER — CORRODED (FUSELAGE) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 354, STR 25R. REPAIRED STRINGER PER SRM.
Part: SKIN — CRACKED (HORIZ STAB) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND LT HORIZ STAB LOWER SKIN CRACKED AT BS 134.00. REMOVED AND REPLACED LT HORIZ STAB PER MM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 25L AND STR 26L. REPAIRED SHEAR TIE PER SRM.
Part: FRAME — CRACKED (BS 360 S14L) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 360, STR 14L. REPAIRED FRAME WEB PER SRM.
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO DOOR AFT FRAME CRACKED AT UPPER END. REMOVED AND REPLACED FRAME PER BOEING DRAWING AND SRM.
Part: STRINGER SPLICE — CORRODED (BS 907 S24L) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, STR 24L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.
Part: SHEAR TIE — CRACKED (BS 520 S22R) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 22R. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO DOOR AFT FRAME CRACKED AT LOWER END. REMOVED AND REPLACED FRAME PER BOEING DRAWING AND SRM.
Part: FITTING — CORRODED (L1 DOOR GIRT BAR) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.
Part: FLOORBEAM — CORRODED (BS 294) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 294.5, LBL 10.5. REPAIRED FLOORBEAM CHORD PER SRM.
Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 867, STR 26L. REPAIRED STRINGER SPLICE PER SRM.
Part: STRINGER CLIP — CRACKED (BS 277 S15R) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER — CRACKED (BS 360 S14L) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND STRINGER 14L CRACKED AT BS 360. REPAIRED STRINGER PER SRM.
Part: STRINGER CLIP — CRACKED (BS 260 S12L) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 260, STR 12L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 787 S26L) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: SHEAR TIE — CRACKED (BS 967 S7L) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 73,738 hrs · 69,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SKIN DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM.
Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 73,738 hrs · 69,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND RT WING OUTBOARD FORE FLAP UPPER SKIN DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM.
Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,738 hrs · 68,940 cycles
DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 73,212 hrs · 68,546 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 583, STR 10L. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 72,918 hrs · 68,331 cycles
DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 323, STR 20R. REPAIRED SKIN PER SWA EA.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,169 hrs · 67,776 cycles
DURING SCHEDULED SERVICE CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: SKIN — CORRODED (FUSELAGE) · airframe 72,169 hrs · 67,776 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 520, STR 28L. REPAIRED SKIN PER SRM.
Part: SKIN — DELAMINATED (L/E SLAT) · airframe 72,169 hrs · 67,776 cycles
DURING SCHEDULED SERVICE CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED AT UPPER SURFACE. REPAIRED SLAT PER SRM.
Part: LENS — OUT OF POSITION (CABIN) · airframe 71,707 hrs · 67,432 cycles
RIGHT OVERWING EMERGENCY EXIT SIGN LENS FELL OFF. INSTALLED LENS PER MM.
2007
Part: GLOWSTRIP — MISSING (CABIN) · airframe 71,207 hrs · 67,065 cycles
DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP MISSING AT ROW 1 DEF. INSTALLED STRIP PER MM.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,207 hrs · 67,065 cycles
DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,207 hrs · 67,065 cycles
DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
Part: TORQUE TUBE — WORN (MLG WW) · airframe 71,207 hrs · 67,065 cycles
DURING SCHEDULED C3 CHECK, FOUND LEFT WING T/E FLAP, FLAP DRIVE MOTOR TORQUE TUBE WORN. REMOVED AND REPLACED TORQUE TUBE PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 71,135 hrs · 67,010 cycles
DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 277 AND BS 299, STR 22R AND STR 23R. REPAIRED SKIN PER SWA EA.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 71,135 hrs · 67,010 cycles
DURING SCHEDULED OTS CHECK, FOUND STRINGER 28R CORRODED AT BS 322. REPAIRED STRINGER PER SRM.
Part: WINDOW — ARCED (COCKPIT) · airframe 71,080 hrs · 66,969 cycles
FLIGHT DECK L1 WINDOW ARCING. REMOVED AND REPLACED WINDOW AND WINDOW HEAT CONTROLLER PER MM.
Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 70,683 hrs · 66,682 cycles
L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
Part: GIRT BAR — LOOSE (FUSELAGE) · airframe 70,298 hrs · 66,373 cycles
DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.
Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 70,298 hrs · 66,373 cycles
DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 70,298 hrs · 66,373 cycles
DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,298 hrs · 66,373 cycles
DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 69,466 hrs · 65,734 cycles
FUSELAGE SKIN CRACKED AT BS 514C, STR 8R. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 69,466 hrs · 65,734 cycles
FUSELAGE SKIN CRACKED AT BS 503C, STR 8R. REPAIRED SKIN PER SWA EA.
Part: SHEAR TIE — CRACKED (BS 360 S26L) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 26L. REPAIRED SHEAR TIE PER ER.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED 10Y CHECK, FOUND AFT CABIN BATTERY CHARGER INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.
Part: SKIN — CRACKED (BS 514D) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514D, STR 12R. REPAIRED SKIN PER ER.
Part: SKIN — CRACKED (BS 304) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 304, STR 10L. REPAIRED SKIN PER ER.
Part: SKIN — CRACKED (FUSELAGE) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 296, STR 14R. REPAIRED SKIN PER ER.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 420, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 380, STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 24L. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: STRINGER CLIP — CRACKED (BS 727D) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER — CRACKED (BS 500D S19R) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER 19R CRACKED AT BS 500D. REPAIRED STRINGER SECTION PER SRM.
