N335SW

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK FOUND, BULKHEAD DOME WEB CRACKED AT BS 1016, STR 23R. REPAIRED WEB IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK FOUND, BULKHEAD DOME WEB CRACKED AT BS 1016, STR 7R. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK FOUND, SKIN CRACKED AT BS 520+7, BETWEEN STR 28L TO STR 28R. REPAIRED SKIN IAW EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK FOUND, SKIN CRACKED AT BS 520+4, STR 28L. REPAIRED SKIN IAW EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK FOUND, FRAME CRACKED AT BS 827, STR 27L. REPAIRED FRAME IAW SRM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK FOUND, KEEL BEAM CHORD CRACKED AT ABS 540, STR 28L. REPAIRED BEAM IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHDULED 24Y CHECK, FOUND FRAME INNER CHORD CRACKED AT BS 727A, STR 17R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 344, BETWEEN STR 23L TO STR 24L. REPAIRED FRAME IAW EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 665.5, RBL 24.5. REPAIRED CHORD IAW SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 669, LBL 24.5. REPAIRED CHORD IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 291.5+11, BETWEEN STR 16R TO STR 17R. REPAIRED SKIN IAW EA.

Part: WEB — CRACKED (HORIZ STAB) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND HORIZONTAL STABILIZER SUPPORT WEB CRACKED AT BS 1138, RBL 13.5. REPAIRED WEB IAW SWA EA.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND STIFFENER CRACKED BETWEEN WBL 104 TO WBL 125. REPAIRED STIFFENER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME IAW SRM AND DWG.

Part: RIB — CRACKED (RT WING) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING RIB UPPER CHORD CRACKED AT WBL 114, STR 2. REPAIRED CHORD IAW EO.

Part: WEB — CRACKED (NLG WW) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND NLG WHEEL WELL WEB CRACKED BETWEEN BS 227.9 TO BS 259.5, BETWEEN WL 167 TO WL 187. REPAIRED WEB IAW EO.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 520, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 2 SLAT SKIN DELAMINATED AT STA 193.40. REPAIRED SKIN IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT STIFFENER CRACKED AT BS 727, LBL 5. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 24.5. REPAIRED BEAM IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,646 hrs · 67,040 cycles

DURING SCHEDULED 24Y CHECK FOUND STRINGER CRACKED AT BS 500C, STR 8R. REPAIRED STRINGER IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW RM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE IAW RM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 16R. REMOVED AND REPLACED CLIP IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND WEB CORRODED BETWEEN BS 727B TO BS 727, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CRACKED AT BS 500B, STR 20L. REPAIRED STRINGER IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING O/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP IAW MM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT STIFFENER CRACKED AT BS 727, RBL 5. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 500C, STR 22L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FLAP — DELAMINATED (LT WING) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK FOUND, LT WING I/B AFT FLAP T/E DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 19R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 6R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 16L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 987, STR 24L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 14R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 13L TO STR 14L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 23L. REMOVED AND REPLACED CLIP IAW DWG AND SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 19L. REMOVED AND REPLACED CLIP IAW DWG AND SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 20L. REMOVED AND REPLACED CLIP IAW DWG AND SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 9L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,821 hrs · 67,233 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 15R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FLAP — DELAMINATED (RT WING) · airframe 75,669 hrs · 67,116 cycles

RIGHT WING I/B TRAILING EDGE FLAP DELAMINATED. REMOVED AND REPLACED T/E FLAP IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 75,374 hrs · 66,881 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: STRUCTURE — WORN (LE SLAT) · airframe 75,317 hrs · 66,835 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT CAN WORN. REPAIRED SLAT CAN PER EA.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 75,226 hrs · 66,769 cycles

FWD ENTRY EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 75,069 hrs · 66,648 cycles

DIVERSION - AT 37,000 FEET AFT CARGO FIRE LIGHT ILLUMINATED. AFTER CLEARING MASTER FIRE WARNING, LIGHT WENT OUT, SYSTEM TEST OK. UPON DISCHARGING FIRE FIRE BOTTLES, AFT CARGO FIRE LIGHT RE-ILLUMINATED, THEN WHEN OUT. INSPECTED FWD AND AFT CARGO COMPARTMENTS, NO SIGNS OF FIRE. REMOVED AND REPLACED AFT CARGO SMOKE DETECTORS PER MM.

Part: HINGE FITTING — BROKEN (SPOILER) · airframe 74,972 hrs · 66,563 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING I/B GROUND SPOILER O/B HINGE FITTING BROKEN. REMOVED AND REPLACED SPOILER PANEL PER MM.

Part: LENS — LOOSE (CABIN) · airframe 74,940 hrs · 66,537 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,435 hrs · 66,138 cycles

FWD EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 74,423 hrs · 66,130 cycles

DURING SCHEDULED SPV CHECK FOUND, LEFT WING NR 3 SLAT CRACKED ON THE LWR SKIN 36 INCHES I/B FROM O/D END. REPAIRED SKIN IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 73,987 hrs · 65,784 cycles

FWD F/A JUMPSEAT EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED EMERGENCY LIGHT LENS.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 73,273 hrs · 65,233 cycles

R2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,163 hrs · 65,152 cycles

DURING SCHEDULED SPV CHECK, FOUND LT OVERWING LOWER EMERGENCY EXIT LIGHT BULB INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 72,912 hrs · 64,947 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT FWD EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: CONTROL BOX — DEFECTIVE (NR 1 ENGINE) · airframe 72,439 hrs · 64,575 cycles

NR 1 ENGINE THRUST LEVER WILL NOT MOVE. REMOVED AND REPLACED NR 1 ENGINE STRUT DRUM CONTROL BOX AND THRUST CONTROL PUSH-PULL CABLE PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 72,423 hrs · 64,562 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER ASSY PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 72,423 hrs · 64,562 cycles

R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 72,415 hrs · 64,556 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 72,415 hrs · 64,556 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — BROKEN (CABIN) · airframe 72,102 hrs · 64,318 cycles

L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,211 hrs · 63,644 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 71,211 hrs · 63,644 cycles

DURING DESCENT THROUGH 7000FT, OUTFLOW VALVE WENT FULL OPEN WITH LOSS OF CABIN PRESSURE. NO AUTO FAIL LIGHT. REMOVED AND REPLACED AFT OUTFLOW VALVE PER MM.

Part: LENS — BROKEN (CABIN) · airframe 70,863 hrs · 63,386 cycles

L1 DOOR LOWER EMERGENCY EXIT DOOR LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 70,656 hrs · 63,235 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — MISSING (CABIN) · airframe 70,141 hrs · 62,864 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING AT ROW 13. INSTALLED LENS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 70,141 hrs · 62,864 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND RT EEPLS COVER CRACKED AT ROW 12. REMOVED AND REPLACED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 420, STR 1 TO STR 2L. REPAIRED SKIN PER ER.

Part: LENS — LOOSE (CABIN) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND BULLNOSE EMERGENCY LIGHT LENS LOOSE AT ROW 23 DEF. SECURED LENS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE CHORD CORRODED AT BS 227, LBL 5, WL 172. REPAIRED CHORD PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 480, STR 14R. REPAIRED FRAME PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 509C, IN SKIN LAP LOWER ROW. REPAIRED SKIN PER ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD BULKHEAD CENTER FRAME FWD SIDE CORRODED AT BS 227, BL 0. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED CLIP PER BAC DWG.

Part: SHEAR TIE — BROKEN (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE BROKEN AT BS 380, BETWEEN STR 18R TO STR 19R. REMOVED AND REPLACED SHEAR TIE SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 707 TO BS 713, BL 0. REPAIRED WEB PER ER.

Part: SHEAR TIE — BROKEN (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE BROKEN AT BS 520, BETWEEN STR 23R TO STR 24R. REMOVED AND REPLACED SHEAR TIE SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,045 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 360, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: WEB — CRACKED (CARGO DOOR) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR NR 4 WEB CRACKED AT AFT END. REMOVED AND REPLACED WEB PER BAC DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 910, STR 24L. REMOVED AND REPLACED SPLICE PER BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 15R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 43. REPAIRED BEAM PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 727E, BETWEEN STR 17R TO STR 18R. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (RT WING) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (RT WING) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 4L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (BS 994 S6R) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 994, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 619, STR 8L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (BS 994 S7R) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 994, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (BS 294 S2R) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 294, STR 2R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8L. REMOVED AND REPLACED CLIP PER SI.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 709, LBL 25. REPAIRED WEB PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 7L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 994, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 291.5, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 619, STR 8L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (BS 360 S10L) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 994, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 4L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (BS 360 S8L) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP PER SI.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 294, STR 2R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 7L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8L. REMOVED AND REPLACED CLIP PER SI.

Part: FLOORBEAM — CRACKED (BS 709) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 709, LBL 25. REPAIRED WEB PER ER.

Part: STRINGER CLIP — CRACKED (BS 291 S5R) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 291.5, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (BS 727C S7R) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP PER SI.

Part: SKIN — CORRODED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CORRODED BETWEEN BS 908 TO BS 987, STR 25R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING I/B FORE FLAP SKIN DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: FITTING — WORN (SPOILER ACTUATOR) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING NR 4 SPOILER ACTUATOR BOLTS LOOSE ON FITTING. REMOVED AND REPLACED FITTING PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 994, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CORRODED AT BS 294.5, LBL 50. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,046 hrs · 62,800 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CRACKED AT BS 312, RBL 24. REPAIRED BEAM PER SRM.

Part: ROD END — DEFECTIVE (LE SLAT) · airframe 69,959 hrs · 62,744 cycles

DECLARED EMERGENCY - L/E FLAP TRANSIT AMBER WARNING ON APPROACH - NR 5 SLAT INDICATOR NOT FULLY EXTENDED AT FLAPS 15 DEGREES, NO ROLL NOTED, SLAT VISUALLY VERIFIED FULLY EXTENDED. REMOVED AND REPLACED NR 5 SLAT ROD END PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,900 hrs · 62,703 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 503D TO BS 515D, BETWEEN STR 18R TO STR 19R. REPAIRED SKIN PER SWA EA.

Part: GASPER FAN — FAULTY (CABIN) · airframe 69,302 hrs · 62,257 cycles

REPORTED HOT RUBBER ODOR IN CABIN. FOUND GASPER FAN BEARINGS BAD. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,166 hrs · 62,144 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 310, WL 235.1. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,844 hrs · 61,897 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 727E + 10, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,844 hrs · 61,897 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 787, STR 17L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,333 hrs · 61,512 cycles

DURING SCHEDULED MV2 CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,271 hrs · 61,464 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 520, STR 15L. REPAIRED SKIN PER SWA EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 67,439 hrs · 60,880 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: LENS — MISSING (CABIN) · airframe 66,999 hrs · 60,555 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD EMERGENCY FLOOR LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: FUSE — FAULTY (HYDRAULIC SYS) · airframe 66,126 hrs · 59,943 cycles

ON APPROACH INTO AUS T/E FLAPS INDICATED 30 DEGREES, NO L/E DEVICES DEPLOYED. CYCLED FLAPS, ON SECOND APPROACH NO L/E DEVICES. REMOVED AND REPLACED L/E HYDRAULIC FUSES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,984 hrs · 59,835 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 300, STR 19R. REPAIRED SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, BETWEEN RBL 40 AND LBL 31. REPAIRED PRESSURE WEB PER SRM.

Part: STIFFENER — CRACKED (BS 178 BULKHEAD) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 178, RBL 5.7, WL 185. REPAIRED STIFFENER PER SWA EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FWD SERVICE DOOR CUTOUT UPPER FWD CORNER STUB FRAME CRACKED AT UPPER STOP FITTING. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: STRINGER — CRACKED (BS 663 S2R) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 2R CRACKED AT BS 663. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (BS 663 S3L) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 3L CRACKED AT BS 663. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (BS 663 S2L) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 2L CRACKED AT BS 663. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (BS 328 S20R) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 328, STR 20R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 360 S20R) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 20R. REPAIRED FRAME PER SWA EA.

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND VERTICAL TEE CHORD CRACKED AT BS 178, LBL 5.7, WL 184. REPAIRED CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (BS 707 S6R) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 707, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STIFFENER — CRACKED (BS 320 S21L) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 320, STR 21L. REMOVED AND REPLACED STIFFENER PER BOEING DRAWING.

Part: STRINGER CLIP — CRACKED (BS 706 S7R) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294.5, STR 3L. REPAIRED FRAME PER SWA EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FWD SERVICE DOOR CUTOUT AFT FRAME CRACKED AT LOWER DOOR STOP. REMOVED AND REPLACED FRAME PER BOEING DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 8L CRACKED AT BS 500A. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 707, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 8L CRACKED AT BS 500B. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT DOOR HANDLE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND CENTER FUEL TANK VERTICAL STIFFENER CRACKED AT STA 547, RBL 57. REMOVED AND REPLACED STIFFENER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CORRODED AT BS 1016, BL 0. REPAIRED WEB PER ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 335, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 312, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CREASED AT BS 787 TO BS 790, STR 27R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED DAL CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED DAL CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16R. REPAIRED FRAME PER SWA EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED DAL CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 291 TO BS 332, STR 17R. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED DAL CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 940, STR 17R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED DAL CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 707, RBL 24.82. REPAIRED WEB PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BS 667, LBL 24.75. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BS 665, LBL 24.75. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BS 663, LBL 24.75. REPAIRED FLOORBEAM PER SWA EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7, WL 187. REPAIRED WEB PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BS 665, RBL 24.50. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BS 670, LBL 24.75. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 709, RBL 24.82. REPAIRED WEB PER SWA EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CRACKED BETWEEN BS 540 AND BS 560, STR 17R. REMOVED AND REPLACED CREASE BEAM WEB PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 708, RBL 24.82. REPAIRED WEB PER SWA EA.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND BELTFRAME CRACKED AT BS 616, RBL 65. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17, WL 225. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 10, WL 234. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, LBL 7 TO RBL 4.5, WL 198 TO WL 206. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,754 cycles

DURING SCHEDULED BRDG CHECK, FOUND RADIAL STIFFENER CRACKED AT BS 1016, 6 0'CLOCK POSITION. REPAIRED STIFFENER PER BOEING DRAWING.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,754 cycles

DURING SCHEDULED BRDG CHECK, FOUND LONGITUDINAL FLOORBEAM VERTICAL STIFFENER CRACKED AT BS 639, RBL 46. REMOVED AND REPLACED STIFFENER PER SWA EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,754 cycles

DURING SCHEDULED BRDG CHECK, FOUND LONGITUDINAL FLOORBEAM VERTICAL STIFFENER CRACKED AT BS 639, LBL 46. REMOVED AND REPLACED STIFFENER PER SWA EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 65,883 hrs · 59,754 cycles

DURING SCHEDULED BRDG CHECK, FOUND KEEL BEAM CORRODED AT BS 540, RBL 6.50. REPAIRED KEEL BEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,883 hrs · 59,754 cycles

DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 907 AND BS 927, STR 17L. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND LEFT HORIZONTAL STABILIZER CENTER SECTION FITTING BEARING HOUSING CORRODED. REPAIRED FITTING PER SWA EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17.1. REPAIRED WEB PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 540, STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR CUTOUT LOWER FWD CORNER STUB FRAME CRACKED. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 65,883 hrs · 59,756 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, STR 27R. REPAIRED FRAME PER ACO.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 65,339 hrs · 59,337 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,337 hrs · 59,336 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 912, STR 24R. REPAIRED SKIN PER SRM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 62,078 hrs · 56,724 cycles

DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT LIGHT LENS CRACKED ABOVE AFT F/A'S SEAT. REMOVED AND REPLACED LIGHT LENS.

Part: SKIN — CRACKED (BS 500C S19R) · airframe 62,570 hrs · 57,173 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 500C S19L) · airframe 62,570 hrs · 57,173 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 19L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 62,413 hrs · 57,059 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 61,846 hrs · 56,623 cycles

R1 COCKPIT WINDOW ARCED AND CRACKED. REMOVED AND REPLACED R1 COCKPIT WINDOW ASSY AND HEAT CONTROLLER PER MM.

Part: LAMP — INOPERATIVE (CABIN) · airframe 61,839 hrs · 56,616 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: GLOWSTRIP — WORN (CABIN FLOOR) · airframe 61,575 hrs · 56,421 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DAMAGED BETWEEN ROWS 6 AND 10. REMOVED AND REPLACED STRIP PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 61,369 hrs · 56,248 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (BS 374 S19R) · airframe 61,137 hrs · 56,063 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 374, STR 19R. REPAIRED SKIN PER SRM.

Part: GLOWSTRIP — CRAZED (CABIN) · airframe 60,612 hrs · 55,632 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP CRAZED AT ROW 7 ABC TO ROW 10 ABC. REMOVED AND REPLACED EEPLS PHOTOLUMINESCENT STRIP PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 60,612 hrs · 55,632 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED LOWER INBOARD SIDE. REMOVED AND REPLACED RT AFT FLAP PER MM.

Part: LIGHT — CRACKED (EMERGENCY EXIT) · airframe 60,612 hrs · 55,632 cycles

DURING SCHEDULED C4 CHECK, FOUND LOWER EMERGENCY EXIT LIGHT CRACKED AT R1 DOOR. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (BS 750) · airframe 60,192 hrs · 55,300 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 971) · airframe 60,192 hrs · 55,300 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 971, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 730) · airframe 60,192 hrs · 55,300 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 750) · airframe 60,192 hrs · 55,300 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 19R. REPAIRED SKIN PER SWA EA.

Part: HINGE FITTING — WORN (ELEVATOR TAB) · airframe 59,635 hrs · 54,858 cycles

DURING SCHEDULED C3 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB NR 1 HINGE FITTING PER SRM.

Part: HINGE FITTING — WORN (ELEVATOR TAB) · airframe 59,635 hrs · 54,858 cycles

DURING SCHEDULED C3 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB NR 1 HINGE FITTING PER SRM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 59,229 hrs · 54,540 cycles

FWD GALLEY OUTBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 58,028 hrs · 53,579 cycles

DURING SCHEDULED 1/4D CHECK, FOUND NR 4 L/E SLAT SKIN CRACKED AT ACTUATOR OUTBOARD STOP FITTING. REPAIRED SLAT PER SRM.

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 58,028 hrs · 53,579 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LEFT MLG W/W VERTICAL STIFFENER CRACKED AT BS 663 BULKHEAD, LBL 6.15. REPAIRED STIFFENER PER SWA EA.

Part: TAB — DELAMINATED (RT WING AILERON) · airframe 58,028 hrs · 53,579 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING AILERON TAB DELAMINATED. REMOVED AND REPLACED TAB PER MM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 58,028 hrs · 53,579 cycles

DURING SCHEDULED 1/4D CHECK, FOUND NR 6 L/E SLAT SKIN CRACKED AT ACTUATOR INBOARD STOP FITTING. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 58,028 hrs · 53,579 cycles

DURING SCHEDULED 1/4D CHECK, FOUND NR 5 L/E SLAT SKIN CRACKED INBOARD OF ACTUATOR. REPAIRED SLAT PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 58,028 hrs · 53,579 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER SPLICE CHANNEL CRACKED AT BS 359, STR 15L. REMOVED AND REPLACED SPLICE CHANNEL PER SRM.

Part: MOUNT — CRACKED (R2 DOOR SLIDE) · airframe 58,028 hrs · 53,579 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD ATTACH MOUNT CRACKED. REMOVED AND REPLACED FWD MOUNT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,028 hrs · 53,579 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 21L. REPAIRED SKIN PER SRM.

Part: BELTFRAME — CRACKED (FWD CARGO) · airframe 58,028 hrs · 53,579 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 500B, ABOVE RT GENERATOR FEEDER CABLES ACCESS HOLE. REPAIRED BELTFRAME PER SWA EA.

Part: SKIN — CRACKED (BS 967) · airframe 57,727 hrs · 53,334 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 21L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (BS 519) · airframe 57,642 hrs · 53,252 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 519, STR 14L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 57,465 hrs · 53,112 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,783 hrs · 52,564 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 766, STR 18R. REPAIRED SKIN PER SRM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 56,783 hrs · 52,564 cycles

DURING SCHEDULED C4 CHECK, LT & RT ELEVATOR TABS FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED LT & RT ELEVATOR TABS NR 1 HINGE BUSHINGS & HARDWARE.

Part: LATCH — OUT OF ADJUST (COCKPIT) · airframe 55,692 hrs · 51,700 cycles

F/O'S ESCAPE SLIDE ROPE COVER RELEASE KNOB, STUCK. ADJUSTED AND LUBED LATCH PER MM.

Part: SKIN — WORN (FUSELAGE) · airframe 45,703 hrs · 41,466 cycles

DURING SCHEDULED SERVICE CHECK, FOUND UPPER FUSELAGE SKIN BETWEEN LEFT & RIGHT BS 870 AND BS 890, WORN. REPAIRED SKIN PER EA.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,208 hrs · 51,332 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 54,905 hrs · 51,102 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING T/E OUTBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED LT FORE FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,565 hrs · 54,359 cycles

DURING SCHEDULED SERVICE CHECK, FOUND SKIN AT BS 530, STRINGER 15R, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,086 hrs · 40,184 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 760, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 44,086 hrs · 40,184 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 44,086 hrs · 40,184 cycles

DURING SCHEDULED C1 CHECK, FOUND RT WING NR 4, 5, 6 L/E SLATS SKIN CRACKED. REPAIRED RT WING L/E SLATS SKIN PER EA.

Part: HOOK — OUT OF ADJUST (L1 DOOR) · airframe 52,237 hrs · 48,920 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVAC SLIDE LATCH HOOK WITH TO LARGE OF A GAP. ADJUSTED L1 DOOR EVAC SLIDE HOOK PER MM.

Part: CABLE — MISROUTED (L2 DOOR) · airframe 52,237 hrs · 48,920 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,237 hrs · 48,920 cycles

DURING SCHEDULED C3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,272 hrs · 48,181 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 925, STR 25R. REPAIRED SKIN PER SRM.

