N348SW
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.
282 reports on file, 1997-03-23 – 2012-04-30.
Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 75,021 hrs · 65,594 cycles
CABIN WARNING HORN SOUNDED AT 36K. CABIN AT 11.5K AT HIGHEST POINT. AT 25K DURING EMERGENCY DESCENT REGAINED CONTROL OF CABIN AT 25K, LEVELED OFF AT 20K. REMOVED AND REPLACED OUT FLOW VALVE AND HEATER GASKET PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,781 hrs · 65,408 cycles
L1 DOOR OPENING HAS EMERGENCY LIGHT STRIP BULB INOP. RELAMPED PER MM.
Part: DUCT — LOOSE (AC BAY) · airframe 74,470 hrs · 65,178 cycles
EMERGENCY DESCENT, LOSS OF PRESSURIZATION AT FL350 CABIN ALT REACHED 15,000FT DURING DESCENT TO 10,000FT LOSS OF PRESS & EMERG DESCENT QRH COMPLETE "PASS OXYGEN ON" LIGHT WITH DROPPED MASK DURING DESCENT. REMOVED AND REPLACED BOOT, DUCT, AND CLAMP PER MM.
Earlier reports · 1997–2011 · 279 reports
2011
Part: FAN — FAULTY (A/C BAY) · airframe 73,672 hrs · 64,564 cycles
AT CRUISE, FLIGHT ATTENDANTS REPORTED FAINT "BURNING RUBBER" ODOR FROM VENTILATION. REMOVED AND REPLACED RECIRULATION FAN PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 73,100 hrs · 64,113 cycles
DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 727E+12.5 TO BS 727E+13, STR 18R. REPAIRED SKIN PER SRM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 73,100 hrs · 64,113 cycles
DURING SCHEDULED SPV CHECK, FOUND FORWARD EMERGENCY EXIT SIGNS INOP. CHARGED BATTERIES PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 73,100 hrs · 64,113 cycles
DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 500B+16, STR 15L. REPAIRED SKIN PER SRM.
Part: BEAM — CRACKED (FUSELAGE) · airframe 73,100 hrs · 64,113 cycles
DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL BEAM WEB CRACKED AT BS 639, RBL 45.5. REPAIRED WEB PER ER.
Part: SKIN — CRACKED (FUSELAGE) · airframe 73,100 hrs · 64,113 cycles
DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 740, STR 18L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 73,100 hrs · 64,113 cycles
DURING SCHEDULE SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 759 TO BS 761.5, STR 16L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 73,100 hrs · 64,113 cycles
DURING SCHEDULE SPV CHECK, FOUND SKIN CRACKED AT BS 500+5, STR 16L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 73,100 hrs · 64,113 cycles
DURING SCHEDULE SPV CHECK, FOUND SKIN CRACKED AT BS 494.5, STR 16L. REPAIRED SKIN PER SRM.
Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 71,913 hrs · 63,190 cycles
R2 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT. RE-INSTALLED SLIDE PER MT.
Part: GASPER FAN — FAULTY (CARGO BAY) · airframe 71,255 hrs · 62,684 cycles
AIR TURNBACK, UPON LEVEL OFF AT FL 310 FLIGHT ATTENDANT REPORTED THERE WAS A STRONG ELECTRICAL SMOKE SMELL IN AFT CABIN. VERIFIED GASPER FAN EMITTING ODOR. REMOVED AND REPLACED GASPER FAN PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 71,191 hrs · 62,642 cycles
DURING SCHEDULED SPV CHECK, FOUND CRACK AT STA 727E +3, BELOW STR 19R. REPAIRED DOUBLER PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 71,189 hrs · 62,641 cycles
DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 911, STR 21L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 71,189 hrs · 62,641 cycles
DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 730E, STR 19R. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 71,189 hrs · 62,641 cycles
DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 730E, STR 19L. REPAIRED SKIN PER SRM.
2010
Part: SKIN — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 821, STR 24R. REPAIRED SKIN PER SRM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 668.75, LBL 24.8. REPAIRED CHORD PER EO.
Part: SKIN — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 328, STR 17R. REPAIRED SKIN PER EO AND EA.
Part: SKIN — CORRODED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND SKIN CORRODED AT BS 1002.5, STR 23L. REMOVED AND REPLACED SKIN PER SRM AND BAC DWG.
Part: SKIN — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 960, STR 17L. REPAIRED SKIN PER EO AND EA.
Part: STRAP — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND SKIN STRAP CRACKED AT BS 950.5, STR 24L. REMOVED AND REPLACED STRAP PER SRM AND BAC DWG.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4R. REMOVED AND REPLACED CLIP PER SRM.
Part: LIGHT — BROKEN (CABIN) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND LT EEPLS BROKEN. REMOVED AND REPLACED EEPLS PER MM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 1112, STR 6R. REPAIRED FRAME PER SRM AND BAC DWG.
Part: LIGHT — BROKEN (CABIN) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND RT EEPLS BROKEN. REMOVED AND REPLACED EEPLS PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND FWD OVERHEAD EMERGENCY EXIT LIGHT BULB INOP. REMOVED AND REPLACED BULB PER MM.
Part: SKIN — DELAMINATED (FOREFLAP) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND RT WING O/B FORE FLAP UPPER SKIN I/B DELAMINATED. REPAIRED SKIN PER SRM.
Part: LIGHT — DAMAGED (CABIN) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND EEPLS DAMAGED. REMOVED AND REPLACED EEPLS PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT BULB INOP. REMOVED AND REPLACED BULB PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT BULB INOP. REMOVED AND REPLACED BULB PER MM.
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND SUPPORT ANGLE CRACKED BETWEEN BS 277 TO BS 291.5, BETWEEN STR 11R TO STR 12R. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.
Part: SKIN — DELAMINATED (FOREFLAP) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND RT WING O/B FORE FLAP SKIN DELAMINATED. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 960, STR 17R. REPAIRED SKIN PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4L. REMOVED AND REPLACED CLIP PER SI.
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND ANGLE SUPPORT CRACKED BETWEEN BS 277 TO BS 291.5, BETWEEN STR 9R TO STR 10R. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER SRM.
Part: SKIN — DELAMINATED (LE SLAT) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND LT WING NR 3 SLAT SKIN I/B END DELAMINATED. REMOVED AND REPLACED SLAT PER MM.
Part: SKIN — DELAMINATED (LE SLAT) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 6 SLAT SKIN O/B DELAMINATED. REMOVED AND REPLACED SLAT PER MM.
Part: SKIN — DELAMINATED (SPOILER) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND LT WING NR 1 SPOILER SKIN DELAMINATED. REPAIRED SKIN PER SRM.
Part: SKIN — DELAMINATED (TE FLAP) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND LT WING AFT FLAP UPPER SKIN DELAMINATED AT O/B END. REPAIRED AFT FLAP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 4R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, LBL 27. REPAIRED BEAM PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND FRAME WEB CRACKED AT BS 277, BETWEEN STR 14R TO STR 15R. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.
Part: FRAME — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND FRAME WEB CRACKED AT BS 277, BETWEEN STR 15R TO STR 16R. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.
Part: SKIN — DELAMINATED (LE SLAT) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND LT WING NR 1 SLAT SKIN DELAMINATED. REPAIRED SKIN PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 294.5, LBL 54. REPAIRED BEAM PER SRM.
Part: WEB — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND SUPPORT STRUCTURE WEB CRACKED BETWEEN BS 294.5 TO BS 305.5, STR 7L. REMOVED AND REPLACED WEB PER BAC DWG.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 967, LBL 5. REPAIRED BEAM PER SRM.
Part: SKIN — DELAMINATED (LE SLAT) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND LT WING NR 2 SLAT SKIN DELAMINATED. REPAIRED SKIN PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 23L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 9L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 712, BBL 0.0. REPAIRED BEAM PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, LBL 49. REPAIRED BEAM PER SRM.
Part: SKIN — DELAMINATED (LE SLAT) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 4 SLAT SKIN DELAMINATED. REPAIRED SKIN PER SRM.
Part: SKIN — DELAMINATED (LE SLAT) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 5 SLAT SKIN DELAMINATED. REPAIRED SKIN PER SRM.
Part: LENS — BROKEN (CABIN) · airframe 70,294 hrs · 61,956 cycles
DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.
Part: SLIDE — OUT OF LIMITS (L1 DOOR) · airframe 70,204 hrs · 61,889 cycles
DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MT.
Part: LIGHT — WORN (CABIN) · airframe 69,474 hrs · 61,315 cycles
DURING SCHEDULED 2HC1 CHECK, FOUND RT EEPLS WORN AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 69,474 hrs · 61,315 cycles
DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 922, STR 23L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 69,474 hrs · 61,315 cycles
DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 377, STR 15L. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 69,321 hrs · 61,195 cycles
DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 923, STR 22L. REPAIRED SKIN PER SWA EA.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,749 hrs · 60,768 cycles
DURING SCHEDULED MV1 CHECK, FOUND FWD EEPLS LAMPS INOP NEAR FWD DOORS. RELAMPED PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,440 hrs · 60,550 cycles
DURING SCHEDULED SPV CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,440 hrs · 60,550 cycles
DURING SCHEDULED SPV CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 68,440 hrs · 60,550 cycles
DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 482, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 68,440 hrs · 60,550 cycles
DURING SCHEDULED SPV CHECK, FOUND SKIN AT BS 328, BETWEEN STR 19R TO STR 20R. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 68,440 hrs · 60,550 cycles
DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 740E, STR 18R. REPAIRED SKIN PER SRM.
2009
Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 68,056 hrs · 60,241 cycles
DURING SCHEDULED SPV CHECK, FOUND R1 DOOR LOWER FRAME WEB CRACKED. REMOVED AND REPLACED DOOR PER SRM.
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,054 hrs · 60,240 cycles
DURING SCHEDULED SPV CHECK, FOUND R1 DOOR LOWER CUTOUT FRAME WEB CRACKED. REPAIRED FRAME PER SRM.
Part: SLAT — DELAMINATED (RT WING) · airframe 68,056 hrs · 60,241 cycles
DURING SCHEDULED SPV CHECK, FOUND RT WING NR 5 L/E SLAT O/B TRAILING EDGE DELAMINATED. REMOVED AND REPLACED SLAT PER SRM.
Part: FITTING — CRACKED (SPOILER) · airframe 68,054 hrs · 60,240 cycles
DURING SCHEDULED HC2 CHECK, FOUND RT WING I/B GROUND SPOILER I/B ACTUATOR MOUNT HOUSING CRACKED. REMOVED AND REPLACED FITTING PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 68,054 hrs · 60,240 cycles
DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 271, STR 16L. REPAIRED SKIN PER SRM.
Part: LUG — CORRODED (VERTICAL STAB) · airframe 67,910 hrs · 60,128 cycles
DURING SCHEDULED 20Y CHECK, FOUND VERTICAL STABILIZER LT AND RT FAIL-SAFE FWD LUG CORRODED. REPAIRED LUG PER EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 66,511 hrs · 59,071 cycles
DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 923, STR 25L. REPAIRED SKIN PER SRM.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 66,059 hrs · 58,752 cycles
DURING SCHEDULED MV1 CHECK, FOUND EXTERNAL EMERGENCY LIGHT AFT OF I/B AFT LT FLAP INOP. RELAMPED PER MM.
2008
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,849 hrs · 57,901 cycles
DURING SCHEDULED 20Y CHECK, FOUND LOWER CHORD CORRODED AT BS 227, BETWEEN BL 0 TO RBL 5. REPAIRED CHORD PER SWA EA.
Part: FITTING — CORRODED (VERTICAL STAB) · airframe 64,849 hrs · 57,901 cycles
DURING SCHEDULED 20Y CHECK, FOUND VERTICAL STABILIZER LT O/B FWD LUG FITTING CORRODED. REPAIRED FITTING PER SWA EA.
Part: FITTING — CORRODED (VERTICAL STAB) · airframe 64,849 hrs · 57,901 cycles
DURING SCHEDULED 20Y CHECK, FOUND VERTICAL STABILIZER RT O/B FWD LUG FITTING CORRODED. REPAIRED FITTING PER SWA EA.
Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 64,849 hrs · 57,901 cycles
DURING SCHEDULED 20Y CHECK, FOUND RT FWD CARGO KEEL BEAM CORRODED AT BS 524. REPAIRED KEEL BEAM PER SRM.
Part: FITTING — CORRODED (VERTICAL STAB) · airframe 64,849 hrs · 57,901 cycles
DURING SCHEDULED 20Y CHECK, FOUND VERTICAL STABILIZER LT OUTBOARD REAR LUG FITTING CORRODED. REPAIRED FITTING PER EA.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,849 hrs · 57,901 cycles
DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE STRINGER ANGLE CRACKED AT BS 301, STR 10L. REPAIRED ANGLE PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 64,849 hrs · 57,901 cycles
DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN AT L1 DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 64,849 hrs · 57,901 cycles
DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN AT L1 DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED SKIN PER EA.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,849 hrs · 57,901 cycles
DURING SCHEDULED 20Y CHECK, FOUND STRINGER CRACKED AT BS 788, STR 16R. REPAIRED STRINGER PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,849 hrs · 57,901 cycles
DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 28L. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,849 hrs · 57,901 cycles
DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 28L. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,849 hrs · 57,901 cycles
DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,849 hrs · 57,901 cycles
DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28R. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,849 hrs · 57,901 cycles
DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,849 hrs · 57,901 cycles
DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 27L. REMOVED AND REPLACED CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,849 hrs · 57,901 cycles
DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 21L. REMOVED AND REPLACED CLIP PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 64,849 hrs · 57,901 cycles
DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BETWEEN BS 415 TO BS 417, STR 1. REPAIRED SKIN PER SWA EA.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 64,832 hrs · 57,885 cycles
DURING SCHEDULED MV2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 64,399 hrs · 57,551 cycles
DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 931, STR 21L. REPAIRED SKIN PER SWA EA.
Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 63,381 hrs · 56,833 cycles
DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR FWD FRAME CRACKED AT LOWER STOP FITTING. REMOVED AND REPLACED L1 DOOR PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 63,381 hrs · 56,833 cycles
DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,189 hrs · 56,684 cycles
DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 63,067 hrs · 56,592 cycles
DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 981, STR 22L. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 62,952 hrs · 56,507 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA BS 390, STR 28R. REPAIRED SKIN PER EA.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,952 hrs · 56,507 cycles
DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 460, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 62,952 hrs · 56,507 cycles
DURING SCHEDULED SPV CHECK, FOUND STRINGER 16L CRACKED BETWEEN BS 348 AND BS 360. REPAIRED STRINGER PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 62,952 hrs · 56,507 cycles
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 410, BL 0. REPAIRED SKIN PER EA AND SB.
Part: SOLENOID — FAULTY (GEAR HANDLE) · airframe 62,434 hrs · 56,112 cycles
DIVERSION/DECLARED EMERGENCY. DURING CLIMBOUT OF TUS LANDING GEAR HANDLE WOULD NOT MOVE FROM THE UP POSITION TO THE OFF POSITION. REMOVED AND REPLACED GEAR HANDLE SOLENOID PER MM.
2007
Part: WINDOW — ARCED (COCKPIT) · airframe 62,089 hrs · 55,848 cycles
FLIGHT DECK R1 WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM.
Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 61,765 hrs · 55,607 cycles
DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,765 hrs · 55,607 cycles
DURING SCHEDULED HC2 CHECK, LT FWD CABIN EMERGENCY EXIT LIGHTS WOULD NOT SHUT OFF WITH PILOT SWITCH. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 61,439 hrs · 55,358 cycles
DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 930 AND BS 952, STR 23R. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 61,439 hrs · 55,359 cycles
FUSELAGE SKIN CRACKED AT BS 518, STR 16L. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 61,439 hrs · 55,358 cycles
DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518D, STR 16L. REPAIRED SKIN PER SWA EA.
Part: FRAME — CRACKED (BS 747 S8L) · airframe 61,328 hrs · 55,275 cycles
DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.
Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 59,985 hrs · 54,210 cycles
DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
Part: SKIN — DELAMINATED (TE FLAP) · airframe 59,814 hrs · 54,068 cycles
DURING SCHEDULED SERVICE CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT LOWER OUTBOARD END. REMOVED AND REPLACED AFT FLAP PER MM.
Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 59,723 hrs · 53,998 cycles
DURING SCHEDULED SERVICE CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,663 hrs · 53,951 cycles
DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
Part: SKIN — CRACKED (BS 791 S17L) · airframe 59,615 hrs · 53,910 cycles
DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 791, STR 17L. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (BS 791 S17L) · airframe 59,615 hrs · 53,910 cycles
DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 791, STR 17L. REPAIRED SKIN PER SRM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,074 hrs · 53,505 cycles
DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 21 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM.
2006
Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 58,898 hrs · 53,363 cycles
L2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. REMOVED AND REPLACED EVAC SLIDE PER MM.
Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 58,847 hrs · 53,321 cycles
L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 58,239 hrs · 52,870 cycles
DURING SCHEDULED MV2 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 58,185 hrs · 52,829 cycles
DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 727B TO BS 727C, STR 17L. REPAIRED WEB PER SWA EA.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 58,185 hrs · 52,829 cycles
DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 907 TO BS 927, STR 17L. REPAIRED WEB PER SWA EA.
Part: DUCT — CRACKED (CABIN) · airframe 58,140 hrs · 52,791 cycles
DURING FLIGHT CREW REPORTED LARGE AMOUNTS OF INSULATION BLEW INTO MID CABIN. REMOVED AND REPLACED MAIN CABIN AIR CENTER DUCT PER MM.
Part: PRESSURE PANEL — CORRODED (NLG WW) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND NLG W/W WEB CORRODED AT RT BS 243 TO BS 251, WL 171. REMOVED AND REPLACED NLG W/W WEB SECTION PER SWA EA.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND LT OVERWING CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.
Part: WEB — CRACKED (BS 243-251) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND NLG W/W WEB CRACKED BETWEEN RT BS 243 AND RT BS 251, WL 174. REPAIRED WEB PER SWA EA.
Part: FRAME — CORRODED (NLG WW) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND RT NLG W/W FRAMECORRODED, BS 243 TO BS 251. REPAIRED W/W FRAME PER SRM.
Part: FRAME — CRACKED (BS 706 S8R-8L) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R AND STR 8L. REPAIRED FRAME SECTION PER ACO.
Part: FRAME — CRACKED (BS 480 S13R) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 13R. REPAIRED FRAME SECTION PER SWA EA.
Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN BATTERY PACK HOUSING CONNECTOR PIN BENT. REMOVED AND REPLACED BATTERY PACK HOUSING PER MM.
Part: FRAME — CRACKED (BS 867 S8R) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME SECTION PER SWA EA.
Part: SKIN — CRACKED (NR 1 SLAT) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT LOWER AUX TRACK CUTOUT SURFACE. REPAIRED NR 1 L/E SLAT PER SRM.
Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND BELT FRAME CRACKED AT BS 420, STR 13L. REPAIRED BELT FRAME PER SWA EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,129 hrs · 82,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME SECTION PER SWA EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,129 hrs · 82,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME SECTION PER SWA EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,129 hrs · 82,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME SECTION PER SWA EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,129 hrs · 82,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME SECTION PER SWA EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,129 hrs · 82,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME SECTION PER SWA EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,129 hrs · 82,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME SECTION PER SWA EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME SECTION PER SWA EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME SECTION PER SWA EA.
Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 664, RBL 40. REPAIRED PRESSURE WEB PER SRM.
Part: FRAME — CRACKED (BS 520 S8L) · airframe 58,129 hrs · 52,871 cycles
DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME SECTION IAW SWA EA.
Part: BRACKET — LOOSE (L1 DOOR SLIDE) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR BRACKET LOOSE. REMOVED AND REPLACED GIRT BAR BRACKET FASTENERS IAW SRM.
Part: BELTFRAME — CRACKED (BS 380 S13L) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 380, STR 13L. REPAIRED BELTFRAME IAW SWA EA.
Part: FRAME — CRACKED (BS 480 S8L) · airframe 58,129 hrs · 52,871 cycles
DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME SECTION IAW SWA EA.
Part: FRAME — CRACKED (BS 500C S8L) · airframe 58,129 hrs · 52,871 cycles
DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME SECTION IAW SWA EA.
Part: SKIN — CRACKED (LT WING SLAT) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND LT WING NR 2 L/E SLAT LOWER SURFACE CRACKED AT OB AUX TRACK LOCATION. REPAIRED SLAT IAW SRM.
Part: FRAME — CRACKED (BS 380 S8R) · airframe 58,129 hrs · 52,871 cycles
DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME SECTION IAW SWA EA.
Part: FRAME — CRACKED (BS 360 S16L) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 360, STR 16L. REPAIRED BELTFRAME PER SWA EA.
Part: STRINGER CLIP — CRACKED (BS 294) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 294) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 360) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: CREASE BEAM — CORRODED (BS 907-927) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 907 TO BS 927, STR 17L. REPAIRED CREASE BEAM WEB PER SRM.
Part: CREASE BEAM — CORRODED (BS 727B-727C) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 727B TO BS 727C, STR 17L. REPAIRED CREASE BEAM WEB PER SWA EA.
Part: STRINGER CLIP — CRACKED (BS 360 S9L) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 360) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 294) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 277 S15R) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 360 S5L) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 277 S10R) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (BS 277 S15L) · airframe 58,129 hrs · 52,781 cycles
DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,382 hrs · 52,144 cycles
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE FRAME CRACKED AT AFT CARGO DOOR CUTOUT FWD FRAME, UPPER STOP FITTING. REPAIRED FRAME SECTION PER SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 57,382 hrs · 52,144 cycles
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR FRAME, LOWER HINGE CUTOUT. REPAIRED SKIN PER EA AND SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 57,382 hrs · 52,144 cycles
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 420, BL 0. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 57,382 hrs · 52,144 cycles
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR FRAME, UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 56,560 hrs · 51,502 cycles
DURING SCHEDULED A1 CHECK, MID CABIN EMERGENCY BULLNOSE EXIT LIGHTS BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
2005
Part: SIGN — BROKEN (CABIN) · airframe 55,806 hrs · 50,935 cycles
LT CABIN EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM.
Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 55,690 hrs · 50,855 cycles
R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATED OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.
Part: SKIN — CORRODED (FUSELAGE) · airframe 55,367 hrs · 50,589 cycles
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 986.5, BL 0. REPAIRED SKIN PER SRM.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,190 hrs · 50,467 cycles
DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 13. RELAMPED LIGHT PER MM.
Part: ACTUATOR — FAULTY (RT MLG WW) · airframe 53,990 hrs · 49,491 cycles
UPON NORMAL GEAR EXTENSION, RT MAIN GEAR DID NOT INDICATE EXTENDED, RED LIGHT ILLUMINATED. MANUALLY EXTENDED RT MAIN GEAR, NORMAL INDICATIONS, GREEN LIGHT ILLUMINATED. REMOVED AND REPLACED UPLOCK ACTUATOR PER MM.
Part: WEB — CRACKED (FUSELAGE) · airframe 53,956 hrs · 49,463 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA FUSELAGE FLOOR WEB CRACKS BETWEEN BS 188 TO BS 196, LBL 30 & RBL 30, WL 208. REPAIRED WEB SECTIONS PER SRM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 53,956 hrs · 49,463 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE BULKHEAD WEB CRACKED AT BS 178, LBL 25, WL 207. REPAIRED WEB PER SRM.
Part: WEB — CRACKED (FUSELAGE) · airframe 53,956 hrs · 49,463 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FLOOR WEB CRACKED AT BS 188 TO BS 196, LBL 30, WL 208. REPAIRED WEB PER SRM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 53,956 hrs · 49,463 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE BULKHEAD WEB CRACKED AT BS 178, LBL 25, WL 207. REPAIRED WEB PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,956 hrs · 49,463 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, LT SIDE, WL 208. REMOVED AND REPLACED STUB FRAME PER SRM.
Part: SHEAR TIE — CRACKED (FWD BULKHEAD) · airframe 53,956 hrs · 49,463 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 178 BLKHD, RBL 31, WL 208. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: WEB — CRACKED (FUSELAGE) · airframe 53,956 hrs · 49,463 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FLOOR WEB CRACKED AT BS 188 TO BS 196, RBL 30, WL 208. REPAIRED WEB PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,956 hrs · 49,463 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, RT SIDE, WL 208. REMOVED AND REPLACED STUB FRAME PER SRM.
Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 53,445 hrs · 49,018 cycles
DURING SCHEDULED C2 CHECK, FOUND CORROSION ON KEELBEAM, LT SIDE, BS 500D. REPAIRED KEEL BEAM PER SWA EA.
Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 53,445 hrs · 49,018 cycles
DURING SCHEDULED C2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR SLIDE PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 53,445 hrs · 49,018 cycles
DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACK AT BS 500D, STR 10R. REPAIRED SKIN PER SWA EA.
Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 53,445 hrs · 49,018 cycles
DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR SLIDE PER MM.
Part: LIGHT — CRACKED (CABIN) · airframe 53,191 hrs · 48,822 cycles
DURING SCHEDULED A2 CHECK, FOUND EMERGENCY EXIT LIGHT HOUSING AT ROW 1 DEF, CRACKED. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.
2004
Part: SKIN — CORRODED (FUSELAGE) · airframe 54,458 hrs · 48,256 cycles
DURING SCHEDULED C1 CHECK, FOUND CORROSION BULGE AT FUSELAGE SKIN BS 440, STR 22R. REPAIRED SKIN PER SRM.
Part: CABLE — MISROUTED (L2 DOOR GIRT BAR) · airframe 52,421 hrs · 48,227 cycles
DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED L2 DOOR CABLE PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 51,599 hrs · 47,573 cycles
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 517, STRINGER 10R, BS 506, STRINGER 10L, CRACKED. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (RT WING SLAT) · airframe 51,599 hrs · 47,573 cycles
DURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 6 L/E SLAT SKIN CRACKED. REPAIRED RIGHT WING NR 6 L/E SLAT SKIN PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 50,997 hrs · 47,054 cycles
DURING SCHEDULED SERVICE CHECK, FOUND 3 EA FUSELAGE SKIN CRACKS AT BS 930 TO BS 947, BETWEEN STRINGERS 21R & 24R. REPAIRED SKIN PER SWA EA & SRM.
Part: GLOWSTRIP — LOOSE (CABIN) · airframe 50,876 hrs · 46,957 cycles
PHOTO LUMINESCENT STRIP LOOSE AT RT ROW 7 AND RT ROW 8. SECURED STRIP PER MM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 50,214 hrs · 46,406 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FWD CARGO DOOR FRAME CUTOUT AT BS 440, LOWER STOP CRACKED. REPAIRED FRAME PER T1-653-044.
Part: LENS — MISSING (EMERGENCY EXIT) · airframe 50,214 hrs · 46,406 cycles
DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY EXIT LIGHT LENS MISSING IN BULLNOSE AT ROW 3 ABC. REINSTALLED EMERGENCY EXIT LIGHT LENS PER MM.
Part: RIB — CRACKED (LT WING) · airframe 50,214 hrs · 46,406 cycles
DURING SCHEDULED 1/2D CHECK, FOUND LT WING RIB LOWER CHORD AT WS 135.5, BETWEEN S-2 AND S-3, CRACKED. REPAIRED LT WING RIB CHORD PER ACO.
Part: FITTING — CORRODED (GIRT BAR) · airframe 50,214 hrs · 64,406 cycles
DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EVAC SLIDE AFT GIRT BAR MOUNT FITTING CORRODED. REMOVED AND REPLACED L1 DOOR EVAC SLIDE MOUNT FITTING PER SRM.
Part: LIGHT — LOOSE (EMERGENCY EXIT) · airframe 50,214 hrs · 46,406 cycles
DURING SCHEDULED 1/2D CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LOOSE AT ROW 14 ABC. SECURED EMERGENCY EXIT LIGHT PER MM.
Part: CLIP — CRACKED (FUSELAGE) · airframe 50,214 hrs · 46,406 cycles
DURING SCHEDULED 1/2D CHECK, FOUND 2 EA STRINGER CLIPS CRACKED AT BS 380, STR 26L & STR 26R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,214 hrs · 46,406 cycles
DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 22R. REMOVED AND REPLACED CLIP PER SRM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,214 hrs · 46,406 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 344, LBL 33 TO RBL 39. REPAIRED FLOORBEAM PER SRM.
Part: SKIN — DELAMINATED (WING SLATS) · airframe 50,214 hrs · 46,406 cycles
DURING SCHEDULED 1/2D CHECK, FOUND NR 2 AND NR 5 L/E SLAT TRAILING EDGES DELAMINATED. REPAIRED SLATS PER SRM.
Part: WEB — CORRODED (FUSELAGE) · airframe 50,214 hrs · 46,406 cycles
DURING SCHEDULED 1/2D CHECK, FOUND WEB CORRODED AT BS 360 TO BS 380, STR 17R. REMOVED AND REPLACED WEB SECTION PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,214 hrs · 46,406 cycles
DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 27L. REPAIRED SHEAR TIE PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,214 hrs · 46,406 cycles
DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 27R. REPAIRED SHEAR TIE PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 50,214 hrs · 46,406 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 65, WL 208. REPAIRED FRAME PER T1-153-018.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,214 hrs · 46,406 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CAP CORRODED AT BS 986.5, LBL 5 TO RBL 5. REPAIRED BEAM PER T1-453-037.
Part: FITTING — CORRODED (RT MLG) · airframe 50,214 hrs · 46,406 cycles
DURING SCHEDULED 1/2D CHECK, FOUND RT MLG FWD STABILIZER BAR ATTACH FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.
Part: CLIP — CRACKED (FUSELAGE) · airframe 50,214 hrs · 46,406 cycles
DURING SCHEDULED 1/2D CHECK, FOUND 2 EA STRINGER CLIPS CRACKED AT BS 787, STR 25L AND BS 807, STR 25L. REMOVED AND REPLACED STR CLIPS PER SRM.
Part: FLOOR SUPPORT — CORRODED (AFT CARGO COMP) · airframe 50,214 hrs · 46,406 cycles
DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO COMPT LONGITUDINAL FLOOR SUPPORT CORRODED AT BS 772, LBL 17 AND RBL 17. REPAIRED SUPPORTS PER SWA EA.
2003
Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 49,176 hrs · 45,623 cycles
DURING SCHEDULED A2 CHECK, FOUND LT WING OUTBD T/E FLAP DELAMINATED AT INBD END. REMOVED AND REPLACED FLAP ASSY PER MM.
Part: FAN — OVERHEATED (A/C COMPT) · airframe 49,027 hrs · 45,509 cycles
ELECTRICAL ODOR THROUGH OUT THE CABIN. REMOVED AND REPLACED A/C RECIRC FAN PER MM.
Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 48,795 hrs · 45,330 cycles
DURING SCHEDULED C1 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT UPPER AFT CORNER. REPAIRED DOOR SKIN PER SWA EA.
Part: SLIDE — OUT OF LIMITS (SERVICE DOOR) · airframe 48,053 hrs · 44,722 cycles
DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 48,017 hrs · 44,690 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 21L, BS 967 AND BS 973. REPAIRED SKIN PER SRM.
Part: SKIN — DELAMINATED (RT ELEVATOR TAB) · airframe 47,896 hrs · 44,591 cycles
DURING SCHEDULED C4 CHECK, FOUND RT ELEVATOR TAB DELAMINATED AT NR 3 HINGE. REMOVED AND REPLACED RT ELEVATOR TAB PER MM.
Part: BUSHING — WORN (RT ELEVATOR) · airframe 47,869 hrs · 44,566 cycles
DURING SCHEDULED C4 CHECK, SWA SI 11139-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB INPUT ROD HARDWARE AND BUSHING.
Part: BUSHING — WORN (LT ELEVATOR) · airframe 47,869 hrs · 44,566 cycles
DURING SCHEDULED C4 CHECK, SWA SI 11139-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB INPUT ROD HARDWARE, BUSHING AND ALL HINGE ATTACH POINT HARDWARE PER MM.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 47,737 hrs · 44,463 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND LT VERTICAL CHORD CRACKED AT BS 179, LBL 5.7. REPAIRED VERTICAL CHORD PER SRM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 47,737 hrs · 44,463 cycles
DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234, LBL 13. REPAIRED BULKHEAD WEB PER SRM.
Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 46,997 hrs · 53,859 cycles
DURING SCHEDULED C3 CHECK, FOUND RT COCKPIT WINDOW C POST CRACKED. REPAIRED POST PER SRM.
2002
Part: SLIDE — LOOSE (L1 DOOR) · airframe 45,878 hrs · 42,954 cycles
FWD ENTRY DOOR EMERGENCY EVACUATION SLIDE COMING OUT OF CONTAINER. REINSTALLED SLIDE ASY PER MM.
Part: FLAP — PEELING (LT WING) · airframe 45,126 hrs · 42,355 cycles
DURING WALK AROUND INSPECTION, FOUND PREVIOUS REPAIR PEELING OFF AT LT T/E INBD FORE FLAP. REMOVED AND REPLACED LT T/E INBD FORE FLAP PER MM.
Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 44,281 hrs · 41,664 cycles
FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,253 hrs · 41,643 cycles
DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT LIGHTS AT FWD AND AFT ENTRY DOORS WITH SEVERAL BULBS INOP. RELAMPED LIGHTS PER MM.
Part: LENS — LOOSE (CABIN) · airframe 44,253 hrs · 41,643 cycles
DURING SCHEDULED C4 CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW NR 14 ABC. SECURED LENS PER MM.
Part: LENS — LOOSE (CABIN) · airframe 43,360 hrs · 40,876 cycles
DURING SCHEDULED BC3 CHECK, FOUND EMERGENCY EXIT LIGHT LENS LOOSE AT LT OVERWING EXIT. SECURED LENS PER MM.
2001
Part: SLIDE — LOOSE (FWD ENTRY DOOR) · airframe 42,026 hrs · 39,792 cycles
FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.
Part: FITTING — CORRODED (CABIN) · airframe 41,602 hrs · 39,455 cycles
DURING SCHEDULED 1/4D CHECK, FOUND BOTH AFT DOOR EVACUATION SLIDE GIRT BAR FLOOR ATTACH BRACKETS CORRODED. REMOVED AND REPLACED ATTACH BRACKETS PER MM.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 41,289 hrs · 39,195 cycles
DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP RT AFT EXTERIOR. RELAMPED LIGHT PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,202 hrs · 39,128 cycles
DURING SCHEDULED RON CHECK, FOUND CABIN EMERGENCY EXIT LIGHTS INOP. RECHARGED BATTERY PACKS PER MM.
Part: WEB — CRACKED (FUSELAGE) · airframe 40,834 hrs · 38,796 cycles
DURING SCHEDULED SPECIAL VISIT CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 180, RBL 17.1. REPAIRED WEB PER SRM.
Part: STIFFENER — CRACKED (MLG WW) · airframe 40,834 hrs · 38,796 cycles
DURING SCHEDULED SPECIAL VISIT CHECK, FOUND VERTICAL STIFFENER CRACKED AT MLG WW BS 663, LBL 6. REPAIRED PER SWA RA.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 40,834 hrs · 38,796 cycles
DURING SCHEDULED SPECIAL VISIT CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, LBL 6 & WL 200. REPAIRED WEB PER SRM.
Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 39,618 hrs · 38,057 cycles
AFT SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. INSTALLED EMERGENCY EVAC IN CONTAINER PER MM.
Part: TAB — WORN (LT ELEVATOR) · airframe 40,660 hrs · 38,637 cycles
DURING SCHEDULED C4 CHECK, FOUND PLAY AT LT ELEVATOR TAB. REMOVED AND REPLACED TAB ASSY PER MM.
Part: BRACKET — LOOSE (ESCAPE SLIDE) · airframe 39,640 hrs · 37,757 cycles
DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BRACKET LOOSE. SECURED GIRT BRACKET PER MM.
Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 39,542 hrs · 37,685 cycles
AFT SVC DOOR EMERGENCY EVAC SLIDE ASSY FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM.
2000
Part: LENS — MISSING (CABIN) · airframe 39,130 hrs · 37,355 cycles
EEPLS LENS MISSING AT MID CABIN. R&R LENS PER MM.
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 38,134 hrs · 36,492 cycles
DURING SCHEDULED A1 CHECK, FOUND EEPLS FWD SECTION INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: SLIDE — DISCHARGED (SERVICE DOOR) · airframe 37,332 hrs · 35,837 cycles
DURING SCHEDULED RON, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR LOW. REMOVED AND REPLACED SLIDE PER MM.
Part: SMOKE — DETECTED (COCKPIT) · airframe 36,663 hrs · 35,274 cycles
AIR TURNBACK -- SMOKE INSIDE COCKPIT AND FWD SIDE OF MAIN CABIN. INSPECTED ACFT A/C SYSTEM, E&E COMPT, BORESCOPED NR 1 ENGINE HPC. NO DISCREPANCIES NOTED R&R LT AIR CYCLE MACHINE PER MM.
Part: SKIN — CRACKED (BS 520)
DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED, RT SIDE OF THE GROUND A/C CONNECT CUT OUT, BS 520. REPAIRED SKIN PER SRM.
1999
Part: SLIDE — OUT OF ADJUST (PAX DOORWAY)
DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY/SERVICE AND AFT ENTRY DOOR EVACUATION SLIDE GIRT ASSY'S EXTENDING OUT OF LIMITS. ADJUSTED SLIDE ASSY'S PER MM.
Part: SLIDE — OUT OF POSITION (SERVICE DOOR)
DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE BOTTLE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.
Part: KEEL BEAM — CRACKED (MLG WW)
DURING SCHEDULED BC2 CHECK, FOUND FUSELAGE KEEL BEAM LOWER PANEL CRACKED AT MLG WHEEL WELL. REPAIRED PER TRM AND SB 737-53-1104.