Part: STRINGER — CRACKED (BS 360-440 S20R) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STR 20R CORRODED AT BS 360 TO BS 440. REMOVED AND REPLACED STRINGER SECTION PER SRM.
Part: SHEAR TIE — CRACKED (BS 420 S21R) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 420, STR 21R. REPAIRED SHEAR TIE PER SRM.
Part: STRINGER SPLICE — CORRODED (BS 908 S22L) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 22L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.
Part: STRINGER CLIP — CRACKED (BS 727B S7R) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 727C S3R) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER — CRACKED (BS 504) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER 14L CRACKED AT BS 504. REMOVED AND REPLACED STRINGER SECTION PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER 22L CRACKED AT BS 1010. REMOVED AND REPLACED STRINGER SECTION PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 13R. REPAIRED FRAME SECTION PER SWA EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 13R. REPAIRED FRAME SECTION PER SWA EA.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER 24L CRACKED AT BS 987. REMOVED AND REPLACED STRINGER SECTION PER SRM.
2006
Part: FRAME — CRACKED (FUSELAGE) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 13R. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 13R. REPAIRED FRAME PER SWA EA.
Part: STRINGER CLIP — CRACKED (BS 807 S4L) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: FRAME — CRACKED (BS 807 S4L) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 4L. REPAIRED FRAME SECTION PER SRM.
Part: FRAME — CRACKED (BS 727C S8R) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727C, STR 8R. REPAIRED FRAME SECTION PER SWA EA.
Part: STRINGER CLIP — CRACKED (BS 747 S6L) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 685 S4R) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 727C S4L) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: FRAME — CRACKED (BS 597 S8R) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME SECTION PER SWA EA.
Part: STRINGER CLIP — CRACKED (BS 747 S4R) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 727A S5-L-R) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5R AND 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 727D S5L) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 727C S6R) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 685 S10L) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 727D S7L) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 597 S9R) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 727B S5R) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 727D S5R) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 727A S7L) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 616 S5R) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 767 S6L) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 727E S7L) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 747 S10R) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8L. REPAIRED FRAME SECTION PER SWA EA.
Part: STRINGER CLIP — CRACKED (BS 727E S5R) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 597 S9L) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME SECTION PER SWA EA.
Part: STRINGER CLIP — CRACKED (BS 727E S4L) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 597 S8L) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 727D S6L) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 68,646 hrs · 65,107 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME SECTION PER SWA EA.
Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 68,419 hrs · 64,920 cycles
DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
Part: SKIN — CRACKED (BS 525) · airframe 68,419 hrs · 64,920 cycles
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 525, STR 1. REPAIRED SKIN PER SWA EA.
Part: SHEAR TIE — CRACKED (BS 360 S15R) · airframe 68,001 hrs · 64,580 cycles
DURING SCHEDULED MV1 CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 15R. REPAIRED SHEAR TIE PER SRM.
Part: SKIN — CRACKED (BS 498 S26L) · airframe 68,001 hrs · 64,580 cycles
DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 498, STR 26L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (BS 485 S26L) · airframe 68,001 hrs · 64,580 cycles
DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 485, STR 26L. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (BS 465 S16R) · airframe 68,001 hrs · 64,580 cycles
DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 465, STR 16R. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (BS 505A S26L) · airframe 68,001 hrs · 64,580 cycles
DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505A, STR 26L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (BS 365 S16R) · airframe 68,001 hrs · 64,580 cycles
DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 365, STR 16R. REPAIRED SKIN PER SWA EA.
Part: GLOWSTRIP — CRAZED (CABIN) · airframe 67,439 hrs · 64,122 cycles
DURING SCHEDULED C3 CHECK, EEPLS PHOTOLUMINESCENT STRIP CRAZED AT ROW 13 ABC TO ROW 15 ABC. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 67,439 hrs · 64,122 cycles
DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 513 B, STR 19R. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (BS 426 S28L) · airframe 67,439 hrs · 64,122 cycles
DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 426, STR 28L, NR 1 RADIO ALTIMETER ANTENNA. MX FERRY TO DHN FOR REPAIRS. REPAIRED SKIN PER EA.
Part: STRUCTURE — CRACKED (FWD SERVICE DOOR) · airframe 67,439 hrs · 64,122 cycles
DURING SCHEDULED C3 CHECK, FOUND FWD SERVICE DOOR FRAME GUIDE ARM CUTOUT CRACKED AT UPPER RADIUS. REMOVED AND REPLACED FWD SERVICE DOOR PER MM.
Part: FITTING — LOOSE (L2 DOOR) · airframe 67,439 hrs · 64,122 cycles
DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FLOOR FITTING LOOSE. SECURED EVAC SLIDE FLOOR FITTING PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 67,119 hrs · 63,882 cycles
DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503, STR 16L. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 67,119 hrs · 63,882 cycles
DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 980, STR 21L. REPAIRED SKIN PER SWA EA AND SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 67,119 hrs · 63,882 cycles
DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506, STR 16L. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 67,119 hrs · 63,882 cycles
DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 513, STR 15L. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (BS 405 S26L) · airframe 67,060 hrs · 63,839 cycles
DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 405, STR 26L. REPAIRED SKIN PER SWA EA AND SRM.
Part: SKIN — CRACKED (BS 925 S25L) · airframe 67,060 hrs · 63,839 cycles
DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 925, STR 25L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 66,844 hrs · 63,667 cycles
DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 16L. REPAIRED SKIN PER SRM AND SWA EA.
