N7710A
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | on 2014-12-12 | Operator named in NTSB report |
Accident & incident history
Operated by Southwest Airlines, Co. (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.
89 reports on file, 2014-06-12 – 2020-03-04.
Part: LENS — LOOSE (EXIT SIGN) · airframe 49,390 hrs · 24,464 cycles
EXIT SIGN LENS IN FORWARD GALLEY WILL NOT STAY ON PLACE R/R EXIT SIGN PER AMM 33-51-01
Part: SIGN — UNSECURE (CABIN) · airframe 493,931 hrs · 24,464 cycles
EXIT SIGN LENS IN FORWARD GALLEY WILL NOT STAY ON PLACE / R/R EXIT SIGN PER AMM 33-51-01
Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,204 hrs · 24,346 cycles
AFT GALLEY EXIT SIGN INOP. / R&R FUSES AT POWER SUPPLY (M1672) AT STA 952 PER AMM.
Part: BAFFLE — CRACKED (BS 500B-500C) · airframe 49,204 hrs · 24,346 cycles
FORWARD CARGO COMPARTMENT FLOOR SUPPORT CRACKED BETWEEN BS. 500B TO BS. 500C, STR. 25L. / R&R FLOOR SUPPORT BAFFLE ASSEMBLY IAW DWG.
Part: GUSSET — CRACKED (BS 500D) · airframe 49,204 hrs · 24,346 cycles
FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS. 500D, STR. 19L. / R&R GUSSET IAW DWG.
Part: CHANNEL — CORRODED (AFT CARGO) · airframe 49,204 hrs · 24,346 cycles
AFT CARGO AREA SURROUND WASTE TANK MAIN DRAIN SHOWS HAVING CORROSION SPOTS INSIDE WEB ENCLOSURE STA 847 TO STA 867 AND LBL 25 APROX. DOT 82-132. AND STRINGERS 25 AND 23 L/H; WL APROX. 165.5 / REMOVED CORRORED INNER CHANNEL AND ASSY PAN FROM AFT CARGO COMP. SURROUND WASTE TANK MAIN DRAIN; PER REF B737 SRM 51-40-020-0G-0; LOCATED AND DRILLED NEW CHANNEL PER REF B737 SRM 51-40-05-0G-0 INSTALLED INNER PAN ASSY WITH NEW CHANNEL PER REF B737 SRM 51-40-02-0G-0_AND DRAWING #146A7402
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 49,204 hrs · 24,346 cycles
AFT CARGO COMPARTMENT RT SIDE Z CHANNEL SUPPORT CORRODED BETWEEN BS 727 TO BS 767, RBL 22. REPAIRED "Z" CHANNEL PER DWG AND SRM.
Part: STRAP — CORRODED (BS 767 FLOORBEAM) · airframe 49,204 hrs · 24,346 cycles
AFT CARGO COMPARTMENT BILGE FLOOR SUPPORT STRAP CORRODED AT BS. 767+5, BETWEEN RBL 11 TO LBL 11. / R&R "TEE" SUPPORT STRAP PER DWG.
Part: FLOOR SUPPORT — CORRODED (BS 755.5-887) · airframe 49,204 hrs · 24,346 cycles
AFT CARGO COMPARTMENT ENTRANCE DOOR ANGLE FLOOR SUPPORT CORDED BETWEEN BS. 755.5 TO BS. 887, RBL 15 AT THE FASTENER HOLES. / R&R FLOOR TRACK PER SRM.
Part: FLOORBEAM — CORRODED (BS 887) · airframe 49,204 hrs · 24,346 cycles
AFT CARGO BILGE AREA STA 887 TOP OF BOTTOM WEB, FLAT SUPPORT FLOOR FITTING CORRODED AT BS. 887, BETWEEN RBL 15 TO LBL 15. / R&R "TEE" SUPPORT STRAP PER DWG.
Part: GUSSET — CRACKED (BS 500D) · airframe 49,204 hrs · 24,346 cycles
FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS. 500D, STR. 19R. / R&R GUSSET IAW DWG.
Part: SUPPORT — CORRODED (BS 500-500D) · airframe 49,204 hrs · 24,346 cycles
CORROSION FWD CARGO COMPARTMENT LT Z ANGLE STA 500 TO STA 500D / REPAIR Z ANGLE (SIDE PANEL SUPPORT) AT FWD CARGO COMPARTMENT BETWEEN FS 480 + 10 TO FS 500D 25L IN REF B737-700 SRM 53-00-53-2R-5 PARAGRAPH 1 TO 4 (A TO O.)
