N7710A
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES CO | Operator | 2014-12-12 – 2014-12-12 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2014-12-12 – 2014-12-12 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
EXIT SIGN LENS IN FORWARD GALLEY WILL NOT STAY ON PLACE / R/R EXIT SIGN PER AMM 33-51-01
EXIT SIGN LENS IN FORWARD GALLEY WILL NOT STAY ON PLACE R/R EXIT SIGN PER AMM 33-51-01
AFT GALLEY EXIT SIGN INOP. / R&R FUSES AT POWER SUPPLY (M1672) AT STA 952 PER AMM.
FORWARD CARGO COMPARTMENT FLOOR SUPPORT CRACKED BETWEEN BS. 500B TO BS. 500C, STR. 25L. / R&R FLOOR SUPPORT BAFFLE ASSEMBLY IAW DWG.
FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS. 500D, STR. 19L. / R&R GUSSET IAW DWG.
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.
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
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.
AFT CARGO COMPARTMENT RT SIDE Z CHANNEL SUPPORT CORRODED BETWEEN BS 727 TO BS 767, RBL 22. REPAIRED "Z" CHANNEL PER DWG AND SRM.
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.
FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS. 500D, STR. 19R. / R&R GUSSET IAW DWG.
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.)
R/H HORIZONTAL STABILIZER #4 INTERNAL RIB #2 STIFFENER CRACKED LOWER AREA. / REPAIRED #2 STIFFENER PER SRM.
L/H HORIZONTAL STABILIZER STA. 129.50 (RIB 5) STIFFENER #3 COUNTING FROM THE BACK CRACKED. / REPAIRED STIFFENER #3 PER SRM.
L/H HORIZONTAL STABILIZER STA. 120.30 (RIB4) STIFFENER #3 COUNTING FROM THE BACK CRACKED. / REPAIRED STIFFENER #3 PER SRM.
R/H HORIZONTAL STABILIZER #4 INTERNAL RIB #3 STIFFENER CRACKED LOWER AREA. / REPAIRED STIFFENER #3 PER SRM.
L/H HORIZONTAL STABILIZER STA. 120.30 (RIB 4) STIFFENER #4 COUNTING FROM THE BACK CRACKED. / REPAIRED #4 STIFFENER PER SRM.
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.
L/H HORIZONTAL STABILIZER STA. 120.30 (RIB 4) STIFFENER #2 COUNTING FROM THE BACK CRACKED. / REPAIRED STIFFENER #2 PER SRM.
FLIGHT DECK FLOOR DAMAGED AT BS. 260, BETWEEN LBL 20 TO RBL 5. / REPAIRED FLIGHT DECK FLOOR WEB IAW EA.
RT EMERGENCY LIGHT INOP. R&R LIGHT ASSEMBLY IAW AMM.
EMERGENCY EXIT LIGHT BATTERY M1672 FAILED TEST. R&R BATTERY PACK PER MM.
FLAPS FAILED TO RETRACT DURING CLIMB OUT. AIR TURNBACK AND AN EMERGENCY DECLARED. R & R THE RATE FLAP SENSOR IAW MM.
LEFT EMERGENCY EXIT HATCH EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE CHARGER IAW AMM.
LEFT EMERGENCY EXIT HATCH EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.
LEFT WING TRAILING EDGE, JUST INBOARD OF THE PYLON SAIL TAIL, WIGGLE PLATE CRACKED. R & R THE PLATE IAW SRM AND DWG.
RIGHT WING TRAILING EDGE, BELOW THE NR 8 SPOILER, AFT LOWER PANEL SUPPORT CHANNEL CRACKED. R & R THE SUPPORT CHANNEL IAW SRM AND DWG.
RT WING TRAILING EDGE BELOW #8 SPOILER, AFT LOWER PANEL SUPPORT CHANNEL CRACKED. R&R CHANNEL IAW SRM AND DWG.
LT WING TRAILING EDGE JUST INBOARD OF PYLON SAIL TAIL, WIGGLE PLATE CRACKED. R&R WIGGLE PLATE IAW SRM AND DWG.
FRAME WEB CRACKED AT BS 747, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.
RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER AMM.
R2 DOOR SLIDE GIRT BAR OUT OF ADJUST. ADJUSTED THE GIRT BAR IAW MT.
LT LOWER OVERWING EMERGENCY EXIT LIGHT LENS MISMARKED. R&R LENS ASSEMBLY IAW AMM.
R2 DOOR EXTERIOR SLIDE LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.
POSSIBLE FUEL LEAKED DURING CLIMB OUT. R & R THE NR 2 FUELING SHUTOFF VALVE IAW AMM.
RIGHT BULLNOSE EMERGENCY LIGHT INOPERTIVE AT SEAT ROW 11. REPLACED THE LAMP IAW AMM.
AFT CTR AISLE EMER EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.
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.
LT OUTBOARD SEAT TRACK CORRODED BETWEEN BS 727B TO 947, LBL 45. R&R SEAT TRACK IAW SRM.
INTERCOSTAL CORRODED AT BS 910, BETWEEN STRINGER 23L - 24L. R & R INTERCOSTAL IAW SRM & DWG.
AFT CARGO DOOR CUT OUT, FWD LOWER CORNER, SCUFF PLATE CRACKED. R & R SCUFF PLATE IAW SRM.
FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 400, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 440, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 787, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED FRAME IAW EA.
AFT CARGO COMPARTMENT LT FLOOR SIDE PLATE CORRODED, BETWEEN BS 727 TO 847. R & R SIDE PLATE IAW SRM.
AFT CARGO COMPARTMENT, RT FLOOR SIDE PLATE CORRODED, BETWEEN BS 727 - 767. REMOVED PLATE IAW SRM.
AFT CARGO COMPARTMENT DOOR THRESHOLD WEB CORRODED, BETWEEN BS 787 - 847. R & R WEB IAW SRM.
RIGHT SIDE PLATE TOP SURFACE, JUST AFT OF FWD CARGO DOOR CUT OUT CORRODED, AT BS 493. R & R SIDE PLATE IAW SRM.
L2 DOOR EXIT SIGN ASSEMBLY MISSING. R & R LIGHT ASSEMBLY AMM.
HORIZONTAL STIFFENER DAMAGED AT BS 178, BWL 185. R & R STIFFENER IAW EA.
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.
PRESSURE BULKHEAD AT NOSE RADOME SKIN DAMAGED AT BS 178, RBL 10. REPAIRED SKIN IAW EA.
LEFT WING INBD LE HINGE RIB ASSEMBLY DAMAGED. REPAIRED RIB IAW EA.
STIFFENER ON PRESS BULKHEAD WEB LOCATED BEHIND DUAL LOCALIZER ANTENNA DAMAGED. REPAIRED WEB IAW EA.
LEFT WING LE INBD OF NR 1 ENG DAMAGED THRU SKIN. R & R SKIN ER SRM.
FLOORBEAM REPAIR DOUBLER FASTENER MISSING AT BS 344, RBL 2. INSTALLED FASTENER IAW SRM.
L1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW CCN.
R1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW CCN.
L2 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW AMM.
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.
RIGHT WING TE WAFFLE PLATE JUST INBD OF NR 2 PYLON AFT TIP CRACKED. R & R WAFFLE PLATE IAW SRM.
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.
L1 DOOR EMER ESCAPE SLIDE COVER BOTH GIRT BAR RETAINER CLIP ASSEMBLY LOOSE. R & R CLIP ASSEMBLY IAW SRM.
R1 DOOR EMER SLIDE COVER BOTH GIRT BAR RETAINER CLIP ASSEMBLY LOOSE. R & R CLIP ASSEMBLY IAW SRM.
RIGHT WING RSS 78 UPPER TE SUPPORT BEAM FWD ATTACH CLIP CRACKED AT REAR SPAR ATTACH POINT. R & R CLIP IAW SRM.
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.
L1 DOOR EMER ESCAPE SLIDE COVER DAMAGED. REPAIRED COVER IAW CMM.
CENTER WING SECTION FLOORBEAM UPPER CHORD CRACKED AT BS 727B-3, LBL 45.5. REPAIRED CHORD IAW ER & EA.
MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663 LBL 43. REPAIRED WEB IAW SRM.
LEFT WING TE CAVITY WIGGLE PLATE CRACKED LOWER AFT SPAR INBD SIDE OF NR 1 ENG STRUT. R & R WIGGLE PLATE IAW SRM.
LEFT WING TE CAVITY SUPPORT INTERCOSTAL CRACKED OTBD END COMMON TO UPPER TE PANEL ABOVE NR 1 ENG STRUT. R & R INTERCOSTAL IAW SRM.
CENTER WING SECTION FLOORBEAM UPPER CHORD CRACKED AT BS 727B-3, RBL 45.5. REPAIRED CHORD IAW ER & EA.
CENTER WING SECTION FLOORBEAM UPPER CHORD CRACKED AT BS 727B-3, RBL 24.75. REPAIRED CHORD IAW ER & EA.
CENTER WING SECTION FLOORBEAM UPPER CHORD CRACKED AT BS 727B-3, LBL 24.75. REPAIRED CHORD IAW ER & EA.
R2 DOOR EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.
EXTERNAL POWER SERVICE DOOR UPPER HINGE BROKEN. R & R HINGE IAW AMM.
MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, RBL 43. REPAIRED WEB IAW EA.
INTERCOSTAL CORRODED BETWEEN BS 294.5 TO 312 LBL 12. R & R INTERCOSTAL IAW SRM.
FLOORBEAM UPPER SURFACE CORRODED AT BS 294 BETWEEN LBL 2 TO LBL 12. REPAIRED FLOORBEAM IAW SRM.
FUSELAGE SKIN CRACKED AT BS 540, STRINGER 22L FWD & AFT LOCATIONS IN SECOND FASTENER ROW. REPAIRED SKIN IAW ER & EA.
FLOORBEAM UPPER SURFACE CORRODED AT BS 344, RBL 1. REPAIRED FLOORBEAM IAW SRM & EA.
EXTERNAL L2 DOOR EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.
LEFT OVERWING LINER LOWER HANDLE CUT OUT COVER PANEL CRACKED. R & R PANEL IAW AMM.
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.
AFT SERVICE DOORS EMER LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM.
AFT SERVICE DOORS EXTERIOR EMER LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM.
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.