Part: CENTERING MECH — INOPERATIVE (FLT CONTROLS) · airframe 66,828 hrs · 63,653 cycles
AIRCRAFT FLIGHT CONTROLS DIFFICULT, AIRCRAFT WOULD NOT ROTATE WITH NORMAL CONTROL INPUTS, HAD TO PULL YOKE FURTHER THAN NORMAL. CONTROLS NORMAL WITH AUTOPILOT ENGAGED. CONTROLS SENSITIVE ON LANDING. REMOVED AND REPLACED ELEVATOR FEEL CENTERING MECHANISM PER MM.
Part: SKIN — CRACKED (BS 460) · airframe 66,499 hrs · 63,412 cycles
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 460, STR 16L. REPAIRED SKIN PER SWA EA & SRM.
Part: TORQUE TUBE — BROKEN (RT WING TE FLAPS) · airframe 66,337 hrs · 63,294 cycles
T/E FLAP POSITION INDICATOR INOP. REMOVED AND REPLACED TORQUE TUBE BETWEEN NR 5 & NR 6 JACKSCREWS & FLAP POSITION INDICATOR PER MM.
Part: SHEAR TIE — CORRODED (BS 847) · airframe 66,174 hrs · 63,175 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 847, BL 0. REPAIRED SHEAR TIE PER SRM.
Part: SHEAR TIE — CORRODED (BS 867) · airframe 66,174 hrs · 63,175 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 867, BL 0. REPAIRED SHEAR TIE PER SRM.
Part: SHEAR TIE — CORRODED (BS 767) · airframe 66,174 hrs · 62,175 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, LBL 8. REPAIRED SHEAR TIE PER SRM.
Part: STRINGER — CORRODED (BS 374-380) · airframe 66,174 hrs · 62,175 cycles
DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CORRODED BETWEEN BS374 TO BS380, STR 28L. REPAIRED STRINGER IAW SRM.
Part: BULKHEAD — CORRODED (BS 1016) · airframe 66,174 hrs · 62,175 cycles
DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 AFT PRESSURE BULKHEAD WEB CORRODED ON RT FWD LOWER SIDE OF BL 0. REPAIRED WEB PER BAC DRAWING & SWA EA.
Part: STRINGER — CORRODED (BS 837-887) · airframe 66,174 hrs · 62,175 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CORRODED BETWEEN BS 867 TO BS 887, STR 26R. REPAIRED STRINGER PER SRM.
Part: STRINGER — CORRODED (BS 374-380) · airframe 66,174 hrs · 63,175 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CORRODED BETWEEN BS 374 TO BS 380, STR 27L. REMOVED AND REPLACED STRINGER SECTION PER SRM.
Part: REPAIR — CORRODED (BS 365-370) · airframe 66,174 hrs · 63,175 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN INTERNAL DOUBLER CORRODED BETWEEN BS 365 TO BS 370, STR 28L. REPAIRED DOUBLER PER SWA EA.
Part: SHEAR TIE — CORRODED (BS 787) · airframe 66,174 hrs · 63,175 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, BL 0. REPAIRED SHEAR TIE PER SRM.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,174 hrs · 63,175 cycles
DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: SPLICE — CORRODED (BS 351) · airframe 66,174 hrs · 63,175 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER SPLICE CORRODED AT BS 351, STR 27L. REMOVED AND REPLACED SPLICE PER SRM.
Part: SKIN — CRACKED (BS 732B) · airframe 66,174 hrs · 63,175 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 732B, STR 14R. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (BS 771) · airframe 66,174 hrs · 63,175 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 771, STR 14R. REPAIRED SKIN PER SWA EA.
Part: FRAME — CRACKED (BS 303) · airframe 66,174 hrs · 63,175 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, STR 16L. REPAIRED FRAME PER BAC DRAWING & SRM.
Part: STRINGER CLIP — CRACKED (BS 947) · airframe 66,174 hrs · 63,175 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 945) · airframe 66,174 hrs · 63,175 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 945, STR 26R. REMOVED AND REPLACED CLIP PER SRM.
Part: SHEAR TIE — CORRODED (BS 967) · airframe 66,174 hrs · 63,175 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 967, RBL 3. REPAIRED SHEAR TIE PER SRM.
Part: FLOORBEAM — CORRODED (BS 732A) · airframe 66,174 hrs · 63,175 cycles
DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 732A, RBL 3. REPAIRED FLOORBEAM PER SWA EA.
Part: FLOORBEAM — CORRODED (BS 729B) · airframe 66,174 hrs · 63,175 cycles
DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 729B, RBL 3. REPAIRED FLOORBEAM PER SWA EA.
Part: STRINGER CLIP — CRACKED (AFT CARGO) · airframe 66,174 hrs · 63,175 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 947.5, STR 26R. REMOVED AND REPLACED CLIP PER SRM.
Part: WEB — CRACKED (BS 665) · airframe 66,174 hrs · 63,175 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BEADED PRESSURE WEB CRACKED AT BS 665, BETWEEN LBL 40 TO LBL 43. REPAIRED WEB PER SWA EA.
Part: BULKHEAD — CRACKED (BS 1016) · airframe 66,174 hrs · 63,175 cycles
DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BLKHD WEB CRACKED NEXT TO DOME CAP AT STR 15L, STR 18R AND STR 21R. REPAIRED WEB PER SRM.
