N371SW
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES CO | Operator | 2009-05-12 – 2009-05-12 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2009-05-12 – 2009-05-12 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
L1 DOOR EMER EVAC SLIDE LOOSE. R & R SLIDE IAW MT.
R2 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW SIP.
RIGHT EMER LIGHT INOPERATIVE AT ROW 1. R & R BATTERY PACK IAW AMM.
ENTRY DOOR EMER LIGHT BROKEN. R & R LIGHT IAW MM.
STRINGER CLIP CRACKED AT BS 500A, STRINGER 16R. R & R CLIP IAW SRM.
FUSELAGE SKIN CRACKED AT BS 478, STRINGER 3L. REPAIRED SKIN IAW EA.
FUSELAGE SKIN CRACKED AT BS 908+1.5, STRINGER 4L. REPAIRED SKIN IAW EA.
FUSELAGE SKIN CRACKED AT BS 362, STRINGER 6R. REPAIRED SKIN IAW EA.
SKIN CRACKED AT BS 435, STRINGER 17L. REPAIRED SKIN IAW SRM.
SKIN CRACKED AT BS 435, STRINGER 16R. REPAIRED SKIN IAW EA.
FUSELAGE SKIN CRACKED BETWEEN BS 453 - 454.5, STRINGER 16R. REPAIRED SKIN IAW EA.
SKIN CRACKED BETWEEN BS 500+15 TO 500+16.5, STRINGER 16R. REPAIRED SKIN IAW EA.
FUSELAGE EXTERIOR SKIN CRACKED AT BS 500+5, STRINGER 15L. REPAIRED SKIN IAW EA.
LEFT OVERWING EXIT LIGHT LENS LOOSE. R & R LENS IAW MM
R2 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW AMM & MT.
RIGHT EMER AISLE LIGHT INOPERATIVE AT ROW 1. R & R BATTERY CHARGER IAW AMM.
RIGHT EMER LIGHT INOPERATIVE AT ROW 1. R & R LIGHT CHARGER ASSEMBLY IAW MM.
DIVERSION, DECLARED EMER DURING CLIMB, ACRID SMELL DEVELOPED IN COCKPIT. FOUND RT AIR CYCLE MACHINE OVER SERVICED OIL IAW MM.
FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727 STRINGER 18A LT LOWER FWD FASTENER HOLE. R & R CHORD IAW EA.
LOWER STUB FRAME CRACKED AT BS 294. R & R STUB FRAME IAW SRM & DWG.
FORWARD EEPLS DELAMINATED. R & R EEPLS IAW MM.
AFT LAVATORY MOUNTED EMER EXIT SIGN FASTENER ATTACH POINTS DELAMINATED. R & R SIGN IAW AMM.
FORWARD LAVATORY MOUNTED EMER EXIT SIGN FASTENER ATTACH POINTS CORRODED. REMOVED & INSTALLED SIGN ASSEMBLY IAW AMM.
RIGHT AFT WING TO BODY FAIRING SUPPORT STRUCTURE HORIZONTAL SHELF OTBD CHORD CRACKED AT BS 727 STRINGER 19R. R & R CHORD IAW SRM & DWG.
VERTICAL STIFFENER CRACKED AT BS 328 RBL 32. R & R STIFFENERS IAW SRM & DWG.
R1 THRESHOLD WEB CORRODED. R & R WEB IAW SRM & DWG.
LEFT WING NR 3 FLAP FAIRING SPRING DOOR, SPRING RETAINER BRACKET CRACKED. R & R BRACKET IAW DWG.
SKIN CRACKED AT BS 360 STRINGER 3R. REPAIRED SKIN IAW AAR & EA.
BUTT JOINT STRINGER SPLICE CRACKED AT BS 908 STRINGER 4. R & R SPLICE IAW EA.
FLOORBEAM CORRODED AT BS 986.5 STRINGER 0. REPAIRED FLOORBEAM IAW SRM.
RIGHT CREASE BEAM CORRODED BETWEEN BS 946.5 TO967. R & R CREASE BEAM IAW SRM & DWG.
FRAME SHEAR TIE ATTACH ANGLE CRACKED AT BS 294.5 STRINGER 13L. R & R ANGLE IAW DWG & SRM.
AFT CARGO DOOR CUT OUT FWD LOWER CORNER FUSELAGE SKIN CRACKED FROM FASTENER TOWARDS SKIN EDGE. REPAIRED CUT OUT IAW SRM.
CREASE BEAM INBD CHORD CORRODED AT AFT GALLEY DOOR THRESHOLD. R & R CREASE BEAM IAW SRM DWG.
