N341SW
Registered owner: 13:4 AVIATION LLC, WI (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
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.
375 reports on file, 1995-03-30 – 2012-04-19.
Part: BRACKET — LOOSE (GIRT BAR) · airframe 76,020 hrs · 67,282 cycles
R1 DOOR GIRT BAR BRACKET NOT SECURING GIRT BAR PROPERLY. PROPERLY SECURED BRACKET IAW MM.
Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 75,759 hrs · 67,069 cycles
FWD DOOR FRAME ANGLE CRACKED. REMOVED AND REPLACED FWD CARGO DOOR PER M/M.
Part: LENS — CRACKED (CABIN) · airframe 75,759 hrs · 67,069 cycles
L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER AMM.
Part: SIGN — UNSECURE (CABIN) · airframe 75,400 hrs · 66,796 cycles
RT OVERWING EMERGENCY "EXIT" SIGN FELL OFF. SECURED SIGN PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,101 hrs · 66,573 cycles
DURING SCHEDULED MV2 CHECK FOUND, RT EMERGENCY EXIT LIGHT INOP AT ROW 23. REMOVED AND REPLACED BULB PER MM.
Earlier reports · 1995–2011 · 370 reports
2011
Part: LENS — LOOSE (CABIN) · airframe 74,885 hrs · 66,419 cycles
DURING SCHEDULED CV CHECK, FOUND FWD OVERHEAD EMERGENCY EXIT SIGN LIGHT LENS LOOSE. SECURED LENS PER MM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 73,872 hrs · 65,642 cycles
DURING SCHEDULED SPV CHECK FOUND FRAME CHORD CRACKED AT BS 639, STR 16L. REPAIRED FRAME IAW EA.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,872 hrs · 65,642 cycles
DURING SCHEDULED SPV CHECK FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB IAW MM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 73,872 hrs · 65,642 cycles
DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 616, STR 17R. REPAIRED FRAME IAW EA.
Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 73,872 hrs · 65,642 cycles
DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW MT.
Part: SIGN — LOOSE (CABIN) · airframe 72,928 hrs · 64,925 cycles
DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.
Part: LENS — LOOSE (EXIT SIGN) · airframe 72,883 hrs · 64,889 cycles
DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING DOOR EMERGENCY EXIT SIGN LIGHT LENS LOOSE. REMOVED AND REPLACED SIGN ASSY PER MM.
Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 72,659 hrs · 64,725 cycles
DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR LOW. REMOVED AND REPLACED SLIDE PER MT.
Part: SKIN PANEL — CRACKED (NLG WW) · airframe 72,294 hrs · 64,456 cycles
DURING SCHEDULED MV1 CHECK, FOUND NOSE WHEEL WELL RT FWD PANEL OPENING SKIN CRACKED. REPAIRED SKIN PER EA.
Part: SKIN PANEL — CRACKED (NLG WW) · airframe 72,294 hrs · 64,456 cycles
DURING SCHEDULED MV1 CHECK, FOUND NOSE WHEEL WELL LT FWD PANEL OPENING SKIN CRACKED. REPAIRED SKIN PER EA.
Part: COVER — LOOSE (EXIT SIGN) · airframe 72,211 hrs · 64,386 cycles
RT OVERHEAD EMERGENCY EXIT SIGN LOOSE. SECURED COVER PER MM.
2010
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 705 TO BS 715, BBL 0. REPAIRED WEB PER ER.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND EEPLS INOP. REMOVED AND REPLACED EEPLS PER MM.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 1010, STR 2L. REMOVED AND REPLACED STRINGER PER ER.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 867, STR 25R. REMOVED AND REPLACED CLIP PER SRM.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 663, RBL 6.15. REMOVED AND REPLACED STIFFENER PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 294, STR 2R. REMOVED AND REPLACED FRAME PER SRM AND BAC DWG.
Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM WEB ATTACHED ANGLE CRACKED AT BS 947.5, STR 17R. REMOVED AND REPLACED ANGLE PER SRM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM LOWER CHORD CRACKED BETWEEN BS 717 TO BS 718, BL 0. REPAIRED BEAM PER ER AND EA.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM ANGLE CRACKED AT BS 727B, RBL 45.5. REPAIRED BEAM PER ER AND EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 320, STR 22L. REPAIRED FRAME PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 20L. REMOVED AND REPLACED CLIP PER SRM.
Part: STIFFENER — CRACKED (CENTER WING) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND FWD VERTICAL STIFFENER CRACKED AT BS 663, LBL 6.15. REMOVED AND REPLACED STIFFENER PER SRM.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND Z-ANGLE CORRODED AT BS 312, LBL 54. REPAIRED Z-ANGLE PER SRM.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND BULKHEAD VERTICAL STIFFENER CRACKED AT BS 727, RBL 5.5. REMOVED AND REPLACED STIFFENER PER SRM AND BAC DWG.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND BULKHEAD VERTICAL STIFFENER CRACKED AT BS 727, LBL 5.5. REMOVED AND REPLACED STIFFENER PER SRM AND BAC DWG.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 26R. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 25L. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 23L. REMOVED AND REPLACED CLIP PER SRM.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND HORIZONTAL STIFFENER CRACKED AT BS 663, RBL 6.15. REMOVED AND REPLACED STIFFENER PER SRM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM ANGLE CRACKED AT BS 727B, LBL 24.8. REPAIRED BEAM PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED CLIP PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND STUB FRAME CRACKED AT BS 956, STR 11R. REMOVED AND REPLACED FRAME PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R. R&R CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1138, STR 27L. REMOVED AND REPLACED CLIP PER SRM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, LBL 11. REPAIRED BEAM PER SRM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM ANGLE CRACKED AT BS 727B, RBL 25. REPAIRED BEAM PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED CLIP PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND STUB FRAME CRACKED AT BS 296, STR 7R. REMOVED AND REPLACED FRAME PER SRM AND BAC DWG.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 25R. REMOVED AND REPLACED CLIP PER SRM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM ANGLE CRACKED AT BS 727B, LBL 45.5. REPAIRED BEAM PER SRM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CRACKED AT BS 727B, LBL 45.5. REPAIRED BEAM PER EA.
Part: FLAP — PUNCTURED (RT WING) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND RT WING I/B FORE FLAP PUNCTURED. REPAIRED FORE FLAP PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 277, STR 3R. REPAIRED FRAME PER SRM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 662, LBL 24.5. REPAIRED BEAM PER EA.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.
Part: STRUCTURE — CORRODED (E&E BAY) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND T- CHORD CORRODED AT BS 323, LBL 6. REMOVED AND REPLACED T-CHORD PER SRM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, BETWEEN RBL 5 TO RBL 44. REPAIRED BEAM PER SRM.
Part: LIGHT — CRACKED (CABIN) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND RT EEPLS CRACKED AT ROW 12. REMOVED AND REPLACED EEPLS PER MM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 15. REPAIRED BEAM PER SRM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 662, RBL 24.5. REPAIRED CHORD PER ER AND EA.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 706 TO BS 713, LBL 24.5. REPAIRED CHORD PER ER AND EA.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,405 hrs · 63,781 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.
Part: SKIN — CRACKED (FUSELAGE) · airframe 70,969 hrs · 63,439 cycles
DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT, BS 947. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 70,969 hrs · 63,439 cycles
DURING SCHEDULED 2HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 907, STR 4L. REPAIRED SKIN PER SRM.
2009
Part: SIGN — INOPERATIVE (CABIN) · airframe 69,432 hrs · 62,286 cycles
DURING SCHEDULED SPV CHECK, FOUND LT EMERGENCY EXIT SIDEWALL SIGN LIGHT INOP. RELAMPED SIGN PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,432 hrs · 62,286 cycles
DURING SCHEDULED SPV CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED LIGHT PER MM.
Part: WEDGE — DELAMINATED (LE SLAT) · airframe 69,361 hrs · 62,237 cycles
DURING SCHEDULE HC2 CHECK, FOUND LT WING NR 2 SLAT UPPER T/E WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PER MM.