2005
Part: LENS — BROKEN (CABIN) · airframe 65,648 hrs · 62,738 cycles
DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.
Part: SKIN — DELAMINATED (LT WING FOREFLAP) · airframe 65,648 hrs · 62,738 cycles
DURING SCHEDULED C1 CHECK, FOUND LT WING OTBD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.
Part: SKIN — CRACKED (BS 445-500B) · airframe 65,007 hrs · 62,220 cycles
DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 445 & BS 500B, STR 18R TO STR 19R. REPAIRED SKIN PER SRM & SWA EA.
Part: SKIN — CRACKED (BS 773-787) · airframe 65,007 hrs · 62,220 cycles
DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 773 & BS 787, STR 18L TO STR 19L. REPAIRED SKIN PER SRM & SWA EA.
Part: SKIN — CRACKED (BS 480-518) · airframe 65,007 hrs · 62,220 cycles
DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT STR 16L, BETWEEN BS 480 & BS 518. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (BS 455) · airframe 64,896 hrs · 62,136 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 455, STR 16L. REPAIRED SKIN PER SWA EA & SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 64,694 hrs · 61,985 cycles
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 750 TO BS 757, STR 18L TO STR 20L. REPAIRED SKIN PER SRM.
Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 64,694 hrs · 61,985 cycles
DURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 63,716 hrs · 61,190 cycles
DURING SCHEDULED C3 CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS AT BS 430 TO BS 450, NR 3 & NR 4 RADIO ALTIMETER ANTENNA'S CUT OUTS. REPAIRED SKIN PER SWA EA.
Part: SLIDE — OUT OF ADJUST (R1 & R2 DOOR) · airframe 63,538 hrs · 61,044 cycles
R1 & R2 DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 63,180 hrs · 60,764 cycles
DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACK AT BS 480, STR 17L. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 63,180 hrs · 60,764 cycles
DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506, STR 16L. REPAIRED SKIN PER SWA EA.
Part: CONTROL PANEL — FAULTY (CABIN PRESSURE) · airframe 63,134 hrs · 60,729 cycles
DECENDING THROUGH 7000 FT, OUTFLOW VALVE WENT TO FULL OPEN & CABIN DIFF PRESSURE INDICATED ZERO. REMOVED AND REPLACED CABIN PRESSURE CONTROL PANEL PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 62,800 hrs · 60,465 cycles
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 947, STRINGER 20L, CRACKED. REPAIRED SKIN PER SRM.
Part: SKIN — DELAMINATED (NR 3 SPOILER) · airframe 62,800 hrs · 60,465 cycles
DURING SCHEDULED C2 CHECK, FOUND LT WING NR 3 SPOILER DELAMINATED. REMOVED AND REPLACED LT WING NR 3 SPOILER PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 62,800 hrs · 60,465 cycles
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 805, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 62,800 hrs · 60,465 cycles
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 427, STRINGER 17L, CRACKED. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 62,800 hrs · 60,465 cycles
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 358, STRINGER 18R, CRACKED. REPAIRED SKIN PER EA.
2004
Part: GUSSET — CRACKED (FUSELAGE) · airframe 62,074 hrs · 59,909 cycles
DURING SCHEDULED RON, FOUND NLG ACTUATOR SUPPORT FITTING GUSSET CRACKED. REMOVED AND REPLACED NLG ACTUATOR SUPPORT GUSSET PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 62,062 hrs · 59,899 cycles
TWO EACH FUSELAGE SKIN CRACKS AT BS 432, STRINGER 17L AND BS 495, STRINGER 16R. REPAIRED SKIN SECTIONS PER EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 61,831 hrs · 59,712 cycles
DURING SCHEDULED C1 CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS BETWEEN BS 435 AND BS 485, STRINGER 26R. REPAIRED SKIN SECTIONS PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 61,831 hrs · 59,712 cycles
DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 944, STRINGER 22R, CRACKED. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 61,831 hrs · 59,712 cycles
DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 480, STRINGER 17R, CRACKED. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 61,738 hrs · 59,633 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727D, STRINGER 20L, CRACKED. REPAIRED SKIN PER EA.
Part: LENS — MISSING (CABIN) · airframe 60,930 hrs · 58,960 cycles
DURING SCHEDULED C4 CHECK, FOUND RT EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED RT LIGHT LENS PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 60,652 hrs · 58,748 cycles
DURING SERVICE CHECK, FOUND FUSELAGE SKIN BELOW R1 DOOR AT TEXAS PATCH, CRACKED. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 60,652 hrs · 58,748 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 307, STRINGER 18R, CRACKED. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 60,652 hrs · 58,748 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 500D + 5, STRINGER 15R, BS 500C + 5, STRINGER 15R, CRACKED. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 60,126 hrs · 58,340 cycles
DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 744, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 60,126 hrs · 58,340 cycles
DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN BS 500A, STRINGER 4R, CRACKED. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 59,921 hrs · 58,181 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 460, WL 208 LT SIDE. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 59,859 hrs · 58,137 cycles
DURING SCHEDULED A1 CHECK, FOUND 3 IN LONG FUSELAGE SKIN CRACK BETWEEN BS 500 -500A, STRINGER 21R. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 59,859 hrs · 58,137 cycles
DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500 AND BS 500A, STRINGER 21R. REPAIRED SKIN PER SRM.
Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 59,499 hrs · 57,855 cycles
EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 17 ABC. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.