INTERCOSTAL CRACKED BETWEEN BS 312 TO 328 RBL 32. R & R INTERCOSTAL IAW SRM & DWG.
INTERCOSTAL ANGLE CRACKED AT BS 348 STRINGER 16L. R & R ANGLE IAW SRM & DWG.
R2 DOOR UPPER HINGE LOOSE. REPAIRED HINGE IAW MM.
FLOORBEAM CORRODED AT BS 344 BETWEEN RBL 2 TO LBL 10. REPAIRED BEAM IAW SRM.
FRAME OTBD CHORD FWD FLANGE CRACKED AT BS 727 STRINGER 18A RT LOWER FWD FASTENER HOLE. R & R CHORD IAW EA.
FORWARD CARGO COMPARTMENT FRAME CRACKED AT BS 520 BETWEEN STRINGER 20L TO 21L. REPAIRED FRAME IAW SRM.
RIGHT WING AILERON TAB WARPED. R & R TAB IAW MM.
LEFT WING INBD AFT FLAP DELAMINATED AT THE INBD LOWER CORNER. REPAIRED AFT FLAP IAW MM.
RIGHT WING INBD AFT FLAP LOOSE. SECURED AFT FLAP IAW MM.
L1 DOOR FLOOR STRUCTURE CREASE BEAM CORRODED. R & R BEAM IAW SRM & DWG.
FUSELAGE SKIN CRACKED AT BS 460+4 STRINGER 16R. REPAIRED SKIN IAW EA.
FUSELAGE SKIN CRACKED AT BS 500A+7 STRINGER 16L. REPAIRED SKIN IAW SRM.
FUSELAGE SKIN CRACKED AT BS 500B+17 STRINGER 16L. REPAIRED SKIN IAW EA.
FUSELAGE SKIN CRACKED AT BS 967+11 STRINGER 21L. REPAIRED SKIN IAW SRM.
LT WING LE SKIN CRACKED AT WS 564.50. REPAIRED LE IAW SRM.
EMERGENCY EXIT LIGHT OVERHEAD BIN INOPERATIVE AT ROW NR 1. R & R BATTERY CHARGER IAW AMM.
LT WING INBD FORE FLAP UPPER SKIN DELAMINATED. REPAIRED FORE FLAP IAW SRM.
LEFT WING OTBD FLAP NR 2 CARRIAGE SPINDLE DELAMINATED. R & R SPINDLE IAW MT.
R2 DOOR EMERGENCY EVAC FWD SLIDE ATTACHMENT BRACKET CRACKED. R & R BRACKET IAW SRM.
LT WING NR 1 FLAP TRACK FAIRING MID CRACKED AT LE. REPAIRED FAIRING IAW EA.
R1 DOOR LOWER EMERGENCY EXIT LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.
LT OVER WING LOWER EMERGENCY EXIT DOOR LIGHT BULBS INOPERATIVE. RELAMPED IAW AMM.
FRAME SHEAR TIE CRACKED AT BS 400 BETWEEN STRINGER 15R & STRINGER 16R. REPAIRED SHEAR TIE IAW SRM.
FUSELAGE SKIN CRACKED BETWEEN BS 500B+6" TO BS 500B+7" STRINGER 15R. REPAIRED SKIN IAW EA.
FUSELAGE SKIN CRACKED BETWEEN BS 503.5 TO BS 504.5 STRINGER 16R. REPAIRED SKIN IAW EA.
FUSELAGE SKIN CRACKED BETWEEN BS 384.5 TO BS 388.5 STRINGER 15R. REPAIRED SKIN IAW EA.
DIVERSION DECLARED, EMERGENCY CLIMB OUT OF JAX LE DEVICE NR 3 WOULD NOT RETRACT, WAS GREEN OVERHEAD TRANSIT LIGHT. THEN LEVELED OFF LE DEVICE NR 3 TURNED AMBER TRANSIT LIGHT & 4 LE DEVICE TURNED AMBER TRANSIT LIGHT. R&R NR 3 LE ACTUATOR IAW MM. O.
L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. R&R SLIDE IAW MT.
ON DESCENT BURNING SMELL NOTICED ON LT SIDE BETWEEN ROW 18 TO ROW 19. R&R GASPER FAN IAW MM.
LEFT OVERWING EXIT SIGN LENS LOOSE. SECURED LENS PER MM.
FUSELAGE SKIN CRACKED AT STA 500D+5.7, STR 16L. REPAIRED SKIN PER SRM.
FUSELAGE SKIN CRACKED AT STA 500A, STR 16R. REPAIRED SKIN PER SRM.