Part: CASTING — BROKEN (SPOILER) · airframe 69,361 hrs · 62,237 cycles
DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 GROUND SPOILER O/B HINGE ACTUATOR CASTING BROKEN. REMOVED AND REPLACED SPOILER PER MM.
Part: LENS — LOOSE (CABIN) · airframe 68,594 hrs · 61,684 cycles
RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER SWA EA.
Part: LENS — INOPERATIVE (CABIN) · airframe 68,353 hrs · 61,496 cycles
OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS INOP AT ROW 12. REMOVED AND REPLACED LENS PER MM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 20R TO STR 21R. REPAIRED FRAME PER ER.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.
Part: SKIN — CORRODED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV, FOUND FUSELAGE SKIN CORRODED AT BS 520, STR 13R TO STR 14R. REPAIRED SKIN PER ER.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 727B, STR 23L TO STR 24L. REPAIRED SHEAR TIE PER ER.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 887, STR 24L. REMOVED AND REPLACED STR CLIP PER SRM.
Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 540, STR 19R. REMOVED AND REPLACED STR SPLICE PER SRM.
Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND KEEL BEAM CORRODED AT BS 540, RBL 6. REPAIRED BEAM PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 420, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER ER.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED CLIP PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 578, STR 14L. REPAIRED FRAME PER ER.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 787, BETWEEN STR 22L & 23L. REPAIRED SHEAR TIE PER ER.
Part: FRAME — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 520, STR 14L. REPAIRED FRAME PER ER.
Part: FRAME — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 727E, BETWEEN STR 22R TO STR 23R. REPAIRED FRAME PER ER.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 24R. REMOVED AND REPLACED CLIP PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 908, STR 25R. REPAIRED SKIN PER ER.
Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM CRACKED AT BS 520, LBL 60. REPAIRED BEAM PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 520, BETWEEN LBL 6 TO RBL 6. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 735A, STR 14R. REPAIRED SKIN PER ER.
Part: FRAME — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 767, STR 14L. REPAIRED FRAME PER ER.
Part: FRAME — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 400, STR 14L. REPAIRED FRAME PER ER.
Part: FRAME — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 559, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER ER.
Part: FRAME — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 440, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER ER.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 777, LBL 60. REMOVED AND REPLACED WEB PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 380, STR 16R. REPAIRED FRAME PER ER.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 986.5, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER BAC DWG.
Part: DOUBLER — CORRODED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND INTERNAL DOUBLER CORRODED AT BS 947, STR 25L. REMOVED AND REPLACED DOUBLER PER BAC DWG.
Part: FRAME SPLICE — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND FRAME SPLICE CRACKED AT BS 727E, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SWA EA.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 5R. R&R CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 908, STR 9L. R&R CLIP PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 967, STR 25L. R&R SHEAR TIE PER SRM.
Part: FRAME SPLICE — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND FRAME SPLICE CRACKED AT BS 520, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SWA EA.
Part: FRAME SPLICE — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND FRAME SPLICE CRACKED AT BS 500B, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SWA EA.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 8R. R&R CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 9R. R&R CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 9R. R&R CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. REMOVED AND REPLACED CLIP PER SI.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8L. REMOVED AND REPLACED CLIP PER SI.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7L. REMOVED AND REPLACED CLIP PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 727A, STR 8L. REPAIRED FRAME PER SWA EA.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED BETWEEN BS 967 TO BS 1016, STR 25L. REMOVED AND REPLACED STRINGER PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. REPAIRED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT STR 727A, STR 15R. REMOVED AND REPLACED CLIP PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 360, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT STR 727A, STR 14L. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 986, STR 27L. REPAIRED STRINGER PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED CLIP PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 25R. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 8R. REPAIRED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8L. REPAIRED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 3R. REMOVED AND REPLACED CLIP PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 887, STR 19L. REPAIRED FRAME PER SRM.
Part: SKIN — CRACKED (HORIZ STAB) · airframe 67,982 hrs · 61,205 cycles
DURING SCHEDULED SPV CHECK, FOUND LT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT REAR SPAR STAB STA 125. REPAIRED SKIN PER SWA EA.
Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 67,616 hrs · 60,959 cycles
DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LOW PRESSURE INDICATION. REMOVED AND REPLACED SLIDE PER MT.
Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 67,427 hrs · 60,834 cycles
R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.
2008
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,595 hrs · 60,259 cycles
DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727B, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 66,595 hrs · 60,259 cycles
DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR SKIN CUTOUT CRACKED AT BS 794, BETWEEN STR 21R TO STR 26R. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 66,595 hrs · 60,259 cycles
DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR SKIN CUTOUT CRACKED AT BS 794, RBL 49. REPAIRED SKIN PER ACO.
Part: RIB — CRACKED (LT WING) · airframe 66,595 hrs · 60,259 cycles
DURING SCHEDULED 20Y CHECK, FOUND LT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 TO STR 3. REPAIRED RIB PER ACO.
Part: FRAME — CRACKED (FUSELAGE) · airframe 66,595 hrs · 60,259 cycles
DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 277, BETWEEN STR 9R TO STR 10R. REPAIRED FRAME PER SRM.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,573 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND STRINGER CRACKED AT BETWEEN BS 430 TO BS 440, STR 28R. REPAIRED STRINGER PER SRM.
Part: SPAR — CRACKED (RT WING) · airframe 66,574 hrs · 60,240 cycles
DURING SCHEDULED 20Y CHECK, FOUND RT WING REAR SPAR WEB CRACKED AT FWD MLG BEAM FITTING. REPAIRED WEB PER PAE ER.
Part: LIGHT — BROKEN (EXTERIOR) · airframe 66,574 hrs · 60,240 cycles
DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: WEDGE — DELAMINATED (TE FLAP) · airframe 66,572 hrs · 60,238 cycles
DURING SCHEDULED SPV CHECK, FOUND RT WING I/B TRAILING EDGE FLAP WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PER SRM.
Part: SKIN — CRACKED (E&E BAY DOOR) · airframe 66,572 hrs · 60,238 cycles
DURING SCHEDULED SPV CHECK, FOUND E/E DOOR EXTERNAL SKIN CRACKED AT RT EDGE. REMOVED AND REPLACED SKIN PER SRM.
Part: SPAR — CRACKED (LT WING) · airframe 66,572 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND LT WING UPPER T/E SPAR CHORD CRACKED AT MLG BEAM TO SPAR FITTING. REPAIRED CHORD PER PAE ER.
Part: FRAME — CRACKED (FUSELAGE) · airframe 66,573 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 344, STR 3R. REPAIRED FRAME PER SRM.
Part: DRAG ANGLE — CORRODED (VERTICAL STAB) · airframe 66,573 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND VERTICAL STAB FITTING DRAG ANGLES CORRODED. REMOVED AND REPLACED DRAG ANGLES PER SRM.
Part: STRUCTURE — CRACKED (LT WING) · airframe 66,572 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND LT WING UPPER CHORD CRACKED AT WBL 114, STR 2. REPAIRED CHORD PER PAE ER.
Part: FITTING — CRACKED (LT MLG) · airframe 66,572 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND LT MLG FITTING CRACKED AT D-HOLE. REPAIRED FITTING PER PAE ER.
Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 66,572 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND CHORD CORRODED AT BS 270, BETWEEN LBL 12 TO RBL 12, WL 208. REMOVED AND REPLACED CHORD PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 66,572 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 2R. REPAIRED FRAME PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 66,572 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 23R. REMOVED AND REPLACED FRAME PER SRM.
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 66,572 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT BS 440, STR 23R. REPAIRED FRAME PER SRM.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,572 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 947 TO BS 996. REMOVED AND REPLACED WEB PER SRM.
Part: MOUNT — CORRODED (GIRT BAR) · airframe 66,573 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND L1 FLOOR MOUNT SLIDE GIRT BAR CORRODED. REMOVED AND REPLACED MOUNT PER SRM.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,573 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND LT CREASE BEAM WEB CORRODED AT BS 400 TO BS 420. REMOVED AND REPLACED WEB PER SRM.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,573 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND RT CREASE BEAM WEB CORRODED AT BS 425 TO BS 440. REMOVED AND REPLACED WEB PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 66,573 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR UPPER HINGE CUTOUT SKIN CRACKED. REPAIRED SKIN PER PAE ER.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,573 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED CLIP PER SRM.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,573 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 450 LT TO 495 LT. REMOVED AND REPLACED BEAM PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 66,573 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR LOWER HINGE CUTOUT SKIN CRACKED. REPAIRED SKIN PER PAE ER.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,573 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 500A + 6 RT. REMOVED AND REPLACED BEAM PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,573 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND STR CLIP CRACKED AT STA 294, STR 13L. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 277 S10R) · airframe 66,573 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 277 S11R) · airframe 66,573 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: CREASE BEAM — CRACKED (BS 637) · airframe 66,573 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 637, RBL 70. REMOVED AND REPLACED WEB PER MM.
Part: CREASE BEAM — CRACKED (BS 637) · airframe 66,573 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 637, LBL 70. REMOVED AND REPLACED WEB PER MM.
Part: STRINGER CLIP — CRACKED (BS 500D S8L) · airframe 66,573 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,573 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 580, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,573 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,573 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,573 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,573 hrs · 60,238 cycles
DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 560, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 66,255 hrs · 60,010 cycles
DURING SCHEDULED MV2 CHECK, FOUND AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.
Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 65,109 hrs · 59,171 cycles
DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
Part: FLAP — DELAMINATED (LT WING) · airframe 65,109 hrs · 59,171 cycles
DURING SCHEDULED C1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 64,697 hrs · 58,848 cycles
DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 291, STR 14R. REPAIRED SKIN PER SWA EA.
Part: LENS — BROKEN (CABIN) · airframe 64,533 hrs · 58,735 cycles
EEPLS LENS BROKEN AT ROW 5ABC. REMOVED AND REPLACED LENS PER MM.
2007
Part: TORQUE TUBE — WORN (T/E FLAP) · airframe 63,663 hrs · 58,054 cycles
DURING SCHEDULED A1 CHECK, FOUND LT WING INBOARD T/E FLAP DRIVE TORQUE TUBE WORN. REMOVED AND REPLACED TORQUE TUBE PER MM.
Part: TORQUE TUBE — WORN (T/E FLAP) · airframe 63,663 hrs · 58,054 cycles
DURING SCHEDULED A1 CHECK, FOUND RIGHT WING INBOARD T/E FLAP DRIVE TORQUE TUBE WORN. REMOVED AND REPLACED TORQUE TUBE PER MM.
Part: TORQUE TUBE — WORN (LT WING TE FLAP) · airframe 63,663 hrs · 58,054 cycles
DURING SCHEDULED A1 CHECK, FOUND LEFT WING NR 4 T/E FLAP DRIVE TORQUE TUBE WORN. REMOVED AND REPLACED TORQUE TUBE PER MM.
Part: TORQUE TUBE — WORN (RT WING TE FLAP) · airframe 63,663 hrs · 58,054 cycles
DURING SCHEDULED A1 CHECK, FOUND RIGHT WING NR 5 T/E FLAP DRIVE TORQUE TUBE WORN. REMOVED AND REPLACED TORQUE TUBE PER MM.
Part: HOOK — LOOSE (L1 DOOR) · airframe 63,368 hrs · 57,818 cycles
DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 63,325 hrs · 57,781 cycles
DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503C, STR 15L. REPAIRED SKIN PER SWA EA.
Part: LAMP — INOPERATIVE (CABIN) · airframe 62,959 hrs · 57,496 cycles
DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 62,959 hrs · 57,496 cycles
DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 759, STR 19R. REPAIRED SKIN PER SRM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,959 hrs · 57,496 cycles
DURING SCHEDULED A1 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
Part: SKIN — CRACKED (BS 500C S15R) · airframe 62,540 hrs · 57,076 cycles
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 15R. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 62,540 hrs · 57,076 cycles
DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT DOOR HANDLE CUTOUT UPPER AFT CORNER. REPAIRED DOOR SKIN PER SWA EA.
Part: SKIN — CRACKED (BS 942 S23R) · airframe 62,540 hrs · 57,076 cycles
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, STR 23R. REPAIRED SKIN PER SRM.
Part: HOUSING — BROKEN (EMERGENCY LIGHT) · airframe 61,247 hrs · 56,141 cycles
DURING SCHEDULED A2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT HOUSING BROKEN. REMOVED AND REPLACED HOUSING ASSY PER MM.
2006
Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 60,503 hrs · 55,542 cycles
DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
Part: SKIN — CRACKED (L/E SLAT) · airframe 60,503 hrs · 55,542 cycles
DURING SCHEDULED C4 CHECK, FOUND LT WING NR 3 L/E SLAT LOWER OUTBOARD SKIN CRACKED AT AFT FASTENER ROW. REPAIRED L/E SLAT PER SWA EA.
Part: SKIN — DELAMINATED (RT FOREFLAP) · airframe 60,503 hrs · 55,542 cycles
DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD FORE FLAP UPPER MID SURFACE DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.
Part: SKIN — CRACKED (BS 753 S14L) · airframe 59,556 hrs · 54,818 cycles
DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 753, STR 14L. REPAIRED SKIN PER SWA EA.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 58,631 hrs · 54,121 cycles
DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 58,611 hrs · 54,093 cycles
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 931 TO BS 944, STR 25R. REPAIRED SKIN PER SWA EA & SRM.
Part: FRAME — CRACKED (BS 492) · airframe 58,173 hrs · 53,763 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492.5, BETWEEN STR 24R TO STR 25R. REPAIRED FRAME PER SWA EA.
Part: STRINGER CLIP — CRACKED (BS 277) · airframe 58,173 hrs · 53,763 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED CLIP PER SRM.
Part: BEAR STRAP — CRACKED (BS 348) · airframe 58,173 hrs · 53,763 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT BS 348, STR 16L. REPAIRED SKIN PER SWA ACO & SRM.
Part: SPLICE — CRACKED (BS 360) · airframe 58,173 hrs · 53,763 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 360, STR 15L. REPAIRED STRINGER SPLICE PER SRM.
Part: GLOWSTRIP — LOOSE (CABIN) · airframe 58,173 hrs · 53,763 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FWD CABIN EEPLS PHOTOLUMINESCENT STRIPS LOOSE. REMOVED AND REPLACED STRIPS PER SWA DRAWING.
Part: KEELBEAM — CORRODED (BS 540) · airframe 58,173 hrs · 53,763 cycles
DURING SCHEDULED 1/4D CHECK, FOUND LT KEEL BEAM CORRODED AT BS 540. REMOVED AND REPLACED KEEL BEAM SECTION PER SRM.
Part: BELTFRAME — CRACKED (BS 500B) · airframe 58,173 hrs · 53,763 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 500B, STR 21L. REPAIRED BELTFRAME PER SWA EA.
Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 58,173 hrs · 53,763 cycles
DURING SCHEDULED 1/4D CHECK, FOUND CABIN EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 10 ABC. SECURED LENS PER MM.
Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 58,173 hrs · 53,763 cycles
DURING SCHEDULED 1/4D CHECK, FOUND CABIN EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 23 DEF. SECURED LENS PER MM.
2005
Part: CABLE — MISROUTED (R2 DOOR) · airframe 57,716 hrs · 53,389 cycles
DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY PER MM.
Part: CASTING — CRACKED (RT WING SPOILER) · airframe 57,716 hrs · 53,389 cycles
DURING SCHEDULED C1 CHECK, FOUND RT WING NR 5 SPOILER OTBD HINGE CASTING CRACKED. REMOVED AND REPLACED NR 5 SPOILER PER MM.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,585 hrs · 53,272 cycles
DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT BATTERY CHARGER INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,585 hrs · 53,272 cycles
DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,568 hrs · 53,255 cycles
DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 16 DEF. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: SIGN — BROKEN (CABIN) · airframe 57,487 hrs · 53,192 cycles
R1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.
