N718SW
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES CO | Operator | 2016-01-28 – 2016-01-28 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2016-01-28 – 2016-01-28 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
SUPPLEMENTAL INFORMATION: RH WING #6 SLAT I/B AUX TRACK COVER TAB ANGLE BRACKET ON THE SLAT IS CRACKED ; / [01] REMOVED AND REPLACED RH WING #6 SLAT I/B AUX TRACK COVER TAB ANGLE SUPPORT BRACKET PER CMM 57-43-03.
SUPPLEMENTAL INFORMATION: RH WING #6 SLAT O/B AUX TRACK COVER TAB ANGLE BRACKET ON THE SLAT IS CRACKED ; / [01] REMOVED/REPLACED #6 O/B AUX TRACK COVER TAB ANGLE BRACKET REF AMM 20-50-11.; [02] VERIFIED
L1 DOOR EMERGENCY AREA LIGHT INOP ; / [01] RELAMPED IAW AMM 33-51-04 OPS CHECK GOOD
EMERGENCY LIGHT PACK OVER RT OVERWING EXIT FAILED CAPACITY CHECK ; / REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.; INSPECTED IAW AMM
LEFT STABILIZER TO BODY LOWER FRONT SLIDING SEAL IS DAMAGED. ; / R&R L/H LOWER SLIDING SEAL PER AMM 53-31-31; R&R L/H LOWER SLIDING SEAL PER AMM 53-31-31
RT WING PANEL 651FW FWD SUPPORT ROD BRACKET CRACKED / REMOVED AND REPLACED RH WING BRACKET PN #115A2162-16 IAW SRM 51-10-02; 51-40-02
INOPERABLE BULLNOSE EMERGENCY LIGHT 20ABC. RE-LAMPED EMERGENCY AREA LIGHT AT 20 ABC, PER AMM 33-51-03.
EMERGENCY LIGHT ABOVE 20 ABC IS INOPERABLE. RE-LAMPED EMERGENCY LIGHT ABOVE 20 ABC, PER AMM 33-51-03.
EMERGENCY LITES @ ROW 16 & 19 RIGHT & AFT GALLEY INOP / REMOVED &N REPLACED BATTERY PACK IN AFT OVERHEAD GALLEY IAW AMM 33-51-06
LH UPPER HORIZONTAL STAB AFT BLADE SEAL RETAINER IS DAMAGED / REMOVED DAMAGED LH UPPER HSTAB AFT BLADE SEAL RETAINER APPLIED TOPCOAT TO NEW PART AND INSTALLED SEAL RETAINER IAW SRM 51-40-02-0G-0 SECTION 9 AND AMM 51-21-73-370-801. ATAG: U10971
EMERGENCY EXIT LIGHT BATTERY PACK M1670 FAILED BATTERY PACK CAPACITY CHECK. / R&R BATTERY PACK M1670 IAW AMM.
LEFT MLG WHEEL WELL STA 663 LBL28 WL 148; VERTICAL STIFFENER IS CRACKED. / REMOVED AND REPLACE LH MLG WHEEL WELL STA 663 LBL 28 WL 148 VERTICAL STIFFENER IAW SRM 51-40-02-0G-0 & 51-40-05-0G-0 & DWG 111A100 REV -
AFT CARGO COMPARTMENT; STA 727A + 14 TO 727B LBL3 WL160; INTERCOSTAL HAS CORROSION ON RH SIDE. / BLENDED CORROSION ON INTERCOSTAL IN AFT CARGO COMPARTMENT STA 727A TO 727B LBL 3 WL 160. OUT OF LIMITS REPLACED INTERCOSTAL IAW BOEING DWG# 146A7500 AND 737 SRM 51-40-02-0G-0. FOUND ORIG T .040' LOSS .021' REMIANING .019' OUT OF LIMITS IAW SRM 53-00-53-1A-2
LEFT WHEEL WELL UPPER ATTACH ANGLE CRACKED AT BS. 663, BETWEEN LBL 44 TO LBL 45. / REPAIRED ANGLE IAW SRM & AMM.
AFT CARGO COMPARTMENT FLOOR STRUCTURE, R/H FACE OF INTERCOSTAL AFT CORRODED AT BS. 847, RBL 6. / R&R INTERCOSTAL IAW SRM, AMM, & DWG.
INSIDE VERTICAL STABILIZER LATERAL SUPPORT ANGLE CRACKED IN RADIUS AT BS. 1016, LBL 12, 8" ABOVE FUSELAGE SKIN / R&R ANGLE IAW DWG AND SRM.
PASSENGER CABIN FLOORBOARD 241DF HAS UPPER PLY DAMAGE. REPAIRED DAMAGE ON FLOOR PANEL 241DF. BONDED REPAIR PLIES AND CURED. TAP TEST GOOD. IAW B737-700 SRM 53-00-50-2R-1 REV 69; SRM 53-00-50-2R-0 REPAIR GENERAL REV 69.
PASSENGER CABIN FLOORBOARD 231ZF HAS UPPER PLY DAMAGE / REPAIRED FRAYING/EXPOSED COMPOSITE AT UPPER SURFACE FACESHEET ON FLOORBOARD 231ZF IAW B737 SRM 53-00-50-2R-1; PAR 3 (A;C;E+F; K1;L1;M1) + SRM 53-00-50-2R-0; PAR 5 - REV 69.
DOT #2; RH HOZ STAB; PANEL 343AB; SLIDING SEAL KNIFED EDGED. / REMOVED AND REPLACED SLIDING SEAL KNIFED EDGED IAW SRM 51-40-02-0G-0 SECTION 4; AMM 51-21-41-370-802 AND 51-21-72-370-801. ATAG: WN2574
DOT #004; LH HOZ STAB; PANEL 333AB; SLIDING SEAL KNIFED EDGED. / REMOVED AND REPLACED L/H HORZ STAB PANEL 333AB SLIDING SEAL IAW B737-700 SRM 51-40-02-0G-0 STEP 4 PAGE 2 WN6447
AFT PIT Z-ANGLE RH SIDE SUPPORT WEB HAS EVIDENCE OF CORROSION FROM STA 747 TO STA 767 RBL 21 AND W/L 158 / REMOVED CORROSION ON Z-ANGLE SUPPORT WEB FROM STA 747 - 767. NO PUBLISHED LIMITS FOUND. OUT OF LIMITS. REMOVED SUPPORT WEB AND DRILLED UP NEW SUPPORT WEB P/N 146A1500-8. INSTALLED SUPPORT WEB IAW SRM 51-40-02-0G-0. REFERENCE USED 51-40-05-0G-0 AND 53-00-53-1A-2 AND DWG 146A7502 REV A (STAT 747 TO 767 RBL 21' AND W/L 158) P/N 146A7505-8 ATAG WN9928
AFT PIT Z-ANGLE L/H SIDE HAD SPOTS OF CORROSION BETWEEN BS. 727E TO BS. 767+8, LBL 24. / R&R Z-ANGLE IAW SRM.
AFT CARGO COMPARTMENT FLOOR TRANSITION STRIP AT STA 887 RBL 20-LBL 15 W/L 157 IS CORRODED / REMOVED AND INSTALLED NEW STRIP ON AFT CARGO COMPARTMENT FLOOR TRANSITION STA 887 RBL 20 LBL 15 W/L 157. SRM 51-40-02-0G-0 & DRAWING #146A9401 REV C.
AFT CARGO COMPARTMENT R/H RAIL CORRODED BETWEEN BS. 767+10 TO BS. 887, RBL 15. / R&R TRACK SECTION IAW SRM.
EXTERNAL FUSELAGE; RH SIDE. STA 1156; LOWER AFT SLIDING SEAL RETAINER HAS CHAFING DAMAGE. / INSPECTED PANEL ASSY AND FOUND NO STRUCTURAL WEAK LIMITS PUBLISHED REMOVED AND REPLACED R/H STA 1156 LOWER AFT SLIDING SEAL RETAINER IAW SRM 51-40-02 AND DWG 181A8050 REV-
LEFT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL IN FUSELAGE IS CRACKED ABOVE AFT CLEVIS / REMOVED AND REPLACED LEFT HORIZONTIAL STAB FWD UPPER SLIDING SEAL IAW B737 AMM 53-31-31.