2003
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 58,180 hrs · 56,789 cycles
DURING SCHEDULED C1 CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED ON AFT SIDE AT STR 5R. REPAIRED BULKHEAD WEB PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 58,180 hrs · 56,789 cycles
DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) BS 747 AT STR 19R, BS 757 AT STR 19R AND BS 797 AT STR 18L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 58,120 hrs · 56,737 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 455, STR 26L. REPAIRED SKIN PER SRM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 616,WL 206 AND RBL 66. REPAIRED FLOORBEAM PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (3 EA) BETWEEN STR 8L AND STR 9L, BS'S 480, 767 AND 867. REPAIRED FRAMES PER BFG ER.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (4 EA) BETWEEN STR 8R AND STR 9R, BS'S 440, 380, 847 AND 867. REPAIRED FRAMES PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (4 EA) BETWEEN STR 8R AND STR 9R, BS'S 440, 380, 847 AND 867. REPAIRED FRAMES PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (4 EA) BETWEEN STR 8R AND STR 9R AT BS'S 400, 500A, 827 AND 887. REPAIRED FRAMES PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (4 EA) BETWEEN STR 8R AND STR 9R, BS'S 440, 380, 847 AND 867. REPAIRED FRAMES PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (4 EA) BETWEEN STR 8R AND STR 9R, BS'S 440, 380, 847 AND 867. REPAIRED FRAMES PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED (3 EA) BETWEEN STR 8L AND STR 9L, BS'S 400, 827 AND 907. REPAIRED FRAMES PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 296, WL 208.5 AND RBL 55. REPAIRED FRAME PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, BETWEEN STR 8R AND STR 9R. REPAIRED FRAME PER BFG ER.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 1091, WL 285 AND LBL 38. REMOVED AND REPLACED FUSELAGE FRAME SECTION PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 3R. REPAIRED FRAME PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED (4 EA) BS 440 AT STR 8R, BS 520 AT STR 8L, BS 597 AT STR 11L AND BS 706 AT STR 11L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 400, STRINGER 4R. REPAIRED STRINGER PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 26R AND STR 27R. REPAIRED SHEAR TIE PER SRM.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND STRINGER CORRODED AT BS 807 + 1, STR 25R. REPAIRED STR PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND STRINGER TIE CLIPS CRACKED (2 EA) BS 727C AT STR 5R AND BS 727D AT STR 2R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED (5 EA) AT BS 727B AT STR 7L, BS 663 AT STR 10L, BS 500D AT STR 8L, BS 380 AT STR 8L AND BS 360 AT STR 5L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 26L AND 27L. REPAIRED SHEAR TIE PER SRM.
Part: ATTACH FITTING — CORRODED (HORIZONTAL STAB) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND HORIZ STAB ATTACH FITTING FWD AND AFT SPAR LUGS CORRODED AT RT SIDE. REPAIRED ATTACH FITTING PER SRM.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND STRINGERS CRACKED (3 EA) AT BS 380 AT STR 8L, BS 400 AT STR 8L AND BS 706 AT STR 11R. REPAIRED STRINGERS PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: ATTACH FITTING — CORRODED (GIRT BAR) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD ATTACH FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER MM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 500C, STR 8L. REPAIRED STRINGER PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND BOTH LT AND RT OUTBD FRAMES CRACKED AT BS 188, WL 207. REMOVED AND REPLACED BOTH LT AND RT FRAMES PER SRM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORRODED AT BS 312, WL 208 AND LBL 11 TO RBL 11. REPAIRED FLOORBEAM PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND STRINGER TIE CLIPS CRACKED (3 EA) AT BS 500D AT STR 4R, BS 500B AT STR 9L AT BS 727C AT STR 7L. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM.
Part: SPLICE — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND STRINGER TIE CLIPS CRACKED (2 EA) AT BS 500D AT STR 7R AND BS 420 AT STR 4R. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT STR 4R, BS 727E AND BS 7827D. REMOVED AND REPLACED STRINGER CLIPS PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,119 hrs · 56,736 cycles
DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 57,568 hrs · 56,287 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND 3.5 INCH LONG FUSELAGE SKIN CRACK, BS 275, STRINGER 18L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 57,258 hrs · 56,049 cycles
DURING SCHEDULED C4 CHECK, FOUND 4 EA FUSELAGE SKIN CRACKS AT STRINGER 10R, BS 727B+15, BS 727C+12, BS 727D+5, AND BS 727E+13. REPAIRED SKIN PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,261 hrs · 56,053 cycles
DURING SCHEDULED C4 CHECK, FOUND STRINGER TIE CLIPS CRACKED (2 EA) AT STR 10R, BS 727E AND BS 727D. REMOVED AND REPLACED STRINGER TIE CLIPS PER SRM.
Part: CONTROLLER — FAULTY (COCKPIT) · airframe 57,016 hrs · 55,867 cycles
L2 WINDOW ARCING, TURNED OFF WINDOW HEAT, ARCING STOPPED. REMOVED AND REPLACED L2 WINDOW HEAT CONTROLLER AND PWR CHORD PER MM.
2002
Part: SKIN — CRACKED (FUSELAGE) · airframe 56,264 hrs · 55,290 cycles
DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKS (2 EA) AT BS 727E AT STR 10R AND BS 747 AT STR 19L. REPAIRED SKIN PER SRM.
Part: CABLE — MISROUTED (AFT CABIN DOORS) · airframe 56,268 hrs · 55,294 cycles
DURING SCHEDULED C3 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE RELEASE CABLES MISROUTED. REROUTED CABLES PER MM.
Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,150 hrs · 55,189 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 56,150 hrs · 55,189 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 14L. REPAIRED SKIN PER BFG ER AND SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 56,150 hrs · 55,189 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS380, STR 14R. REPAIRED SKIN PER BFG ER.
Part: SKIN — CRACKED (FUSELAGE) · airframe 56,150 hrs · 55,189 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 500A + 11, STR 10L. REPAIRED SKIN PER SRM.
Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,150 hrs · 55,189 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 56,150 hrs · 55,189 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 411, STR 4L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 56,150 hrs · 55,189 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 14R, BS 867 AND BS 897. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 55,264 hrs · 54,448 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND LOWER SKIN CRACKED ON RT HORIZ STAB AFT SPAR AT NR 1 BALANCE BAY. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 55,004 hrs · 54,236 cycles
DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED BETWEEN BS'S 747 AND 767, STR 10R. REPAIRED SKIN PER SWA RA.
Part: FLAP — DELAMINATED (RT WING) · airframe 55,004 hrs · 54,236 cycles
DURING SCHEDULED SERVICE CHECK, FOUND RT OTBD AFT T/E FLAP DELAMINATED AT INBD END. REMOVED AND REPLACED RT OTBD AFT T/E FLAP PER MM.
Part: BUSHING — WORN (LT ELEVATOR) · airframe 54,515 hrs · 53,845 cycles
DURING SCHEDULED PM CHECK, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB BUSHINGS PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,500 hrs · 53,830 cycles
DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727A, ABOVE STR 10R. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,421 hrs · 53,767 cycles
DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 15L, BS'S 390 AND 395. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,421 hrs · 53,767 cycles
DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 18L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,421 hrs · 53,767 cycles
DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 943, STR 24L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,366 hrs · 53,721 cycles
DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 17L. REPAIRED SKIN PER SRM.
Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 53,604 hrs · 53,091 cycles
DURING SCHEDULED C4 CHECK, FOUND RT KEEL BEAM LOWER CHORD CORRODED BETWEEN BS 500C AND 500D, STR 28R. REPAIRED CHORD PER SWA RA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 53,604 hrs · 53,091 cycles
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 770, ABOVE STR 18L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 53,604 hrs · 53,091 cycles
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT STR 10R, BS'S 727C, 750 AND 520. REPAIRED SKIN PER SRM.
2001
Part: WEB — CRACKED (FUSELAGE) · airframe 53,016 hrs · 52,623 cycles
DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS178, RBL 17.1. R&R WEB PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,016 hrs · 52,623 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 15L. REPAIRED FRAME PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,016 hrs · 52,623 cycles
DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL CHORD CRACKED AT BS 178, LBL 5.7 AND WL 185. REPAIRED CHORD PER SWA RA.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,016 hrs · 52,623 cycles
DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14L & 15L. REPAIRED SHEAR TIE PER SRM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 52,848 hrs · 52,473 cycles
DURING SCHEDULED PM CHECK, FOUND EEPLS INOP FWD CABIN. REMOVED AND REPLACED BATTERY PER MM.
Part: LIGHT — LOOSE (CABIN) · airframe 52,696 hrs · 52,350 cycles
DURING SCHEDULED C3 CHECK, FOUND EEPLS LOOSE AT FWD CABIN. SECURED EEPLS PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 52,476 hrs · 52,157 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 1.7 INCH LONG AT BS 523-524, STR 16R. REPAIRED SKIN PER SRM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 52,465 hrs · 52,148 cycles
DURING SCHEDULED RON, FOUND EEPLS INOP AT AFT SECTION OF CABIN. REMOVED AND REPLACED BATTERY PER MM.
Part: BUSHING — WORN (LH ELEVATOR) · airframe 51,917 hrs · 51,682 cycles
DURING SCHEDULED C2 CHECK, LH ELEVATOR TAB FAILED FREE PLAY CHECK. R&R ELEVATOR TAB BUSHINGS PER MM.
Part: BUSHING — WORN (ELEVATOR TAB) · airframe 51,813 hrs · 51,596 cycles
DURING SCHEDULED C2 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB ATTACH BUSHINGS PER MM.
Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 51,813 hrs · 51,596 cycles
DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 51,735 hrs · 51,533 cycles
DURING WALKAROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED ABOVE WINDOW 10R. REPAIRED SKIN PER SRM.
2000
Part: FLAP — DELAMINATED (RT WING) · airframe 49,909 hrs · 49,995 cycles
DURING SCHEDULED C4 CHECK, FOUND RT WING INBD & OTBD FORE FLAPS DELAMINATED. R&R FORE FLAPS PER MM.
Part: WEDGE — DELAMINATED (L/E SLAT) · airframe 49,909 hrs · 49,995 cycles
DURING SCHEDULED C4 CHECK, FOUND NR 2, NR 5 & NR 6 L/E SLAT T/E WEDGES DELAMINATED. R&R SLATS PER MM.
Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 49,909 hrs · 49,995 cycles
DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. READJUSTED EVAC SLIDE ASSY PER MM.
Part: TIRE — SEPARATED (MLG) · airframe 49,010 hrs · 49,222 cycles
DECLARED EMERGENCY. SUSPECT TIRE DELAMINATION DURING ROTATION AT LAS. FOUND NR 1 MLG TIRE DAMAGED. REMOVED AND REPLACED NR 1 MLG TIRE/WHEEL ASSY PER MM.
