N771SA
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.
216 reports on file, 2001-08-08 – 2019-08-24.
Part: TRUNNION — OUT OF TOLERANCE (LT MLG) · airframe 67,164 hrs · 39,468 cycles
LEFT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER OUTBOARD BORE INNER DIAMETER EXCEEDS LIMITS. / REPAIRED BORE PER EA.
Part: TRUNNION — CORRODED (RT MLG) · airframe 67,164 hrs · 39,468 cycles
R/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD FUSE PIN BORE OUTER FACE CORRODED. REPAIRED BORE PER EA.
Part: TRUNNION — OUT OF TOLERANCE (RT MLG) · airframe 67,164 hrs · 39,468 cycles
R/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD FUSE PIN BORE INNER DIAMETER EXCEEDS LIMITS. REPAIRED BORE PER EA.
Part: TRUNNION — OUT OF TOLERANCE (RT MLG) · airframe 67,164 hrs · 39,468 cycles
R/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD FUSE PIN BORE INNER DIAMETER EXCEEDS LIMITS. / REPAIRED BORE PER EA.
Part: TRUNNION — CORRODED (LT MLG) · airframe 67,164 hrs · 39,468 cycles
L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD FUSE PIN BORE OUTER FACE CORRODED. / REPAIRED BORE PER EA.
Part: TRUNNION — OUT OF TOLERANCE (LT MLG) · airframe 67,164 hrs · 39,468 cycles
L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD BORE INNER DIAMETER EXCEEDS LIMITS. / REPAIRED BORE PER EA.
Part: TRUNNION — CORRODED (RT MLG) · airframe 67,164 hrs · 39,468 cycles
R/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD FUSE PIN BORE OUTER FACE CORRODED. / REPAIRED BORE PER EA.
Part: TRUNNION — OUT OF TOLERANCE (RT MLG) · airframe 67,164 hrs · 39,468 cycles
R/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER OUTBOARD FUSE PIN BORE INNER DIAMETER EXCEEDS LIMITS. REPAIRED BORE PER EA.
Part: TRUNNION — CORRODED (RT MLG) · airframe 67,164 hrs · 39,468 cycles
R/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD FUSE PIN BORE OUTER FACE CORRODED. REPAIRED BORE PER EA.
Part: TRUNNION — OUT OF TOLERANCE (LT MLG) · airframe 67,164 hrs · 39,468 cycles
L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD FUSE PIN BORE INNER DIAMETER EXCEEDS LIMITS. / REPAIRED BORE PER EA.
Part: TRUNNION — OUT OF TOLERANCE (LT MLG) · airframe 67,164 hrs · 39,468 cycles
L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD FUSE PIN BORE INNER DIAMETER EXCEEDS LIMITS. / REPAIRED BORE PER EA.
Part: TRUNNION — OUT OF TOLERANCE (LT MLG) · airframe 67,164 hrs · 39,468 cycles
L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD FUSE PIN BORE OUTER CORRODED. REPAIRED BORE PER EA.
Part: TRUNNION — OUT OF TOLERANCE (RT MLG) · airframe 67,164 hrs · 39,468 cycles
R/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD FUSE PIN BORE INNER DIAMETER EXCEEDS LIMITS. REPAIRED BORE PER EA.
Part: TRUNNION — CORRODED (LT MLG) · airframe 67,164 hrs · 39,468 cycles
L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD FUSE PIN BORE OUTER FACE CORRODED. REPAIRED BORE PER EA.
Part: PANEL — DAMAGED (LT WING) · airframe 67,164 hrs · 39,468 cycles
LEFT WING LOWER FIXED TRAILING EDGE PANEL INBOARD END NEXT TO FUSELAGE FIXED FAIRING PANEL CRACKED AND LEADING EDGE DAMAGED. R&R PANEL PER AMM.
Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 66,289 hrs · 38,922 cycles
L1 DOOR SLIDE GAUGE PRESSURE LOW. R&R L1 DOOR SLIDE ASSEMBLY PER MT.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,290 hrs · 38,302 cycles
FORWARD L1 EMERGENCY LIGHT INOP. R&R BATTERY PACK PER AMM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,290 hrs · 38,302 cycles
FORWARD RT EMERGENCY LIGHT INOP AT ROW 6. R&R BATTERY PACK PER AMM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,290 hrs · 38,302 cycles
FORWARD RT EMERGENCY LIGHT INOP AT ROW 3. R&R BATTERY PACK PER AMM.
Earlier reports · 2001–2018 · 197 reports
2018
Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 64,237 hrs · 37,600 cycles
L1 DOOR ESCAPE SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.
Part: CHECK VALVE — BROKEN (AC BAY) · airframe 63,881 hrs · 37,376 cycles
AIR TURNBACK/DECLARED EMERGENCY, AIRCRAFT SLOWLY STOPPED PRESSURING. DURING CLIMB- NO LIGHTS FOR PRESS PANEL OR DOOR LIGHTS. R&R GROUND CONDITIONED AIR CHECK VALVE PER MM.
Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 63,446 hrs · 37,098 cycles
R1 DOOR SLIDE HAD LOW PRESSURE. R&R SLIDE IAW MT.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 62,827 hrs · 36,684 cycles
LT UPPER VAPOR BARRIER ANGLE COMMON TO CENTER FUEL TANK CRACKED AT BS 663, LBL 27. REPAIRED ANGLE IAW EA.
Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 62,827 hrs · 36,684 cycles
R1 DOOR CUT OUT BEAR STRAP CRACKED AT BS 294.5, STR 9R. REPAIRED BEAR STRAP IAW EA.
Part: VAPOR BARRIER — CRACKED (FUSELAGE) · airframe 62,827 hrs · 36,684 cycles
LT AC BAY AFT VAPOR BARRIER CRACKED AT BS 663. R&R WEB IAW SRM & DWG.
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,827 hrs · 36,684 cycles
R1 DOOR CUTOUT STA 294.5 JUST ABOVE CREASE BEAM WEB, DOOR FRAME CRACKED. REPAIRED STUB FRAME IAW EA.
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,827 hrs · 36,684 cycles
R1 DOOR FRAME CUTOUT CRACKED AT BS 294.5, STR 9R. R&R STUB FRAME IAW DWG.
Part: FLOORBEAM — CORRODED (BS 947) · airframe 62,827 hrs · 36,684 cycles
AFT PAX CABIN FLOORBEAM UPPER TEE CORRODED, BS 947.5, BETWEEN LBL 6 TO RBL 5. R & R THE FLOORBEAM IAW EA AND SRM.
Part: FLOOR SUPPORT — CORRODED (BS 960-990) · airframe 62,827 hrs · 36,684 cycles
PASSENGER CABIN FLOOR SUPPORT CORRODED BETWEEN BS 960 TO 990, LBL 52. R & R IAW SRM & DWG.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,827 hrs · 36,684 cycles
AFT CARGO COMPARTMENT FLOOR STRUCTURE INTERCOSTAL CORRODED BETWEEN BS 867 TO BS 877, LBL 9. R&R INTERCOSTAL IAW SRM & DWG.
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 62,827 hrs · 36,684 cycles
AFT CARGO PIT BULKHEAD LATERAL SUPPORT ANGLE CORRODED AT BS 947 FLOOR LINE. R&R ANGLE IAW SRM & DWG.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,827 hrs · 36,684 cycles
AFT CARGO RT Z-ANGLE CORRODED BETWEEN BS 727E+12 TO BS 767. R&R Z ANGLE IAW SRM.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,827 hrs · 36,684 cycles
AFT CARGO LONGITUDINAL FLOOR SUPPORT CORRODED AT BS 727D+5, LBL 8.1. R&R ANGLE IAW SRM AND EA.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,827 hrs · 36,684 cycles
AFT CARGO FLOOR SUPPORT RAIL ANGLE CORRODED AT BS 767+5, LBL 17.24. R&R ANGLE IAW SRM & EA.
Part: ANGLE — CORRODED (BS 727E-847) · airframe 62,827 hrs · 36,684 cycles
AFT CARGO LEFT ZEE ANGLE CORRODED AROUND NUTPLATE HOLES BETWEEN BS 727E TO 847, LBL 21. R & R THE ZEE ANGLE IAW SRM.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,827 hrs · 36,684 cycles
AFT CARGO FLOOR SUPPORT RAIL CORRODED AT BS 767+5, LBL 12.5. R&R ANGLE IAW SRM & EA.
Part: FLOOR SUPPORT — CORRODED (BS 767) · airframe 62,827 hrs · 36,684 cycles
AFT CARGO FLOOR SUPPORT CORRODED AT BS. 767+5, LBL 3. R & R THE FLOOR SUPPORT IAW SRM AND EA.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,827 hrs · 36,684 cycles
AFT CARGO FLOOR SUPPORT RAIL CORRODED AT BS 767+5, RBL 3. R&R ANGLE IAW SRM AND EA.
Part: FLOOR SUPPORT — CORRODED (BS 767) · airframe 62,827 hrs · 36,684 cycles
AFT CARGO FLOOR SUPPORT CORRODED AT BS 767+5, LBL 8.1. R & R THE FLOOR SUPPORT IAW SRM AND EA.
Part: ANGLE — CORRODED (BS 727-727E) · airframe 62,827 hrs · 36,684 cycles
AFT CARGO LEFT ZEE ANGLE CORRODED BETWEEN BS 727 TO 727E, LBL 21. R & R THE ANGLE IAW SRM.
Part: FLOOR SUPPORT — CORRODED (BS 727D) · airframe 62,827 hrs · 36,684 cycles
AFT CARGO LONGITUDINAL FLOOR SUPPORT CORRODED AT BS 727D+5, LBL 3. R & R THE FLOOR SUPPORT IAW SRM AND EA.
Part: ANGLE — CORRODED (BS 500A-500D) · airframe 62,827 hrs · 36,684 cycles
FORWARD CARGO BAY, THE RT ZEE ANGLE CORRODED BETWEEN BS 500A TO 500D, RBL 23. REPAIRED THE ANGLE IAW SRM & DWG.
Part: ANGLE — CORRODED (BS 400-500D) · airframe 62,827 hrs · 36,684 cycles
FORWARD CARGO BAY, LT ZEE ANGLE CORRODED BETWEEN BS 400 TO 500D, LBL 23. R & R THE ANGLE IAW SRM.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,827 hrs · 36,684 cycles
AFT CARGO FLOOR SUPPORT RAIL CORRODED AT BS 767+5, RBL 8.1. R&R ANGLE IAW SRM AND EA.
Part: SKIN — CRACKED (LE SLAT) · airframe 62,827 hrs · 36,684 cycles
RT WING NR 5 SLAT NOSE SKIN LOWER SURFACE AT ACT RIB FASTENER HOLE CRACKED. REPAIRED NR 5 SLAT SKIN IAW SRM.
Part: ELEMENT — FAULTY (FIRE DETECTOR) · airframe 62,486 hrs · 36,479 cycles
WHEEL WELL FIRE INDICATION. DECLARED EMERGENCY. R & R THE ELEMENT IAW AMM.
Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,328 hrs · 36,384 cycles
LEFT OVERWING EXIT SIGN INOPERATIVE. REPAIRED THE SIGN IAW MM.
Part: LENS — LOOSE (L2 DOOR) · airframe 62,191 hrs · 36,300 cycles
L2 DOOR SLIDE COVER LENS LOOSE. R&R LENS PER MT AND AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 62,191 hrs · 36,300 cycles
EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M01672. R&R BATTERY PACK PER AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 62,191 hrs · 36,300 cycles
EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M01673. R&R BATTERY PACK PER AMM.
Part: LENS — LOOSE (L1 DOOR) · airframe 62,191 hrs · 36,300 cycles
L1 DOOR SLIDE COVER LENS LOOSE. R&R LENS MT AND AMM.
2017
Part: BULKHEAD WEB — CRACKED (RT WING WW) · airframe 60,861 hrs · 35,414 cycles
RIGHT WHEEL WELL PRESSURE DECK BEADED WEB CRACKED AT BS 664, RBL 43. REPAIRED THE WEB IAW EA.
Part: COVER — MISSING (EXIT SIGN) · airframe 60,783 hrs · 35,372 cycles
RT DOOR EMERGENCY EXIT SIGN COVER MISSING. R&R COVER PER AMM.
Part: BOTTLE — LOW PRESSURE (R1 DOOR SLIDE) · airframe 60,018 hrs · 34,934 cycles
R1 DOOR SLIDE PRESSURE INDICATOR READS LOW. R & R THE SLIDE ASSY IAW MM.
Part: RETAINER — LOOSE (R2 DOOR SLIDE) · airframe 59,630 hrs · 34,693 cycles
R2 DOOR SLIDE MOUNTED GIRT BAR RETAINER LOOSE. / SECURED THE RETAINER IAW SIP.
2016
Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 58,169 hrs · 33,818 cycles
RT PHOTO LUMINESCENT STRIP DAMAGED AT ROW 1. R&R STRIP PER AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 58,169 hrs · 33,818 cycles
ONE BATTERY PACK AT POSITION M1668 FAILED CAPACITY CHECK. R&R BATTERY PACK PER AMM.
Part: PLUG — DIRTY (WHEEL WELL) · airframe 58,152 hrs · 33,805 cycles
DECLARED EMERGENCY, WHEEL WELL FIRE WARNING LIGHT AND BELL CAME ON AT 12,000 MSL 230KIAS. BOTH WENT OUT/OFF WHEN GEAR WAS EXTENDED. CLEANED WHEEL WELL SENSING ELEMENT CONNECTOR PLUGS PER AMM.
Part: VENT — FAULTY (LT WING) · airframe 57,898 hrs · 33,636 cycles
AFTER TAKE-OFF, TOWER NOTIFIED FLIGHT CREW OF POSSIBLE SMOKE TRAILING FROM LEFT WING. NO ABNORMAL INDICATIONS NOTED. ALL FLIGHT CONTROLS NORMAL. RETURNED TO DEPARTURE SUSPECTED FUEL LEAK, NO LOSS OF FUEL NOTED FROM LEFT TANK. FIRST OFFICER NOTED FUEL ON UNDERSIDE OF LEFT WING NEAR FUEL VENT THAT WASN'T PRESENT ON PRE-FLIGHT. R &R THE LEFT WING LOWER FUEL PANEL VENT IAW AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,138 hrs · 33,196 cycles
FORWARD GALLEY EMERGENCY ENTRY LIGHT INOPERATIVE. R & R THE LIGHT IAW AMM.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,138 hrs · 33,196 cycles
FORWARD GALLEY EMERGENCY ENTRY LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,138 hrs · 33,196 cycles
RIGHT EMERGENCY LIGHT INOPERATIVE BETWEEN ROW 2 TO ROW 5. R & R THE BATTERY PACK IAW AMM.
Part: DOOR — CRACKED (LT MLG) · airframe 57,138 hrs · 33,196 cycles
LEFT MAIN LANDING GEAR CENTER DOOR CRACKED. R & R THE MLG DOOR IAW AMM.
Part: FLAP — DELAMINATED (LT WING) · airframe 57,138 hrs · 33,196 cycles
LT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD LOWER CORNER. REPAIRED AFT FLAP IAW SRM.
Part: SKIN — DELAMINATED (RT SPOILER) · airframe 57,138 hrs · 33,196 cycles
RT WING NR 7 GROUND SPOILER DELAMINATED ON LOWER SURFACE. REPAIRED SPOILER IAW SRM.
Part: SKIN — DELAMINATED (LT WING SPOILER) · airframe 57,138 hrs · 33,196 cycles
LEFT WING NR 6 GROUND SPOILER SKIN DELAMINATED ON LOWER SURFACE, 9 INCHES INBOARD EDGE AND 13 INCHES FROM TRAILING EDGE. REPAIRED THE GROUND SPOILER IAW EA.
Part: SUPPORT ANGLE — CRACKED (BS 520) · airframe 57,138 hrs · 33,196 cycles
FORWARD BELLY FAIRING SUPPORT ANGLE CRACKED AT BS 520, STRINGER 20L. R & R THE SUPPORT ANGLE IAW SRM AND DWG.
Part: SKIN — DELAMINATED (LT WING SPOILER) · airframe 57,138 hrs · 33,196 cycles
LEFT WING NR 6 SPOILER SKIN DELAMINATED, 36 INCHES FROM INBOARD EDGE. REPAIRED THE SPOILER IAW SRM.
Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 57,138 hrs · 33,196 cycles
LOWER FUSELAGE WEB CRACKED AT BS 663.75, RBL 12. REPAIRED WEB IAW SRM.
Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 57,138 hrs · 33,196 cycles
LOWER FUSELAGE WEB CRACKED AT BS 663.75, LBL 30. REPAIRED WEB IAW EA.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,138 hrs · 33,196 cycles
LEFT SIDE HATCH EMERGENCY EXIT UPPER LAMP INOPERATIVE. R & R LAMP IAW AMM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,138 hrs · 33,196 cycles
FRAME CRACKED AT BS 440, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,138 hrs · 33,196 cycles
FRAME CRACKED AT BS 867, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,138 hrs · 33,196 cycles
FRAME CRACKED AT BS 867, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,138 hrs · 33,196 cycles
FRAME CRACKED AT BS 727B, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,138 hrs · 33,196 cycles
FRAME CRACKED AT BS 727D, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,138 hrs · 33,196 cycles
FRAME CRACKED AT BS 500A, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,138 hrs · 33,196 cycles
FRAME CRACKED AT BS 500C, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,138 hrs · 33,196 cycles
FRAME CRACKED AT BS 440, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,138 hrs · 33,196 cycles
FRAME CRACKED AT BS 500A, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,138 hrs · 33,196 cycles
FRAME CRACKED AT BS 727B, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.
Part: FAIRING — CRACKED (TE FLAP) · airframe 57,138 hrs · 33,196 cycles
LEFT WING NR 3 FLAP TRACK FAIRING CRACKED. REPAIRED FAIRING IAW SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,138 hrs · 33,196 cycles
FRAME WEB CRACKED AT BS 727, WL 200 LT SIDE. REPAIRED WEB IAW EA.
Part: LENS — BROKEN (CABIN) · airframe 57,138 hrs · 33,196 cycles
AFT GALLEY AREA EMERGENCY LIGHT LENS BROKEN. R & R LENS IAW AMM.
Part: SUPPORT — CRACKED (FUSELAGE) · airframe 57,138 hrs · 33,196 cycles
ANGLE SUPPORT CRACKED AT BS 663.75, RBL 7. R & R SUPPORT IAW SRM AND DWG.
Part: LENS — BROKEN (CABIN) · airframe 57,138 hrs · 33,196 cycles
FORWARD GALLEY AREA EMERGENCY LIGHT LENS BROKEN. R & R LENS IAW AMM.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 57,138 hrs · 33,196 cycles
STIFFENER CRACKED AT BS 663.75, BETWEEN RBL 5 TO RBL 24. R & R STIFFENER IAW SRM AND DWG.
Part: FAIRING — CRACKED (TE FLAP) · airframe 57,138 hrs · 33,196 cycles
LT WING FLAP TRACK NR 1 FAIRING CRACKED ON INTERNAL AREA. REPAIRED NR 1 FAIRING IAW EA.
Part: FAIRING — CRACKED (TE FLAP) · airframe 57,138 hrs · 33,196 cycles
RIGHT WING NR 6 FLAP TRACK FAIRING CRACKED. REPAIRED FAIRING IAW SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,138 hrs · 33,196 cycles
FRAME WEB CRACKED AT BS 727, RBL 45.5+18. REPAIRED WEB IAW EA.
Part: SKIN — CRACKED (LE SLAT) · airframe 57,138 hrs · 33,196 cycles
LT WING L/E NOSE SKIN ON NR 1 SLAT CRACKED AT STA 451.97. REPAIRED SKIN IAW SRM.
Part: SKIN — CRACKED (RT WING) · airframe 57,138 hrs · 33,196 cycles
RIGHT WING NR 7 L/E NOSE SKIN CRACKED AT STA 322.71, ACTUATOR RIB AROUND FASTENER. REPAIRED SKIN IAW SRM.
Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 56,367 hrs · 32,751 cycles
L2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT & AMM.
Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 56,367 hrs · 32,751 cycles
L1 DOOR EMER EVAC SLIDE, GIRT BAR OUT OF POSITION. REPOSITIONED SLIDE IAW MT & AMM.
Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 56,367 hrs · 32,751 cycles
R2 DOOR EMER EVAC SLIDE GIRT BAR OUT OF POSITION. REPOSITIONED SLIDE IAW MT AMM.
Part: BATTERY — FAILED (CABIN) · airframe 56,367 hrs · 32,751 cycles
CABIN EMER LIGHTING BATTERY PACK M1675 FAILED CAPACITY CHECK. R & R BATTERY IAW MM.
2015
Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 55,355 hrs · 32,183 cycles
DIVERSION, AFT LAVATORY SMOKE DETECTOR GOING OFF INFLIGHT. R & R NR 2 AFT COFFEE MAKER IAW MM.
Part: LENS — MISSING (CABIN) · airframe 53,233 hrs · 30,944 cycles
RIGHT OVERWING EMER EXIT HATCH LIGHT COVER LENS MISSING. INSTALLED LENS IAW EA.
Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 52,927 hrs · 30,775 cycles
R1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.
Part: LIGHT — CRACKED (CABIN) · airframe 52,927 hrs · 30,775 cycles
LEFT FWD EMER FLOORLIGHT STRIP CRACKED AT ROW 1. R & R LIGHT IAW AMM.
2014
Part: CHANNEL — CRACKED (VERTICAL STAB) · airframe 51,843 hrs · 30,170 cycles
RIGHT INTERNAL VERTICAL STABILIZER LOWER CHANNEL CRACKED AT STATION 1016 + 8 INCHES. R & R CHANNEL IAW SRM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 51,843 hrs · 30,170 cycles
AFT GALLEY RT EMER LIGHT BATTERY PACKS FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 51,843 hrs · 30,170 cycles
AFT GALLEY LT EMER LIGHT BATTERY PACKS FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.
Part: LENS — BROKEN (EXIT SIGN) · airframe 50,279 hrs · 29,300 cycles
FORWARD LAVATORY, AFT FACING WALL, EMER EXIT SIGN LENS BROKEN. R & R SIGN ASSEMBLY IAW AMM.
Part: LENS — BROKEN (EXIT SIGN) · airframe 50,279 hrs · 29,300 cycles
LEFT SIDEWALL EMER EXIT SIGN LENS BROKEN. R & R LENS IAW AMM.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 50,279 hrs · 29,300 cycles
FUSELAGE UPPER CROWN SKIN DAMAGED BETWEEN BS 853 TO 888, STRINGER 2L. REPAIRED SKIN IAW SRM & DWG.
Part: STRAP — CRACKED (FUSELAGE) · airframe 50,279 hrs · 29,300 cycles
SEAT TRACK SPLICE STRAP CRACKED FWD OF BS 727B, LBL 25. REPAIRED STRAP IAW EA.
Part: BRACKET — CRACKED (LT WING) · airframe 50,279 hrs · 29,300 cycles
LEFT WING TE OTBD OF MLG AT HINGED ACCESS PANEL OTBD SIDE, BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,279 hrs · 29,300 cycles
SEAT TRACK FLANGE CRACKED AT BS 727B, LBL 45.5 OTBD AFT & BOTH INBD HOLES. REPAIRED FLANGE IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,279 hrs · 29,300 cycles
SEAT TRACK FLANGE CRACKED AT BS 727B, LBL 24.75 OTBD AFT & BOTH INBD HOLES. REPAIRED FLANGE IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,279 hrs · 29,300 cycles
SEAT TRACK FLANGE CRACKED AT BS 727B, RBL 24.75 OTBD AFT & BOTH INBD HOLES. REPAIRED FLANGE IAW EA.
Part: BATTERY PACK — FAILED (CABIN) · airframe 49,683 hrs · 28,958 cycles
EMERGENCY CABIN LIGHT AT ROW 8 - 12 DEF FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.
Part: BRACKET — LOOSE (R1 DOOR) · airframe 49,518 hrs · 28,864 cycles
R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR DOOR BRACKET LOOSE. SECURED BRACKET IAW SIP.
Part: SKIN — CRACKED (FUSELAGE) · airframe 49,284 hrs · 28,731 cycles
EXTERNAL POWER DOOR CUTOUT CRACKED BELOW LOWER HINGE. REPAIRED CUTOUT IAW EA.
Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 49,284 hrs · 28,731 cycles
RT HORIZONTAL STABILIZER RIB STATION 92.7, 3RD VERTICAL STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.
Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 49,284 hrs · 28,731 cycles
RT HORIZONTAL STABILIZER STATION 92.7 VERTICAL STIFFENER SECOND ONE CRACKED BOTH INBD & OTBD OF THE WEB. REPAIRED STIFFENER IAW SRM.
Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 49,284 hrs · 28,731 cycles
RT HORIZONTAL STABILIZER RIB STATION 92.7, 4TH VERTICAL STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.
Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 49,284 hrs · 28,731 cycles
LT NR 3 WINDOW FRAME E F POST, SECOND FASTENER HOLE FROM BOTTOM CRACKED. REPAIRED FRAME IAW ACO.
Part: POST — CRACKED (FUSELAGE) · airframe 49,284 hrs · 28,731 cycles
LT NR 3 WINDOW FRAME E F POST, SECOND FASTENER HOLE FROM BOTTOM CRACKED. REPAIRED POST IAW AAR EA.
Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 49,284 hrs · 28,731 cycles
FLIGHT DECK LT NR 1 WINDOW FRAME OTBD UPPER CORNER CRACKED. R & R FRAME IAW ACO.
Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 49,284 hrs · 28,731 cycles
RT NR 3 WINDOW FRAME E F POST SECOND FASTENER HOLE FROM BOTTOM CRACKED. REPAIRED FRAME IAW ACO.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 49,208 hrs · 28,685 cycles
R1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.
2013
Part: BATTERY PACK — FAILED (CABIN) · airframe 47,582 hrs · 27,732 cycles
R1 DOOR UPPER EMERGENCY EXIT LIGHTS FAILED CAPACITY CHECK. R&R BATTERY PACKS IAW AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 47,582 hrs · 27,732 cycles
RT EMERGENCY EXIT LIGHTS FAILED CAPACITY CHECK BETWEEN ROW 8 TO ROW 13. R&R BATTERY PACKS IAW AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 47,582 hrs · 27,732 cycles
L1 DOOR EMERGENCY EXIT LIGHTS FAILED CAPACITY CHECK. R&R BATTERY PACK IAW AMM.
Part: SIGN — LOOSE (CABIN) · airframe 46,385 hrs · 27,038 cycles
EMERGENCY EXIT SIGN ON CEILING OVERWING LOOSE. REMOVED AND REPLACED SIGN PER MM.
Part: HANDLE — BROKEN (E&E DOOR) · airframe 45,969 hrs · 26,768 cycles
MAIN E&E DOOR HANDLE BROKEN. REMOVED AND REPLACED HANDLE ASSY IAW MM.
2012
Part: SEAL — CRACKED (STABILIZER) · airframe 45,292 hrs · 26,316 cycles
LEFT LOWER STAB SLIDER SEAL IS CRACKED. REMOVED AND REPLACED PER AMM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 44,042 hrs · 25,528 cycles
FRAME CRACKED AT BS 400, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 44,042 hrs · 25,528 cycles
FRAME CRACKED AT BS 727D, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,042 hrs · 25,528 cycles
FLOORBEAM CORRODED AT BS 986.5, BETWEEN RBL 7 TO RBL 38. REPAIRED BEAM PER EA.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 44,042 hrs · 25,528 cycles
LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 120.30. REPAIRED SKIN PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 44,042 hrs · 25,528 cycles
FRAME CRACKED AT BS 480, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 44,042 hrs · 25,528 cycles
FRAME CRACKED AT BS 907, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 44,042 hrs · 25,528 cycles
FRAME CRACKED AT BS 867, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER EA.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 44,042 hrs · 25,528 cycles
STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM.
Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 44,042 hrs · 25,528 cycles
RIGHT VERTICAL WEB CRACKED AT BS 663, BETWEEN RBL 24.75 TO RBL 45.50. REPAIRED WEB PER EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 44,042 hrs · 25,528 cycles
FRAME CRACKED AT BS 400, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 44,042 hrs · 25,528 cycles
FRAME CRACKED AT BS 360, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 44,042 hrs · 25,528 cycles
FRAME CRACKED AT BS 480, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 44,042 hrs · 25,528 cycles
FRAME CRACKED AT BS 827, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 44,042 hrs · 25,528 cycles
FRAME CRACKED AT BS 787, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 44,042 hrs · 25,528 cycles
FRAME CRACKED AT BS 747, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 44,042 hrs · 25,528 cycles
FRAME CRACKED AT BS 787, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 44,042 hrs · 25,528 cycles
FRAME CRACKED AT BS 907, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,056 hrs · 24,972 cycles
EMERGENCY EXIT BULL NOSE LIGHT INOP AT 5 DEF. RELAMPED PER MM.
Part: LIGHT — LOOSE (CABIN) · airframe 42,367 hrs · 24,564 cycles
EEPLS LOOSE. SECURED EEPLS PER MM.
2011
Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,185 hrs · 24,443 cycles
DURING SCHEDULED CV CHECK, FOUND LT OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 13. RELAMPED PER MM.
Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 41,676 hrs · 24,129 cycles
R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE PER MT.
Part: LIGHT — LOOSE (CABIN) · airframe 41,014 hrs · 23,752 cycles
DURING SCHEDULED HC2 CHECK, FOUND LT EEPLS LOOSE AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.
Part: SIGN — BROKEN (R1 DOOR) · airframe 40,751 hrs · 23,593 cycles
R1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.
Part: REGULATOR — FAULTY (BLEED AIR SYS) · airframe 40,581 hrs · 23,498 cycles
DECLARED EMERGENCY - LT ENGINE BLEED TRIP OFF ILLUMINATED AROUND FL 390 CABIN ALT REACHED APPX 21000. REMOVED AND REPLACED HIGH STAGE REGULATOR PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,571 hrs · 23,493 cycles
DURING SCHEDULED MV2 CHECK, FOUND RT FWD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: SIGN — BROKEN (CABIN) · airframe 40,523 hrs · 23,466 cycles
R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 39,442 hrs · 22,819 cycles
DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EXTERIOR LIGHT INOP. RELAMPED LIGHT PER MM.
Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 38,785 hrs · 22,457 cycles
DURING SCHEDULED OTS CHECK, FOUND LT MLG WHEEL WELL FWD BULKHEAD CRACKED AT BS 663, LBL 43. REPAIRED BULKHEAD PER ER AND EA.
2010
Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,705 hrs · 21,853 cycles
R2 DOOR EEPLS INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: FITTING — LOOSE (GIRT BAR) · airframe 37,072 hrs · 21,501 cycles
DURING SCHEDULED OTS CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FLOOR FITTING LOOSE. SECURED FITTING PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,072 hrs · 21,501 cycles
DURING SCHEDULED OTS CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT BULBS INOP. REMOVED AND REPLACED LIGHT PER MM.
Part: WEB — CRACKED (RT WING) · airframe 36,981 hrs · 21,442 cycles
DURING SCHEDULED 10Y CHECK, FOUND RT WING L/E WEB CRACKED. REMOVED AND REPLACED WEB PER SRM.
Part: FLAP — DELAMINATED (LT WING) · airframe 36,981 hrs · 21,442 cycles
DURING SCHEDULED 10Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED AT I/B TRAILING EDGE. REPAIRED AFT FLAP PER MM.
Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,981 hrs · 21,442 cycles
DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547, LBL 6. REMOVED AND REPLACED FITTING PER SRM.
Part: FLAP — DELAMINATED (RT WING) · airframe 36,981 hrs · 21,442 cycles
DURING SCHEDULED 10Y CHECK, FOUND RT WING O/B TRAILING EDGE FLAP, TRAILING EDGE FLAP I/B CORNER DELAMINATED. REMOVED AND REPLACED O/B FLAP PER SRM.
Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,981 hrs · 21,442 cycles
DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547, RBL 6. REMOVED AND REPLACED FITTING PER SRM.
Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,981 hrs · 21,442 cycles
DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547, RBL 41. REMOVED AND REPLACED FITTING PER SRM.
Part: FITTING — CRACKED (CENTER WING BOX) · airframe 36,981 hrs · 21,442 cycles
DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 547, LBL 41. REMOVED AND REPLACED FITTING PER SRM.
Part: SKIN — CRACKED (LE SLAT) · airframe 36,981 hrs · 21,442 cycles
DURING SCHEDULED 10Y CHECK, FOUND RT WING L/E NR 6 SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 36,981 hrs · 21,442 cycles
DURING SCHEDULED 10Y CHECK, FOUND FWD CARGO COMPT SURFACE CHANNEL CORRODED BETWEEN BS 500A TO BS 500B, LBL 3. REMOVED AND REPLACED CHANNEL PER SRM AND BAC DWG.
Part: SIGN — LOOSE (CABIN) · airframe 36,193 hrs · 20,994 cycles
R1 DOOR EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: FLAP — PUNCTURED (LT WING) · airframe 36,016 hrs · 20,872 cycles
LEFT WING I/B TRAILING EDGE FLAP PUNCTURED. REMOVED AND REPLACED FLAP PER SRM.
2009
Part: SIGN — BROKEN (CABIN) · airframe 35,125 hrs · 20,303 cycles
L2 DOOR EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.
Part: CABLE — LOOSE (EVAC SLIDE) · airframe 35,052 hrs · 20,259 cycles
L2 DOOR EVAC SLIDE CONTAINER CABLE LOOSE. SECURED CABLE PER MM.
Part: FITTING — CORRODED (LT MLG) · airframe 35,032 hrs · 20,248 cycles
DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.
Part: FITTING — CORRODED (RT MLG) · airframe 35,032 hrs · 20,248 cycles
DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.
Part: LIGHT — LOOSE (CABIN) · airframe 32,844 hrs · 18,898 cycles
EEPLS LOOSE AT ROW 9. SECURED EEPLS PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,672 hrs · 18,796 cycles
LT EMERGENCY EXIT LIGHT INOP AT ROW 1. RELAMPED PER MM.
Part: LIGHT — WORN (CABIN) · airframe 32,253 hrs · 18,536 cycles
DURING SCHEDULED HC2 CHECK, FOUND EEPLS WORN BETWEEN ROW 22 TO ROW 23. REMOVED AND REPLACED EEPLS PER MM.
Part: LIGHT — WORN (CABIN) · airframe 32,253 hrs · 18,536 cycles
DURING SCHEDULED HC2 CHECK, FOUND EEPLS WORN BETWEEN ROW 11 TO ROW 13. REMOVED AND REPLACED EEPLS PER MM.
Part: LIGHT — WORN (CABIN) · airframe 32,253 hrs · 18,536 cycles
DURING SCHEDULED HC2 CHECK, FOUND EEPLS WORN BETWEEN ROW 9 TO ROW 10. REMOVED AND REPLACED EEPLS PER MM.
2008
Part: LIGHT — BROKEN (CABIN) · airframe 30,270 hrs · 17,339 cycles
DURING SCHEDULED 8Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 30,270 hrs · 17,339 cycles
DURING SCHEDULED 8Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 947 AND BS 986.5, RBL 65. REPAIRED BEAM PER SRM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 30,270 hrs · 17,339 cycles
DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 951, BL 0. REPAIRED BEAM PER SRM.
Part: SKIN — CRACKED (HORIZ STAB) · airframe 29,998 hrs · 17,179 cycles
DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (HORIZ STAB) · airframe 29,998 hrs · 17,179 cycles
DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (HORIZ STAB) · airframe 29,998 hrs · 17,179 cycles
DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 147. REPAIRED SKIN PER SRM.
2007
Part: GLOWSTRIP — WORN (CABIN) · airframe 27,545 hrs · 15,654 cycles
DURING SCHEDULED HC2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 7 ABC. REMOVED AND REPLACED STRIP PER MM.
Part: GLOWSTRIP — WORN (CABIN) · airframe 27,545 hrs · 15,654 cycles
DURING SCHEDULED HC2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 1 ABC. REMOVED AND REPLACED STRIP PER MM.
Part: LIGHT — BROKEN (CABIN) · airframe 27,544 hrs · 16,551 cycles
FWD CABIN EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 26,508 hrs · 15,056 cycles
AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.
Part: SLIDE — DISLODGED (L1 DOOR) · airframe 26,234 hrs · 14,887 cycles
L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 25,949 hrs · 14,712 cycles
FOUND R1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.
Part: BATTERY — FAILED (CABIN) · airframe 24,945 hrs · 14,167 cycles
DURING SCHEDULED HC1 CHECK, LT OVERWING EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY — FAILED (CABIN) · airframe 24,945 hrs · 14,167 cycles
DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.
Part: BATTERY — FAILED (CABIN) · airframe 24,945 hrs · 14,167 cycles
DURING SCHEDULED HC1 CHECK, FWD CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.
Part: BATTERY — FAILED (CABIN) · airframe 24,945 hrs · 14,167 cycles
DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 24,784 hrs · 14,074 cycles
R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
2006
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,161 hrs · 13,703 cycles
DURING SCHEDULED MV1 CHECK, FOUND RIGHT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,116 hrs · 13,463 cycles
DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
2005
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,930 hrs · 11,284 cycles
DURING SCHEDULED HC1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.
Part: SKIN — CRACKED (RUDDER) · airframe 19,930 hrs · 11,284 cycles
DURING SCHEDULED HC1 CHECK, FOUND RUDDER L/E CRACKED AT BOTTOM RT SIDE. REPAIRED RUDDER PER SRM.
Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 19,114 hrs · 10,819 cycles
R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 19,091 hrs · 10,810 cycles
R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
Part: COVER — MISSING (EMERGENCY EXIT) · airframe 19,016 hrs · 10,769 cycles
MID CABIN EMERGENCY EXIT SIGN COVER MISSING. INSTALLED COVER PER MM.
Part: FLOORBEAM — CORRODED (BS 727D) · airframe 18,712 hrs · 10,599 cycles
DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 727D, BETWEEN LBL 8 TO RBL 8. REPAIRED FLOORBEAM PER SWA EA.
Part: FLOORBEAM — CORRODED (BS 772) · airframe 18,712 hrs · 10,599 cycles
DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 772, BETWEEN LBL 8 TO LBL 12. REPAIRED FLOORBEAM PER SWA EA.
2004
Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,293 hrs · 9,236 cycles
DURING SCHEDULED MV2 CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST PER MM.
Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 15,019 hrs · 8,536 cycles
DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.
Part: SLIDE — DISLODGED (R1 DOOR) · airframe 14,469 hrs · 8,231 cycles
R1 DOOR EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. INSTALLED R1 DOOR EVAC SLIDE PER MM.
Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 13,856 hrs · 7,904 cycles
DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.
2003
Part: COVER — CRACKED (CABIN) · airframe 10,207 hrs · 5,907 cycles
DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED BETWEEN ROW NR 2 & ROW 23. REMOVED AND REPLACED EEPLS COVERS PER MM.
2002
Part: LENS — MISSING (CABIN) · airframe 8,369 hrs · 4,902 cycles
DURING SCHEDULED SERVICE CHECK, FOUND EEPLS RED LENS MISSING IN AFT CABIN. INSTALLED LENS PER MM.
Part: FITTING — LOOSE (FWD ENTRY DOOR) · airframe 8,215 hrs · 4,815 cycles
FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTING LOOSE. SECURED FITTING PER MM.
Part: COVER — CRACKED (CABIN) · airframe 6,727 hrs · 3,939 cycles
DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 1. REMOVED AND REPLACED COVER PER MM.
Part: WIRE — EXPOSED (CABIN) · airframe 6,355 hrs · 3,698 cycles
EEPLS WIRES EXPOSED. SECURED WIRES PER MM.
Part: LIGHT — BROKEN (SERVICE DOOR) · airframe 6,067 hrs · 3,546 cycles
AFT SVC DOOR EMERGENCY EXIT LIGHT BRACKET BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
2001
Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,237 hrs · 2,466 cycles
DURING SCHEDULED SERVICE CHECK, FOUND RT EMERGENCY EXIT WINDOW LIGHT INOP AT ROW 11. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM.