N649SW
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | on 2015-12-15 | Operator named in NTSB report |
Accident & incident history
Operated by Southwest Airlines (per NTSB report)
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.
247 reports on file, 1997-10-31 – 2015-09-21.
Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 57,932 hrs · 45,689 cycles
R2 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW AMM.
Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 57,459 hrs · 45,338 cycles
R2 DOOR EVAC SLIDE PRESS LOW. R & R SLIDE ASSEMBLY IAW MM.
Part: CONTROL CABLE — OUT OF ADJUST (LANDING GEAR) · airframe 57,330 hrs · 45,242 cycles
WHEN SELECTING LG DOWN, ALL SIX LIGHTS ILLUMINATED & STAYED ON. THREE RED & THREE GREEN, NOSE, LT & RT. EXECUTED A GO AROUND & RECYCLED THE LG & THE GREEN LG SAFE LIGHTS STAYED ON & THE THREE UNSAFE WENT DARK. ADJUSTED LG CONTROL SYS CABLES IAW AMM 32-31-00.
Part: HINGE — BROKEN (GROUND SPOILER) · airframe 57,080 hrs · 45,058 cycles
FOUND THE RIGHT WING INBOARD GROUND SPOILER OUTBD HINGE BROKEN. R & R THE SPOILER IAW MM.
Part: WIRE HARNESS — FAULTY (FUEL QTY) · airframe 57,080 hrs · 45,059 cycles
PERFORMED AN AIR TURNBACK AND AN EMERGENCY WAS DELARED, DUE TO THE FUEL QTY INDICATOR WAS ERRATIC WITH A FUEL IMBALANCE. R & R LEFT TSD FUEL TANK HARNESS IAW MM.
Part: HINGE — BROKEN (LT GRND SPOILER) · airframe 57,080 hrs · 45,058 cycles
FOUND THE LEFT WING INBD GROUND SPOILER OUTBOARD HINGE BROKEN. R & R THE SPOILER IAW MM.
Part: PROBE — FAULTY (FUEL QTY) · airframe 57,080 hrs · 45,059 cycles
PERFORMED AN AIR TURNBACK AND AN EMERGENCY WAS DELARED, DUE TO A FUEL QTY INDICATOR BEING ERRATIC AND WITH A FUEL IMBALANCE. R & R LEFT TANK NR 6 PROBE IAW MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,947 hrs · 44,969 cycles
LEFT EMER LIGHT INOPERATIVE AT ROW 18. RELAMPED LIGHT IAW AMM.
Part: STIFFENER — CRACKED (NLG WW) · airframe 56,947 hrs · 44,969 cycles
RIGHT NLG WW HORIZONTAL STIFFENER CRACKED AT BS 294.5, OTBD CORNER. R & R STIFFENER IAW ER & EA.
Part: WEB — CRACKED (NLG WW) · airframe 56,947 hrs · 44,969 cycles
RIGHT NLG WW BULKHEAD TRUNNION VERTICAL WEB CRACKED AT BS 294.5. REPAIRED WEB ASSEMBLY IAW EA.
Part: COVER — MISSING (EXIT SIGN) · airframe 56,858 hrs · 44,910 cycles
RIGHT OVERWING EXIT SIGN COVER MISSING. INSTALLED COVER IAW MM.
Earlier reports · 1997–2014 · 236 reports
2014
Part: SLIDE — LOOSE (L1 DOOR) · airframe 55,464 hrs · 43,945 cycles
L1 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.
Part: LENS — LOOSE (CABIN) · airframe 55,331 hrs · 43,863 cycles
MID CABIN CEILING EMER LIGHT LENS LOOSE. SECURED LENS IAW MM.
Part: CIRCUIT BREAKER — TRIPPED (CABIN) · airframe 54,841 hrs · 43,513 cycles
EMERGENCY EXIT LIGHT FAULTY. FOUND EMER EXIT LIGHT CB TRIPPED. RESET CB IAW MM.
Part: ACTUATOR — FAULTY (RT MLG) · airframe 54,620 hrs · 43,356 cycles
AIR TURN BACK & DECLARED EMER. AFTER TAKEOFF GEAR HANDLE UP HAD A RT MAIN RED UNSAFE LIGHT. WHEN GEAR HANDLE IN OFF POSITION HAD RT MAIN RED & GREEN LIGHT. WHEN LANDING HANDLE IN DOWN POSITION RED LIGHT UNSAFE OUT. R & R RT MLG UPLOCK ACTUATOR IAW MM.
Part: FUSE — BLOWN (CABIN) · airframe 54,495 hrs · 43,269 cycles
RIGHT FWD EMER EXIT LIGHT INOPERATIVE AT BS 360. R & R F2 FUSE IAW AMM.
Part: FUSE — BLOWN (CABIN) · airframe 54,495 hrs · 43,269 cycles
GALLEY 1 EMER EXIT LIGHT INOPERATIVE. R & R F2 FUSE IAW AMM.
Part: SKIN — CRACKED (LE SLAT) · airframe 54,495 hrs · 43,269 cycles
RIGHT WING NR 6 SLAT SKIN LE CRACKED. REPAIRED SKIN IAW SRM.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 54,495 hrs · 43,269 cycles
SKIN CREASED BETWEEN BS 794 TO 807 BETWEEN STRINGER 25R TO 26R. REPAIRED SKIN IAW EA.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,495 hrs · 43,269 cycles
SHEAR TIE CRACKED AT BS 328 STRINGER 17R. R & R SHEAR TIE IAW SRM & DWG.