Part: SCREW — MISSING (EXIT LIGHT) · airframe 48,962 hrs · 49,185 cycles
DURING SCHEDULED C3 CHECK, FOUND FWD SERVICE DOOR EXTERNAL EMERGENCY EXIT LIGHT LENS ATTACH SCREW MISSING. INSTALLED SCREW PER MM.
Part: LIGHT — LOOSE (ROW 11) · airframe 48,938 hrs · 49,164 cycles
DURING SCHEDULE SPECIAL VISIT, FOUND CABIN EGRESS LIGHT LOOSE AT ROW 11. RESECURED LIGHT ASSY PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 48,905 hrs · 49,128 cycles
DURING SCHEDULED RON, FOUND 2 FUSELAGE EXTERNAL SKIN CRACKS, BS 500C, STRINGER 14L, AND JUST BELOW AFT ENTRY DOOR. REPAIRED SKIN PER SRM.
Part: LIGHT — LOOSE (ROW 5) · airframe 48,160 hrs · 48,489 cycles
BULLNOSE EMERGENCY EXIT LIGHT LOOSE AT ROW 5 DEF. SECURED LIGHT ASSY PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 48,123 hrs · 40,461 cycles
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 750, STRINGER 18R. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 48,114 hrs · 48,452 cycles
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 710, STR 17L AND BS 750, STR 18R. REPAIRED SKIN PER SRM.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 47,753 hrs · 48,133 cycles
DURING SCHEDULED A2 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 18 ABC. REMOVED AND REPLACED BATTERY CHARGER PER MM.
Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 47,649 hrs · 48,048 cycles
FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.
Part: SKIN — CRACKED (BS 767 - 787)
DURING SCHEDULED SERVICE CHECK, FOUND 3 INCH LONG CRACK ON FUSELAGE EXTERNAL SKIN. STRINGER 19R, BETWEEN BS 767-787. REPAIRED SKIN PER SRM.
1999
Part: SKIN — CRACKED (BS 847 - 867)
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 847-867, STRINGER 18R. REPAIRED SKIN PER SRM.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND EEPLS FWD SECTION INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: LIGHT — INOP (RT EMER EXIT)
DURING SCHEDULED A1 CHECK, FOUND RT FWD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: BATTERY CHARGER — INOP (CABIN)
DURING SCHEDULED A1 CHECK, FOUND EEPLS INOP AT FWD END. REMOVED AND REPLACED BATTERY CHARGER PER MM.
Part: BULKHEAD — CRACKED (BS 178)
DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD CRACKED AT LBL 9, WL 234. REPAIRED BULKHEAD PER SRM.
Part: FRAME — CRACKED (SERVICE DOOR)
DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR FRAME CRACKED IN AFT LOWER CORNER. REPAIRED FRAME PER BAC DRAWING.
Part: POST — CRACKED (LT COCKPIT)
DURING SCHEDULED 1/2D CHECK, FOUND 0.5 INCH LONG CRACK ON UPPER OUTBD CORNER OF CAPTAIN'S NR 1 WINDOW POST. REPAIRED WINDOW POST PER SWA RA NR 1 A53-1156.
Part: SKIN — CRACKED (SERVICE DOORWAY)
DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED ON AFT SERVICE DOOR, UPPER HINGE ARM CUTOUT. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (SERVICE DOORWAY)
DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED ON FWD SERVICE DOOR, LOWER FWD CUTOUT CORNER. REPAIRED SKIN PER SWA RA NR 1-353-2095.
Part: BRACKET — CORRODED (PASSENGER DOOR)
DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT BOTH FWD ENTRY DOOR GIRT BAR FLOOR ATTACH BRACKETS. REMOVED AND REPLACED BRACKETS PER SRM.
Part: BULKHEAD CHORD — CRACKED (BS 178)
DURING SCHEDULED 1/2D CHECK, FOUND LT AND RT SIDE CHORDS CRACKED, BS 178, BL 26, WL 207. REMOVED AND REPLACED CHORDS PER SRM.
Part: BULKHEAD — CRACKED (BS 178)
DURING SCHEDULED 1/2D CHECK, FOUND LT AND RT SIDE BULKHEAD CRACKED, BS 178, BL 1, WL 189. REPAIRED BULKHEAD PER SRM.
Part: FLOORBEAM — CORRODED (BS 312)
DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAM UPPER T-CAP, BS 312, LBL2. REPAIRED BEAM PER SRM.
Part: FRAME — CRACKED (BS 639)
DURING SCHEDULED 1/2D CHECK, FOUND FRAME CRACKED AT BS 639, BETWEEN STRINGERS 16L-17L. REPAIRED FRAME PER SRM.
Part: SKIN — CRACKED (BS 500)
DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, ABOVE STRINGER 16L. REPAIRED SKIN PER SRM.
Part: FLOORBEAM — CRACKED (BS 660)
DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED, BS 660, BL 0. REPAIRED BEAM PER SWA RA NR 1 -357-0705.
Part: CLIP — CRACKED (BS 663.75)
DURING SCHEDULED 1/2D CHECK, FOUND 2 EA STRINGER CLIPS CRACKED AT BS 663.75, STRINGERS 10L AND 10R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.
Part: FLOORBEAM — CORRODED (BS 1006)
DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM AFT FLANGE, BS 1006, LBL 29. REPAIRED FLOORBEAM PER SRM.