FUSELAGE SKIN CRACKED AT STA 974, STR 21L. REPAIRED SKIN PER SRM.
A 3.5 INCH SURFACE CRACK LOCATED 5 INCHES AFT OF STATION 440 ABOVE STRINGER 16R. INSTALLED INTERIM REPAIR PER SRM 53-00-01-2R, REPAIR 31, DETAIL 11 AND EA- 1-353-21821.
A 2.0 INCH FUSELAGE SUBSURFACE CRACK FOUND AT BODY STATION 400 PLUS 5 INCHES ABOVE STRINGER 16R. INSTALLED INTERIM REPAIR PER SRM 53-00-01-2R, REPAIR 31, DETAIL 11 AND EA- 1-353-21822.
DURING WALKAROUND NOTED SKIN CRACK APPROX 3" LONG STA 500D +13" ON STR 15L. REPAIRED SKIN CRACK PER EA 1-353-21570 CONTACT ENGINEERING BEFORE 2800 CYCLES REF SAM 943 S/N T031858
DURING WALKAROUND NOTED SKIN CRACK APPROX 3" LONG STA 500D +13" ON STR 15L. REPAIRED SKIN CRACK PER EA 1-353-21570 CONTACT ENGINEERING BEFORE 2800 CYCLES REF SAM 943 S/N T031858 FACT AS A RESULT OF POST REPAIR INSPECTION
CRACK FUSELAGE SKIN LEFT STR 1 AT BS 392. REMOVED AND REPLACED SKIN IAW EA.
FWD CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB IAW AMM.
LEFT WING PUNCTURED ON I/B FORE FLAP LOWER SURFACE. REPAIRED FORE FLAP IAW SRM.
STRINGER TIE CRACKED AT BS 500B, STR 1. REMOVED AND REPLACED TIE IAW SRM AND DWG.
STRINGER TIE CLIP CRACKED AT BS 500C, STR 2L. REMOVED AND REPLACED TIE CLIP IAW DWG AMD SRM.
STRINGER TIE CRACKED AT BS 500C, STR 2R. REMOVED AND REPLACED TIE IAW SRM & DWG.
STRINGER TIE CRACKED AT BS 500B, STR 2R. REMOVED AND REPLACED TIE IAW DWG AND SRM.
STRINGER TIE CRACKED AT BS 500B, STR 3R. REMOVED AND REPLACED TIE IAW SRM AND DWG.
STRINGER TIE CRACKED AT BS 500C, STR 3R. REMOVED AND REPLACED TIE IAW SRM AND DWG.
STRINGER TIE CRACKED AT BS 500C, STR 1. REMOVED AND REPLACED TIE IAW DWG AND SRM.
STRINGER TIE CRACKED AT BS 500B, STR 2L. REMOVED AND REPLACED TIE IAW SRM & DWG.
TIE CLIP CRACKED AT BS 500A, STR 1. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
TIE CLIP CRACKED AT BS 500A, STR 2L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
TIE CLIP CRACKED AT BS 500A, STR 2R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
TIE CLIP AT BS 520, STR 2L. REMOVED AND REPLACED TIE CLIP IAW DWG AND SRM.
LEFT HORIZONTAL STABILIZER RIB LOWER CHORD CRACKED AT STA 120.30. REMOVED AND REPLACED CHORD IAW SRM AND DWG.
VERTICAL STABILIZER WEB CRACKED AT STA 13.33. REMOVED AND REPLACED WEB PER SRM AND DWG.
RIGHT WING NR 5 SLAT O/B END DELAMINATED. REPAIRED NR 5 SLAT IAW SRM.
LEFT WING NR 1 O/B FLAP O/B SPINDLE CARRIAGE CRACKED. REMOVED AND REPLACED SPINDLE IAW AMM AND MT.
WEB CRACKED BETWEEN BS 927 TO BS 947.5, LBL 17.2. REMOVED AND REPLACED WEB IAW SRM AND DWG.
CLIP CRACKED AT BS 320, STR 20L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.
CLIP CRACKED AT BS 328, STR 20L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.
TIE CLIP CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
CLIP CRACKED AT BS 336, STR 20L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.
STRAP CRACKED BETWEEN BS 312 TO BS 360, LBL 45.6. REMOVED AND REPLACED STRAP IAW SRM AND DWG.
NLG WHEEL WELL DOUBLER CRACKED AT BETWEEN BS 251.6 TO BS 268.25, BETWEEN WL 169.1 TO WL 185. REPAIRED DOUBLER IAW SRM.
RIGHT WING NR 6 SLAT SKIN CRACKED. REPAIRED SKIN IAW SRM.
TIE CLIP CRACKED AT BS 727E, STR 21L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
WEB CRACKED BETWEEN BS 500A TO BS 500B, STR 26L. REMOVED AND REPLACED WEB IAW SRM AND DWG.
FRAME CRACKED AT BS 500D, BETWEEN STR 20R AND STR 23R. REPAIRED FRAME IAW EO AND EA.
FRAME CORRODED AT BS 500C, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME IAW SRM.
FRAME CORRODED AT BS 500C, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME IAW SRM.
FUSELAGE FRAME CRACKED AT BS 947.5, STRINGER 19L. REPAIRED SKIN PER SRM.
FRAME CRACKED AT BS 500C, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME IAW SRM.
LEFT WING CRACKED ON ANGLE LOCATED AT LEVEL RSS 527 TRAILING EDG AREA. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.
ANGLE CRACKED AT BS 792, STR 18R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.
STRINGER SPLICE CORRODED AT BS 907+5, STR 18L. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.
TIE CLIP CRACKED AT BS 747, STR 22L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
TIE CLIP CRACKED AT BS 787, STR 20R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
TIE CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.
TIE CLIP CRACKED AT BS 867, STR 27R. REMOVED AND REPLACED TIE CLIP IAW SRM AND IAW SRM & DWG.
STRINGER CRACKED AT BS 867, STR 26R. REPAIRED STRINGER PER SRM.
TIE CLIP CRACKED AT BS 927, STR 25R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
TIE CLIP CRACKED AT BS 947.5, STR 25R. REPAIRED TIE CLIP IAW EA.
TIE CLIP CRACKED AT BS 727A, STR 26L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
TIE CLIP CRACKED AT BS 867, STR 27L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.
SUPPORT ANGLE CRACKED AT BS 727A, BETWEEN STR 25L AND STR 26L. REMOVED AND REPLACED ANGLE IAW SRM & DWG.
WEB CRACKED BETWEEN BS 500B TO BS 500C, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED WEB IAW SRM AND DWG.
CLIP CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.
LEFT KEEL BEAM ANGLE CRACKED AT BS 520+14. REMOVED AND REPLACED ANGLE IAW SRM & DWG.
WEB CRACKED BETWEEN BS 400 TO BS 420, STR 26R. REMOVED AND REPLACED WEB IAW SRM AND DWG.
FUSELAGE SKIN CRACKED AT BS 520+5, STR 2R. REPAIRED SKIN IAW EA AND SRM.
LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 671, RBL 24.5. REPAIRED CHORD IAW EA AND EO.
FUSELAGE SKIN CRACKED AT BS 520+3, STRINGER 28L. REPAIRED SKIN PER SRM.
SHEAR TIE CORRODED AT BS 500, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.
LEFT WING OUTBOARD AFT FLAP DELAMINATED ON UPPER SURFACE OF TRAILING EDGE WEDGE. REMOVED & REPLACED AFT FLAP PER M/M.
FUSELAGE SKIN CRACKED AT BS 908+7, STR 24R. REPAIRED SKIN PER SRM.
LEFT EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 6. REMOVED AND REPLACED BULB PER AMM.
RIGHT EMERGENCY EXIT LIGHT COVER MISSING AT ROW 12. REMOVED AND REPLACED COVER PER MM.
STRINGER CLIP CRACKED AT BS 500B, STR 3R. REMOVED AND REPLACED CLIP PER SRM.
STRINGER CLIP CRACKED AT BS 500B, STR 2R. REMOVED AND REPLACED CLIP PER SRM.
EMERGENCY LIGHT INOP AT ROW 10 ABC. RELAMPED PER MM.
FUSELAGE SKIN CRACKED AT BS 500A +14, STR 2R. REPAIRED SKIN PER SRM.
NR 2 SLAT HAS 4EA SKIN CRACKS ON LOWER SKIN AT AFT ROW OF FASTENERS (BELOW O/B AUX TRACK). VERIFIED WITH HFEC. REPAIRED LEFT WING SLAT NR 2 TEE CHORD BETWEEN SS175 AND SS220 IAW EA N 1-357-7551 REV 0 AND EO N AEM-HC57-230/12.R0
DURING SCHEDULED SPV CHECK, FOUND LT STRINGER CLIP CRACKED AT BS 639, LBL 45.5. REMOVED AND REPLACED CLIP IAW SRM AND DWG.
DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 416, STR 1. REPAIRED SKIN PER EA.
DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE CROWN SKIN CRACKED AT BS 442, STR 2R. REPAIRED SKIN PER EA.
DECLARED EMERGENCY -- LEADING EDGE DEVICES WOULD NOT EXTEND FOR LANDING. REMOVED AND REPLACED NR 3 L/E FLAP ACTUATOR IAW MM.
DURING SCHEDULED 18Y CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP AT ROW 8. REPAIRED WIRE PER SWPM.
DURING SCHEDULED 18Y CHECK, FOUND LT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED 18Y CHECK, FOUND RT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED 18Y CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 867, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.
DURING SCHEDULED 18Y CHECK, FOUND LT EMERGENCY EXIT LIGHT INOP AT ROW 17. RELAMPED PER MM.
DURING SCHEDULED 18Y CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT BS 400. REPAIRED WIRE PER WDM.
DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.
DURING SCHEDULED 18Y CHECK, FOUND LT EEPLS INOP AT ROW 21. INSTALLED BATTERY PACK PER MM.
DURING SCHEDULED 18Y CHECK, FOUND RT EEPLS INOP AT ROW 23. INSTALLED BATTERY PACK PER MM.
DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 24.8. REPAIRED BEAM PER EA.
DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD CARGO DOOR CUTOUT, BS 490, STR 24R. REPAIRED SKIN PER SRM.
DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B+13 TO BS 727B+15.4, STR 4R. REPAIRED SKIN PER SRM.
DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 831 TO BS 832.4, STR 4L. REPAIRED SKIN PER SRM.
DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 887, STR 7L. REPAIRED SKIN PER SRM.
DURING SCHEDULED 18Y CHECK, FOUND R2 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM.
DURING SCHEDULED 18Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 6L. REMOVED AND REPLACED STR SPLICE PER SRM.
DURING SCHEDULED 18Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 5L. REMOVED AND REPLACED STR SPLICE PER SRM.
DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 887, STR 7L. REPAIRED SKIN PER SRM.
DURING SCHEDULED 18Y CHECK, FOUND LT CREASE BEAM CRACKED BETWEEN BS 360 TO BS 380, LBL 70. REMOVED AND REPLACED BEAM PER SRM.
DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 500B, STR 1R. REPAIRED FRAME PER SRM.
DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 933, STR 25R. REPAIRED SKIN PER SRM.
DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 514A, STR 10L. REPAIRED SKIN PER SRM.
DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 943 TO BS 945.2, STR 24R. REPAIRED SKIN PER SRM.
DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 772, STR 4L. REPAIRED SKIN PER EA.
DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 514A, STR 10L. REPAIRED SKIN PER SRM.
DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 514, STR 10L. REPAIRED SKIN PER SRM.
LEFT WING I/B GROUND SPOILER O/B ACTUATOR ATTACHMENT LUG BROKEN. REMOVED AND REPLACED GROUND SPOILER PER MM.
DURING SCHEDULED HC1 CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 5L. REPAIRED WEB PER SRM.
LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 115.00. REPAIRED SKIN IAW EA AND EO.
DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY INOP AT BS 332, LBL 7. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 733B, STR 4L. REPAIRED SKIN PER EA.
DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 434 TO BS 437, STR 1. REPAIRED SKIN PER ER.
DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 453 TO BS 456, STR 10L. REPAIRED SKIN PER SRM.
DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 505, STR 10R. REPAIRED SKIN PER SRM.
DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 504D, STR 16R. REPAIRED SKIN PER SRM.
DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 485, STR 16R. REPAIRED SKIN PER SRM.
DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 493 TO BS 497, STR 10L. REPAIRED SKIN PER SRM.
DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 442.5 TO BS 445.5, STR 1. REPAIRED SKIN PER ER.
DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 434 TO BS 445.5, STR 1. REPAIRED SKIN PER ER.
DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 504D, STR 16R. REPAIRED SKIN PER SRM.
DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 493 TO BS 497, STR 10L. REPAIRED SKIN PER SRM.
DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 453 TO BS 456, STR 10L. REPAIRED SKIN PER SRM.
DURING SCHEDULED 2HC2 CHECK, FOUND FUSELAGE SKIN CRACKED L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER EA.
DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 520, STR 9R. REPAIRED SKIN PER EA.
DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 512D, STR 10L. REPAIRED SKIN PER EA.
DURING SCHEDULED MV2 CHECK, FOUND FWD EEPLS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED 2HC1 CHECK, FOUND AFT SERVICE OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.
RT MLG TIRE NR 3 & 4 BLEW ON LANDING. SUBSEQUENT WHEEL FIRE. R&R RT MLG TIRES PER MM.
AFT FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 941, STR 24L. REPAIRED SKIN PER AAR EA.
DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 24L. R&R CLIP PER SRM.
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 941 TO BS 943, STR 24L. REPAIRED SKIN PER EA.
