N787SA
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.
177 reports on file, 2001-02-26 – 2020-03-11.
Part: SUPPORT BRACKET — CRACKED (LT A/C BAY) · airframe 67,685 hrs · 40,066 cycles
LH AC BAY FWD BULKHEAD AT THE KEEL BEAM HAS A BLEED AIR DUCT SUPPORT BRACKET CRACKED AT MOUNT BOLTS / REMOVED AND REPLACED BLEED AIR DUCT SUPPORT BRACKET AT LH AC BAY FWD BULKHEAD AT THE KEEL BEAM PER AMM 36-13-01.
Part: BATTERY PACK — FAILED (CABIN) · airframe 67,685 hrs · 40,066 cycles
3 EACH CABIN EMERGENCY LIGHTING BATTERY PACKS FAIL CAPACITY TEST. REMOVED AND REPLACED 3 EACH CABIN EMERGENCY LIGHTING BATTERY PACKS AT POSITIONS M1670, M1672, AND M1674 PER AMM 33-51-06 AND ENG DWG 33500005.
Earlier reports · 2001–2019 · 175 reports
2019
Part: COVER — MISSING (R2 DOOR SLIDE) · airframe 66,827 hrs · 39,539 cycles
R2 DOOR ESCAPE SLIDES MISSING COVERS ON INFLATION PULL HANDLES. / REATTACHED COVERS PER MT.
Part: COVER — MISSING (L2 DOOR SLIDE) · airframe 66,827 hrs · 39,539 cycles
L2 DOOR ESCAPE SLIDES MISSING COVERS ON INFLATION PULL HANDLES. / REATTACHED COVERS PER MT.
Part: GIRT BAR — DAMAGED (L2 DOOR) · airframe 66,721 hrs · 39,479 cycles
L2 DOOR AFT SLIDES "Z" FOLDS IN GIRT FLAPS CAME OUT.SECURED "Z" FOLDS PER AMM
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 65,639 hrs · 38,795 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1668. R&R BATTERY PACK PER AMM.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 65,639 hrs · 38,795 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1669. R&R BATTERY PACK PER AMM.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 65,639 hrs · 38,795 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1674. R&R BATTERY PACK PER AMM.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 65,639 hrs · 38,795 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1670. R&R BATTERY PACK PER AMM.
Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 65,633 hrs · 38,791 cycles
EMERGENCY EXIT SIGN MID CABIN AT OVERWING EXIT WAS KNOCKED DOWN. R&R SIGN PER AMM.
Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 65,633 hrs · 38,791 cycles
EMERGENCY EXIT SIGN MID CABIN AT OVERWING EXIT WAS KNOCKED DOWN. FOUND FUSE BLOWN ON BATTERY PACK M1668. R&R BATTERY PACK PER AMM.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,250 hrs · 38,533 cycles
R/H WING AFT EMERGENCY LIGHT INOP. RELAMPED LIGHT IAW AMM.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 65,084 hrs · 38,428 cycles
RIGHT HORIZONTAL STABILIZER LEADING EDGE CRACKED ON RIB AT LEADING EDGE STA. 105.26. / R&R RIB PER SRM.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 65,084 hrs · 38,428 cycles
R/H LEADING EDGE HORIZONTAL STABILIZER RIB AT LEADING EDGE STA. 114.55 CRACKED. R & R RIB PER SRM.
Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 65,084 hrs · 38,428 cycles
R/H HORIZONTAL STABILIZER RIB AT STAB. STA. 120.3 4TH VERTICAL STIFFENER CRACKED. REPAIRED STIFFENER PER SRM.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 65,084 hrs · 38,428 cycles
R/H HORIZONTAL STABILIZER RIB CRACKED AT STA. 120, 3RD VERTICAL STIFFENER. REPAIRED RIB PER SRM.
Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 64,344 hrs · 37,945 cycles
R2 DOOR SLIDE PARTIALLY OUT OF SLIDE PACK COMPARTMENT. REPOSITION SLIDE PER MT.
2018
Part: COVER — LOOSE (R2 DOOR) · airframe 63,559 hrs · 37,438 cycles
R2 DOOR SLIDE COVER LOOSE. SECURED COVER IAW CMM.