Part: SKIN — CRACKED (BS 500D) · airframe 57,208 hrs · 52,973 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16L. REPAIRED SKIN PER SWA EA & SRM.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,042 hrs · 52,842 cycles
DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.
Part: DOOR FRAME — CRACKED (AFT CARGO BAY) · airframe 56,734 hrs · 52,617 cycles
DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR FWD VERTICAL FRAME CRACKED AT UPPER OUTBOARD FASTENER. REMOVED AND REPLACED AFT CARGO DOOR PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 56,734 hrs · 52,617 cycles
DURING SCHEDULED C4 CHECK, FOUND LOWER FUSELAGE SKIN CRACKED AT BS 727D, BL 0. REPAIRED SKIN PER SWA EA & SRM.
Part: SLIDE — DISLODGED (L1 DOOR) · airframe 56,173 hrs · 52,165 cycles
L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE PER MM.
Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 55,771 hrs · 51,826 cycles
DURING SCHEDULED C3 CHECK, FOUND PHOTOLUMINESCENT STRIPS DISCOLORED AT ROWS 1D, 7D & 9D. REMOVED AND REPLACED STRIPS PER MM.
Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 55,684 hrs · 51,756 cycles
L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 55,321 hrs · 51,459 cycles
DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 919, STR 22L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 55,321 hrs · 51,459 cycles
DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 925, STR 20R. REPAIRED SKIN PER SRM.
Part: DOOR FRAME — CRACKED (FWD SERVICE) · airframe 54,846 hrs · 51,088 cycles
DURING SCHEDULED C2 CHECK, FOUND FWD SERVICE DOOR LOWER FRAME AFT CORNER CRACKED. REMOVED AND REPLACED FWD SERVICE DOOR PER MM.
Part: SKIN — WORN (FUSELAGE) · airframe 54,540 hrs · 50,856 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN UNDER DORSAL FIN FROM BS 867 TO BS 973, WORN. REPAIRED FUSELAGE SKIN PER EA.
2004
Part: SKIN — CRACKED (FUSELAGE) · airframe 53,912 hrs · 50,389 cycles
DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 17L, CRACKED. REPAIRED SKIN PER SRM.
Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 52,943 hrs · 49,611 cycles
DURING SCHEDULED C4 CHECK, FOUND L1 & L2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L1 & L2 DOOR EVAC SLIDES PER MM.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,943 hrs · 49,611 cycles
DURING SCHEDULED C4 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT AT ROW 23 DEF, INOP. RELAMPED BULL NOSE LIGHT PER MM.
Part: SPLICE — CRACKED (FUSELAGE) · airframe 52,928 hrs · 49,600 cycles
DURING SPV, FOUND STRINGER SPLICES AT BS 540, STRINGER 14R, BS 540, STRINGER 10R, CRACKED. REMOVED AND REPLACED STRINGER SPLICES PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 52,928 hrs · 49,600 cycles
DURING SPV, FOUND BUTTSTRAPS AT BS 360, STRINGER 10R, BS 360 STRINGER 14R, CRACKED. REPAIRED BUTTSTRAPS PER SRM.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 52,928 hrs · 49,600 cycles
DURING SPV, FOUND SHEAR TIE AT BS 360, STRINGER 14L, CRACKED. REPAIRED SHEAR TIE PER SRM.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 52,919 hrs · 49,591 cycles
DURING SPV, FOUND SHEAR TIE AT BS 520, STRINGER 10R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: SPLICE — CRACKED (BS 360) · airframe 52,919 hrs · 49,591 cycles
DURING SPV, FOUND STRINGER SPLICE AT BS 360, BETWEEN STRINGER 4L AND 4R CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,919 hrs · 49,591 cycles
DURING SPV, FOUND STRINGER 6L AT BS 374, CRACKED. REPAIRED STRINGER SECTION PER SRM.
Part: SKIN — DELAMINATED (LT WING FOREFLAP) · airframe 52,911 hrs · 49,583 cycles
DURING SPV, FOUND LT WING OUTBOARD FOREFLAP DELAMINATED. REMOVED AND REPLACED LT WING OUTBOARD FOREFLAP PER MM.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,911 hrs · 49,582 cycles
DURING SPV, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP DURING TEST. RELAMPED LIGHT PER MM.
Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 52,369 hrs · 49,141 cycles
L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED AND SECURED L1 DOOR EVAC SLIDE PER MM.
Part: SPINDLE — CRACKED (TE FLAP) · airframe 51,588 hrs · 48,504 cycles
DURING SCHEDULED PM CHECK, FOUND LT WING NR 1 T/E FLAP SPINDLE WITH A CRACK INDICATION. REMOVED AND REPLACED NR 1 FLAP SPINDLE PER MM.
2003
Part: BEARING — WORN (RT ELEVATOR) · airframe 51,016 hrs · 48,035 cycles
DURING SCHEDULED C2 CHECK, BOTH LT AND RT ELEVATORS FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED BOTH LT AND RT ELEVATOR CONTROL ROD AFT BEARINGS PER MM
Part: FIRE LOOP — FAULTY (APU BAY) · airframe 50,611 hrs · 47,695 cycles
DECLARED EMERGENCY, APU FIRE WARNING LIGHT ILLUMINATED, DISCHARGED BOTTLE. INSPECTED APU COMPARTMENT, NO EVIDENCE OF FIRE. REMOVED AND REPLACED FWD APU FIRE DETECTOR LOOP PER MM.
Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 50,159 hrs · 47,317 cycles
DURING SCHEDULED 1/2D CHECK, FOUND NLG W/W UPPER WEB CRACKED AT THE LT/RT TIRE BRAKE ATTACH HOLES. REPAIRED UPPER WEB PER SWA EA.
Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 48,396 hrs · 45,270 cycles
DURING SCHEDULED 1/2D CHECK, FOUND MAIN W/W FWD PRESS BULKHEAD CRACKED AT BS 663, WL 200 AND LBL 33. REPAIRED BULKHEAD PER SWA EA.
Part: LIGHT — LOOSE (MID CABIN) · airframe 50,159 hrs · 47,317 cycles
DURING SCHEDULED 1/2D CHECK, FOUND OVERHEAD BIN EMERGENCY EXIT BULLNOSE LIGHT LOOSE AT ROW NR 14 ABC. SECURED EXIT LIGHT PER MM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 50,159 hrs · 47,317 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 363, BETWEEN STR 13R AND STR 14R. REPAIRED FRAME PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,159 hrs · 47,317 cycles
DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CORRODED AT BS 363, BETWEEN STR 14R AND STR 15R. REPAIRED SHEAR TIE PER SRM.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 50,159 hrs · 47,317 cycles
DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CRACKED AT BS 363, BETWEEN STR 13R AND STR 14R. REPAIRED SHEAR TIE PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,159 hrs · 47,317 cycles
DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 50,159 hrs · 47,317 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 10R. REPAIRED SKIN PER SRM.
Part: BRACKET — CORRODED (GIRT BAR) · airframe 50,159 hrs · 47,317 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE, BOTH FWD AND AFT GIRT BAR BRACKETS CORRODED. REMOVED AND REPLACED FWD AND AFT BRACKETS PER MM.
Part: SLIDE — OUT OF ADJUST (AFT ENTRY DOOR) · airframe 50,153 hrs · 47,314 cycles
DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.
Part: LENS — LOOSE (CABIN) · airframe 50,153 hrs · 47,314 cycles
DURING SCHEDULED C1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.
Part: ROD END — WORN (LT ELEVATOR TAB) · airframe 49,248 hrs · 46,589 cycles
DURING SCHEDULED C4 CHECK, SWA SI 11139-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB AFT ROD END ASSY PER MM.
2002
Part: SPOILER — CRACKED (LT WING) · airframe 47,286 hrs · 44,999 cycles
DURING SCHEDULED BC2 CHECK, FOUND NR 4 GROUND SPOILER INBD HINGE FITTING CRACKED. REMOVED AND REPLACED NR 4 GROUND SPOILER PER MM.
Part: LENS — LOOSE (CABIN) · airframe 47,286 hrs · 44,999 cycles
DURING SCHEDULED C2 CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY LIGHT LENS LOOSE AT ROWS NR 11 ABC AND NR 14 ABC. SECURED LENSES PER MM.