DURING SCHEDULED 16Y CHECK, FOUND FWD GALLEY DOOR AFT FRAME CRACKED. REPAIRED FRAME PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND RT WING FUEL TANK WING RIB LOWER CHORD CRACKED AT WBL 135, BETWEEN STR 2 TO STR 3. REPAIRED RIB PER ACO.
DURING SCHEDULED 16Y CHECK, FOUND LT WING FUEL TANK WING RIB LOWER CHORD CRACKED AT WBL 135, BETWEEN STR 2 TO STR 3. REPAIRED RIB PER ACO.
DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR FRAME CRACKED AT BS 303, STR 16L. REPAIRED FRAME PER ACO.
DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN DAMAGED AT BS 500B, STR 2R. REPAIRED SKIN PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND CENTER BOX WING, LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 667, LBL 24. REPAIRED BEAM PER EA.
DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 22R. REMOVED AND REPLACED CLIP PER SRM.
DURING SCHEDULED 6Y CHECK, FOUND FUSELAGE SKIN DAMAGED AT BS 559, STR 2R. REPAIRED SKIN PER EA.
DURING SCHEDULED 16Y CHECK, FOUND RT CREASE BEAM WEB BETWEEN BS 727D TO 727E CORRODED. REMOVED AND REPLACED BEAM PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND CENTER WING BOX LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 671, LBL 24. REPAIRED BEAM PER EA.
DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED R1 DOOR UPPER HINGE CUTOUT, BS 304, WL 258. REPAIRED SKIN PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED R1 DOOR LOWER HINGE CUTOUT, BS 291, WL 233. REPAIRED SKIN PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND RT CREASE BEAM CORRODED AT BETWEEN BS 727E TO BS 747. REMOVED AND REPLACED BEAM PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 747, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND BEAR STRAP SKIN CORRODED AT BS 493, BETWEEN STR 27R TO STR 28R. REPAIRED SKIN PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE HINGE FITTING CRACKED AT L1 DOOR UPPER HINGE CUTOUT. R&R FITTING PER BAC DWG.
DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 627, STR 6R. REMOVED AND REPLACED CLIP PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BETWEEN BS 807 TO BS 827, STR 17L. REMOVED AND REPLACED WEB PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND RT CREASE BEAM WEB CORRODED AT BETWEEN BS 727E TO BS 747. REMOVED AND REPLACED WEB PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT UPPER STOP FITTING. REPAIRED FRAME PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CORRODED AT R2 DOOR BETWEEN BS 996 TO BS 947. REMOVED AND REPLACED BEAM PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CORRODED AT L2 DOOR, BETWEEN BS 950 TO BS 990. REMOVED AND REPLACED BEAM PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 22R. REMOVED AND REPLACED CLIP PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.
DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 18. REPAIRED BEAM PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 16R. REMOVED AND REPLACED CLIP PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 8L. REMOVED AND REPLACED CLIP PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT I/B END DELAMINATED AT EDGE. REPAIRED SLAT PER SRM.
DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 38, STR 21L. REMOVED AND REPLACED CLIP PER SRM.
DURING SCHEDULED MV2 CHECK, FOUND RT MLG SIDE SUPPORT FITTING LUG CORRODED AT BS 685. REPAIRED FITTING PER SWA EA.
DURING SCHEDULED MV2 CHECK, FOUND LT MLG SIDE SUPPORT FITTING LUG CORRODED AT BS 685. REPAIRED FITTING PER SWA EA.
DURING SCHEDULED 14Y CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED AT BS 1016, STR 6L. REPAIRED BULKHEAD PER SRM.
DURING SCHEDULED 14Y CHECK, FOUND RT OVERWING EMERGENCY EXIT HATCH LOWER FRAME CRACKED AT LOWER CENTER FITTING. REMOVED AND REPLACED LOWER FRAME PER SRM.
DURING SCHEDULED 14Y CHECK, FOUND VERTICAL STABILIZER STANDBY ACTUATOR, INPUT ROD END BROKEN. REMOVED AND REPLACED ROD END PER MM.
DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.
DURING SCHEDULED A1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD EDGE. REMOVED AND REPLACED AFT FLAP PER MM.
NR 1 ENGINE EGT EXCEEDED LIMITS ON CLIMBOUT. MAX OF 934 FOR APPROX 2 SECONDS. FOUND VBV SHAFT BROKEN. REMOVED AND REPLACED VBV MOTOR AND SHAFT ASSY PER MM.
DURING SCHEDULED C3 CHECK, FOUND LT WING NR 4 GROUND SPOILER HINGE FITTING SHEARED. REMOVED AND REPLACED NR 4 SPOILER PER MM.
DURING SCHEDULED C3 CHECK, FOUND LT WING NR 5 GROUND SPOILER HINGE FITTING SHEARED. REMOVED AND REPLACED NR 5 SPOILER PER MM.
ON SHORT FINAL -A- HYDRAULIC SYSTEM LOW PRESSURE LIGHT ILLUMINATED. AFTER LANDING -A- HYDRAULIC SYSTEM QUANTITY FELL TO ZERO. REMOVED AND REPLACED FLIGHT CONTROL SHUTOFF VALVE PER MM.
DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.
DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.
DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 12L. REPAIRED SKIN PER ER.
DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 358, STR 14L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.
DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.
EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 6 ABC TO ROW 8 ABC. REMOVED AND REPLACED EEPLS STRIP PER MM.
DURING SCHEDULED C1 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE HARDWARE PER MM.
DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 25R. REPAIRED SKIN PER SRM.
DURING SCHEDULED A2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.
DURING SCHEDULED A1 CHECK, FOUND PHOTOLUMINESCENT STRIP WORN AT ROW 8. REMOVED AND REPLACED STRIP PER MM.
DURING SCHEDULED C4 CHECK, FOUND NR 5 L/E SLAT UPPER WEDGE DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED SLAT PER MM.
DURING SCHEDULED SERVICE CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.
DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 12R. REPAIRED SKIN PER SRM & SWA EA.
DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 15R. REPAIRED SKIN PER SRM & SWA EA.
DURING SCHEDULED 1/4D CHECK, FOUND RT MLG STABILIZER BEAM FWD & AFT ATTACH FITTINGS CORRODED. REMOVED AND REPLACED STABILIZER BEAM PER MM.
DURING SCHEDULED 1/4D CHECK, FOUND 2 EA AFT CARGO FLOOR SUPPORT BEAMS CORRODED AT BS 770, LBL 3 & RBL 8. REPAIRED BEAMS PER SWA EA.
R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.
R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.
DURING SCHEDULED C4 CHECK, LT ELEVATOR FAILED TAB FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BUSHING PER MM.
DURING SCHEDULED C4 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RIGHT AFT FLAP PER MM.
DURING SCHEDULED C2 CHECK, FOUND RIGHT WING L/E SKIN AT WS 213, CRACKED. REPAIRED L/E SKIN PER ER.
DURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD AFT FLAP T/E DELAMINATED. REPAIRED RT AFT T/E FLAP PER SRM.
R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.
DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 957, STR 17R. REPAIRED SKIN PER BFG ER.
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17L. REMOVED AND REPLACED FRAME PER SRM.
DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME PER SRM.
FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER WHEN DOOR WAS OPENED. REINSTALLED SLIDE PER MM.
DURING SCHEDULED C4 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT BALLAST PER MM.
DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED BUSHINGS FOR LT OTBD LOCKOUT MECHANISM PER MM.
DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR ONERHEAD EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LENS PER MM.
DURING SCHEDULED C1 CHECK, FOUND # 1 L/E SLAT CRACKED ( 2 EA ) AT AFT ROW OF FASTENERS NEAR CENTER AUX TRACK. REPAIRED SLAT PER SWA RA 1-357-1107.
B SYSTEM HYDRAULIC FAILURE DURING LANDING. R & R B HYDRAULIC SYS MODULE PER MM.
DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE MOUNT LOOSE. SECURED MOUNT PER MM.
DIVERSION - APU OVERSPEED LIGHT ILLUMINATED. LEFT BUS OFF LIGHT ILLUMINATED. (NR 1 GENERATOR ALREADY ON MEL). REMOVED AND REPLACED APU 3-SPEED SWITCH PER MM.
FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER WHEN DOOR WAS OPENED. REINSTALLED EVAC SLIDE MM.
AIR TURNBACK WHILE APU WAS OFF, RECEIVED APU FIRE INDICATION, BOTTLE WAS DISCHARGED AND LIGHT EXTINGUISHED. R&R LOWER APU FIRE LOOP DETECTOR - OPS CHECK GOOD PER MM.
DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.
DURING SCHEDULED 1/4D CHECK, FOUND F/O P-1 WINDOW FRAME CRACKED AT UPPER OTBD CORNER. REPAIRED FRAME PER SRM.
DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR LOWER FRAME CRACKED AT AFT CORNER. R&R FWD SVC DOOR PER MM.
DURING SCHEDULED 1/4D CHECK, FOUND NR 4 GALLEY EMERGENCY EXIT LIGHT LENS CRACKED. R&R LENS PER MM.
DURING SCHEDULED 1/4D CHECK, FOUND 1.5 CRACK ON LT HORIZ STAB LOWER SKIN BELOW INBD BALANCE BAY. REPAIRED SKIN PER SRM.
DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD EMERGENCY EXIT SIGN LENS LOOSE. SECURED LIGHT ASSY PER MM.
AIR TURNBACK, AIRCRAFT RADAR FAILED DURING FLIGHT. REMOVED AND REPLACED INDICATOR (P/N 2041222-321) AND R/T UNIT PER MM.
EEPLS TRACK LIGHT COVER LOOSE AT ROW 14. SECURED TRACK COVER PER MM.
DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP BETWEEN ROWS 15 AND 16. RECONNECTED WIRING PER MM.
DURING SCHEDULED C3 CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED AROUND AFT SERVICE DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.
AIR TURNBACK, DURING CLIMB NR 2 ENG INGESTED BIRD. VIBRATION DEVELOPED IN ENG. C/W BIRD STRIKE INSP, BORESCOPE INSP. NO DAMAGED NOTED EXCEPT FOR NR 2 AND NR 27 FAN BLADES WHICH WERE SHINGLED. UNSHINGLED FAN BLADES PER MM.
DURING SCHEDULED RON, FOUND LT OVERWING EMERGENCY DOOR HANDLE COVERPLATE BROKEN. REMOVED AND REPLACED HANDLE PER MM.
ABORTED TAKEOFF, NR 2 ENGINE SLOW TO ACCELERATE, MAX N1 WAS 76 PERCENT TAKEOFF ABORTED AT 90 KNOTS. REMOVED AND REPLACED VARIABLE BLEED VALVE MOTOR AND MASTER BLEED VALVE (P/N 10042AV) PER MM.
NR 2 FUEL FLOW INDICATOR SPORADIC, RUNS TO ZERO AND BACK UP. REMOVED AND REPLACED FUEL FLOW INDICATOR PER MM.
DURING PREFLIGHT, FOUND FLOOR TRACK LIGHTING IN MID CABIN INOP. REPLACED AND REPAIRED WIRING AS REQUIRED PER BOEING M/M.
DURING SCHEDULED C2 CHECK, FOUND FLOORBEAM STRAP CRACKED JUST ABOVE AND O/B OF BATTERY IN E & E BAY OF BS 344. REPAIRED FLOORBEAM STRAP PER BOEING SRM.
DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY TRACK LIGHTING INOP 5 LIGHTS AT OVERWING EXIT ROW. RECONNECTED WIRING TO LIGHTS. OPS CHECK OK PER BOEING MM.
DURING WALKAROUND CHECK, FOUND EMERGENCY EGRESS LIGHTS OUT MID AIRCRAFT WIRING LOOSE AND COVERS. REINSTALLED TRACK LIGHTING WIRING PER BOEING MM.
DURING SCHEDULED 1/2D CHECK, FOUND CRACKED I/B FOREFLAP SKIN O/B OF TRACK. REPAIRED PER BOEING SRM.
DURING SCHEDULED 1/2D CHECK, FOUND CRACKED FLOORBEAM UNDER CARGO NET TIE DOWN LUG AT BS 747, RBL 14. REPAIRED PER BOEING SRM.
DURING SCHEDULED 1/2D CHECK, FOUND CRACKED INTERCOSTAL AT BS 380-400 C/L. REPAIRED PER BOEING SRM.
DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FWD SERVICE DOOR ENTRY Z ANGLE. REMOVED AND REPLACED PER BOEING SRM.
DURING SCHEDULED 1/2D CHECK, FOUND CRACKED INTERCOSTAL FWD SIDE AND AFT SIDE AT BS 540, RBL 1; AND AFT SIDE AT 540, LBL 1. REMOVED AND REPLACED PER BOEING SRM.
DURING SCHEDULED 1/2D CHECK, FOUND CORRODED RT TRANSITION ANGLE AT BS 727- 767. REMOVED AND REPLACED PER BOEING SRM.
DURING SCHEDULED SERVICE CHECK, FOUND DAMAGED CLOSURE WEB EDGE AT BS 485 ABOVE STR 25R. REPAIRED PER BOEING SRM.
DURING SCHEDULED 1/2D CHECK, FOUND CORRODED RT Z ANGLE AT BS 947 - 993, RBL 50. REMOVED AND REPLACED PER BOEING SRM.
DURING SCHEDULED 1/2D CHECK, FOUND FWD DOOR POST CRACKED AT FLOOR LEVEL BS 286. REPAIRED PER BOEING SRM.