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 49,204 hrs · 24,346 cycles
L/H HORIZONTAL STABILIZER STA. 120.30 (RIB 4) STIFFENER #2 COUNTING FROM THE BACK CRACKED. / REPAIRED STIFFENER #2 PER SRM.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 49,204 hrs · 24,346 cycles
R/H HORIZONTAL STABILIZER #4 INTERNAL RIB #2 STIFFENER CRACKED LOWER AREA. / REPAIRED #2 STIFFENER PER SRM.
Part: WEB — CORRODED (BS 440-492) · airframe 49,204 hrs · 24,346 cycles
FORWARD CARGO DOOR THRESHOLD LOWER WEB CORRODED AROUND NUT PLATE HOLES BETWEEN BS. 440 TO BS. 492, RBL 25. / R&R WEB PER SRM AND DWG.
Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 49,204 hrs · 24,346 cycles
L/H HORIZONTAL STABILIZER STA. 120.30 (RIB 4) STIFFENER #4 COUNTING FROM THE BACK CRACKED. / REPAIRED #4 STIFFENER PER SRM.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 49,204 hrs · 24,346 cycles
L/H HORIZONTAL STABILIZER STA. 129.50 (RIB 5) STIFFENER #3 COUNTING FROM THE BACK CRACKED. / REPAIRED STIFFENER #3 PER SRM.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 49,204 hrs · 24,346 cycles
L/H HORIZONTAL STABILIZER STA. 120.30 (RIB4) STIFFENER #3 COUNTING FROM THE BACK CRACKED. / REPAIRED STIFFENER #3 PER SRM.
Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 49,204 hrs · 24,346 cycles
R/H HORIZONTAL STABILIZER #4 INTERNAL RIB #3 STIFFENER CRACKED LOWER AREA. / REPAIRED STIFFENER #3 PER SRM.
Part: FLOOR SKIN — DAMAGED (BS 260) · airframe 49,204 hrs · 24,346 cycles
FLIGHT DECK FLOOR DAMAGED AT BS. 260, BETWEEN LBL 20 TO RBL 5. / REPAIRED FLIGHT DECK FLOOR WEB IAW EA.
Earlier reports · 2014–2019 · 69 reports
2019
Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,289 hrs · 22,568 cycles
RT EMERGENCY LIGHT INOP. R&R LIGHT ASSEMBLY IAW AMM.
2018
Part: BATTERY — FAILED (CABIN) · airframe 44,111 hrs · 21,222 cycles
EMERGENCY EXIT LIGHT BATTERY M1672 FAILED TEST. R&R BATTERY PACK PER MM.
Part: SENSOR — FAILED (TE FLAPS) · airframe 43,271 hrs · 20,699 cycles
FLAPS FAILED TO RETRACT DURING CLIMB OUT. AIR TURNBACK AND AN EMERGENCY DECLARED. R & R THE RATE FLAP SENSOR IAW MM.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,800 hrs · 20,421 cycles
LEFT EMERGENCY EXIT HATCH EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE CHARGER IAW AMM.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,800 hrs · 20,421 cycles
LEFT EMERGENCY EXIT HATCH EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.
Part: SUPPORT CHANNEL — CRACKED (RT WING) · airframe 42,660 hrs · 20,347 cycles
RT WING TRAILING EDGE BELOW #8 SPOILER, AFT LOWER PANEL SUPPORT CHANNEL CRACKED. R&R CHANNEL IAW SRM AND DWG.
Part: SUPPORT CHANNEL — CRACKED (RT WING) · airframe 42,660 hrs · 20,347 cycles
RIGHT WING TRAILING EDGE, BELOW THE NR 8 SPOILER, AFT LOWER PANEL SUPPORT CHANNEL CRACKED. R & R THE SUPPORT CHANNEL IAW SRM AND DWG.
Part: PLATE — CRACKED (LT WING) · airframe 42,660 hrs · 20,347 cycles
LT WING TRAILING EDGE JUST INBOARD OF PYLON SAIL TAIL, WIGGLE PLATE CRACKED. R&R WIGGLE PLATE IAW SRM AND DWG.
Part: PLATE — CRACKED (LT WING) · airframe 42,660 hrs · 20,347 cycles
LEFT WING TRAILING EDGE, JUST INBOARD OF THE PYLON SAIL TAIL, WIGGLE PLATE CRACKED. R & R THE PLATE IAW SRM AND DWG.
Part: FRAME — CRACKED (FUSELAGE) · airframe 42,605 hrs · 20,316 cycles
FRAME WEB CRACKED AT BS 747, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.
2017
Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,480 hrs · 19,003 cycles
RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER AMM.
Part: GIRT BAR — OUT OF ADJUST (R2 DOOR SLIDE) · airframe 39,854 hrs · 18,643 cycles
R2 DOOR SLIDE GIRT BAR OUT OF ADJUST. ADJUSTED THE GIRT BAR IAW MT.
Part: LENS — MISMARKED (CABIN) · airframe 39,358 hrs · 18,352 cycles
LT LOWER OVERWING EMERGENCY EXIT LIGHT LENS MISMARKED. R&R LENS ASSEMBLY IAW AMM.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,256 hrs · 18,296 cycles
R2 DOOR EXTERIOR SLIDE LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.
2016
Part: SHUTOFF VALVE — LEAKING (RT WING) · airframe 37,822 hrs · 17,488 cycles
POSSIBLE FUEL LEAKED DURING CLIMB OUT. R & R THE NR 2 FUELING SHUTOFF VALVE IAW AMM.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,688 hrs · 17,409 cycles
RIGHT BULLNOSE EMERGENCY LIGHT INOPERTIVE AT SEAT ROW 11. REPLACED THE LAMP IAW AMM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,943 hrs · 16,415 cycles
AFT CTR AISLE EMER EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.
Part: PLATE — CRACKED (FUSELAGE) · airframe 35,943 hrs · 16,415 cycles
FORWARD CARGO COMPARTMENT R/H INSIDE AND AFT OF FORWARD CARGO DOOR CUT-OUT INTERCOSTAL SIDE-PLATE CRACKED BETWEEN BS 492 TO BS 500A. R&R SIDE PLATE IAW DWG & SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,943 hrs · 16,415 cycles
LT OUTBOARD SEAT TRACK CORRODED BETWEEN BS 727B TO 947, LBL 45. R&R SEAT TRACK IAW SRM.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 35,943 hrs · 16,415 cycles
INTERCOSTAL CORRODED AT BS 910, BETWEEN STRINGER 23L - 24L. R & R INTERCOSTAL IAW SRM & DWG.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,943 hrs · 16,415 cycles
FRAME CRACKED AT BS 440, STRINGER 8L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,943 hrs · 16,415 cycles
FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,943 hrs · 16,415 cycles
FRAME CRACKED AT BS 400, STRINGER 8L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,943 hrs · 16,415 cycles
FRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,943 hrs · 16,415 cycles
FRAME CRACKED AT BS 787, STRINGER 8L. REPAIRED FRAME IAW EA.
Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 35,943 hrs · 16,415 cycles
AFT CARGO DOOR CUT OUT, FWD LOWER CORNER, SCUFF PLATE CRACKED. R & R SCUFF PLATE IAW SRM.
Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 35,943 hrs · 16,415 cycles
AFT CARGO COMPARTMENT DOOR THRESHOLD WEB CORRODED, BETWEEN BS 787 - 847. R & R WEB IAW SRM.
Part: PLATE — CORRODED (FUSELAGE) · airframe 35,943 hrs · 16,415 cycles
AFT CARGO COMPARTMENT LT FLOOR SIDE PLATE CORRODED, BETWEEN BS 727 TO 847. R & R SIDE PLATE IAW SRM.
Part: PLATE — CORRODED (FUSELAGE) · airframe 35,943 hrs · 16,415 cycles
AFT CARGO COMPARTMENT, RT FLOOR SIDE PLATE CORRODED, BETWEEN BS 727 - 767. REMOVED PLATE IAW SRM.
Part: PLATE — CORRODED (FUSELAGE) · airframe 35,943 hrs · 16,415 cycles
RIGHT SIDE PLATE TOP SURFACE, JUST AFT OF FWD CARGO DOOR CUT OUT CORRODED, AT BS 493. R & R SIDE PLATE IAW SRM.
2015
Part: SIGN — MISSING (CABIN) · airframe 34,314 hrs · 15,478 cycles
L2 DOOR EXIT SIGN ASSEMBLY MISSING. R & R LIGHT ASSEMBLY AMM.
Part: STIFFENER — DAMAGED (FUSELAGE) · airframe 32,606 hrs · 14,508 cycles
HORIZONTAL STIFFENER DAMAGED AT BS 178, BWL 185. R & R STIFFENER IAW EA.
Part: FRAME — CRACKED (LT WING) · airframe 32,606 hrs · 14,508 cycles
LEFT WING LE INBD OF THE NR 1 ENG LOWER ZEE FRAME CHORD CRACKED UNDER WING LE SKIN AT STATION 156. REPAIRED ZEE CHORD IAW SRM.
2014
Part: RIB — DAMAGED (LT WING) · airframe 32,606 hrs · 14,508 cycles
LEFT WING INBD LE HINGE RIB ASSEMBLY DAMAGED. REPAIRED RIB IAW EA.
Part: STIFFENER — DAMAGED (FUSELAGE) · airframe 32,606 hrs · 14,508 cycles
STIFFENER ON PRESS BULKHEAD WEB LOCATED BEHIND DUAL LOCALIZER ANTENNA DAMAGED. REPAIRED WEB IAW EA.
Part: SKIN — DAMAGED (LT WING) · airframe 32,606 hrs · 14,508 cycles
LEFT WING LE INBD OF NR 1 ENG DAMAGED THRU SKIN. R & R SKIN ER SRM.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 32,606 hrs · 14,508 cycles
PRESSURE BULKHEAD AT NOSE RADOME SKIN DAMAGED AT BS 178, RBL 10. REPAIRED SKIN IAW EA.
Part: FASTENER — MISSING (FUSELAGE) · airframe 32,211 hrs · 14,327 cycles
FLOORBEAM REPAIR DOUBLER FASTENER MISSING AT BS 344, RBL 2. INSTALLED FASTENER IAW SRM.
Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 32,211 hrs · 14,327 cycles
L1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW CCN.
Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 32,211 hrs · 14,327 cycles
R1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW CCN.
Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 32,211 hrs · 14,327 cycles
L2 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW AMM.
Part: RIB — CRACKED (LT HORIZ STAB) · airframe 32,211 hrs · 14,327 cycles
LEFT HORIZONTAL STABILIZER CRACKED RIB VERTICAL STIFFENER AT RIB STATION 92.70, LOWER END OF SECOND VERTICAL STIFFENER FROM FRONT SPAR. REPAIRED RIB IAW SRM.
Part: PLATE — CRACKED (RT WING) · airframe 32,211 hrs · 14,327 cycles
RIGHT WING TE WAFFLE PLATE JUST INBD OF NR 2 PYLON AFT TIP CRACKED. R & R WAFFLE PLATE IAW SRM.
Part: GUSSET — CRACKED (RT WING) · airframe 32,211 hrs · 14,327 cycles
RIGHT WING UPPER TE PANEL LOWER SUPPORT GUSSET CRACKED AT TRANSVERSE WEB LOWER ATTACH POINT ABOVE NR 2 PYLON AFT TIP. R & R GUSSET IAW SRM.
Part: ATTACH FITTING — CRACKED (RT WING) · airframe 32,211 hrs · 14,327 cycles
RIGHT WING RSS 78 UPPER TE SUPPORT BEAM FWD ATTACH CLIP CRACKED AT REAR SPAR ATTACH POINT. R & R CLIP IAW SRM.
Part: RETAINING CLIP — LOOSE (R1 DOOR) · airframe 32,211 hrs · 14,327 cycles
R1 DOOR EMER SLIDE COVER BOTH GIRT BAR RETAINER CLIP ASSEMBLY LOOSE. R & R CLIP ASSEMBLY IAW SRM.
Part: COVER — DAMAGED (L1 DOOR) · airframe 32,211 hrs · 14,327 cycles
L1 DOOR EMER ESCAPE SLIDE COVER DAMAGED. REPAIRED COVER IAW CMM.
Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 32,211 hrs · 14,327 cycles
RIGHT WING TRANSVERSE WEB UPPER ATTACH ANGLE ABOVE NR 2 PYLON AFT TIP CRACKED JUST INBD OF PROGRAM ROLLER SUPPORT ARM ATTACH POINT. R & R ANGLE IAW SRM.
Part: RETAINING CLIP — LOOSE (L1 DOOR) · airframe 32,211 hrs · 14,327 cycles
L1 DOOR EMER ESCAPE SLIDE COVER BOTH GIRT BAR RETAINER CLIP ASSEMBLY LOOSE. R & R CLIP ASSEMBLY IAW SRM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 32,211 hrs · 14,327 cycles
CENTER WING SECTION FLOORBEAM UPPER CHORD CRACKED AT BS 727B-3, RBL 24.75. REPAIRED CHORD IAW ER & EA.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 32,211 hrs · 14,327 cycles
CENTER WING SECTION FLOORBEAM UPPER CHORD CRACKED AT BS 727B-3, LBL 24.75. REPAIRED CHORD IAW ER & EA.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 32,211 hrs · 14,327 cycles
CENTER WING SECTION FLOORBEAM UPPER CHORD CRACKED AT BS 727B-3, RBL 45.5. REPAIRED CHORD IAW ER & EA.
Part: INTERCOSTAL — CRACKED (LT WING) · airframe 32,211 hrs · 14,327 cycles
LEFT WING TE CAVITY SUPPORT INTERCOSTAL CRACKED OTBD END COMMON TO UPPER TE PANEL ABOVE NR 1 ENG STRUT. R & R INTERCOSTAL IAW SRM.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 32,211 hrs · 14,327 cycles
CENTER WING SECTION FLOORBEAM UPPER CHORD CRACKED AT BS 727B-3, LBL 45.5. REPAIRED CHORD IAW ER & EA.
Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 32,211 hrs · 14,327 cycles
MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663 LBL 43. REPAIRED WEB IAW SRM.
Part: PLATE — CRACKED (LT WING) · airframe 32,211 hrs · 14,327 cycles
LEFT WING TE CAVITY WIGGLE PLATE CRACKED LOWER AFT SPAR INBD SIDE OF NR 1 ENG STRUT. R & R WIGGLE PLATE IAW SRM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,211 hrs · 14,327 cycles
R2 DOOR EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.
Part: HINGE — BROKEN (SERVICE DOOR) · airframe 32,211 hrs · 14,327 cycles
EXTERNAL POWER SERVICE DOOR UPPER HINGE BROKEN. R & R HINGE IAW AMM.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,211 hrs · 14,327 cycles
EXTERNAL L2 DOOR EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.
Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 32,211 hrs · 14,327 cycles
MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, RBL 43. REPAIRED WEB IAW EA.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,211 hrs · 14,327 cycles
FLOORBEAM UPPER SURFACE CORRODED AT BS 294 BETWEEN LBL 2 TO LBL 12. REPAIRED FLOORBEAM IAW SRM.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 32,211 hrs · 14,327 cycles
INTERCOSTAL CORRODED BETWEEN BS 294.5 TO 312 LBL 12. R & R INTERCOSTAL IAW SRM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 32,211 hrs · 14,327 cycles
FUSELAGE SKIN CRACKED AT BS 540, STRINGER 22L FWD & AFT LOCATIONS IN SECOND FASTENER ROW. REPAIRED SKIN IAW ER & EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 32,211 hrs · 14,327 cycles
SEAT TRACK CORRODED ON UPPER SURFACE INSIDE CHANNEL AROUND FASTENER HOLES BETWEEN BS 727B TO 727B+5, RBL 45. R & R SEAT TRACK IAW SRM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,211 hrs · 14,327 cycles
FLOORBEAM UPPER SURFACE CORRODED AT BS 344, RBL 1. REPAIRED FLOORBEAM IAW SRM & EA.
Part: PANEL — CRACKED (OVERWING EXIT) · airframe 32,211 hrs · 14,327 cycles
LEFT OVERWING LINER LOWER HANDLE CUT OUT COVER PANEL CRACKED. R & R PANEL IAW AMM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,296 hrs · 14,362 cycles
AFT SERVICE DOORS EMER LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,296 hrs · 14,362 cycles
AFT SERVICE DOORS EXTERIOR EMER LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM.
Part: SPAR — CORRODED (ZONE 500) · airframe 4,040 hrs
TWO AREAS OF CORROSION WAS FOUND ON THE UPPER SURFACE OF ANGLE ATTACHED TO THE LOWER PORTION OF THE LT WING SPAR ASSY, AT WING STATIONS 41.00 & 47.50. AREAS OF CORROSION APPEARED TO HAVE STARTED INSIDE THE MATERIAL OF THE ANGLE WITH NO EXTERNAL INFLUENCE.