Part: SIGN — UNSECURE (CABIN) · airframe 63,538 hrs · 37,420 cycles
L1 DOOR LAV EMERGENCY EXIT SIGN FELL OFF. R&R SIGN PER AMM.
Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 63,269 hrs · 37,254 cycles
FORWARD GALLEY AREA ALL EMERGENCY LIGHTS INOP. RECONNECTED CONNECTOR IAW SWPM & AMM.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 63,269 hrs · 37,254 cycles
UPPER VAPOR BARRIER CHORD CRACKED AT BS 663, LBL 8. REPAIRED CHORD IAW EA.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,269 hrs · 37,254 cycles
R2 CREASE BEAM WEB CORRODED BETWEEN BS 951 TO BS 992, RBL 55. R&R WEB IAW SRM & DWG.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 63,269 hrs · 37,254 cycles
VERTICAL PRESSURE DECK LOWER ATTACH ANGLE WEB CRACKED AT BS 663, RBL 34. REPAIRED ANGLE IAW EA.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,269 hrs · 37,254 cycles
INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 46. R&R INTERCOSTAL IAW SRM AND DWG.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,269 hrs · 37,254 cycles
L1 DOOR CREASE BEAM CHORD CORRODED BETWEEN BS 312 TO BS 340. R&R CREASE BEAM IAW DWG.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,269 hrs · 37,254 cycles
INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, BL 0. R&R INTERCOSTAL IAW DWG AND SRM.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,269 hrs · 37,254 cycles
LT INNER CREASE BEAM CHORD CORRODED BETWEEN BS 947 TO BS 990. R&R CREASE BEAM IAW DWG AND SRM.
Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 63,269 hrs · 37,254 cycles
L1 DOOR CREASE BEAM CHORD CRACKED AT BS 302. R&R CREASE BEAM IAW SRM & DWG.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,269 hrs · 37,254 cycles
INTERCOSTAL CRACKED BETWEEN BS 278 TO BS 294, BL 0. R&R INTERCOSTAL IAW SRM & DWG.
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,269 hrs · 37,254 cycles
R1 DOOR LOWER CUTOUT STUB FRAME CRACKED AT BS 294. R&R STUB FRAME IAW SRM AND DWG.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,269 hrs · 37,254 cycles
RT INNER CREASE BEAM CHORD CORRODED BETWEEN BS 947 TO BS 1006. R&R CREASE BEAM IAW SRM.
Part: CAP — CORRODED (FUSELAGE) · airframe 63,269 hrs · 37,254 cycles
T CAP FRAME CORRODED AT BS 986, RBL 45. REPAIRED T CAP IAW SRM AND EA.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,269 hrs · 37,254 cycles
INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 46. R&R INTERCOSTAL IAW SRM & DWG.
Part: BEAM — CRACKED (R1 DOOR) · airframe 63,269 hrs · 37,254 cycles
R1 DOOR NR 4 LOWER BEAM CRACKED IN THE INSPECTION AREA INBOARD OF MOST INBOARD MOUNT HOLE. R&R NR 4 BEAM IAW EO.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,269 hrs · 37,254 cycles
AFT CARGO COMPARTMENT BULKHEAD SUPPORT CORRODED AT BS 947.5, BETWEEN RBL 20 TO LBL 12. R&R BULKHEAD SUPPORT IAW SRM & DWG.
Part: STIFFENER — CRACKED (LT WING) · airframe 63,269 hrs · 37,254 cycles
LT WING FIXED TRAILING EDGE JUST ABOVE SAIL TAIL, CENTER ANGLE STIFFENER CRACKED. R&R STIFFENER IAW DWG.
Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 63,269 hrs · 37,254 cycles
LT WING FIXED TRAILING EDGE 6 INCHES OUTBOARD OF SAIL TAIL, ATTACH ANGLE COMMON TO DEFLECTOR RIB CRACKED. R&R ANGLE IAW DWG.
Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 63,269 hrs · 37,254 cycles
LT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN LBL 25 TO LBL 45. R&R WEB IAW SRM.
Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 63,269 hrs · 37,254 cycles
RT MAIN WHEEL WELL VAPOR BARRIER WEB CRACKED AT BS 663, RBL 12. REPAIRED WEB IAW SRM.
Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 63,232 hrs · 37,234 cycles
L2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER SIP.
Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 63,221 hrs · 37,228 cycles
L2 DOOR SLIDE PACK OUT OF POSITION. R&R SLIDE PACK PER MM AND MT.
Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 61,782 hrs · 36,302 cycles
LEFT FWD EMERGENCY LIGHT BATTERY PACK FAILED A CAPACITY CHECK. R & R THE BATTERY PACK IAW MM.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 61,782 hrs · 36,302 cycles
RIGHT AFT EMERGENCY LIGHT BATTERY PACK FAILED A CAPACITY CHECK. R & R THE BATTERY PACK IAW MM.
Part: SLIDE — DISLODGED (R2 DOOR) · airframe 61,180 hrs · 35,928 cycles
R2 DOOR SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. INSTALLED THE SLIDE IAW MT.
Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 61,117 hrs · 35,891 cycles
L2 DOOR SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MT.
2017
Part: COVER — LOOSE (L1 DOOR) · airframe 60,617 hrs · 35,569 cycles
L1 DOOR ESCAPE SLIDE COVER LOOSE. SECURED COVER IAW AMM.
Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 60,195 hrs · 35,301 cycles
RIGHT OVERWING DOOR EXIT SIGN BROKEN. R & R THE SIGN MM.
Part: HOOK — OUT OF ADJUST (L1 DOOR GIRT BAR) · airframe 60,067 hrs · 35,226 cycles
L1 DOOR EMERGENCY SLIDE GIRT BAR STOW HOOKS OUT OF ADJUST. ADJUSTED THE STOW HOOKS IAW SIP.
Part: SLIDE — LOOSE (R1 DOOR) · airframe 59,943 hrs · 35,148 cycles
R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.
Part: FITTING — LOOSE (R2 DOOR) · airframe 59,336 hrs · 34,780 cycles
R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FORWARD FLOOR FITTING LOOSE. SECURED FITTING IAW AMM.
Part: FITTING — LOOSE (L1 DOOR) · airframe 59,336 hrs · 34,780 cycles
L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FORWARD FLOOR FITTING LOOSE. SECURED FITTING IAW AMM.
Part: FITTING — LOOSE (L1 DOOR) · airframe 59,336 hrs · 34,780 cycles
L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT FLOOR FITTING LOOSE. SECURED FITTING IAW AMM.
Part: LENS — LOOSE (CABIN) · airframe 58,718 hrs · 34,410 cycles
EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 19 DEF. SECURED LENS PER MM.
Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 57,818 hrs · 33,883 cycles
FLOOR SUPPORT CRACKED AT BS 540, RIGHT OF CENTERLINE CRACKED IN A/C DISTRIBUTION BAY. R & R THE SUPPORT IAW SRM.
2016
Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,801 hrs · 33,261 cycles
R2 DOOR EMERGENCY LIGHT BULB INOP. R&R LIGHT PER AMM.
Part: TEE FITTING — CORRODED (FLOOR PANEL) · airframe 56,801 hrs · 33,261 cycles
FLOOR PANEL TEE ASSEMBLY CORRODED AT BS 887, BETWEEN LBL 20 TO RBL 20. R&R TEE ASSEMBLY PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 56,801 hrs · 33,261 cycles
LT INBOARD LOWER FRAME CRACKED AT BS 727, WL 200. REPAIRED FRAME PER EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 56,801 hrs · 33,261 cycles
RT INBOARD LOWER FRAME CRACKED AT BS 727, WBL 200. REPAIRED FRAME PER EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 56,801 hrs · 33,261 cycles
SKIN CRACKED AT BS 540, BETWEEN STR 22L TO STR 23L. REPAIRED SKIN IAW EA.
Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 56,473 hrs · 33,053 cycles
R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW AMM AND MAINTENANCE.
Part: LIGHT — LOOSE (CABIN) · airframe 56,016 hrs · 32,777 cycles
FORWARD CABIN RT EMERGENCY LIGHT LOOSE. SECURED THE LIGHT IAW SIP.
2015
Part: SIGN — BROKEN (CABIN) · airframe 53,791 hrs · 31,517 cycles
CENTER AISLE EMER EXIT SIGN BROKEN. R & R SIGN IAW AMM.
Part: LENS — LOOSE (CABIN) · airframe 52,760 hrs · 30,906 cycles
RIGHT BULLNOSE EMER LIGHT LENS LOOSE AT ROW 11. REPAIRED LENS IAW AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 51,554 hrs · 30,173 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1670. R & R BATTERY PACK IAW AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 51,554 hrs · 30,173 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1668. R & R BATTERY PACK IAW AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 51,554 hrs · 30,173 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675. R & R BATTERY PACK IAW AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 51,554 hrs · 30,173 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1669. R & R BATTERY PACK IAW AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 51,554 hrs · 30,173 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1674. R & R BATTERY PACK IAW AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 51,554 hrs · 30,173 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R & R BATTERY PACK IAW AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 51,554 hrs · 30,173 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1672. R & R BATTERY PACK IAW AMM.
2014
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 50,209 hrs · 29,399 cycles
FORWARD SEAT TRACK INBD FWD HOLE DAMAGED AT BS 727B, RBL 24.5. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,209 hrs · 29,399 cycles
FORWARD SEAT TRACK OTBD AFT CRACKED AT BS 727B LBL 24.5. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 50,209 hrs · 29,399 cycles
AFT SEAT TRACK OTBD HOLE DAMAGED AT BS 727B, RBL 24.5. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,209 hrs · 29,399 cycles
FORWARD SEAT TRACK INBD FWD HOLE CRACKED AT BS 727B LBL 24.5. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 50,209 hrs · 29,399 cycles
FORWARD SEAT TRACK OTBD FWD HOLE DAMAGED AT BS 727B RBL 24.5. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,209 hrs · 29,399 cycles
FORWARD SEAT TRACK INBD AFT HOLE CRACKED AT BS 727B LBL 24.5. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 50,209 hrs · 29,399 cycles
FORWARD SEAT TRACK INBD FWD HOLE DAMAGED AT BS 727B RBL 45. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 50,209 hrs · 29,399 cycles
AFT SEAT TRACK INBD HOLE DAMAGED AT BS 727B RBL 24.5. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 50,209 hrs · 29,399 cycles
FORWARD SEAT TRACK INBD AFT HOLE DAMAGED AT BS 727B LBL 45. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 50,209 hrs · 29,399 cycles
FORWARD SEAT TRACK OTBD FWD HOLE DAMAGED AT BS 727B LBL 24.5. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,209 hrs · 29,399 cycles
FORWARD SEAT TRACK OTBD AFT HOLE CRACKED AT BS 727B LBL 45. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 50,209 hrs · 29,399 cycles
AFT SEAT TRACK INBD FWD HOLE DAMAGED AT BS 727B LBL 24.5. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 50,209 hrs · 29,399 cycles
FORWARD SEAT TRACK OTBD AFT HOLE DAMAGED AT BS 727B RBL 45. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,209 hrs · 29,399 cycles
FORWARD SEAT TRACK OTBD FWD HOLE CRACKED AT BS 727B LBL 45. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 50,209 hrs · 29,399 cycles
FORWARD SEAT TRACK OTBD FWD HOLE DAMAGED AT BS 727B, RBL 45. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 50,209 hrs · 29,399 cycles
AFT SEAT TRACK OTBD HOLE DAMAGED AT BS 727B LBL 24.5. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,209 hrs · 29,399 cycles
FORWARD SEAT TRACK INBD FWD HOLE CRACKED AT BS 727B LBL 45. REPAIRED SEAT TRACK IAW EA.
Part: SKIN — CRACKED (LE SLAT) · airframe 50,209 hrs · 29,399 cycles
LEFT WING LE NR 3 SLAT NOSE SKIN AT THE ACTUATOR RIB CRACKED AROUND INBD AFT FASTENER. REPAIRED SKIN IAW SRM.
Part: LENS — CRACKED (CABIN) · airframe 50,209 hrs · 29,399 cycles
RIGHT EMER LIGHT LENS CRACKED AT ROW 11. R & R LENS IAW MM.
Part: LENS — CRACKED (CABIN) · airframe 50,209 hrs · 29,399 cycles
RIGHT EMER LIGHT LENS CRACKED BETWEEN ROW 8 & 9. R & R LENS IAW MM.
2013
Part: RIB — CRACKED (RT HORIZ STAB) · airframe 47,456 hrs · 27,812 cycles
RT HORIZONTAL STABILIZER, STABILIZER STATION 92.7, 18" AFT OF FWD SPAR, RIB CRACKED 1" ABOVE LOWER CHORD AT VERTICAL STIFFENER. REPAIRED RIB IAW SRM.
Part: RIB — CRACKED (LT HORIZ STAB) · airframe 47,456 hrs · 27,812 cycles
LT HORIZONTAL STABILIZER, STABILIZER STATION 129.50, 8" AFT OF FWD SPAR, RIB CRACKED 1" ABOVE LOWER CHORD AT VERTICAL STIFFENER. REPAIRED RIB IAW SRM.
Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 47,456 hrs · 27,812 cycles
RT NR 3 WINDOW FRAME, EF POST LOWER 3 FASTENER HOLES CRACKED. REPAIRED FRAME IAW ACO.
Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 47,456 hrs · 27,812 cycles
LT NR 3 WINDOW FRAME EF POST, 2ND & 3RD FASTENER HOLES FROM BOTTOM CRACKED. REPAIRED FRAME IAW ACO.
Part: RIB — CRACKED (RT HORIZ STAB) · airframe 47,456 hrs · 27,812 cycles
RT HORIZONTAL STABILIZER, STATION 147.9, 15" AFT OF FWD SPAR, RIB CRACKED AT LOWER CHORD AT VERTICAL STIFFENER. REPAIRED RIB ASSEMBLY IAW EA.
Part: RIB — CRACKED (RT HORIZ STAB) · airframe 47,456 hrs · 27,812 cycles
RT HORIZONTAL STABILIZER STATION 92.7, 27" AFT OF FWD SPAR, RIB CRACKED 1" ABOVE LOWER CHORD AT VERTICAL STIFFENER. REPAIRED RIB ASSEMBLY IAW SRM.
Part: RIB — CRACKED (RT HORIZ STAB) · airframe 47,456 hrs · 27,812 cycles
RT HORIZONTAL STABILIZER STATION 92.7, 9" AFT OF FWD SPAR, RIB CRACKED 1" ABOVE LOWER CHORD AT VERTICAL STIFFENER. REPAIRED RIB ASSEMBLY IAW SRM.
Part: RIB — CRACKED (RT HORIZ STAB) · airframe 47,456 hrs · 27,812 cycles
RT HORIZONTAL STABILIZER, STATION 147.9, 23" AFT OF FWD SPAR, RIB CRACKED AT LOWER CHORD AT VERTICAL STIFFENER. REPAIRED RIB ASSEMBLY IAW EA.
Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 47,456 hrs · 27,812 cycles
FLIGHT DECK RT NR 1 WINDOW FRAME CRACKED IN UPPER OTBD CORNER. REPAIRED FRAME IAW EA.
Part: LIGHT — MISSING (CABIN) · airframe 46,248 hrs · 27,070 cycles
RT FWD EEPLS MISSING. INSTALLED EEPLS STRIP IAW AMM.
Part: SIGN — BROKEN (CABIN) · airframe 45,765 hrs · 26,785 cycles
MID CABIN OVERHEAD EMERGENCY EXIT SIGN BROKEN. R&R SIGN PER SIP & AMM.
Part: RETAINER — CRACKED (LT WING) · airframe 45,056 hrs · 26,331 cycles
LEFT WING I/B TRAILING EDGE FLAP O/B UPPER FIXED PANEL VERTICAL SUPPORT SEAL RETAINER CRACKED. REMOVED AND REPLACED RETAINER PER SRM.
2012
Part: FUSE — BLOWN (CABIN) · airframe 43,475 hrs · 25,330 cycles
RIGHT EMERGENCY EXIT DOOR LOWER FORWARD LIGHT INOP. REMOVED & REPLACED FUSE IAW AMM.
Part: PLATE — PUNCTURED (COCKPIT) · airframe 43,475 hrs · 25,330 cycles
FLIGHT DECK FLOOR AFT OF PEDESTAL PUNCTURED AT BS 255.5, RBL 3.5. REPAIRED PLATE IAW SRM.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 43,475 hrs · 25,330 cycles
FORWARD CARGO COMPARTMENT AFT ANGLE CRACKED AT BS 500C, STR 25R. REMOVED AND REPLACED ANGLE IAW SRM & DWG.
Part: RIB — CRACKED (LT HORIZ STAB) · airframe 43,475 hrs · 25,330 cycles
LEFT HORIZONTAL STAB INSPAR RIB STAB STA 138.70 CRACKED FORWARD LOWER OUTBOARD SIDE. REPAIRED RIB IAW EA.
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 43,475 hrs · 25,330 cycles
R1 DOOR LOWER STUB FRAME CRACKED AT BS 294. REPAIRED FRAME IAW SRM.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 44,775 hrs · 26,150 cycles
LEFT RAM AIR TRANSITION DUCT FWD I/B VERTICAL ANGLE, BS 540, LBL 43, AS VIEWED FROM INSIDE DUCT IS CRACKED. REMOVED AND REPLACED ANGLE PER SRM.
Part: ANGLE — CRACKED (LT MLG WW) · airframe 43,475 hrs · 25,330 cycles
LEFT MAIN WHEEL WELL BAY LOWER BULKHEAD VERTICAL STIFFENER ANGLE CRACKED AT BS 663, LBL 28. REMOVED AND REPLACED ANGLE IAW SRM & DWG.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,475 hrs · 25,330 cycles
FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,475 hrs · 25,330 cycles
FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME IAW EA.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 43,475 hrs · 25,330 cycles
FORWARD CARGO ANGLE CRACKED AT BS 500C, STR 25R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,475 hrs · 25,330 cycles
FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,475 hrs · 25,330 cycles
FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,475 hrs · 25,330 cycles
FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME IAW EA AND DWG.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,475 hrs · 25,330 cycles
FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME IAW EA.
Part: GUSSET — CRACKED (FUSELAGE) · airframe 43,475 hrs · 25,330 cycles
SHEAR TIE ANGLE GUSSET CRACKED AT BS 500D, STR 18L. REMOVED AND REPLACED GUSSET IAW SRM AND DWG.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,475 hrs · 25,330 cycles
FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME AT IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,475 hrs · 25,330 cycles
FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME IAW SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,475 hrs · 25,330 cycles
FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,475 hrs · 25,330 cycles
FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME IAW SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,475 hrs · 25,330 cycles
STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.
Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 43,475 hrs · 25,330 cycles
KEEL BEAM CRACKED AT BS 663, LBL 15. REMOVED AND REPLACED BEAM IAW SRM AND DWG.
Part: BRACKET — CRACKED (FUSELAGE) · airframe 43,475 hrs · 25,330 cycles
KEEL BEAM AFT SECTION BRACKET CRACKED AT BS 663, LBL 28. REMOVED AND REPLACED BRACKET IAW SRM AND DWG.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,475 hrs · 25,330 cycles
CREASE BEAM INNER CORD CORRODED AT BS 328, RBL 62. REMOVED AND REPLACED BEAM IAW SRM AND DWG.
Part: SKATE ANGLE — CHAFED (FUSELAGE) · airframe 43,475 hrs · 25,330 cycles
RIGHT OF FUSELAGE BELOW VERTICAL STABILIZER SKATE ANGLE CHAFED AT STA 1016. REMOVED AND REPLACED SKATE ANGLE IAW SRM AND DWG.
Part: SKATE ANGLE — CHAFED (FUSELAGE) · airframe 43,475 hrs · 25,330 cycles
LEFT OF FUSELAGE BELOW VERTICAL STABILIZER SKATE ANGLE CHAFED. REMOVED AND REPLACED SKATE ANGLE IAW SRM AND DWG.
Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,475 hrs · 25,330 cycles
LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN IAW SRM.
Part: SKIN — DELAMINATED (TE FLAP) · airframe 43,475 hrs · 25,330 cycles
LEFT WING O\B AFT FLAP LOWER SURFACE I\B AFT CORNER OF FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP IAW AMM.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,475 hrs · 25,330 cycles
RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 157.10. REPAIRED SKIN IAW SRM.
Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,475 hrs · 25,330 cycles
LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 147.9, 17. REPAIRED SKIN IAW SRM.