Part: WEB — CRACKED (BS 663)
DURING SCHEDULED A1 CHECK, FOUND BEADED PRESS WEB CRACKED, BS 663, LBL 33. REPAIRED WEB PER SWA RA NR1-353-2117.
Part: FRAME — CRACKED (BS 787)
DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 787, BETWEEN STRINGERS 8R-9R. REPAIRED FRAME PER SRM.
Part: KEEL BEAM — CORRODED (BS 713-720)
DURING SCHEDULED D-CHECK, FOUND CORROSION AT KEEL BEAM RT SIDE BS 713 TO 720. REPAIRED BEAM PER ER N99-5203A.
Part: SKIN — CRACKED (RT HORZ STAB)
DURING SCHEDULED D-CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED 1 INCH FWD OF REAR SPAR CENTER LINE AT STA 125 (CRACK IS APPROX 1 INCH LONG). REPAIRED SKIN PER ER 99-5225.
Part: FRAME — CRACKED (BS 360)
DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME BS 360, STRINGER 15R. REPAIRED FRAME PER SRM.
Part: FRAME — CRACKED (FUSELAGE)
DURING SCHEDULED D-CHECK, FOUND CRACKED FRAMES AT BS 400, 440 BETWEEN STRINGERS 8L-9L AND AT BS 380, 400, BETWEEN STRINGERS 8R-9R. REPAIRED PER SRM AND ER NR 99-5198.
Part: FRAME — CRACKED (BS 616)
DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME BS 616 WL 201 LBL 65. REPAIRED FRAME PER SRM AND ER NR 99-5197.
Part: SPLICE — CRACKED (BS 908)
DURING SCHEDULED D-CHECK, FOUND STRINGER 4L SPLICE CRACKED AT BS 908. REPAIRED SPLICE PER SRM.
Part: FRAME — CRACKED (FUSELAGE)
DURING SCHEDULED D-CHECK, FOUND 5 CRACKS AT FRAMES BS 827, 867 BETWEEN STRINGERS 8L-9L AND BS 727B, 747 AND 867, BETWEEN STRINGERS 8R-9R. REPAIRED PER SRM AND ER 99-5198.
Part: STRINGER — CRACKED (BS 500)
DURING SCHEDULED D-CHECK, FOUND STRINGER 19L CRACKED AT BS 500D. REPAIRED STRINGER PER SRM.
Part: PLATE — CORRODED (PAX DOORWAY)
DURING SCHEDULED D-CHECK, FOUND CORROSION AT FWD ENTRY DOOR GIRT BAR MOUNTING PLATES. REMOVED AND REPLACED PLATES PER SRM.
Part: BULKHEAD WEB — CRACKED (BS 178)
DURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB BS 178 CRACKED IN 5 PLACES, RBL 6 TO LBL 11. REPAIRED WEB PER SRM.
Part: CLIPS — CRACKED (BS 500)
DURING SCHEDULED D-CHECK, FOUND 2 STRINGER CLIPS CRACKED AT BS 500D, STRINGERS 19L AND 19R. REPAIRED CLIPS PER SRM.
Part: SKIN — CRACKED (BS 727)
DURING SCHEDULED SC CHECK, FOUND 2 INCH CRACK BELOW STRINGER 22L, BETWEEN BS 727C AND D. REPAIRED PER BOEING SRM.
1998
Part: BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED SC CHECK, FOUND EMERGENCY FLASHLIGHT AT FWD GALLEY BATTERY LOW. REPLACED PER BOEING M/M.
Part: FLOORBEAM — CORRODED (COCKPIT)
DURING SCHEDULED RON, FOUND COCKPIT FLOORBEAM CORROSION. REPAIRED PER BOEING SRM.
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING SCHEDULED WALKAROUND CHECK, FOUND 1X AFT EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED AFT UPPER FLASHLIGHT BATTERY PER BOEING MM.
Part: INTERCOSTAL — CRACKED (CARGO DOOR)
DURING SCHEDULED C2 CHECK, FOUND CARGO DOOR LATCH BRACKET INTERCOSTAL CRACKED. REPAIRED PER BOEING SRM.
Part: INTERCOSTAL — CRACKED (CARGO DOORWAY)
DURING SCHEDULED C1 CHECK, FOUND CRACKED INTERCOSTAL FOR DOOR UPLATCH HOOK. REMOVED AND REPLACED PER BOEING SRM.
Part: SKIN — GOUGED (PAX DOORWAY)
DURING SCHEDULED TERMINAL CHECK, FOUND GOUGED BELOW FWD ENTRY DOOR. REPAIRED PER BOEING SRM.
Part: SKIN — GOUGED (L1 DOORWAY)
DURING SCHEDULED RON CHECK, FOUND GOUGE BELOW L-1 DOOR. REPAIRED PER BOEING SRM.
Part: FUSELAGE — CRACKED (BS 980)
DURING SCHEDULED RON CHECK, FOUND CRACKED FUSELAGE AT BS 980 STR 21 ABOUT 2 LONG HFEC. REPAIRED PER BOEING SRM.
Part: PANEL — CRACKED (LT WING)
DURING SCHEDULED C4 CHECK, FOUND LEFT WING UPPER SURFACE TRAILING EDGE PANEL HAS TWO CRACKS. REPAIRED PER BOEING SRM.
1997
Part: BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED RON, FOUND FLOOR TRACK LIGHTS AT AFT CABIN AREA INOP. REPLACED BATTERY PER BOEING M/M.