Part: FRAME — CRACKED (BS 616)
DURING SCHEDULED 1/2D CHECK, FOUND 2 BELTFRAMES CRACKED AT BS 616 LT AND RT, WL 208. REPAIRED FRAMES PER SWA TR NR T1-A53-026.
Part: STRINGER — CRACKED (BS 1016)
DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 6L CRACKED AT BS 1016. REPAIRED STRINGER PER SWA RA NR 1-353-2088.
Part: SKIN — CRACKED (BS 947)
DURING SCHEDULED 1/2D CHECK, FOUND A 4 INCH LONG CRACK ON FUSELAGE SKIN, BS 947, BETWEEN STRINGERS 24R-25R. REPAIRED SKIN PER SRM.
Part: BATTERY PACK — DISCHARGED (SERVICE DOOR)
DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: WEB — CRACKED (BS 665)
DURING SCHEDULED A1 CHECK, FOUND BEADED PRESSURE WEB HAVING SEVERAL CRACKS AT BS 665, RBL 40, AND LBL 32. REPAIRED WEB PER SWA RA'S NR 1-353-2054 AND NR 1-353-2053.
Part: STRAP — CRACKED (E & E COMPT)
DURING SCHEDULED BC1 CHECK, FOUND FLOORBEAM STRAPS CRACKED IN E & E COMPT. REPAIRED PER BOEING SRM.
1998
Part: BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED CHECK, FOUND FWD CABIN TRACK EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.
Part: BATTERY PACK — DISCHARGED (PAX DOOR)
DURING SERVICE CHECK, FOUND ON FWD ENTRY DOOR, EMERGENCY LIGHT INOPERATIVE. RESEATED BATTERY PACK PER BOEING MM.
Part: PUMP — FAILED (A HYD SYST)
AIRCRAFT FLT HOU-TUL, DIVERTED INTO DAL DUE TO HYDRAULIC A SYSTEM ENGINE DRIVEN PUMP FAILED IN FLIGHT. REMOVED AND REPLACED ENG DRIVEN HYDRAULIC PUMP PER BOEING MM, LK CHECK AND FUNCTION CHECK GOOD.
Part: STRINGER — CRACKED (BS 727)
DURING SERVICE CHECK, FOUND 2 CRACK IN SKIN AT STRINGER 17, 4 AFT AT BS 727C. REPAIRED PER BOEING SRM.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SCHEDULED RON CHECK, FOUND RT OVER EMERGENCY EXIT DOOR INNER AND LT EXIT OVER WING EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER BOEING MM.
Part: SKIN — CRACKED (GALLEY DOORWAY)
DURING SCHEDULED C3, FOUND AFT GALLEY DOORWAY LOWER HINGE CUTOUT CRACKED. REPAIRED PER BOEING SRM.
1997
Part: SKIN — CRACKED (BS 727)
DURING SCHEDULED TERM CHECK, FOUND RIGHT SIDE FUSELAGE SKIN CRACK APPROX 2 AFT OF BS 727E, AT S18R. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (FUSELAGE)
DURING SCHEDULED TERM CHECK, FOUND A 4 FUSELAGE SKIN CRACK ABOVE AFT CARGO BIN DOOR. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (R2 DOORWAY)
DURING SCHEDULED C4 CHECK, FOUND AFT SERVICE DOOR LOWER FWD HINGE CUTOUT CRACKED. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (L2 DOORWAY)
DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR LOWER FWD AND UPPER FWD HINGE CUTOUTS CRACKED. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (NR 3 LE SLAT)
DURING SCHEDULED BC2 CHECK, FOUND LT WING NR 3 SLAT, LOWER T/E SKIN CRACKED. REPAIRED PER SWA RA 1-A57-0377.
Part: BULKHEAD — CRACKED (BS 178)
DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT THE FOLLOWING LOCATIONS: RBL 4.7 WL 200.5 TO 201, RBL 4.7 WL 198.75 TO 197.5, RBL 6.7 WL 198 TO 198.5 LBL 4.7 WL 198.25 TO 198.5, AT LBL 6.7, WL 200.75 TO 201, RBL 12 TO 12.5 WL 220 , LBL 10 TO 9 WL 218, RBL 4.7 WL 212 TO 212.5, LBL 10.5 WL 218 AND AT LBL 12 TO 12.5, WL 218. REPAIRED ALL PER BOEING SRM.
Part: FRAME — CRACKED (BS 827)
DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, BL 0, WL 148. REPAIRED ALL PER BOEING SRM.
1996
Part: BALLAST — OVERHEAT (AFT LAV)
IN FLIGHT, AIRCRAFT DIVERTED TO PHX DUE TO CHEMICAL SMELL IN AFT CABIN AREA. AIRCRAFT LANDED AT PHX WITHOUT INCIDENT. INSPECTED AND FOUND MIRROR LIGHT C/B TRIPPED. AFT LAVATORY BALLAST HAD OVERHEATED AND WAS CAUSING SMELL. REPLACED BALLAST AND SOCKET PER BOEING M/M.
Part: BATTERY PACK — DISCHARGED (COCKPIT)
DURING SCHEDULED SERVICE CHECK, FOUND COCKPIT EMERGENCY LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M.
1995
Part: PANEL — CRACKED (NLG WW)
DURING SCHEDULED A2 CHECK, FOUND NOSE WHEEL WELL CEILING PANEL OPENING CRACKED 2.125 AT AFT INBOARD RADIUS. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
Part: EEL BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M.