AFT PIT Z-ANGLE LH SIDE HAS SPOTS OF CORROSION FROM STA 727C TO 727E WL 156 LBL24 REMOVED CORROSION ON L.H ZANGLE PN 146A75021 STA 727C-727E FOUND ORIG T .040' WITH .015' LOSS .025' REMAINING. OUT OF LIMITS IAW SRM 5300531A1. REPAIRED Z ANGLE ON NRC Y164910
AFT PIT LH ZANGLE HAS SPOTS OF CORROSION FROM STA 767+8' TO STA 827 WL 156 LBL 24 REMOVED CORROSION ON LH ZANGLE PN 146A75021 STA 767+8' TO STA 827. FOUND ORIG T .040' LOSS .020' REMAINING .020' OUT OF LIMITS IAW SRM 5300531A1 REPAIRED Z ANGLE ON NRC Y164910
AFT PIT Z-ANGLE R/H SIDE HAD SPOTS OF CORROSION BETWEEN BS. 747 TO BS. 767, RBL 21. / R&R Z-ANGLE IAW SRM.
CABIN FLOOR STRUCTURE; PANEL BREAK CRACKED AT FASTENER STA 540 LBL 1 WL 208 / REPLACED CABIN FLOOR STRUCTURE PANEL BREAK IAW SRM 51-40-02 AND BOEING DWG 143A5240 REV- STA 540 LBL 1. 'A' TAG WN6323
LT WING REAR SPAR LOWER CHORD 10" INBOARD OF #3 FLAP TRACK WIGGLE PLATE HAD EVIDENCE OF A CRACK AT FASTENER HOLE. R&R WIGGLE PLATE IAW SRM.
L1 DOOR HANDLE; CAM PLATE IS DAMAGED. / REMOVED AND REPLACED WITH A NEW L1 DOOR HANDLE CAM PLATE I/A/W CMM 52-16-01.
LT WING TRAILING EDGE PANEL 551GB WIGGLE PLATE CRACKED. R&R WIGGLE PLATE IAW SRM & DWG.
R1 DOOR SLIDE PULL HANDLE YELLOW COVER WAS NOT SHOWING/ PULLED COVER DOWN AND SECURED TO VELCRO IAW SIP.
AFT GALLEY AREA L/H AND R/H EGRESS STRIPS DELAMINATED. R&R EGRESS STRIPS PER DRAWING.
AFT OF R/H WING EMERGENCY LIGHT INOP. R&R LIGHT PER AMM.
DECLARED EMERGENCY, ON TAKEOFF OUT OF SMF LEADING EDGE FLAP TRANSMIT LIGHT ILLUMINATED. RAN QRH. LIGHT EXTINGUISHED. ON APPROACH TO LAX. PUT FLAP LEVER TO POSITION I, NO MOVEMENT ON FLAP GAUGE OR LE DEVICES PANEL. FLAP GAUGE NEEDLES HAD A SMALL SPLIT. RAN QRH FOR TRAILING EDGE FLAPS UP LANDING WITH FLAP ASYMMETRY LANDING UNEVENTFUL. R&R NR 1 FLAP SKEW DETECTION SENSOR PER MM.
FORWARD LAV SMOKE ALARM WENT OFF IN FLIGHT. R&R SMOKE DETECTOR PER AMM.
LT EMERGENCY LIGHT INOP AT ROW 1. RELAMPED LIGHT IAW AMM.
R2 WINDOW ARCED. R&R WINDOW PER MT.
R2 WINDOW ARCED. R&R R2 WINDOW HEAT CONTROLLER PER MM.
R2 DOOR SLIDE GIRT BAR RETAINING HOOK LOOSE. R & R THE GIRT BAR IAW SRM.
RT OVERWING EMERGENCY EXIT HATCH LIGHT COVER BROKEN. R&R LIGHT PER AMM.
RIGHT EMERGENCY EXIT DOOR, CLOSING STRAP HANDLE COVER LOOSE. SECURED THE HOOK AND LOOP IAW SIP.
R2 DOOR EMERGENCY EVAC SLIDE EMERGENCY LIGHT INOP. RELAMPED LIGHT IAW AMM.
AFT FUSELAGE DRAIN CRACKED AT BS 1016. R&R DRAIN IAW SRM AND DWG.
EMERGENCY EXIT BATTERY DID NOT PASS CAPACITY CHECK AT BS 603, LBL 67. R&R BATTERY PACK IAW AMM.
EMERGENCY BATTERY PACK DID NOT PASS CAPACITY CHECK AT BS 603, RBL 67. R&R BATTERY PACK IAW AMM.
LOWER FUSELAGE ATTACH ANGLE CRACKED BETWEEN BS 653 TO 663, LBL 27.5. R & R THE ATTACH ANGLE IAW SRM AND DWG.
G4 GALLEY EMERGENCY EXIT LIGHT CONNECTORS MISSING. R&R CONNECTORS IAW SWPM AND AMM.
FUSELAGE FRAME CRACKED AT BS 312, BETWEEN STRINGERS 5L TO 6L. REPAIRED THE FRAME IAW EA.
LEFT HORIZONTAL STABILIZER LEADING EDGE RIB FLANGE CRACKED AT HSS 78.29. R & R THE RIB IAW SRM AND DWG.
COCKPIT ENTRY FLOORBEAM ANGLE CORRODED AT BS 270, LBL 9 TO RBL 9. R & R THE FLOORBEAM ANGLE IAW SRM AND EA.
BULKHEAD TO TOP SKIN PANEL CRACKED AT BS 663, LBL 35. REPAIRED ANGLE IAW EA.
RT WING INBOARD OF INBOARD DEFLECTOR RIB, UPPER FIXED PANEL CENTER CURVED STIFFENER ANGLE RIB CRACKED. R&R ANGLE IAW SRM AND DWG.
VERTICAL STABILIZER PANEL 324AR METAL CHANNEL CRACKED. R&R CHANNEL IAW SRM AND DWG.
RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB FLANGE CRACKED AT HSS 105.26. R & R THE RIB IAW SRM AND DWG.
RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB FLANGE CRACKED AT HSS 95.96. R & R THE RIB ASSEMBLY IAW SRM AND DWG.
RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB FLANGE CRACKED AT HSS 151.75. R & R THE RIB IAW SRM AND DWG.
RT HORIZONTAL STABILIZER LEADING EDGE RIB FLANGE CRACKED AT STA 142.45. R&R RIB ASSEMBLY IAW SRM AND DWG.
FORWARD CARGO PIT FORWARD GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET IAW SRM AND DWG.
RT AIR CONDITION BAY BULKHEAD ''L'' ANGLE CRACKED AT BS 663. REPAIRED "L" ANGLE IAW EA..
RT L ANGLE STIFFENER CRACKED AT BS 663. R&R STIFFENER IAW SRM & DWG.
RT WHEEL WELL U SHAPED STIFFENER CRACKED AT BS 663, RBL 15. R&R STIFFENER IAW SRM AND DWG.
RT WING LOWER TRAILING EDGE WAFFLE PLATE CRACKED AT STA ORSS 261. R&R PLATE IAW SRM AND DWG.
EXTERNAL FUSELAGE FAIRING ATTACH STRUCTURE FRAME CRACKED AT BS 500D, BETWEEN STR 18L TO STR 19L. R&R FRAME IAW SRM AND DWG.
FORWARD CARGO PIT FORWARD CORNER SCUFF PLATE CRACKED. R&R SCUFF PLATE IAW SRM AND EA.
HORIZONTAL PRESSURE DECK CRACKED AT BS 663+2, BETWEEN LBL 32 TO LBL 34. R&R WEB IAW EA.
FORWARD CARGO BAY AFT CORNER SCUFF PLATE CRACKED. REPAIRED THE SCUFF PLATE IAW EA.
BS 663 BULKHEAD LEADING EDGE STIFFENER CRACKED, RBL 50. REPAIRED THE BULKHEAD IAW EA.
RT WING NR 5 SLAT NOSE SKIN CRACKED AT STA 85.19 AT OUTBOARD LOWER FASTENER HOLE. REPAIRED SKIN IAW SRM.
R2 DOOR EMERGENCY EXIT SIGN LENS COVER LOOSE. R&R SIGN ASSEMBLY IAW AMM.
R1 DOOR EMERGENCY EVAC SLIDE AFT LANYARD CLIP LADDER TIE MISSING. INSTALLED LADDER TIE PER SIP.
LT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING CORRODED. REPAIRED FITTING PER EA.
RT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING CORRODED. REPAIRED FITTING PER EA.
CABIN PRESSURE FAILED AT TOD, THROTTLES RETARDED AND CABIN PRESSURE WAS LOST. MANUAL SELECTED & CABIN PRESSURE RISE STOPPED AT 11,000 MSL, THEN PRESSURE RECOVERED TO 5000' EMERGENCY DESCENT CONTINUE TO 24,000 THEN FURTHER TO 16000'. DECLARED EMERGENCY. R & R NR 1 CABIN PRESSURE CONTROLLER IAW AMM.
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1670. R&R BATTERY PER AMM.
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1672. R&R BATTERY PER AMM.
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675. R&R BATTERY PER AMM.
L2 DOOR SLIDE LINER HOLDING CLIP LOOSE. SECURED CLIP IAW SIP.
L2 DOOR SLIDE FORWARD MOUNTING BOLT FOR AFT DOOR THREADS MISSING. R & R THE MOUNTING ASSEMBLY IAW MT & AMM.
RIGHT BULLNOSE EMER LIGHT LENS MISSING AT ROW 6. INSTALLED LENS IAW MM.
LEFT WING INBD FLAP, INBD CARRIAGE SECONDARY TORQUE TUBE CORRODED. R & R TORQUE TUBE IAW AMM.
LEFT WING INBD FLAP, INBD CARRIAGE PRIMARY TORQUE TUBE CORRODED. R & R TORQUE TUBE IAW AMM.
INTERCOSTAL CORRODED, BETWEEN BS 1006 - 1016, RBL 39. R & R INTERCOSTAL IAW SRM.
WEB DAMAGED, BETWEEN BS 987 - 1006, BETWEEN LBL 31 - 41. R & R WEB IAW SRM.
LEFT WING NR 2 SLAT DELAMINATED ON LOWER SIDE OF TE OF WEDGE. R & R NR 2 SLAT IAW SRM.
TOP T CAP OF FLOORBEAM SKIN, CORRODED AT BS 987, BETWEEN RBL 51 TO LBL 51. REPAIRED SKIN IAW SRM.
AFT CARGO FLOOR CARGO TIE DOWN CRACKED, AT BS 767, RBL 14. R & R TRACK IAW SRM.
R1 DOOR FWD FRAME CRACKED, AT STATION 294.5, LOWER CORNER. REPAIRED FRAME IAW SRM.
RIGHT L ANGLE CORRODED, BETWEEN BS 947 - 997, RBL 55. R & R L ANGLE IAW SRM.
FASTENER HOLES & GALLEY MOUNT BRACKET WEBBING CORRODED, BETWEEN BS 987 - 1016, RBL 40. REPAIRED WEB IAW SRM.
AFT GALLEY DOOR FRAME CORRODED AT BS 992, BEHIND SPACER BLOCK AT FLOOR Z ANGLE. REPAIRED FRAME IAW SRM.
LEFT L ANGLE CORRODED, BETWEEN BS 955 - 940, LBL 50. R & R L ANGLE IAW SRM.
SHEAR TIE AT FRAME CRACKED AT BS 380, STRINGER 17L. R & R SHEAR TIE IAW SRM.
INTERCOSTAL CRACKED, BETWEEN BS 312 - 328, RBL 31. R & R INTERCOSTAL IAW SRM.
INTERCOSTAL CORRODED AT BS 807, RBL 6. R & R INTERCOSTAL IAW SRM.
INTERCOSTAL CORRODED, BETWEEN BS 767 - 787, RBL 6. R & R INTERCOSTAL IAW SRM.
INTERCOSTAL CRACKED, BETWEEN BS 312 - 328, LBL 44. R & R INTERCOSTAL IAW SRM.
RIGHT LOWER Z ANGLE CORRODED, BETWEEN BS 291 - 360. R & R Z ANGLE IAW SRM.
INTERCOSTAL CRACKED, BETWEEN BS 328 - 344, LBL 44. R & R INTERCOSTAL IAW SRM.
LEFT WING UPPER TE SHELF PANEL, INBD OF DEFLECTION RIB WS 253, AFT SUPPORT BRACKET CRACKED. REPAIRED BRACKET IAW SRM.
LEFT WING LOWER TE SHELF PANEL INBD OF DEFLECTION RIB WS 261, WAFFLE PLATE CRACKED. R & R WAFFLE PLATE IAW SRM.
AFT CARGO FLOOR WEB CORRODED, BETWEEN BS 847 - 867, RBL 20. R & R WEB IAW SRM.
FORWARD CARGO DOOR SKIN CREASED IN FWD LOWER CORNER, 3" ABOVE SKIN LOWER EDGE. REPAIRED SKIN IAW EA.
FUSELAGE SKIN CREASED, BETWEEN BS 378 - 381.5, STRINGER 17L. REPAIRED SKIN IAW SRM.
LEFT EMER EXIT, LOWER LIGHT LENS COVER DETERIORATED. R & R COVER IAW AMM.
LEFT WING OTBD AFT FLAP TE DELAMINATED ON INBD TE. R & R AFT FLAP IAW MM.
L1 DOOR EMER EXIT LENS MISSING. R & R LENS IAW MM.
L1 DOOR EXIT LIGHT COVER MISSING. REPLACED COVER IAW MM.
VERTICAL FIN LE HF ANTENNA PANEL HAS A HOLE ERODED THROUGH. REPAIRED PANEL IAW EA.
EMERGENCY LIGHT BATTERY PACK M1673 FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.
RIGHT EEPLS INOPERATIVE AT ROW 6. RELAMPED EEPLS IAW AMM.
RIGHT NR 1 WINDOW FRAME UPPER HOLE CRACKED IN OTBD WINDOW POST. R & R FRAME IAW ACO.
LEFT HORIZONTAL STAB VERTICAL STIFFENER RIB CRACKED AT STATION 147.9. REPAIRED STIFFENER RIB PER EA.
RIGHT HORIZONTAL STABILIZER RIB AT STAB STATION 92.7 CRACKED AT 2ND & 3RD VERTICAL STIFFENERS AFT AT BOTTOM. REPAIRED RIB IAW SRM.
RIGHT NR 1 FLIGHT DECK WINDOW FRAME, 1ST INBD HOLE CRACKED AT BS 217, WL 258. R & R FRAME IAW ACO.
COCKPIT LT WINDOW NR 3 POST FRAME CRACKED. R & R FRAME IAW SRM.
COCKPIT RT WINDOW NR 3 POST FRAME CRACKED. R & R FRAME IAW SRM.
LONGITUDINAL FLOORBEAM INBD & OTBD FLANGE HOLES CRACKED AT BS 727A+18.25, LBL 24.75. REPAIRED FLANGE IAW ER & EA.
LONGITUDINAL FLOORBEAM FLANGE HOLES CRACKED BETWEEN BS 727A+17 TO 727A+18, RBL 45.5. REPAIRED FLANGE IAW ER & EA.
FLIGHT DECK RT NR 1 WINDOW FRAME UPPER OTBD CORNER CRACKED. R & R FRAME IAW ACO.
FRAME CRACKED AT BS 480, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 727D, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 480, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 360, STRINGER 8R. REPAIRED FRAME IAW ER & EA.
FUSELAGE FRAME CRACKED AT STATION 520, STRINGER 8L. REPAIRED FRAME IAW SRM & EA.
FUSELAGE FRAME CRACKED AT STATION 440, STRINGER 8R. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT STATION 827, STRINGER 8R. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT STATION 787, STRINGER 8L. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT STATION 747, STRINGER 8L. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT STATION 400, STRINGER 8L. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT STATION 747, STRINGER 8R. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT STATION 500A, STRINGER 8R. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT STATION 400, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 827, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 787, STRINGER 8R. REPAIRED FRAME IAW EA.
CENTER WING LOWER BULKHEAD CHORD CRACKED AT BS 540, BETWEEN STRINGER 22R TO 23R. REPAIRED CHORD IAW EA.
LEFT WING NR 3 SLAT SKIN CRACKED. REPAIRED SKIN IAW SRM.
DIVERSION, FUEL IMBALANCE IN FLIGHT CROSS FEED CB POPPED IN FLIGHT. R & R ENGINE FUEL CROSS FEED VLV ACTUATOR IAW AMM.
DIVERSION ON CLIMB OUT, "FUEL EMPTY " ALERT. P6-3:B7 CB POPPED. RESET FUEL CROSS FEED VLV CB & CLEANED CONNECTOR IAW MM.
R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT RETAINER CLIP LOOSE. SECURED CLIP IAW SRM.
L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD & AFT RETAINER CLIPS LOOSE. SECURED CLIPS IAW SRM.
RT AFT EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. R&R BATTERY IAW AMM.
PUT RIGHT PACK ON FOR AIR AND IMMEDIATELY SMELLED AN ODOR SIMILAR TO A BLOWN OUT MATCH. GASPER FAN AND RECIRC FAN SWITCHES WERE BOTH IN THE OFF POSITION. REMOVED AND REPLACED CEILING LIGHT ASSY BALLAST AT ROW 14 TO 16 RIGHT SIDE DUE TO EXCESS / BALLAST HEAT AS PER M/M.
NR 12 SPOILER ACTUATOR HOUSING IS CRACKED. REMOVED AND REPLACED NR 12 SPOILER ACTUATOR PER M/M.
R1 DOOR EGRESS LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW MM.
RIGHT WING INBOARD MAIN FLAP LOWER SURFACE TRAILING EDGE DELAMINATED. REPAIRED MAIN FLAP IAW SRM & AMM.
AFT LT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER AMM.
FWD LT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER AMM.
AFT RIGHT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER AMM.
RT HORIZ STAB LOWER SKIN CRACKED AT STAB STA 129.5. REPAIRED SKIN IAW AMM AND SRM.
L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY. SLIDE WILL BE RE-INSTALLED PER MM.
DURING SCHEDULED HC1D CHECK, R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC1D CHECK, L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.
DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 15. REMOVED AND REPLACED SHEAR TIE PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 7. REMOVED AND REPLACED SHEAR TIE PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND RT WING I/B NR 7 GROUND SPOILER LOWER SKIN PUNCTURED. REMOVED AND REPLACED SPOILER PER MM.
DURING SCHEDULED 12Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 15. REMOVED AND REPLACED SHEAR TIE PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 6.14. REMOVED AND REPLACED SHEAR TIE PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND LT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED 12Y CHECK, FOUND FWD CARGO COMPT FLOOR LEFT Z-ANGLE CORRODED BETWEEN BS 493 TO BS 511B. REMOVED AND REPLACED Z-ANGLE SECTION PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED 12Y CHECK, FOUND RT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED 12Y CHECK, FOUND RT WING I/B AFT FLAP LOWER SURFACED PUNCTURED. REMOVED AND REPLACED AFT FLAP PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND RT CREASE BEAM CORRODED AT BS 330.65. REPAIRED BEAM PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND LT WING I/B AFT FLAP LOWER SURFACE PUNCTURED. REMOVED AND REPLACED AFT FLAP ASSY PER MM.
DURING SCHEDULED 12Y CHECK, FOUND CREASE BEAM FORWARD OF L1 DOOR CRACKED AT BS 302.5. REMOVED AND REPLACED CHORD PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND CREASE BEAM AT R2 DOOR CORRODED, BETWEEN BS 967 TO BS 986.5. REPAIRED BEAM PER SRM.
L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
R1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED 10Y CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT ASSY LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT EXTERNAL POWER RECEPTACLE DOOR CUTOUT. REPAIRED SKIN PER SWA EA.
DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.
DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.
DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.
DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
EEPLS PHOTOLUMINESCENT STRIP LOOSE BETWEEN ROW 6 DEF AND ROW 11 DEF. REMOVED AND REPLACED STRIP PER MM.
L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.
DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 36 TO LBL 40. REPAIRED FLOORBEAM PER SWA EA.
DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 508, BL 0. REPAIRED SKIN PER SRM.
DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 5 TO RBL 44. REPAIRED FLOORBEAM PER SWA EA.
DURING SCHEDULED 8Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 772, RBL 3. REPAIRED FLOORBEAM PER SWA EA.
DURING SCHEDULED 8Y CHECK, FOUND LT AND RT HORIZONTAL STAB LUG FACES CORRODED. REPAIRED HORIZONTAL STAB PER SWA EA.
DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, LBL 8 TO RBL 12. REPAIRED FLOORBEAM PER SWA EA.
EEPLS LIGHT COVER LOOSE AT ROW 6 ABC TO ROW 8 ABC. REMOVED AND REPLACED LIGHT COVER PER MM.
DECLARED EMERGENCY, NR 1 ENGINE FUEL LEAK AT CRUISE, 1500 LBS PER HOUR MORE THAN NR 2 ENGINE. REMOVED AND REPLACED NR 1 ENGINE FUEL/OIL HEAT EXCHANGER PER MM.
DURING SCHEDULED HC2 CHECK, LEFT AFT CABIN EMERGENCY EXIT LIGHT FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC2 CHECK, FWD CABIN EMERGENCY EXIT LIGHTS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.
DURING SCHEDULED HC2 CHECK, ROW 16 ABC EMERGENCY EXIT LIGHT FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC2 CHECK, RT OVERWING EMERGENCY EXIT LIGHT FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
R2 DOOR EMERGENCY EXIT EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
DURING SCHEDULED RON CHECK, FOUND EEPLS STRIP DAMAGED. REMOVED AND REPLACED STRIP PER MM.
DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
DURING SCHEDULED MV1 CHECK, FOUND LT WING T/E INBD AFT FLAP SKIN PUNCTURED NEAR INBOARD END. REPAIRED AFT FLAP PER SWA EA.
DURING SCHEDULED MV2 CHECK, FOUND 2 EACH SECTIONS OF EEPLS STRIPS BETWEEN ROWS 6 DEF AND 10 DEF, DELAMINATED. REMOVED AND REPLACED EEPLS STRIPS PER MM.
DURING SPV, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS AT ROW 19 ABC, BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.
DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.
DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY PACKS FAILED FUNCTIONAL CHECK. REMOVED AND REPLACED BATTERY PACKS PER MM.
IN-FLT SHUTDOWN, DIVERSION, DECLARED EMERGENCY. EN ROUTE TO MCI, NR 1 ENGINE FLAMED OUT. REMOVED AND REPLACED NR 1 ENGINE PER MM.
IN-FLIGHT SHUTDOWN, DECLARED EMERGENCY. DURING CRUISE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. REMOVED AND REPLACED NR 1 ENGINE SUPPLY OIL FILTER & SCAVENGE OIL FILTER PER MM. C/W ENGINE RUN, NO DEFECTS FOUND.
AIR TURNBACK, DECLARED EMERGENCY, SLIGHT HYDRAULIC SMELL DURING TAXI, STRONG HYDRAULIC SMELL AT HIGH POWER DURING TAKEOFF. REMOVED AND REPLACED HYDRAULIC RESEVOIR AIR PRESSURE MODULE, BOTH COALESCER BAGS AND HEPA FILTER PER MM.
DURING SCHEDULED PM CHECK, SWA SI 11075-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE PER SRM.
EEPLS LENS MISSING AT ROW NR 11. INSTALLED LENS PER MM.
INFLIGHT SHUT DOWN, DIVERSION, DURING CRUISE NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED, LIGHT REMAINED ON EVEN AT IDLE. REMOVED AND REPLACED NR 2 ENGINE PER MM.
DURING SCHEDULED C2 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM.
DURING SCHEDULED SERVICE CHECK, SI 11038-55, FOUND BOTH LT AND RT ELEVATOR TAB HINGE BUSHINGS WORN. REMOVED AND REPLACED ALL 4 HINGE BUSHINGS ON BOTH TABS PER MM.
DURING SCHEDULED SERVICE CHECK, FOUND EEPLS COVER MISSING AT ROW 2. INSTALLED COVER PER MM.
FWD ENTRY DOOR EMERGENCY EVAC SLIDE CONTAINER RH ATTACH BRACKET LOOSE. SECURED BRACKET PER MM.
DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED OVERWING EXIT LIGHT PER MM.
DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVERS CRACKED AT ROW'S 1, 2, 4, 6, 13, 15, 16, 17 & 23. R&R EEPLS TRACK COVERS PER MM.
DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD EMERGENCY LIGHT INOP AT ROW 19 RT. REMOVED AND LAMP PER MM.
FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER INADVERTENTLY. REINSTALLED SLIDE ASSY PER MM.
CABIN PRESS ALT WARNING HORN SOUNDED, DESCENDED TO 10,000 FT AND O2 MASKS DEPLOYED. C/W SINGLE PACK CONFIDENCE CK. OPS CK GOOD PER MM. RESTOWED O2 MASKS PER MM.
EEPLS COVER LOOSE AT FWD END. SECURED TRACK COVER PER MM.
FWD SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.
EMERGENCY ESCAPE FLOOR TRACK LIGHTING KICKED OUT OF PLACE AND DAMAGED AT ROW 1 ABC. REMOVED AND REPLACED TRACK ASSY PER MM.
BELT LOADER CONTACTED FUSELAGE APPROXIMATELY BS 348L WL 265 SHEETMETAL REPAIR ACCOMPLISHED PER SWA RA 1-753-1964 AND SRM UNDER ATTACHED SAM FORM 326.
F/A REPORTED SMELLING SMOKE FROM AN ELECTRICAL SOURCE FROM AFT GALLEY. AFTER PULLING BOTH COFFEEMAKERS AND CIRCUIT BREAKERS, SMOKE SMELL DISSIPATED. CLEAN DEBRIS OFF AFT GALLEY COFFEEMAKER RACKS. OPS CK GOOD PER MM.
JUST PRIOR TO ENGINE START AN ACRID ELECTRICAL SMELL ENTERED CABIN AT THE TIME THE DUS WENT BLANK AND SEVERAL SYSTEMS FELL OFF LINE. FOUND P-91 WIRES TO BE BURNT. REMOVED AND REPLACED POWER DISTRIBUTION PANEL 91 PER M/M 24-21-21-4 OPERATIONAL CHECK OF SYSTEM OK.