Part: FLAP — DELAMINATED (RT WING) · airframe 54,495 hrs · 43,269 cycles
RIGHT WING AFT FLAP OTBD EDGE DELAMINATED. REPAIRED AFT FLAP IAW SRM.
Part: ANGLE — CRACKED (LT WING) · airframe 54,495 hrs · 43,269 cycles
LEFT WING FIXED TE ANGLE CRACKED AT WBL 198.60. R & R ANGLE IAW SRM & DWG.
Part: FITTING — CRACKED (FUSELAGE) · airframe 54,495 hrs · 43,269 cycles
CLIP CRACKED AT BS 348.2 STRINGER 15L. R & R CLIP IAW SRM & DWG.
Part: ANGLE — CRACKED (RT WING) · airframe 54,495 hrs · 43,269 cycles
RIGHT WING TE WBL 204.40 ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 54,495 hrs · 43,269 cycles
INNER CHORD CRACKED AT BS 348.2 STRINGER 15L. R & R CHORD IAW EA.
Part: SKIN — DELAMINATED (TE FLAP) · airframe 54,495 hrs · 43,269 cycles
RIGHT WING INBD FORE FLAP DELAMINATED ON UPPER SURFACE. REPAIRED FORE FLAP IAW SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,495 hrs · 43,269 cycles
SKIN CRACKED AT BS 328 STRINGER 17R. REPAIRED SKIN IAW EA.
Part: RIB — CRACKED (RT WING) · airframe 54,495 hrs · 43,269 cycles
RIGHT WING FUEL TANK RIB LOWER CHORD CRACKED AT WBL 135.5 BETWEEN STRINGER 2R TO 3R. REPAIRED CHORD IAW EA.
Part: FLAP — DELAMINATED (LT WING) · airframe 54,495 hrs · 43,269 cycles
LEFT WING INBD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.
Part: FLAP — DELAMINATED (RT WING) · airframe 54,495 hrs · 43,269 cycles
RIGHT WING INBD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,495 hrs · 43,269 cycles
LEFT EMER EXIT LIGHT LAMP INOPERATIVE. R & R LAMP IAW AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,495 hrs · 43,269 cycles
RIGHT EMER EXIT LIGHT LAMP INOPERATIVE. R & R LAMP IAW AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,495 hrs · 43,269 cycles
AFT LAVATORY EMER EXIT LIGHT BULB INOPERATIVE. R & R BULB IAW MM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 54,495 hrs · 43,269 cycles
LEFT FRAME INNER CHORD CRACKED AT BS 616 WL 202. REPAIRED CHORD IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 54,495 hrs · 43,269 cycles
RIGHT FRAME INNER CHORD CRACKED AT BS 616 WL 208. REPAIRED CHORD IAW EA.
Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 54,495 hrs · 43,269 cycles
AFT CARGO DOOR CROSSBEAM E T CHORD AFT END CRACKED. REPAIRED E T CHORD IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 54,495 hrs · 43,269 cycles
FRAME OTBD CHORD CRACKED AT BS 727 BETWEEN STRINGER 18A & 27L. REPAIRED CHORD IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 54,495 hrs · 43,269 cycles
FRAME OTBD CHORD CRACKED AT BS 727 STRINGER 8A LT. REPAIRED CHORD IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 54,495 hrs · 43,269 cycles
FRAME CHORD CRACKED AT BS 727 STRINGER 18. REPAIRED CHORD IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 54,495 hrs · 43,269 cycles
FRAME OTBD CHORD CRACKED AT BS 727 STRINGER 18R. REPAIRED CHORD IAW EA.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,099 hrs · 42,983 cycles
STRINGER CLIP CRACKED AT BS 400, STR 9L. R & R CLIP IAW SRM & BAC.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 54,099 hrs · 42,983 cycles
STRINGER CRACKED AT BS 500A+2, STRINGER 4R. REPAIRED STRINGER IAW SB.
Part: STRINGER SPLICE — DAMAGED (FUSELAGE) · airframe 54,099 hrs · 42,983 cycles
STRINGER SPLICE DAMAGED AT STATION 663, STRINGER 4R. R & R SPLICE IAW SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,099 hrs · 42,983 cycles
STRINGER CLIP CRACKED AT BS 380, STRINGER 8L. R & R CLIP IAW DWG.
Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 54,099 hrs · 42,983 cycles
STRINGER SPLICE CRACKED AT BS 540, STRINGER 14L. R &R SPLICE IAW SRM & DWG.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 54,099 hrs · 42,983 cycles
STRINGER CRACKED AT BS 471, STRINGER 5L. REPAIRED STRINGER IAW SB.
Part: FRAME — GOUGED (FUSELAGE) · airframe 54,099 hrs · 42,983 cycles
FRAME GOUGED AT BS 400, STRINGER 8L. REPAIRED FRAME IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,099 hrs · 42,983 cycles
RIGHT BS 887+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,099 hrs · 42,983 cycles
RIGHT BS 500C+10 UPPER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW SB.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,099 hrs · 42,983 cycles
RIGHT BS 360+10 LOWER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,099 hrs · 42,983 cycles
RIGHT BS 520+10 LOWER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,099 hrs · 42,983 cycles
RIGHT BS 807+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,099 hrs · 42,983 cycles
RIGHT BS 500B+10 UPPER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW SB.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,099 hrs · 42,983 cycles
RIGHT BS 500B+10 LOWER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,099 hrs · 42,983 cycles
RIGHT BS 867+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
Part: FORGING — CRACKED (FUSELAGE) · airframe 54,099 hrs · 42,983 cycles
RIGHT BS 887+10, CRACKED AT HOLE NR 8 IN LOWER FWD CORNER. R & R FORGING IAW DWG.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,099 hrs · 42,983 cycles
RIGHT BS 520+10 UPPER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,099 hrs · 42,983 cycles
RIGHT BS 827+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.
Part: FORGING — CRACKED (FUSELAGE) · airframe 54,099 hrs · 42,983 cycles
RIGHT BS 887+10 UPPER AFT WINDOW CORNER CRACKED. REPAIRED FORGING IAW SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 53,989 hrs · 42,907 cycles
FUSELAGE SKIN CRACKED AT BS 727B+9, STRINGER 10R. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 53,989 hrs · 42,907 cycles
FUSELAGE SKIN CRACKED AT BS 500D+10, STRINGER 10L. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 53,843 hrs · 42,803 cycles
FUSELAGE SKIN CRACKED AT STATION 365.5 TO STATION 368.5, STRINGER 16R. REPAIRED SKIN IAW SWA EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 53,843 hrs · 42,803 cycles
FUSELAGE SKIN CRACKED BETWEEN BS 365.5 TO BS 368.5, STRINGER 16R. REPAIRED SKIN IAW EA.
Part: COALESCER BAG — FAULTY (AC BAY) · airframe 53,497 hrs · 42,563 cycles
ON DEPARTURE FLIGHT ATTENDANT REPORTED SMOKE & FUMES IN CABIN. R & R COALESCENT BAG & CABIN RECIRCULATING FILTER IAW AMM.
Part: ACM — FAULTY (AC BAY) · airframe 53,505 hrs · 42,571 cycles
AIR TURN BACK, DECLARED EMERGENCY. CREW REPORTED LT PACK TURN ON, GOES TO OVERTEMP NO CONTROL WITH MANUAL OR AUTO MODE. R & R AIR CYCLE MACHINE & AIR MIX VLV IAW MM.
Part: MODULE — FAULTY (HYDRAULIC SYS) · airframe 53,497 hrs · 42,563 cycles
AIR TURN BACK, DECLARED EMERGENCY ON DEPARTURE, FLIGHT ATTENDANT REPORTED SMOKE & FUMES IN CABIN, PERFORMED QRH. DURING QRH PROCEDURES, SMOKE DISSIPATED AFTER PACK SELECTED OFF. RETURNED TO DTW. R & R HYD RESERVOIR AIR PRESSURE MODULE & LT COALESCENT BAG IAW MM.
Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 53,494 hrs · 42,559 cycles
AFT LAVATORY SMOKE DETECTOR WENT OFF IN FLIGHT. R & R DETECTOR IAW MM.
Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 53,497 hrs · 42,563 cycles
AFT LAVATORY SMOKE DETECTOR ALARM SOUNDED. NO SMOKE, NO FIRE DETECTED. R & R DETECTOR IAW MM.
2013
Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 53,071 hrs · 42,276 cycles
L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. R & R SLIDE IAW AMM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 52,922 hrs · 42,173 cycles
SKIN CRACKED AT BS 727C, STRINGER 10L. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 52,922 hrs · 42,173 cycles
SKIN CRACKED AT BS 727C, STRINGER 10L. REPAIRED SKIN IAW EA.
Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 52,916 hrs · 42,168 cycles
RT WING NR 7 FLAP TRACK CORRODED AT AFT ATTACH POINT. R & R NR 7 FLAP TRACK IAW MM & MT.
Part: SUPPORT — LOOSE (FLAP TRACK) · airframe 52,916 hrs · 42,168 cycles
LT WING NR 2 FLAP TRACK A FRAME FWD ATTACH POINT LOOSE. R &R SUPPORT ARM ASSEMBLY IAW MM.
Part: SPOILER — DELAMINATED (LT WING) · airframe 52,785 hrs · 42,083 cycles
NR 2 FLIGHT SPOILER DELAMINATED. R & R NR 2 FLT SPOILER IAW MM.
Part: TIRE — SEPARATED (LT MLG) · airframe 52,658 hrs · 41,987 cycles
AIR TURNBACK, DECLARED EMERGENCY, AT ROTATION FLT CONTROL ANNOUNCE LIGHT & "A" SIDE HYD LOW PRESSURE LIGHT ILLUMINATED. LANDING GEAR DID NOT RETRACT, FOUND NR 2 TIRE LOST TREAD. R & R NR 2 MAIN TIRE IAW MM.
Part: LENS — LOOSE (CABIN) · airframe 52,540 hrs · 41,894 cycles
CENTER CABIN CEILING EMERGENCY EXIT SIGN LENS ON LOWER SURFACE LOOSE. SECURED LENS IAW AMM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 52,461 hrs · 41,833 cycles
FS SKIN CRACKED AT BS 724B+12 STRINGER 10L. REPAIRED SKIN IAW EA.
Part: FLAP — DELAMINATED (LT WING) · airframe 52,279 hrs · 41,685 cycles
LT WING INBD AFT FLAP DELAMINATED. R&R AFT FLAP IAW AMM.
Part: FLAP — DELAMINATED (RT WING) · airframe 52,279 hrs · 41,685 cycles
RT WING OTBD AFT FLAP DELAMINATED ON INBD END. R&R AFT FLAP IAW AMM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 51,941 hrs · 41,418 cycles
CROWN SKIN CRACKED AT BS 727A- 9.5. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 51,941 hrs · 41,418 cycles
CROWN SKIN CRACKED AT BS 727D, STRINGER 10L. REPAIRED SKIN IAW EA.
Part: SLIDE — OUT OF LIMITS (R2 DOOR) · airframe 51,697 hrs · 41,229 cycles
R2 DOOR EMERGENCY EVAC SLIDE ASSY PRESSURE OUT OF LIMITS. R & R SLIDE ASSY IAW MT.
Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 50,988 hrs · 40,720 cycles
L2 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT. RE-INSTALLED SLIDE IAW MT.
2012
Part: SIGN — BROKEN (CABIN) · airframe 49,801 hrs · 39,866 cycles
R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER AMM.
Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
TIE CLIP CRACKED AT BS 947.5, BETWEEN STR 23R AND STR 25R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
TIE CLIP CRACKED AT BS 440, STR 8R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
ANGLE LOWER CHORD CRACKED AT BS 706+4, BBL 0.07. REPAIRED ANGLE IAW EO AND EA.
Part: STRUCTURE — CRACKED (RT HORIZ STAB) · airframe 49,298 hrs · 39,483 cycles
RIGHT HORIZONTAL STABILIZER L/E CRACKED AT STA 111.10. REPAIRED STABILIZER IAW SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
FRAME CRACKED AT BS 188, BETWEEN STR 17L TO STR 18L. REPAIRED FRAME IAW SRM.
Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
TIE CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
Part: FRAME — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
FRAME CRACKED AT BS 440, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
STUB FRAME CRACKED AT BS 951, STR 17R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.
Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.
Part: FRAME — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
FRAME CRACKED AT BS 747, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
STRINGER CRACKED AT BS 787, STR 8L. REPAIRED STRINGER IAW SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
FRAME CRACKED AT BS 747, BETWEEN STR 8L AND STR 9L. REPAIRED FRAME IAW EA.
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
SUPPORT ANGLE CRACKED AT BS 294.5, STR 23L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.
Part: FITTING — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
CLIP CRACKED AT BS 706, STR 10R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.
Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
TIE CLIP CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
TIE CLIP CRACKED AT BS 663.75, STR 10L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
ANGLE CORRODED AT BS 887+16, STR 17R. REMOVED AND REPLACED ANGLE SRM AND DWG.
Part: SKIN — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
SKIN CRACKED AT BS 360+1, STR 28L. REMOVED AND REPLACED SKIN IAW EA AND EO.
Part: FRAME — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
FRAME CRACKED AT BS 827, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EO AND EA.
Part: FITTING — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
CLIP CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.
Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.
Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
TIE CLIP CORRODED AT BS 947.5, STR 23L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
TIE CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
TIE CLIP CRACKED AT BS 360, STR 16R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG
Part: FRAME — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME IAW SRM.
Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
BULKHEAD SUPPORT CHANNEL CRACKED AT BS 727, RBL 3.00. REMOVED AND REPLACED CHANNEL IAW SRM AND DWG.
Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
SUPPORT CHANNEL CRACKED AT BS 540, BETWEEN BL 0 TO LBL 24.5. REMOVED AND REPLACED CHANNEL IAW SRM AND DWG.
Part: FITTING — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
CLIP CRACKED AT BS 597, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.
Part: FRAME — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
STUB FRAME CRACKED AT BS 294.5, STR 7R. REPAIRED FRAME IAW EO AND EA.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
Z-ANGLE CORRODED BETWEEN BS 947.5 TO BS 1006, LBL 51. REMOVED AND REPLACED Z-ANGLE IAW SRM AND DWG.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
ANGLE CRACKED BETWEEN BS 277 AND BS 291.5, BETWEEN STR 13R TO STR 14R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.
Part: STRAP — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
STRAP CRACKED BETWEEN BS 328 TO BS 344, LBL 46. REMOVED AND REPLACED STRAP IAW SRM.
Part: FLAP — DELAMINATED (LT WING) · airframe 49,298 hrs · 39,483 cycles
LEFT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP IAW SRM & AMM.
Part: FRAME — CORRODED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
FRAME CORRODED AT BS 993, STR 17R. REPAIRED FRAME IAW EA.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
FLOORBEAM UPPER CHORD CRACKED AT BS 312, RBL 34. REPAIRED CHORD IAW SRM & DWG.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
FLOORBEAM UPPER CHORD CRACKED AT BS 328, BETWEEN LBL 35 TO LBL 20. REPAIRED CHORD IAW SRM.
Part: STRAP — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
STRAP CRACKED BETWEEN BS 328 TO BS 344, RBL 47. REMOVED AND REPLACED STRAP IAW SRM.
Part: SKIN — DELAMINATED (LE SLAT) · airframe 49,298 hrs · 39,483 cycles
RIGHT WING NR 5 SLAT TRAILING EDGE SKIN DELAMINATED. REPAIRED SKIN IAW SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
AFT GALLEY DOOR CUT OUT, FWD LOWER CORNER CRACKED, BETWEEN BS 947.5 TO BS 967 AND BETWEEN STR 16R TO STR 18R. REPAIRED SKIN IAW SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
SKIN CRACKED AT BS 360+19, STR 28L. REPAIRED SKIN IAW EA.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 707 TO BS 710, LBL 24.5. REPAIRED FLOORBEAM WEB IAW EA AND EO.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 49,298 hrs · 39,483 cycles
LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN STA 706 TO STA 714, BBL 0.07. REPAIRED WEB IAW EO AND EA.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 48,978 hrs · 39,242 cycles
STRINGER CORRODED BETWEEN BS 948 TO BS 952, STR 1R. REPAIRED STRINGER PER SRM.
Part: MOUNT — BROKEN (R2 DOOR) · airframe 48,974 hrs · 39,241 cycles
R2 DOOR EMERGENCY EVAC SLIDE AFT MOUNT BROKEN. REMOVED AND REPLACED MOUNT PER M/M.
Part: SKIN — DAMAGED (LE SLAT) · airframe 48,642 hrs · 38,979 cycles
RT WING NR 6 SLAT DAMAGED COVER SKIN AT MAIN TRACK AND TRAILING EDGE WEDGE BOND ASSEMBLY. REMOVED AND REPLACED NR 6 SLAT ASSY PER MM.
Part: LENS — CRACKED (CABIN) · airframe 48,037 hrs · 38,527 cycles
FWD ENTRY DOOR FLOOR EMERGENCY LIGHT LENS COVER CRACKED. REMOVED AND REPLACED COVER PER AMM.
2011
Part: SLIDE — LOOSE (R2 DOOR) · airframe 47,367 hrs · 38,023 cycles
R2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.
Part: GARLOCK SEAL — LEAKING (NR 1 ENGINE) · airframe 47,386 hrs · 38,037 cycles
DECLARED EMERGENCY - OIL QUANTITY FELL FROM 2.5 GALLONS EN ROUTE AT FL 350 (NR 1 ENGINE) TO 1.5 GALLONS IN 60 MINS. REMOVED AND REPLACED NR 1 ENGINE STARTED GARLOCK SEAL IAW MM.
Part: OUTLET — BURNED (GALLEY POWER) · airframe 46,981 hrs · 37,729 cycles
REAR GALLEY ELECTRICAL OUTLET APPEARS TO BE BURN. REMOVED AND REPLACED OUTLET PER MM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,097 hrs · 36,870 cycles
DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER EA AND ER.
Part: SKIN — DELAMINATED (FOREFLAP) · airframe 45,747 hrs · 36,792 cycles
DURING SCHEDULED SPV CHECK FOUND, RT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 45,211 hrs · 36,396 cycles
DURING SCHEDULED 14Y CHECK, FOUND BS 178, BULKHEAD, RT CHORD CRACKED AT WL 207.5. REMOVED AND REPLACED CHORD PER ACO.
Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 45,211 hrs · 36,396 cycles
DURING SCHEDULED 14Y CHECK, FOUND BS 178 BULKHEAD RT SIDE PRESSURE WEB DAMAGED. REMOVED AND REPLACED PRESSURE WEB PER SRM AND ACO.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 45,211 hrs · 36,396 cycles
DURING SCHEDULED 14Y CHECK, FOUND CHORD CRACKED AT BS 178, WL 207.5 LT SIDE. REMOVED AND REPLACED LT CHORD PER ACO.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,211 hrs · 36,396 cycles
DURING SCHEDULED 14Y CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 45,211 hrs · 36,396 cycles
DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 907, LBL 3. REPAIRED SHEAR TIE PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 45,211 hrs · 36,396 cycles
DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, RBL 9. REPAIRED SHEAR TIE PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,211 hrs · 36,396 cycles
DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED CLIP PER SI.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,211 hrs · 36,396 cycles
DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4L. REMOVED AND REPLACED CLIP PER SI.
Part: WEB — CRACKED (FUSELAGE) · airframe 45,211 hrs · 36,396 cycles
DURING SCHEDULED 14Y CHECK, FOUND FLIGHT DECK FLOOR WEB CRACKED AT BS 180, LBL 27. REMOVED AND REPLACED WEB PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,211 hrs · 36,396 cycles
DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 1R. REMOVED AND REPLACED CLIP PER SI.
Part: WEB — CRACKED (FUSELAGE) · airframe 45,211 hrs · 36,396 cycles
DURING SCHEDULED 14Y CHECK, FOUND FLIGHT DECK FLOOR WEB CRACKED AT BS 184, LBL 17. REMOVED AND REPLACED WEB PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,211 hrs · 36,396 cycles
DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED CLIP PER SI.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,211 hrs · 36,396 cycles
DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 1R. REMOVED AND REPLACED CLIP PER SI.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,211 hrs · 36,396 cycles
DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8R. REMOVED AND REPLACED CLIP PER SI.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,211 hrs · 36,396 cycles
DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 6R. REMOVED AND REPLACED CLIP PER SI.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,211 hrs · 36,396 cycles
DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2R. REMOVED AND REPLACED CLIP PER SI.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,211 hrs · 36,396 cycles
DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED CLIP PER SI.
Part: WEB — CRACKED (FUSELAGE) · airframe 45,211 hrs · 36,396 cycles
DURING SCHEDULED 14Y CHECK, FOUND O/B FWD BRACKET MOUNT HOLE FOR COMPUTER CRADLE FLOOR WEB CRACKED. REPAIRED FLOOR WEB PER ACO.
2010
Part: FLAP — DELAMINATED (LT WING) · airframe 43,672 hrs · 35,209 cycles
DURING SCHEDULED MV2 CHECK, FOUND LT WING O/B TRAILING EDGE FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.
Part: FLAP — DELAMINATED (LT WING) · airframe 43,562 hrs · 35,117 cycles
DURING SCHEDULED HC2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.
Part: SLAT — DELAMINATED (LT WING) · airframe 43,562 hrs · 35,117 cycles
DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED AT I/B AFT CORNER. REMOVED AND REPLACED SLAT PER MM.
Part: TAB — PUNCTURED (ELEVATOR) · airframe 42,699 hrs · 34,465 cycles
DURING SCHEDULED CV CHECK, FOUND RT ELEVATOR TAB PUNCTURED ON UPPER SURFACE. REMOVED AND REPLACED TAB PER MM.
Part: LUG — BROKEN (SPOILER) · airframe 42,699 hrs · 34,465 cycles
DURING SCHEDULED CV CHECK, FOUND RT WING NR 5 GROUND SPOILER MIDDLE RT CASTING LUG BROKEN. REMOVED AND REPLACED NR 5 SPOILER PER MM.
Part: CLAMP — LOOSE (BLEED AIR DUCT) · airframe 42,599 hrs · 34,389 cycles
CABIN ALT WARNING HORN WENT OFF AT FL 340. NO AUTO FAIL LIGHTS CAME ON. FOUND CLAMP LOOSE AT APU BLEED DUCT PRESSURIZATION SEAL AT KEELBEAM. SECURED CLAMP PER MT.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 42,334 hrs · 34,187 cycles
DURING SCHEDULED MV2 CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT INOP AT L1 DOOR. RELAMPED PER MM.
2009
Part: COVER — MISSING (CABIN) · airframe 41,759 hrs · 33,740 cycles
RT OVERWING EMERGENCY EXIT SIGN COVER MISSING. INSTALLED COVER PER MM.
Part: PUSHROD — CORRODED (ELEVATOR) · airframe 41,193 hrs · 33,292 cycles
DURING SCHEDULED CV CHECK, FOUND LT ELEVATOR CONTROL PUSHRODS CORRODED. REMOVED AND REPLACED PUSHRODS PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,773 hrs · 32,970 cycles
DURING SCHEDULED MV3 CHECK, FOUND FWD EEPLS LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,773 hrs · 32,970 cycles
DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,773 hrs · 32,970 cycles
DURING SCHEDULED MV3 CHECK, FOUND OVERHEAD BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 2. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 40,352 hrs · 32,681 cycles
DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.
Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 40,352 hrs · 32,681 cycles
DURING SCHEDULED 2HC2 CHECK, FOUND L1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 40,302 hrs · 32,646 cycles
DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CRACKED AT BS 1121, STR 1L. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: LIGHT — DAMAGED (CABIN) · airframe 40,302 hrs · 32,646 cycles
DURING SCHEDULED 12Y CHECK, FOUND EEPLS DAMAGED. REMOVED AND REPLACED EEPLS PER MM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,302 hrs · 32,646 cycles
DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN LBL 5 TO RBL 14. REPAIRED SHEAR TIE PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 40,302 hrs · 32,646 cycles
DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 302, WL 234.05. REPAIRED SKIN PER SWA EA.
Part: SKIN — CRACKED (LE SLAT) · airframe 40,302 hrs · 32,646 cycles
DURING SCHEDULED 12Y CHECK, FOUND RT WING NR 5 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 40,302 hrs · 32,646 cycles
DURING SCHEDULED 12Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 45.5. REPAIRED BEAM PER SWA EA.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 40,302 hrs · 32,646 cycles
DURING SCHEDULED 12Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 45.5. REPAIRED BEAM PER SWA EA.
Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 40,302 hrs · 32,646 cycles
DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 787, RBL 15. REMOVED AND REPLACED CLIP PER SRM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 39,978 hrs · 32,405 cycles
DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR UPPER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY ASSY PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,016 hrs · 32,434 cycles
DURING SCHEDULED MV2 CHECK, FOUND LT FWD EGRESS LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,996 hrs · 32,418 cycles
DURING SCHEDULED MV1 CHECK, FOUND FWD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,950 hrs · 32,382 cycles
DURING SCHEDULED MV2 CHECK, FOUND LT FWD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: SKIN — PEELING (TE FLAP) · airframe 39,341 hrs · 31,936 cycles
DURING SCHEDULED MV1 CHECK, FOUND LT WING I/B AFT FLAP SKIN PEELING OFF. REMOVED AND REPLACED AFT FLAP PER MM.
2008
Part: SLAT — CRACKED (RT WING) · airframe 37,299 hrs · 30,465 cycles
DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 L/E SLAT CRACKED AT INBOARD END. REPAIRED SLAT PER SWA EA.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 37,104 hrs · 30,314 cycles
L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.
Part: WINDOW — ARCED (COCKPIT) · airframe 36,789 hrs · 30,080 cycles
CREW REPORTED FLIGHT DECK L2 WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM.
Part: SIGN — LOOSE (CABIN) · airframe 35,994 hrs · 29,476 cycles
FWD CABIN EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED EXIT SIGN PER MM.
2007
Part: COVER — MISSING (CABIN) · airframe 35,568 hrs · 29,149 cycles
FWD CABIN EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM.
Part: SKIN — DELAMINATED (TE FLAP) · airframe 35,499 hrs · 29,099 cycles
DURING SCHEDULED MV2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP LOWER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.
Part: FAN — FAULTY (E&E BAY) · airframe 35,153 hrs · 28,824 cycles
F/A REPORTED SMOKE SMELL IN FIRST 5 ROWS OF CABIN, SMELL GOES AWAY WITH RECIRC AND GASPER FANS OFF. REMOVED AND REPLACED RECIRC AND GASPER FANS PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,798 hrs · 27,763 cycles
DURING SCHEDULED 10Y CHECK, FOUND R2 DOOR EMERGENCY EXIT SLIDE LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: FLAP — DEBONDED (LT WING) · airframe 33,798 hrs · 27,763 cycles
DURING SCHEDULED 10Y CHECK, FOUND LEFT WING INBOARD MID FLAP DISBONDED AT INBOARD END. REPAIRED FLAP PER SRM.
Part: FLOORBEAM — CRACKED (BS 1006) · airframe 33,798 hrs · 27,763 cycles
DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 1006, RBL 50. REMOVED AND REPLACED WEB PER SRM.
Part: FRAME — CORRODED (BS 994 S13R) · airframe 33,798 hrs · 27,763 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 994.5, STR 16R. REPAIRED FRAME PER SRM.
Part: PUSHROD — WORN (LT ELEVATOR) · airframe 33,798 hrs · 27,763 cycles
DURING SCHEDULED 10Y CHECK, LEFT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEVATOR PUSHROD PER MM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,798 hrs · 27,763 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R AND 8L. REPAIRED FRAME PER SWA EA.
Part: SKIN — DELAMINATED (T/E FLAP) · airframe 33,798 hrs · 27,763 cycles
DURING SCHEDULED 10Y CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD LOWER SURFACE. REPAIRED FLAP PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,798 hrs · 27,763 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,798 hrs · 27,763 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.
Part: SKIN — DELAMINATED (T/E FLAP) · airframe 33,798 hrs · 27,763 cycles
DURING SCHEDULED 10Y CHECK, FOUND LEFT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD LOWER SURFACE. REPAIRED FLAP PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,798 hrs · 27,763 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,798 hrs · 27,763 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,798 hrs · 27,763 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,798 hrs · 27,763 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R AND 8L. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,798 hrs · 27,763 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 33,798 hrs · 27,763 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,798 hrs · 27,763 cycles
DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 20L. REMOVED AND REPLACED STRINGER CLIP PER SRM.
Part: FITTING — CORRODED (L1 DOOR) · airframe 33,798 hrs · 27,763 cycles
DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.
Part: FRAME — CORRODED (FUSELAGE) · airframe 33,798 hrs · 27,763 cycles
DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 947, STR 17R. REPAIRED FRAME PER SRM.
Part: FITTING — CORRODED (L1 DOOR) · airframe 33,798 hrs · 27,763 cycles
DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.
Part: FITTING — LOOSE (L2 DOOR) · airframe 33,798 hrs · 27,763 cycles
DURING SCHEDULED 10Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM.
Part: WEDGE — DELAMINATED (L/E SLAT) · airframe 33,798 hrs · 27,763 cycles
DURING SCHEDULED 10Y CHECK, FOUND LEFT WING NR 2 LEADING EDGE SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 4 L/E SLAT PER MM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 33,798 hrs · 27,763 cycles
DURING SCHEDULED 10Y CHECK, FOUND FLOOR BEAM CRACKED AT BS 328, RBL 50. REPAIRED FLOOR BEAM PER SRM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 33,798 hrs · 27,763 cycles
DURING SCHEDULED 10Y CHECK, FOUND FLOOR BEAM WEB CRACKED AT BS 727B, LBL 26. R&R WEB PER SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 66,049 hrs · 56,707 cycles
DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 540, STR 16R. REPAIRED SKIN PER SRM.
2006
Part: DOWNLOCK SENSOR — FAULTY (NLG) · airframe 32,674 hrs · 26,914 cycles
AIRTURN BACK, UPON GEAR RETRACTION BOTH RED AND GREEN NLG LIGHTS ILLUMINATED. AFTER EXTENSION LIGHTS INDICATED NORMAL. REMOVED AND REPLACED NLG DOWNLOCK SENSOR PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,330 hrs · 26,634 cycles
FOUND FWD RT EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 31,941 hrs · 26,332 cycles
DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 31,659 hrs · 26,115 cycles
L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 31,112 hrs · 25,653 cycles
DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED EVAC SLIDE CABLE PER MM.
Part: SKIN — CRACKED (BS 747 S18L) · airframe 30,551 hrs · 25,208 cycles
FUSELAGE SKIN CRACKED AT BS 747, STR 18L. REPAIRED SKIN PER SRM.
Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 30,185 hrs · 24,942 cycles
R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATES LOW. REMOVED AND REPLACED SLIDE PER MM.
Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 56,078 hrs · 45,868 cycles
DURING SCHEDULED C4 CHECK, FOUND NLG W/W CEILING WEB CRACKED AT BS 294.5, RBL 8. REPAIRED WEB PER SWA EA.
Part: MEC — FAULTY (NR 1 ENGINE) · airframe 30,146 hrs · 24,911 cycles
NR 2 ENG N1 POWER ROLLED BACK 6 PERCENT. REMOVED AND REPLACED NR 2 ENG MEC PER MM.
2005
Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 29,164 hrs · 24,143 cycles
DURING SCHEDULED C4 CHECK, FOUND LT WING T/E OTBD AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.
Part: PANEL — CRACKED (FUSELAGE) · airframe 29,164 hrs · 24,143 cycles
DURING SCHEDULED C4 CHECK, FOUND FUSELAGE KEEL BEAM PANEL CRACKED AT BS 670, STR 28R. REPAIRED KEEL BEAM PANEL PER SRM.
Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 26,412 hrs · 21,918 cycles
DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.
Part: SKIN — WORN (FUSELAGE) · airframe 26,141 hrs · 21,702 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT DORSAL FIN WORN. REPAIRED SKIN PER EA.
2004
Part: SLIDE — DISLODGED (L1 DOOR) · airframe 25,623 hrs · 21,310 cycles
L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM.
Part: MEC — FAULTY (NR 2 ENGINE) · airframe 25,559 hrs · 21,267 cycles
AIR TURNBACK, DURING CLIMBOUT EXPERIENCED 4 SERIES OF ABRUPT NR 2 ENGINE ROLLBACKS, BETWEEN 800 FT AND 2000 FT AT 2000 FT PULLED NR 2 ENGINE THRUST BACK ABOUT 10 TO 20 PERCENT. REMOVED AND REPLACED FUEL PUMP AND MEC PER MM.
Part: CABLE — MISROUTED (R2 DOOR SLIDE) · airframe 25,508 hrs · 21,223 cycles
DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED R2 DOOR EVAC SLIDE CABLE PER MM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 25,352 hrs · 21,086 cycles
DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 767, RBL 8, CORRODED. REPAIRED SHEAR TIE PER SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 25,352 hrs · 21,086 cycles
DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 747, LBL 10, CORRODED. REPAIRED SHEAR TIE PER SRM.
Part: DOOR FRAME — CRACKED (R2 DOOR) · airframe 25,352 hrs · 21,086 cycles
DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT SIDE FRAME AT THIRD STOP FITTING CRACKED. REPAIRED FRAME SECTION PER SRM.
Part: SIGN — BROKEN (CABIN) · airframe 24,622 hrs · 20,496 cycles
FWD ENTRY DOOR EMERGENCY EXIT SIGN COVER BROKE. REMOVED AND REPLACED EMERGENCY EXIT SIGN ASSEMBLY PER MM.
Part: CABLE — LOOSE (L2 DOOR SLIDE) · airframe 23,660 hrs · 19,709 cycles
DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE LOOSE. SECURED L2 DOOR EVAC SLIDE CABLE PER MM.
Part: STARTER — INOPERATIVE (NR 2 ENGINE) · airframe 23,438 hrs · 19,527 cycles
WHILE STARTING NR 2 ENG, NOTICED SPARKS FROM COWLING. REMOVED AND REPLACED NR 2 ENG STARTER PER MM.
2003
Part: UPLOCK SENSOR — FAULTY (LT MLG) · airframe 21,305 hrs · 17,848 cycles
LT MLG UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION, RECYCLED GEAR ALL GEAR LIGHTS NORMAL. REMOVED AND REPLACED LT MLG UPLOCK SENSOR PER MM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 19,948 hrs · 16,761 cycles
DURING SCHEDULED RON, FOUND OVERHEAD BIN EMERGENCY EXIT BULL NOSE LIGHT INOP AT RT FWD CABIN. REMOVED AND REPLACED BATTERY PER MM.
Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 19,853 hrs · 16,674 cycles
DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.
2002
Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 18,913 hrs · 15,938 cycles
DURING SCHEDULED BC1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.
Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 17,049 hrs · 14,438 cycles
DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS727, STR 15L. REMOVED AND REPLACED TIE CLIP PER SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 17,049 hrs · 14,438 cycles
DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS440, STR 16R. REMOVED AND REPLACED STR CLIP PER SRM.
Part: BRACKET — CORRODED (CABIN) · airframe 58,478 hrs · 37,818 cycles
DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH BRACKETS CORRODED. REMOVED AND REPLACED ATTACH BRACKETS PER SRM.
2001
Part: SKIN — DELAMINATED (T/E FLAP) · airframe 13,221 hrs · 11,254 cycles
DURING SCHEDULED C3 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED ON UPPER SKIN. REMOVED AND REPLACED AFT FLAP PER MM.
Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 13,221 hrs · 11,254 cycles
DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM.
2000
Part: COVER — LOOSE (CABIN) · airframe 12,131 hrs · 10,370 cycles
EEPLS LOOSE AT ROW 8. SECURED EEPLS TRACK COVER PER MM.
1999
Part: LENS — MISSING (SERV DOORWAY)
DURING SCHEDULED SERVICE CK CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT LENS MISSING. REPLACED LENS ASSY PER MM.
1998
Part: SKIN — DAMAGE (BS 837)
AIRCRAFT DAMGE BY BAG CART, DENTED AND GAUGE AFT LEFT HAND FUSELAGE BS 837 AT LOWER SKIN LAP JOINT. WATER LINE STRINGER FLANGE BENT AFT CARGO HOLD FLOOR. OPENED CARGO PANEL, CUT OUT DAMAGE AREA, FABRICATED AND INSTALLED REPAIR DOUBLER PER BOEING SRM. CLOSED CARGO PANEL AND RESTORED ORIGINAL FINISH.
1997
Part: APU — FAILED (AFT FUSELAGE)
SLIGHT SMOKE IN CABIN DURING APU OPERATION. VERIFIED APU WAS THE CAUSE \NDEFERRED APU OPERATION PER MEL\N\NREPLACED APU ASSEMBLY DURING OVERNIGHT MAINT CHECK PER BOEING M/M