Part: COVER — OUT OF POSITION (CABIN) · airframe 43,376 hrs · 25,266 cycles
L1 DOOR EMERGENCY EXIT LIGHT COVER CAME OFF. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 43,054 hrs · 25,072 cycles
L1 WINDOW FRAME CRACKED. REMOVED AND REPLACED FRAME PER BOEING DWG AND SRM.
Part: BATTERY — FAILED (CABIN) · airframe 41,288 hrs · 24,025 cycles
DURING SCHEDULED HC2 CHECK, RT AFT EMERGENCY EXIT LIGHT FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER MM.
2011
Part: SKIN — CRACKED (HORIZ STAB) · airframe 38,969 hrs · 22,663 cycles
DURING SCHEDULED HC1 CHECK FOUND, LT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.
Part: LENS — BROKEN (CABIN) · airframe 37,678 hrs · 21,913 cycles
R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
2010
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 37,036 hrs · 21,550 cycles
DURING SCHEDULED 10Y CHECK, FOUND INTERCOSTAL CORRODED AT BS 270, BETWEEN LBL 10 TO RBL 10. REPAIRED INTERCOSTAL PER EA.
Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,978 hrs · 21,518 cycles
DURING SCHEDULED 10Y CHECK, FOUND STIFFENER CRACKED AT BS 548, RBL 7. REMOVED AND REPLACED STIFFENER PER SRM.
Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,978 hrs · 21,518 cycles
DURING SCHEDULED 10Y CHECK, FOUND STIFFENER CRACKED AT BS 548, LBL 32. REMOVED AND REPLACED STIFFENER PER SRM.
Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,978 hrs · 21,518 cycles
DURING SCHEDULED 10Y CHECK, FOUND STIFFENER CRACKED AT BS 548, LBL 55. REMOVED AND REPLACED STIFFENER PER SRM.
Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,978 hrs · 21,518 cycles
DURING SCHEDULED 10Y CHECK, FOUND STIFFENER CRACKED AT BS 548, LBL 15. REMOVED AND REPLACED STIFFENER PER SRM.
Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,978 hrs · 21,518 cycles
DURING SCHEDULED 10Y CHECK, FOUND STIFFENER CRACKED AT BS 548, RBL 55. REMOVED AND REPLACED STIFFENER PER SRM.
Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,978 hrs · 21,518 cycles
DURING SCHEDULED 10Y CHECK, FOUND STIFFENER CRACKED AT BS 548, LBL 7. REMOVED AND REPLACED STIFFENER PER SRM.
Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,978 hrs · 21,518 cycles
DURING SCHEDULED 10Y CHECK, FOUND STIFFENER CRACKED AT BS 548, RBL 42. REMOVED AND REPLACED STIFFENER PER SRM.
Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,978 hrs · 21,518 cycles
DURING SCHEDULED 10Y CHECK, FOUND STIFFENER CRACKED AT BS 548, RBL 32. REMOVED AND REPLACED STIFFENER PER SRM.
Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 36,978 hrs · 21,518 cycles
DURING SCHEDULED 10Y CHECK, FOUND STIFFENER CRACKED AT BS 548, RBL 15. REMOVED AND REPLACED STIFFENER PER SRM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 36,809 hrs · 21,417 cycles
DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT LIGHT FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,348 hrs · 20,526 cycles
DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.
Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,348 hrs · 20,526 cycles
DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.
Part: BATTERY PACK — FAILED (CABIN) · airframe 34,521 hrs · 20,035 cycles
DURING SCHEDULED HC1 CHECK, LT EMERGENCY EXIT LIGHT FAILED CAPACITY CHECK AT ROW 16. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,375 hrs · 19,941 cycles
DURING SCHEDULED MV2 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 13. RELAMPED PER MM.
2009
Part: LENS — MISSING (CABIN) · airframe 32,373 hrs · 18,708 cycles
RT OVERWING LOWER EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LENS ASSY PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,907 hrs · 18,438 cycles
DURING SCHEDULED MV1 CHECK, FOUND FWD EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.
2008
Part: SKIN — CRACKED (HORIZ STAB) · airframe 30,512 hrs · 17,596 cycles
DURING SCHEDULED 8Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT BS 142. REPAIRED SKIN PER SWA EA.
Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 28,506 hrs · 16,342 cycles
L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
Part: LENS — LOOSE (CABIN) · airframe 27,684 hrs · 15,840 cycles
DURING SCHEDULED HC2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM.