Part: TRACK — MISSING (CABIN) · airframe 47,220 hrs · 44,939 cycles
EEPLS STRIP MISSING AND LOOSE AT ROW NR 9 LT. INSTALLED STRIP AND SECURED PER MM.
Part: SLIDE — OUT OF ADJUST (BOTH FWD DOORS) · airframe 45,414 hrs · 43,454 cycles
DURING SCHEDULED C4 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT STRAP PLAY OUTS OUT OF ADJUST. ADJUSTED SLIDES PER MM.
Part: LIGHT — DEFECTIVE (SERVICE DOOR) · airframe 45,414 hrs · 43,454 cycles
DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EXIT LIGHT DIM. RELAMPED EXIT LIGHT PER MM.
2001
Part: SLIDE — OUT OF ADJ (R2 DOOR) · airframe 44,655 hrs · 42,846 cycles
DURING SCHEDULED BC3 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. ADJUSTED SLIDE PER MM.
Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 48,625 hrs · 47,315 cycles
DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 43,575 hrs · 41,930 cycles
DURING SCHEDULED 1/4D CHECK, FOUND EXTERIOR EMERGENCY LIGHT INOP AFT OF FWD SVC DOOR. RELAMPED PER MM.
Part: HYDRAULIC LINE — BROKEN (HYD SYSTEM) · airframe 42,252 hrs · 40,816 cycles
DIVERSION, LOST B-HYDRAULIC SYSTEM PRESS AND FLUID. REMOVED AND REPLACED BROKEN HYDRAULIC LINE AT B-SYSTEM ELECTRIC PUMP PER MM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 42,200 hrs · 40,773 cycles
DURING SCHEDULED 1/4D CHECK, FOUND BS 660 CENTER WING BOX LONGITUDINAL FLOORBEAM TEE CHORD CRACKED AT BL 0. REPAIRED FLOORBEAM TEE CHORD PER SWA RA.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 42,200 hrs · 40,773 cycles
DURING SCHEDULED 1/4D CHECK, FOUND BS 663 CENTER WING BOX LONGITUDINAL FLOORBEAM TEE CHORD CRACKED AT BL 0.7. REPAIRED FLOORBEAM TEE CHORD PER SWA RA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 42,200 hrs · 40,773 cycles
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, STR 25L. REPAIRED SKIN PER SRM.
Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 42,200 hrs · 40,773 cycles
DURING SCHEDULED 1/4D CHECK, FOUND NLG W/W BOX VERTICAL WEB CRACKED AT BS 233, BL 0. REPAIRED WEB PER SRM.
Part: TAB — DELAMINATED (LT AILERON) · airframe 42,200 hrs · 40,773 cycles
DURING SCHEDULED 1/4D CHECK, FOUND LT AILERON TAB DELAMINATED AROUND HINGE POINTS. REMOVED AND REPLACED AILERON TAB PER MM.
Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 42,200 hrs · 40,773 cycles
DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 664, LBL 31. REPAIRED BEADED PRESSURE WEB PER TI-353-046.
Part: SKIN — CRACKED (FUSELAGE) · airframe 41,904 hrs · 40,519 cycles
DURING SCHEDULED C4 CHECK, FOUND EXTERNAL FUSELAGE SKIN DOUBLER CRACKED AT AFT SVC DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA RA.
Part: CAP — MISSING (CABIN) · airframe 41,904 hrs · 40,519 cycles
DURING SCHEDULED C4 CHECK, FOUND EEPLS END CAP MISSING AT AFT SECTION. INSTALLED END CAP PER MM.
Part: SLIDE — DETACHED (FWD SERVICE DOOR) · airframe 41,602 hrs · 40,278 cycles
FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER WHEN ARMED FOR TAXI. REINSTALLED EVAC SLIDE ASSY PER MM.
Part: SLIDE — OUT OF POSITION (PAX DOOR) · airframe 41,553 hrs · 40,235 cycles
FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.
2000
Part: BOTTLE — DISCHARGED (ESCAPE SLIDE) · airframe 57,907 hrs · 62,063 cycles
DURING SCHEDULED RON CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM.
Part: SKIN — CRACKED (RT WING SLAT) · airframe 40,017 hrs · 38,914 cycles
DURING SCHEDULED C2 CHECK, FOUND NR 6 L/E SLAT SKIN CRACKED AT MID AUX TRACK CUT OUT. REPAIRED SLAT PER SWA RA.
Part: REGULATOR — ERRATIC (NR 1 ENGINE)
AIR TURNBACK, UNABLE TO CONTROL CABIN PRESSURE DURING CLIMB. REMOVED AND REPLACED NR 1 ENG HIGH STAGE BLEED AIR REGULATOR PER MM.
1999
Part: FRAME — CRACKED (FUSELAGE)
DURING SCHEDULED C3 CHECK, FOUND FWD SERVICE DOOR UPPER FUSELAGE CUT OUT STUB FRAME CRACKED. REPAIRED FRAME PER SWA RA NR 1-353-2169.
Part: WARNING HORN — ACTIVATED (COCKPIT)
ABORTED TAKEOFF, AT 20 KNOTS TAKEOFF WARNING HORN ON POWER ADVANCE. OPS CHECKED, TAKEOFF WARNING SYSTEM. NO FAULTS NOTED.
Part: SLIDE — PRESS LOW (PAX DOOR)
AFT ENTRY DOOR SLIDE HAS LOW PRESSURE. REMOVED AND REPLACED AFT ENTRY DOOR SLIDE PER MM.
Part: INDICATOR — INOP (NR 2 FUEL FLOW)
EN ROUTE, NR 2 ENG FUEL FLOW METER INDICATOR WENT INOP. REMOVED AND REPLACED FUEL FLOW METER INDICATOR PER MM.
Part: INDICATOR — FAULTY (NR 1 FUEL FLOW)
NR 1 FUEL FLOW INDICATOR DROPPED TO ZERO ON TAKEOFF ROLL, ALL OTHER ENG INDICATIONS NORMAL. RETURNED TO NORMAL FUEL FLOW INDICATION DURING ROTATION. REPLACED THE NR 1 FUEL FLOW INDICATOR PER MM.
1998
Part: AIR DIST — ODOR (CABIN)
GATE RETURN DUE TO STRONG ODOR IN CABIN DURING TAXI OUT FOR DEPARTURE. INSPECTED BOTH AIR COND SYSTEMS, ELECTRICAL SYSTEMS, BOTH CARGO PITS, GALLEYS, LAVS AND ENGINES. FOUND NO SOURCE OF ODORS, NO DEFECTS NOTED ALL PER BOEING MM (LPG NR 256051).
Part: SKIN — GOUGED (BS 863)
DURING SCHEDULED D CHECK, FOUND GOUGED SKIN AT BS 863, STR 1. REMOVED AND REPLACED PER BOEING SRM.
Part: ANGLE — CRACKED (BS 301)
DURING SCHEDULED D CHECK, FOUND L ANGLE CRACKED AT BS 301, LBL 56, WL 257. REMOVED AND REPLACED PER BOEING SRM.
Part: STRINGER — CRACKED (BS 293)
DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 293, STR 11 LT. REMOVED AND REPLACED PER BOEING SRM.
Part: COLLAR — CRACKED (BS 727)
DURING SCHEDULED D CHECK, FOUND FASTENER COLLAR CRACKED AT RT I/B FWD SIDE OF FRAME SPLICE AT BS 727 STRINGER NR 13 WL 237. REMOVED AND REPLACED PER BOEING SRM.
Part: STRINGER — CRACKED (BS 359)
DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 359, STR 14 LT. REMOVED AND REPLACED PER BOEING SRM.
Part: STRINGER — CRACKED (BS 907)
DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4RT. REMOVED AND REPLACED PER BOEING SRM.
Part: INTERCOSTAL — CRACKED (BS 294-298)
DURING SCHEDULED D CHECK, FOUND INTERCOSTAL CRACKED AT BS 294-298, STR 16 LT. REMOVED AND REPLACED PER BOEING SRM.
Part: STRINGER — CRACKED (BS 663)
DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 663, STR 10 LT AND RT. REMOVED AND REPLACED PER BOEING SRM.
Part: FRAME — CRACKED (BS 616)
DURING SCHEDULED D CHECK, FOUND INBOARD FRAME CHORD CRACKED AT BS 616, LBL 64, WL 201. REPAIRED PER BOEING SRM.
Part: WEB — DAMAGED (BS 535)
DURING SCHEDULED D CHECK, FOUND CHAFING DAMAGE ON WEB AT BS 535, BL 53, WL 175. REMOVED AND REPLACED PER BOEING SRM.
Part: ANGLE — CORRODED (BS 300-328)
DURING SCHEDULED D CHECK, FOUND NUMEROUS UPPER SURFACE CORRODED AT I/B SIDE THRESHOLD ANGLE SUPPORT AT BS 300-328, RBL 56.5-59, WL 208. REMOVED AND REPLACED PER BOEING SRM.
Part: SUPPORT — CRACKED (BS 540)
DURING SCHEDULED D CHECK, FOUND FLOOR SUPPORT CRACKED AT BS 540, LBL 1, WL 208. REMOVED AND REPLACED PER BOEING SRM
Part: SUPPORT — CRACKED (BS 540)
DURING SCHEDULED D CHECK, FOUND FLOOR SUPPORT CRACKED AT BS 540, RBL 1, WL 208. REMOVED AND REPLACED PER BOEING SRM
Part: FRAME — CORRODED (GALLEY DOORWAY)
DURING SCHEDULED D CHECK, FOUND AFT GALLEY DOOR FRAME 4 Z-ANGLES CORRODED. REMOVED AND REPLACED PER BOEING SRM.
Part: FRAME — CRACKED (BS 440)
DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 9 RT, 8 RT AT BS 440. REPAIRED PER BOEING TI-630-072.
Part: FRAME — CRACKED (BS 480/500/747)
DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 9 LT, 8LT AT BS 747, BS 500A, AND 480. REPAIRED PER BOEING TI-653-072.
Part: CHORD — CORRODED (BS 270)
DURING SCHEDULED D CHECK, FOUND CORRODED AT BS 270 Z-CHORD FROM LBL 11, RBL 11M WL 208. REMOVED AND REPLACED PER BOEING SRM.
Part: SKIN — BENT (BS 1136)
DURING SCHEDULED D CHECK, FOUND OUTER SKIN BENT AT BS 1136, WL 240 LT. REPAIRED PER BOEING SRM.
Part: FLOORBEAM — CRACKED (BS 947)
DURING SCHEDULED D CHECK, FOUND FLOORBEAM CRACKED AT FLOORBOARD FASTENER HOLE AT BS 947 LBL 53, WL 208. REPAIRED PER BOEING SRM.
Part: FRAME — CRACKED (BS 400/440)
DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 9 LT, 8LT AT BS440, AND BS 400. REPAIRED PER BOEING TI-653-072.
Part: CLIP — CRACKED (BS 500D)
DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 500 D STR 19 LT AND RT. REPAIRED PER BOEING SRM.
Part: SKIN — GOUGED (BS 500A+9.5)
DURING SCHEDULED D CHECK, FOUND GOUGED SKIN AT BS 500A+9.5, 3 BELOW STR 22L, WL 170. REMOVED AND REPLACED PER BOEING SRM.
Part: FLOORBEAM — CORRODED (BS 986.5)
DURING SCHEDULED D CHECK, FOUND CORRODED AT BS 986.5 FLOORBEAM FASTENER HOLES LBL 5, 35.5 RBL 4.5, 31, 39, WL 208 AND 207. REMOVED AND REPLACED PER BOEING SRM.
Part: FRAME — CRACKED (BS 480/727/867)
DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 9 RT, 8 RT AT BS 867, BS 727D AND BS 480. REPAIRED PER BOEING TI-630-072.
Part: WEB — CORRODED (BS 1016)
DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR WEB AT BS 1016, RBL 14, WL 208. REMOVED AND REPLACED PER BOEING SRM.
Part: FRAME — CRACKED (BS 827/867/907)
DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 9 LT, 8LT AT BS 907, BS 867 AND BS 827. REPAIRED PER BOEING TI-6553-072.
Part: ANGLE — CRACKED (BS 943)
DURING SCHEDULED D CHECK, FOUND SHEAR WEB UPPER ATTACH L-ANGLE CRACKED AT BS 943, WL 208, BL0. REPAIRED PER BOEING SRM.
Part: ANGLE — CRACKED (BS 569)
DURING SCHEDULED D CHECK, FOUND LT SKATE ANGLE CRACKED AT BS 569, LBL 48, WL 173. REMOVED AND REPLACED PER BOEING SRM.
Part: SKIN — GOUGED (BS 500)
DURING SCHEDULED D CHECK, FOUND GOUGE SKIN AT BS 500+18, 1 BELOW STR 22 RT. REPAIR PER BOEING SRM.
Part: SKIN — DENTED (BS 377)
DURING SCHEDULED D CHECK, FOUND DENTED SKIN AT BS 377, STR 22 RT. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (LT WING)
DURING SCHEDULED D CHECK, FOUND AFT CARGO BAY, FLOORBEAM STRAP CORRODED AT BS 859, RBL 20, LBL 20, WL 156. REMOVED AND REPLACED PER BOEING SRM.
Part: ANGLE — CRACKED (BS 535.5)
DURING SCHEDULED D CHECK, FOUND CRACKED WEB SUPPORT ANGLE AT BS 535.5, LBL 51, WL 175. REMOVED AND REPLACED PER BOEING SRM.
Part: ANGLE — CRACKED (BS 569)
DURING SCHEDULED D CHECK, FOUND RT SKATE ANGLE CRACKED AT BS 569, RBL 48, WL 173. REMOVED AND REPLACED PER BOEING SRM.
Part: SKIN — DENTED (BS 206)
DURING SCHEDULED D CHECK, FOUND DENTED SKIN AT SHEAR TIE BS 206, WL 173, 5 BELOW STR 24L. REMOVED AND REPLACED PER BOEING SRM.
Part: SKIN — CREASED (BS 914)
DURING SCHEDULED D CHECK, FOUND SKIN CREASED AT BS 914, 4 ABOVE STR 25 RT. REPAIRED PER BOEING SRM.
Part: SKIN — DENTED (BS 379)
DURING SCHEDULED D CHECK, FOUND DENTED SKIN AT BS 379, 4 BELOW STR 17 RT. REMOVED AND REPLACED PER BOEING SRM.
Part: SKIN — DENTED (BS 384 & 387)
DURING SCHEDULED D CHECK, FOUND TWO DENTED SKIN AT BS 384, 5.6 ABOVE STR 21 RT AND BS 387 1 ABOVE STR 21 RT. REPAIRED PER BOEING SRM.
Part: FRAME — CRACKED (BS 727)
DURING SCHEDULED D CHECK, FOUND LT FRAME DOUBLER CRACKED ON AFT SIDE AT BS 727, STR NR 14, WL 231.5. REPAIRED PER BOEING SRM.
Part: SKIN — DENTED (BS 227)
DURING SCHEDULED D CHECK, FOUND DENTED AT BS 227, STRINGER 16 RT MEASURES 3.0. REPAIRED PER BOEING SRM.
Part: TIP — DAMAGED (HORIZ STAB)
DURING SCHEDULED D CHECK, FOUND LT HORIZ STAB TIP, L/E AROUND SCREW HOLE DAMAGED. REPAIRED PER BOEING SRM.
Part: FRAME — CRACKED (BS 747)
DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET BETWEEN STR 8 RT AND 9 RT AT BS 747. REPAIRED PER BOEING SRM.
Part: CHORD — CRACKED (BS 178)
DURING SCHEDULED D CHECK, FOUND SIDE CHORD CRACKED AT BS 178, LBL 29, WL 207. REPAIRED PER BOEING SRM.
Part: FRAME — CRACKED (BS 727B)
DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET BETWEEN STR 8 RT AND 9 RT AT BS 727B. REPAIRED PER BOEING SRM.
Part: FLOORBEAM — CORRODED (BS 727-947)
DURING SCHEDULED D CHECK, FOUND CORRODED CARGO FLOORBEAM AROUND NUTPLATE LOCATIONS AT BS 727-947, LBL 8, WL 159. REMOVED AND REPLACED PER BOEING SRM.
Part: CLIP — CRACKED (BS 420)
DURING SCHEDULED D CHECK, FOUND CRACKED STRINGER CLIP AT BS 420, STR 22 RT. REMOVED AND REPLACED PER BOEING SRM.
Part: ANGLE — WORN (BS 727)
DURING SCHEDULED D CHECK, FOUND FWD END OF T-ANGLE OF FAIRING SUPPORT IS WORN AT BS 727, RBL 69, WL 183. REMOVED AND REPLACED PER BOEING SRM.
Part: FRAME — CORRODED (BS 500)
DURING SCHEDULED D CHECK, FOUND CORRODED AROUND NUTPLATE HOLE ON FRAME AT BS 500 RBL 25, WL 157. REMOVED AND REPLACED PER BOEING SRM.
Part: SHIM — CORRODED (BS 794.3)
DURING SCHEDULED D CHECK, FOUND CORRODED AFT BAY DOOR ROLLER BLOCK SHIMS AT BS 794.3, RBL 50, WL 165. REMOVED AND REPLACED PER BOEING SRM.
Part: STRAP — CORRODED (BS 847-850)
DURING SCHEDULED D CHECK, FOUND CORRODED LOWER TIE STRAP AT BS 847-850, RBL 19, WL 162. REPAIRED PER BOEING SRM.
Part: FRAME — DENTED (BS 827)
DURING SCHEDULED D CHECK, FOUND 2 DENTS IN FRAME AT BS 827, LBL 24.5 AND LBL 28.5, WL 156. REPAIRED PER BOEING SRM.
Part: FRAME — CORRODED (PAX DOORWAY)
DURING SCHEDULED D CHECK, FOUND CORRODED DOOR FRAME COVERPLATE AT BS 492-496, RBL 25-31, WL 158. REMOVED AND REPLACED PER BOEING SRM.
Part: BULKHEAD ANGLE — CORRODED (BS 947)
DURING SCHEDULED D CHECK, FOUND CORROSION ON FLOOR TO BULKHEAD SUPPORT ANGLE AT BS 947, LBL 21, RBL 21, WL 180. REMOVED AND REPLACED PER BOEING SRM.
Part: FRAME — DENTED (EMER EXIT DRWAY)
DURING SCHEDULED D CHECK, FOUND DOOR FRAME COVERPLATE DENTED AND GOUGED AT BS 790-794, RBL 22-36, WL 160. REMOVED AND REPLACED PER BOEING SRM.
Part: SKIN — CRACKED (BS 327)
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD GALLEY DOORWAY AFT LOWER SKIN CUTOUT AT BS 327, WL 210. REPAIRED PER BOEING SRM.
Part: WEB — CORRODED (BS 767-787)
DURING SCHEDULED D CHECK, FOUND VERTICAL SUPPORT WEB CORRODED AT BS 767-787, RBL 21, WL 158. REPAIRED PER BOEING SRM.
Part: BRACKET — CRACKED (FUSELAGE)
DURING SCHEDULED D CHECK, FOUND E1-3 RACK CRACKED AT L BRACKET FRONT AND CENTER. REMOVED AND REPLACED PER BOEING SRM.
Part: FRAME — DENTED (BS 767)
DURING SCHEDULED D CHECK, FOUND DENTED FRAME AT BS 767, RBL 32, WL 159. REMOVED AND REPLACED PER BOEING SRM.
Part: SKIN — DENTED (BS 937)
DURING SCHEDULED D CHECK, FOUND DENTED SKIN AT BS 937, 3 ABOVE STR 19L, WL 199. REPAIRED PER BOEING SRM.
Part: WEB — CORRODED (BS 847-867)
DURING SCHEDULED D CHECK, FOUND VERTICAL SUPPORT WEB CORRODED AT BS 847-867, RBL 18, WL 162. REPAIRED PER BOEING SRM.
Part: STRAP — CORRODED (BS 787-854)
DURING SCHEDULED D CHECK, FOUND CORRODED SILL WEB TIE STRAP AT BS 787-854, RBL 19, WL 157. REMOVED AND REPLACED PER BOEING SRM.
Part: FRAME — CRACKED (BS 328)
DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 328, RT STR 20. REPAIRED PER BOEING SRM.
Part: CLIP — CRACKED (BS 927)
DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 26 RT. REMOVED AND REPLACED PER BOEING SRM.
Part: FLOORBEAM — CORRODED (BS 727-947)
DURING SCHEDULED D CHECK, FOUND CORRODED ON CARGO FLOORBEAM AROUND NUTPLATE LOCATIONS AT BS 727-947, LBL 12.5, WL 159. REMOVED AND REPLACED PER BOEING SRM.
Part: WEB — CORRODED (BS 794-847)
DURING SCHEDULED D CHECK, FOUND CORRODED SILL WEB AT BS 794-847, RBL 19, WL 162. REMOVED AND REPLACED PER BOEING SRM.
Part: FLOORBEAM — CORRODED (BS 727-947)
DURING SCHEDULED D CHECK, FOUND CORRODED CARGO FLOORBEAM AROUND NUTPLATE AT BS 727-947, LBL 3, WL 159. REMOVED AND RELACED PER BOEING SRM.
Part: FRAME — CORRODED (BS 847)
DURING SCHEDULED D CHECK, FOUND CORRODED CARGO BAY DOOR FRAME AT BS 847, RBL 23-27, WL 163. REMOVED AND REPLACED PER BOEING SRM.
Part: STIFFENER — CRACKED (BS 178)
DURING SCHEDULED D CHECK, FOUND CRACKED VERTICAL STIFFENER AT BS 178, LBL 5.7, WL 185. REMOVED AND REPLACED PER BOEING SRM.
Part: FLOORBEAM — CORRODED (BS 727-947)
DURING SCHEDULED D CHECK, FOUND CORRODED CARGO FLOORBEAM AROUND NUTPLATE AT BS 727-947, RBL 3, WL 159. REMOVED AND REPLACED PER BOEING SRM.
Part: KEEL BEAM — DAMAGED (BS 720-727)
DURING SCHEDULED D CHECK, FOUND CHAFING DAMAGED TO KEELBEAM AT BS 720-727 O/B FLANGE. REPAIRED PER TRAMCO EWO 98-0834
Part: WEB — CRACKED (BS 178-180)
DURING SCHEDULED D CHECK, FOUND CRACKED VERTICAL BEAM WEB AT BS 178-180, LBL 5.7, WL 188. REMOVED AND REPLACED PER BOEING SRM.
Part: FLOORBEAM — CORRODED (BS 727-947)
DURING SCHEDULED D CHECK, FOUND CORRODED CARGO FLOORBEAM AROUND NUTPLATE AT BS 727-947, RBL 8, WL 159. REMOVED AND REPLACED PER BOEING SRM.
Part: CLIP — BENT (BS 727)
DURING SCHEDULED D CHECK, FOUND STRINGER CLIP BENT AT BS 727, STR 26 LT. REMOVED AND REPLACED PER BOEING SRM.
Part: STRINGER — CRACKED (BS 1143)
DURING SCHEDULED D CHECK, FOUND STRINGER 5 LT LOWER CHORD CRACKED AT BS 1143. REMOVED AND REPLACED PER BOEING SRM.
Part: ANGLE — CRACKED (BS 178)
DURING SCHEDULED D CHECK, FOUND CRACKED FLOOR SUPPORT ANGLE AT BS 178, LBL 18 WL 207. REPAIRED PER BOEING SRM.
Part: SKIN — CRACKED (BS 178)
DURING SCHEDULED D CHECK, FOUND CRACKED AT BS 178, WL 194-198, RBL 4.5. REPAIRED PER BOEING SRM.
Part: TIE DOWN — CORRODED (BS 847)
DURING SCHEDULED D CHECK, FOUND CORRODED CARGO TIE DOWN STANSIONS AT BS 847, LBL 31-59, WL 174. REMOVED AND REPLACED PER BOEING SRM.
Part: ANGLE — WORN (BS 717)
DURING SCHEDULED D CHECK, FOUND RT WHEEL WELL ATTACH ANGLE HAS ELONGATED FASTENER HOLES AT BS 717, RBL 20, WL 149. REPAIRED PER BOEING SRM.
Part: ANGLE — CRACKED (BS 178)
DURING SCHEDULED D CHECK, FOUND CRACKED SUPPORT ANGLE AT BS 178, RBL 28 WL 207. REPAIRED PER BOEING SRM.
Part: STRAP — CRACKED (BS 312)
DURING SCHEDULED D CHECK, FOUND STABILIZER STRAP CRACKED AT BS 312, LBL 12, WL 200. REPAIRED PER BOEING SRM.
Part: STIFFENER — CRACKED (VERT STAB)
DURING SCHEDULED D CHECK, FOUND CRACKED STIFFENER ON RT VERTICAL FIN REAR SPAR AT FIN BS 119.0 IN TRAILING EDGE CAVITY. REPAIRED PER BOEING SRM.
Part: INTERCOSTAL — CRACKED (BS 380 - 400)
DURING SCHEDULED D CHECK, FOUND INTERCOSTAL ATTACH BRACKETS ARE CRACKED AT BS 380 AND BS 400, RBL 25, WL 154. REPAIRED PER BOEING SRM.
Part: ANGLE — DENTED (BS 947)
DURING SCHEDULED D CHECK, FOUND SUPPORT ANGLE CRACKED AFT SIDE OF FRAME AT BS 947, STR 22 LT.; AND BS 947 AT STR 23 LT. REPAIRED PER BOEING SRM.
Part: INTERCOSTAL — CRACKED (BS 420)
DURING SCHEDULED D CHECK, FOUND INTERCOSTAL ATTACH BRACKETS ARE CRACKED AT BS 420, RBL 25, WL 154. REPAIRED PER BOEING SRM.
Part: WEB — CRACKED (BS 178)
DURING SCHEDULED D CHECK, FOUND CRACKED FLOOR WEB AT BS 178, RBL 25-29, WL 207. REPAIRED PER BOEING SRM.
Part: FRAME — DENTED (BS 807)
DURING SCHEDULED D CHECK, FOUND DENTED FRAME AT BS 807, LBL 48, WL 172. REMOVED AND REPLACED PER BOEING SRM.
Part: DOUBLER — DAMAGED (BS 683)
DURING SCHEDULED D CHECK, FOUND DAMAGED AREA AT BS 683, BETWEEN STR 6R AND STR 7R. REPAIRED PER BOEING SRM.
Part: SHEAR TIE — GOUGE (BS 1121)
DURING SCHEDULED D CHECK, FOUND GOUGE IN SHEAR TIE AT BS 1121, STR 2L. REPAIRED PER BOEING SRM.
Part: ANGLE — CRACKED (BS 348.2)
DURING SCHEDULED D CHECK, FOUND CRACKED AT BS 348.2, WL 221, LBL 65. REMOVED AND REPLACED PER BOEING SRM.
Part: INTERCOSTAL — CRACKED (BS 360)
DURING SCHEDULED D CHECK, FOUND CRACKED BS 360 AT STR 11 ON INTERCOSTAL WL 254, LBL 60. REPAIRED PER BOEING SRM.
Part: FRAME — DENTED (BS 727)
DURING SCHEDULED D CHECK, FOUND DENTED FRAME AT BS 727E, LBL 42, WL 166. REPAIRED PER BOEING SRM.
Part: BULKHEAD — CRACKED (BS 178)
DURING SCHEDULED D CHECK, FOUND BULKHEAD CRACKED AT BS 178, WL 197.5-199.75, LBL 4.7; WL 199-200, LBL 6.7 AND WL 210-2210.75 LBL 6.7. REPAIRED PER BOEING SRM.
Part: STRAP — CORRODED (BS 772)
DURING SCHEDULED D CHECK, FOUND FLOOR PANEL TIE STRAP CORRODED AT BS 772, RBL 21 LBL 21 WL 156. REMOVED AND REPLACED PER BOEING SRM.
Part: SHEAR TIE — CRACKED (BS 360)
DURING SCHEDULED D CHECK, FOUND CRACKED SHEAR TIE BETWEEN STRINGER 14 AND 15 AT BS 360, WL 228, LBL 69. REPAIRED PER BOEING SRM.
Part: BULKHEAD — CRACKED (BS 178)
DURING SCHEDULED D CHECK, FOUND BULKHEAD CRACKED AT BS 178, WL 197.5-198, RBL 6.7; WL 210-210.5, RBL 6.7 AND WL 209-210, RBL 4.7. REPAIRED PER BOEING SRM.
Part: STRINGER — CRACKED (BS 907)
DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4 L/T. REPAIRED PER BOEING SRM.
Part: INTERCOSTAL — CRACKED (BS 380)
DURING SCHEDULED D CHECK, FOUND CRACKED FWD END OF INTERCOSTAL AT BS 380 LBL 25, W156. REPAIRED PER BOEING SRM.
Part: FLOORBEAM — CRACKED (BS 328)
DURING SCHEDULED D CHECK, FOUND FLOORBEAM STIFFENER ANGLE CRACKED AT BS 328, RBL 32, WL 200. REPAIRED PER BOEING SRM.
Part: BULKHEAD WEB — CRACKED (BS 178)
DURING SCHEDULED D CHECK, FOUND CRACKED BULKHEAD WEB AT BS 178, RBL 5, LBL 5, WL 188. REPAIRED PER BOEING SRM.
Part: ANGLE — CRACKED (BS 535.5)
DURING SCHEDULED D CHECK, FOUND WEB SUPPORT ANGLE CRACKED AT BS 535.5, RBL51, WL 175. REPAIRED PER BOEING SRM.
Part: BRACKET — CRACKED (BS 328)
DURING SCHEDULED D CHECK, FOUND LOWER AIRSTAIR DOOR SILL, FRAME ATTACH BRACKET CRACKED AT BS 328.
Part: INTERCOSTAL — CRACKED (BS 295)
DURING SCHEDULED D CHECK, FOUND CRACKED BS 295, STR 12 ON INTERCOSTAL WL 244, LBL 55. REPAIRED PER TI-A53-02.
Part: SEAL — WORN (RT LE FLAP)
DURING SCHEDULED C2 CHECK, FOUND K-FLAP BULB SEAL WORN. REMOVED AND REPLACED PER BOEING SRM.
Part: SEAL — WORN (RT LE FLAP)
DURING SCHEDULED C2 CHECK, FOUND O/B K-FLAP TEFLON RUBSTRIP AND SEAL WORN. REMOVED AND REPLACED PER BOEING SRM.
1997
Part: LAMP — INOPERATIVE (CABIN)
DURING SCHEDULED C3 CHECK, FOUND TWO RED TRACK LIGHTS INOP. RELAMPED PER BOEING M/M.
1996
Part: SKIN — DENTED (BS 350)
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN DENTED AT BS 350, S18R. REPAIRED PER BOEING SRM.
Part: BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY OVERHEAD EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.
1995
Part: SKIN — CRACKED (BS 727D)
DURING SCHEDULED TERM CHECK, FOUND A 1.7 FUSELAGE SKIN CRACK AT S23R, BS 727D AND AT S23R, MEASURING 1.6 LONG. REPAIRED BOTH PER BOEING STRUCTURAL REPAIR MANUAL.
Part: ADC — INOP (RT FLIGHT DECK)
ON TAKEOFF, FIRST OFFICER'S AIRSPEED AND ALTIMETER INDICATORS BECAME INOPERATIVE. BUFFET ALERT ON CDU, AND SPEED TRIM FAIL LIGHT ILLUMINATED. AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING. REPLACED FIRST OFFICER'S AIR DATA COMPUTER PER BOEING MM.