Part: CIRCUIT CARD — FAULTY (E/E BAY) · airframe 50,250 hrs · 47,352 cycles

AIR TURNBACK, LANDING GEAR WOULD NOT RETRACT. REMOVED AND REPLACED M991 CARDS ON E-11 LANDING GEAR LOGIC SHELF.

Part: FLOORBEAM — CRACKED (CABIN) · airframe 49,877 hrs · 47,062 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CABIN FLOORBEAM CRACKED, BS 947.5, LBL 53. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (CARGO BAY) · airframe 49,877 hrs · 47,062 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 500C + 16, LBL 19. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,877 hrs · 47,062 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CRACKED (AFT CABIN) · airframe 49,877 hrs · 47,062 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED AT BS 661, BL 0. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 49,877 hrs · 47,062 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 794, RBL 3. REPAIRED FLOORBEAM PER SWA EA.

Part: RIB — CRACKED (LT/RT WING) · airframe 49,877 hrs · 47,062 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BOTH LT/RT WINGS RIBS CRACKED ON THE LOWER SECTION AT WBL 135.5. REPAIRED LOWER CHORDS PER SWA EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 49,877 hrs · 47,062 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM CORRODED FROM BS 390 TO BS 500B, LT SIDE. REPAIRED CREASE BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FWD CARGO) · airframe 49,877 hrs · 47,062 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,877 hrs · 47,062 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIPS CRACKED (4 EA) AT BS 827 AT STR 25L, BS 847 AT STR 22L, BS 787 AT STR 25L & BS 807 AT STR 25L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 49,877 hrs · 47,062 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM CORRODED FROM BS 390 TO BS 500C + 17, RT SIDE. REPAIRED CREASE BEAM PER SRM.

Part: LIGHT — INOPERATIVE (AFT CABIN) · airframe 49,653 hrs · 46,890 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT AT FLOOR LEVEL INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY AND BATTERY PACK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,275 hrs · 46,582 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 767, STRINGER 14R. REPAIRED SKIN PER ERO.

Part: STRAP — CRACKED (FUSELAGE) · airframe 49,273 hrs · 46,580 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BEAR STRAP CRACKED AT BS 360, STR 4R. REPAIRED BEAR STRAP PER SRM AND ERO.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,273 hrs · 46,580 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER 11R CRACKED AT BS 530. REPAIRED STRINGER PER ERO.

Part: FRAME — CRACKED (CABIN) · airframe 49,273 hrs · 46,580 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND PAX WINDOW FRAMES CRACKED AT BS 530, STR 12R AND BS 450, STR 5R. REMOVED AND REPLACED BOTH WINDOW FRAMES PER SRM AND SWA AE.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 49,273 hrs · 46,580 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER SPLICES CRACKED (2 EA) AT STR 4L, BS 360 & BS 908. REMOVED AND REPLACED STRINGER SPLICES PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,273 hrs · 46,580 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, BELOW STR 14L. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,273 hrs · 46,580 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 867, BELOW STR 13R AND BS 847, BELOW STR 14R. REPAIRED SKIN PER SWA ACO AND ERO.

Part: COVER — CRACKED (CABIN) · airframe 48,594 hrs · 46,052 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS CRACKED BETWEEN ROWS NR 6 AND NR 9. REMOVED AND REPLACED COVERS PER MM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 47,687 hrs · 45,323 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED OTBD T/E AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,687 hrs · 45,323 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, ABOVE STR 14R. REPAIRED SKIN PER SRM.

Part: BRAKE — OUT OF ADJ (MLG) · airframe 45,235 hrs · 43,338 cycles

BRAKES SPONGY, FOUND THE CLEARANCE BETWEEN THE LEFT NORMAL BRAKE METERING VALVE PLUNGER AND ROLLER OUT OF TOLERANCE. ADJUSTED SAME GAP TO WITHIN TOLERANCE IAW MM. PERFORMED BRAKE SYSTEM TEST AND A/C TAXI CHECK, BRAKES OPERATE NORMAL.

Part: SLAT — CRACKED (LH WING) · airframe 34,564 hrs · 32,374 cycles

DURING SCHEDULED C3 CHECK, FOUND ( 7 EA ) CRACKS AT # 2 L/E SLAT ON AFT ROW OF RIVETS LOWER T/E. REPAIRED SLAT PER SWA RA 1-357-1125.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,564 hrs · 32,374 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED 2.5 INCHES AT BS 520, STR 12L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 43,878 hrs · 42,183 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED EMERGENCY EVAC SLIDE ASSY PER MM.

Part: COVER — LOOSE (CABIN FLOOR) · airframe 43,878 hrs · 42,183 cycles

EEPLS COVER NOT SECURED AT ROW 8. SECURED COVER PER MM.

Part: COALESCER BAG — DIRTY (A/C BAY) · airframe 42,673 hrs · 41,168 cycles

AIR TURNBACK. SMOKE AND FUMES IN CABIN. FOUND WATER SEPARATOR BAGS DIRTY. REMOVED AND REPLACED BAGS AND RAN BOTH ENGINES AT 75 PERCENT N1 FOR 10 MINS. NO SMOKE OR FUMES NOTED. REPLACED WATER SEPARATOR BAGS AGAIN FOR MX CONVENIENCE OP''S CHECK GOOD PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,024 hrs · 40,638 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIES CORRODED AT BS 767, STR 27R & BS 787, STR 26R TO STR 27R. REPAIRED SHEAR TIES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,024 hrs · 40,638 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FRAMES CRACKED AT BS 440, STR 24R & BS 492.4, STR 24R. REPAIRED FRAMES PER SRM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 40,303 hrs · 39,148 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUST. REINSTALLED SLIDE ASSY PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 40,303 hrs · 39,148 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: TRANSMITTER — MALFUNCTIONED (HYD MODULE) · airframe 39,678 hrs · 38,565 cycles

AIR TURNBACK -B- SYS HYD ELECTRIC PUMP LOW PRESS LIGHT ILLUMINATED. ALL HYD QTY AND PRESS INDICATORS NORMAL. R&R B-SYS HYD PRESS TRANSMITTER AND -B- SYS HYD ELECTRIC PUMP PER MM.

Part: AXLE — SHEARED (NLG)

ON ARRIVAL TO GATE, FOUND RT NLG TIRE/WHEEL ASSY MISSING. FOUND NLG RT AXLE SHEARED JUST OUTBOARD OF INNER BEARING. REMOVED AND REPLACED LOWER STRUT ASSY AND REMOVED AND REPLACED BOTH NLG TIRE/WHEEL ASSY'S PER MM.

Part: FRAME — CRACKED (R1 DOORWAY)

DURING SCHEDULED C1 CHECK, FOUND A CRACK 3.7 INCH AFT LOWER CORNER OF R1 DOOR FRAME OF FUSELAGE. REPAIRED FRAME PER SRM.

Part: LIGHT — LOOSE (CABIN)

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT LIGHT ASSY LOOSE ABOVE 5D. REPAIRED EMERGENCY LIGHT ASSY PER BOEING MM.\N\N\N\N\N\N\N\NREPLACED LIGHT & LENS ASSY'S AS PER BOEING MM.\N\N\N\N\N\N\N\N\N\NREPAIRED PER BOEING SRM.\N\N\N\N\N\N\N\N\N\N\N\N\N\N\N\NREPAIRED PER BOEING SRM.

Part: SHEAR WEB — CORRODED (BS 472-480)

DURING SCHEDULED D-CHECK, FOUND CORROSION AT BS 472 TO 480, RBL 68, WL 208 ON SHEAR WEB. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 736-947)

DURING SCHEDULED D-CHECK, FOUND CORRODED AFT CARGO FLOOR SUPPORT ZEE ANGLE LBL 21, UPPER SURFACE BETWEEN BS 736 AND BS 947. REMOVED AND REPLACED PER BOEING SRM.

Part: CHORD — CORRODED (BS 270)

DURING SCHEDULED D-CHECK, FOUND CORRODED Z-CHORD AT BS 270 RBL 11, LBL 11 WL 208. REPAIRED PER BOEING SRM.

Part: SKIN — WORN (BS 967-987)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE CROWN SKIN HAS A WORN AREA AT BS 967 TO 987, RBL 12 COMMON TO DORSAL FIN, BS 967 TO 986 LBL 12, 7, BS 920 TO 967 RBL 10. REPAIRED PER BOEING SRM.

Part: STRAP — CORRODED (BS 794 - 850)

DURING SCHEDULED D CHECK, FOUND TEAR STRAP CORRODED AT BS 794 TO 850, RBL 20.5. REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 727/773)

DURING SCHEDULED D-CHECK, FOUND CORRODED AFT CARGO FLOOR SUPPORT AROUND FASTENER HOLE AT BS 727D+5, RBL 8, WL 155, BS 727D+5, RBL 3, WL 155, AND BS 773, LBL 2, WL 175. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 827)

DURING SCHEDULED D-CHECK, FOUND CRACKED FUSELAGE FRAME AT BS 827, BETWEEN STR 8 AND 9 RT AND BS 827, BETWEEN STR 8 AND 9 RT. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 787)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME PAX CABIN UPPER LOBE STRUCTURE, RIGHT HAND SIDE AT BS 787 BETWEEN STR 8 AND 9. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 344-360)

DURING SCHEDULED D-CHECK, FOUND CRACKED INTERCOSTAL AT BS 344 TO 360, LBL 0, WL 208 AND BS 312 TO 328, RBL 35, WL 208. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — DAMAGED (BS 328)

DURING SCHEDULED D-CHECK, FOUND DAMAGED FLOORBEAM WEB AT BS 328, RBL 35, WL 206. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 440)

DURING SCHEDULED D-CHECK, FOUND CRACKED FUSELAGE FRAME AT BS 787, BETWEEN STR 9 AND 9L, BS 907 BETWEEN STR 8 AND 9L AND BS 867 BETWEEN STR 8 AND 9L. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 440)

DURING SCHEDULED D-CHECK, FOUND CRACKED FUSELAGE FRAME AT RT HAT RACK SUPPORT BS 440 BETWEEN STR 8 AND STR 9 RT. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 727/773)

DURING SCHEDULED D-CHECK, FOUND CORRODED AFT CARGO FLOOR SUPPORT AROUND FASTENER HOLE AT BS 727E+3, LBL 2, WL 155, BS 773, LBL 11, WL 156, AND BS 754, RBL 3, WL 155. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 992)

DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 992, LBL 34, WL 208. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 727/747)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME PAX CABIN UPPER LOBE STRUCTURE LEFT HAND AT BS 727D BETWEEN STR 8 AND 9, BS 727D RIGHT HAND SIDE BETWEEN STR 8 AND 9 AND BS 747 RIGHT HAD SIDE BETWEEN STR 8 AND 9. REPAIRED PER BOEING SRM.

Part: BEAM — CORRODED (BS 400-420)

DURING SCHEDULED D-CHECK, FOUND CORRODED PASSENGER COMPARTMENT, SHEAR WEB, CREASE BEAM, BETWEEN BS 400 TO 420, WL 208, LBL 64 TO 71, AND BS 460 TO 480, WL 208, LBL 69. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 773)

DURING SCHEDULED D-CHECK, FOUND CORRODED AFT CARGO FLOOR SUPPORT AROUND FASTENER HOLE AT BS 773, RBL 8, WL 156. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 792-801)

DURING SCHEDULED D-CHECK, FOUND CORRODED AFT CARGO FLOOR SUPPORT AT BS 792 TO 801, RBL 8, WL 157. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 993)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 993, LBL 25 TO 28, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 480/500)

DURING SCHEDULED D-CHECK, FOUND CRACKED FUSELAGE FRAME AT BS 480, BETWEEN STR 8 AND 9 RT, BS 500A BETWEEN STR 8 AND 9 RT AND BS 500C BETWEEN STR 8 AND 9 RT. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 344)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT LOWER END CORNER AT BS 344, LBL 37, WL 285. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 1037)

DURING SCHEDULED D-CHECK, FOUND DENTED AT BS 1037 BETWEEN STRS 12 AND 14 LT (SKIN). REPAIRED PER BOEING SRM.

Part: ANGLES — CORRODED (GALLEY DOORWAY)

DURING SCHEDULED D-CHECK, FOUND CORRODED FWD GALLEY DOORWAY LOWER SILL SUPPORT Z-ANGLES, NR 1, 3, 4. REPAIRED PER BOEING SRM.

Part: STRINGER — DAMAGED (BS 500)

DURING SCHEDULED D-CHECK, FOUND STRINGER 28L, AT BS 500+7 EFFECTS INSTALLATION OF VHF SUPPORT STRUCTURE MODIFICATION. REPAIRED SECTION OF STRINGER PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 344-360)

DURING SCHEDULED D-CHECK, FOUND CORRODED INTERCOSTAL AT BS 344 TO 360, LBL 11, WL 208. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACKED AT BS 178 BULKHEAD WEB WL 197 TO 201.4, RBL 4.7. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — WORN (VERT STAB)

DURING SCHEDULED D-CHECK, FOUND RT FUSELAGE TO VERTICAL STAB SKATE ANGLE WORN. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACKED BS 178, WL 207 LBL 55, 178 BULKHEAD SIDE CHORD, BS 178 WL 207, RBL 55, 178 BULKHEAD SIDE CHORD AND BS 178 BULKHEAD, LBL 1, WL 185 HAS 1 CRACKED. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOOR — CORRODED (BS 1030)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR WEB AT BS 1030, LBL 9, WL 208. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 860)

DURING SCHEDULED D-CHECK, FOUND CORRODED AFT CARGO FLOOR SUPPORT AROUND FASTENER HOLE AT BS 860, RBL 8, WL 164. REPAIRED PER BOEING SRM.

Part: WEB — DAMAGED (BS 500)

DURING SCHEDULED D-CHECK, FOUND DAMAGED WEB AT BS 500 TO 500A, RBL 6.5, WL 147. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED D-CHECK, FOUND CORRODED FLOORBEAM AT BS 312, LBL 10 TO 12, RBL 10 TO 12, LBL 21. REPAIRED PER BOEING SRM.

Part: STRAP — CORRODED (BS 1015-1030)

DURING SCHEDULED D-CHECK, FOUND CORRODED STRAP AT BS 1015 TO 1030, LBL 3 WL 208. REPAIRED PER BOEING SRM.

Part: STIFFENER — CRACKED (BS 328)

DURING SCHEDULED D-CHECK, FOUND CRACKED VERTICAL STIFFENER AT BS 328 FLOORBEAM (FWD SIDE), RBL 35, WL 20. REPAIRED PER BOEING SRM.

Part: WEB — CORRODED (BS 315)

DURING SCHEDULED D-CHECK, FOUND CORRODED WEB AT BS 315, RBL 60, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND CRACK INDICATIONS AT BS 178 BULKHEAD WEB WL 197.3 TO 201.9, LBL 4.7. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — WORN (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND LT FUSELAGE TO VERTICAL STAB SKATE ANGLE IS WORN. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED D CHECK, FOUND CORRODED FLOORBEAM AT BS 986, LBL 4-43, WL 208 AROUND FASTENER HOLES UPPER AND LOWER SIDES. REMOVED AND REPLACED PER BOEING MM.

Part: ANGLE — CRACKED (HORIZ STAB)

DURING SCHEDULED D CHECK, FOUND LT HORIZ STAB WEB AT HSS 175.5 HAS CRACKED L ANGLE STIFFENER APPROX 30 AFT OF FRONT SPAR. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 947)

DURING SCHEDULED D CHECK, FOUND CORRODED AFT CARGO FLOOR SUPPORT ANGLE UPPER SURFACE IN SEVERAL AREAS, AT BS 947, LBL 21 TO RBL 21, WL 179. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 983)

DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 983, LBL 18, WL 208. REMOVED AND REPLACED PER BOEING MM.

Part: ANGLE — CRACKED (BS 328)

DURING SCHEDULED D CHECK, FOUND CRACKED ANGLE AT BS 328, WL 200-207, LBL 45, FORWARD SIDE OF FLOORBEAM AND AT BS 328, WL 200-207, LBL 45 AFT SIDE OF FLOORBEAM. REMOVED AND REPLACED PER BOEING SRM.

Part: TIP — CRACKED (HORIZ STAB)

DURING SCHEDULED D CHECK, FOUND RT HORIZONTAL STAB TIP HAS 2 CRACK INTERNAL AND EXTERNAL SURFACES 4 FROM L/E AT LOWER EDGE. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 380-400)

DURING SCHEDULED D CHECK, FOUND CRACKED L ANGLE BETWEEN BS 380 AND 400, BL 0, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: STOP PADS — WORN (EMERG EXIT)

DURING SCHEDULED D CHECK, FOUND LEFT AND RIGHT EMERGENCY EXIT HATCH STOP PADS WORN 6 EACH. REMOVED AND REPLACED PER BOEING MM.

Part: SKIN — DENTED (BS 500)

DURING SCHEDULED D CHECK, FOUND DENTED FUSELAGE SKIN AT BS 500A+12 STR 23L. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (NR 7 SPOILER)

DURING SCHEDULED D CHECK, FOUND NR 7 SPOILER UPPER SURFACE HAS 2 DENT 14 FROM I/B END 5 FROM T/E. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (NR 4 LE SLAT)

DURING SCHEDULED D CHECK, FOUND CRACKED NR 4 SLAT ON LOWER SKIN, O/B OF PUSHROD SITTING. REPAIRED PER TRAMCO EO NR 98-0440.

Part: SKIN — DENTED (BS 500)

DURING SCHEDULED D CHECK, FOUND DENTED FUSELAGE SKIN, AT BS 500A +1 BETWEEN STRINGERS 21R AND 22R. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED D CHECK, FOUND CORRODED FLOORBEAM AT BS 986 RBL 26-BL 0 WL 208 AROUND FASTENER HOLES UPPER AND LOWER SIDE. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED D CHECK, FOUND CORRODED FLOORBEAM AROUND NUTPLATE AT BS 986 RBL 43, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 180)

DURING SCHEDULED D CHECK, FOUND CRACKED WEB AT BS 180 WL 208, RBL 24; BS 180, WL 208, LBL 24. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND CRACKED INDICATIONS NOTED AT BS 178 BULKHEAD WEB AT WL 209.7 TO 212.6 LBL 4.7; AND WL 209.5 TO 212.7 RBL 4.7. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND CRACKED INDICATIONS NOTED AT BS 178 BULKHEAD WEB AT WL 209.3 TO 212.7 LBL 6.7; AND BS 178 WL 212 TO 212.9 RBL 6.7. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — CRACKED (RT MLG WW)

DURING SCHEDULED BC3 CHECK, FOUND STRINGER 18A IN RT W/W CRACKED. REPAIRED PER ACO 1-353-1800.

Part: SKIN — CRACKED (BS 881-885)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE CRACKED AT BS 881 TO 885 BETWEEN STR 24R AND 25R. REPAIRED PER BOEING SRM.

Part: CARD — FAILED (E/E BAY)

AFTER TAKEOFF, AND NORMAL GEAR RETRACTION, GEAR HANDLE CENTERED. GEAR EXTENDED WITH BOTH RED AND GREEN LIGHTS. RAISED HANDLE, GEAR RETRACTED, BUT RED UNSAFE LIGHTS REMAINED ON. GEAR WAS AGAIN EXTENDED AND RETRACTED BUT TOOK EXCESSIVE AMOUNT OF TIME TO RETRACT. REPLACED PC CARD 986 AND PERFORMED RETRACT TEST PER BOEING M/M.

Part: STRAP — CRACKED (BS 312)

DURING SCHEDULED BC1 CHECK, FOUND FLOORBEAM SUPPORT STRAP CRACKED AT BS 312, AT BL 0 AND RBL 33 AND 46. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED BC1 CHECK, FOUND A 1.5 FUSELAGE SKIN CRACK AT E&E COOLIN AND DUCT CUTOUT. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 747)

DURING SCHEDULED BC1 CHECK, FOUND A 4 FUSELAGE SKIN CRACK 4 FWD OF OS BS 747, S26R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING RON, FOUND CRACK AT AFT SERVICE DOOR LOWER HINGE CUTOUT, UNDER PRODUCTION MOD DOUBLER. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 847)

DURING SCHEDULED TERMINAL CHECK, FOUND FUSELAGE SKIN CRACK AT BS 847, S28R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 762)

DURING SCHEDULED BC2 CHECK, FOUND A 3.25 INCH FUSELAGE SKIN CRACK AT BS 762, ABOVE S26R. REPAIRED PER BOEING SRM.

Part: CONNECTOR — LOOSE (NR 2 ENGINE)

PRECAUTIONARY SHUTDOWN OF NUMBER 2 ENGINE, DUE TO OIL QUANTITY AND PRESSURE INDICATION FLUCTUATIONS. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED AND DISCOVERED ENGINE OIL QUANTITY WAS NORMAL AND NO LEAKS WERE NOTED. REPLACED OIL QUANTITY TRANSMITTER CANNON PLUG PER M/M.

Part: CONNECTOR — LOOSE (NR 2 ENGINE)

EXPERIENCED NUMBER 2 ENGINE LOW OIL QUANTITY INDICATION. CREW PERFORMED ENGINE SHUTDOWN PROCEDURES. AIRCRAFT DIVERTED AND LANDED IN RNO WITHOUT INCIDENT. INSPECTED AND FOUND ENGINE OIL QUANTITY NORMAL. CLEANED AND RESEATED OIL PRESSURE TRANSMITTER CANNON PLUG AND REPLACED INDICATOR PER BOEING M/M.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED BC4 CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 22R INOP. REPLACED LIGHT ASSEMBLY PER BOEING M/M.

Part: EEL WIRE — BROKEN (CABIN)

FIFTEEN MINUTES BEFORE PUSHBACK, EMERGENCY LIGHTS ILLUMINATED WITH NORMAL AIRCRAFT POWER APPLIED AND SWITCH IN ARMED POSITION. INSPECTED AND REPAIRED WIRE ON AFT GALLEY EMERGENCY LIGHT SWITCH PER BOEING MM.

Part: EEL BALLAST — INOP (RT OVERWING)

DURING SCHEDULED SERVICE CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED LIGHT BALLAST ASSEMBLY PER BOEING M/M.