2007
Part: LENS — LOOSE (CABIN) · airframe 24,837 hrs · 14,134 cycles
EEPLS LENS LOOSE AT ROW 3 ABC. REMOVED AND REPLACED LENS PER MM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 25,736 hrs · 14,657 cycles
DURING SCHEDULED MV2 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,487 hrs · 14,524 cycles
DURING SCHEDULED MV2 CHECK, FOUND LEFT MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
2006
Part: CHARGER — FAILED (CABIN) · airframe 21,199 hrs · 12,010 cycles
DURING SCHEDULED MV1 CHECK, EMERGENCY EXIT LIGHT BATTERY CHARGER FAILED AT BS 952, RBL 14. REMOVED AND REPLACED BATTERY CHARGER PER MM.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,991 hrs · 11,885 cycles
DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY EXIT BULL NOSE LIGHT INOP AT ROW 9L AND ROW 11L. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 20,991 hrs · 11,885 cycles
DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT BATTERY PACK DISCHARGED. REMOVED AND REPLACED BATTERY PACK PER MM.
2005
Part: SLIDE — LOW (L2 DOOR) · airframe 19,052 hrs · 10,786 cycles
L2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATED OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.
2004
Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 15,505 hrs · 8,776 cycles
DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,077 hrs · 8,527 cycles
THREE EACH FWD CABIN EEPLS INOP. REMOVED AND REPLACED BATTERY PER MM.
Part: LENS — LOOSE (EMERGNECY LIGHT) · airframe 14,847 hrs · 8,369 cycles
AFT SERVICE DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,144 hrs · 7,980 cycles
DURING SCHEDULED MV1 CHECK, FOUND AFT EEPLS AND AFT OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM.
2003
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 11,769 hrs · 6,721 cycles
FWD SECTION OF EEPLS AT ROWS 1 AND 2 INOP. REPLACED EEPLS BATTERY PACK PER MM.
Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 11,695 hrs · 6,680 cycles
DURING SCHEDULED C2 CHECK, FOUND L2 DOOR SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE PER MM.
Part: CLIP — LOOSE (FWD ENTRY DOOR) · airframe 10,484 hrs · 5,996 cycles
DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT RETAINER CLIP LOOSE. SECURED RETAINER CLIP PER MM.
Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 9,316 hrs · 5,354 cycles
DURING SCHEDULED C4 CHECK, FOUND NUMEROUS EEPLS COVERS CRACKED BETWEEN ROW NR 2 & ROW NR 23. REMOVED AND REPLACED COVERS PER MM.
2002
Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 8,084 hrs · 4,687 cycles
DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.
Part: ENGINE — OVERTEMP (RT WING) · airframe 6,336 hrs · 3,687 cycles
AIR TURN BACK, NR 2 ENG EGT IND OVERTEMP, (965 DEGREES FOR 1 SECOND). COMPLIED WITH ENG BOROSCOPE INSPECTION AND PWR ASSURANCE RUN. NO DAMAGE NOTED. OPS CK GOOD PER MM. MAINTENANCE FERRY TO PHX AND REMOVED AND REPLACED NR 2 ENG PER MM.
2001
Part: COMPRESSOR — DAMAGED (NR 1 ENGINE) · airframe 3,495 hrs · 2,069 cycles
AIR TURNBACK, VIBRATION STARTED ON NR 1 ENGINE CLIMBING THROUGH 16,000 FEET, FOLLOWED BY AN ELECTRICAL ODOR. FOUND FWD FAN BLADE PLATFORM BROKEN BETWEEN FAN BLADES NR 19 & 20. REMOVED AND REPLACED ENGINE PER MM.
Part: COVER — BROKEN (CABIN) · airframe 2,156 hrs · 1,276 cycles
DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER BROKEN AT OVERWING EXIT. Removed and replaced EEPLS COVER PER MM.
Part: BUSHING — WORN (ELEVATOR TAB) · airframe 1,959 hrs · 1,155 cycles
DURING SCHEDULED SERVICE CHECK, SWA SI 11052-55, FOUND LT ELEVATOR, NR 2 & 3 TAB HINGE BUSHINGS WORN. REMOVED AND REPLACED BUSHINGS PER MM.
Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 1,091 hrs · 688 cycles
FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM.