N334SW

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,646 hrs · 67,040 cycles

DURING SCHEDULED 24Y CHECK, BULLNOSE EMERGENCY LIGHT ROW 20 AND 21 LT INOP. REMOVED AND REPLACED BULB MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,646 hrs · 67,040 cycles

DURING SCHEDULED 24Y CHECK, FOUND EMERGENCY LIGHT AFT LAV INOP. REMOVED AND REPLACED BULB ACO.

Part: SKIN — CRACKED (L1 DOOR) · airframe 75,385 hrs · 67,974 cycles

DURING SCHEDULED 24Y CHECK, FOUND L1 DOOR INTERNAL SKIN CRACKED AT UPPER HINGE. REPAIRED SKIN PER SRM & BAC DRAWING.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 75,385 hrs · 67,974 cycles

DURING SCHEDULED 24Y CHECK, FOUND L1 DOOR FRAME CRACKED. REPAIRED FRAME PER EA.

Part: SPLICE — BROKEN (CABIN) · airframe 75,646 hrs · 67,040 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN SPLICE BROKEN. REPAIRED WIRE SPLICE PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 75,646 hrs · 67,040 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM WEB CORRODED BETWEEN BS 420 TO BS 440, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

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

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 328, BETWEEN STR 20R TO STR 21R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

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

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

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

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 344, STR 17R. REPAIRED SKIN IAW EA.

Part: PANEL — CRACKED (NLG WW) · airframe 75,646 hrs · 67,040 cycles

DURING SCHEDULED 24Y CHECK, FOUND NLG WHEEL LT SIDEWALL PANEL CRACKED AT STA 243.7. REPAIRED SKIN PER EA.

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

DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO PIT DOOR CUTOUT AREA LOWER AFT INNER AREA TORQUE BOX SKIN CRACKED. REMOVED AND REPLACED SKIN PER SRM AND DWG.

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

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 20R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

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

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 727A, STR 17R. REPAIRED FRAME IAW DWG.

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

DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO COMPARTMENT FRAME CRACKED AT BS 492.4. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 75,646 hrs · 67,040 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT OUTBD FWD FLAP INBD SIDE DEMALINATED. REMOVED AND REPLACED DAMAGED SKIN PER MM.

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

DURING SCHDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 344, BETWEEN STR 24R TO STR 25R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,646 hrs · 67,040 cycles

DURING SCHEDULED 24Y CHECK FOUND FWD CARGO COMPARTMENT FRAME CORRODED AT BS 500C, BETWEEN STR 28R TO STR 28L. REPAIRED FRAME IAW SRM AND DWG.

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

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

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

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO COMPARTMENT LOWER CORNER TORQUE BOX SKIN CRACKED. REMOVED AND REPLACED SKIN PER SRM.

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

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM BRACKET CRACKED AT BS 540, RBL 1. REMOVED AND REPLACED BRACKET PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 75,646 hrs · 67,040 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOOR WEB CORRODED BETWEEN BS 400 TO BS 420, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SKIN — CRACKED (R2 DOOR) · airframe 75,646 hrs · 67,040 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT GALLEY R2 DOOR CRACKED AT INNER MID SKIN. REPAIRED SKIN IAW SRM.

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

DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM BRACKET CRACKED AT BS 540, LBL 1. REMOVED AND REPLACED BRACKET PER SRM.

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

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 312+10, STR 20L. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

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

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 10L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

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

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 388, STR 8R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

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

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 10L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

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

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

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

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 15R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

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

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

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

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,408 hrs · 66,849 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 639, LBL 63. REPAIRED FRAME IAW ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,408 hrs · 66,849 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 639, BETWEEN STR 14L TO STR 16L. REPAIRED FRAME IAW ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,408 hrs · 66,849 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT BS 500C, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,013 hrs · 67,044 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 663.75, RBL 24.5. REPAIRED CHORD IAW EA.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 74,631 hrs · 66,259 cycles

L2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 73,443 hrs · 65,380 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR FWD SIDE UPPER STUB FRAME CRACKED. REMOVED AND REPLACED SUBFRAME PER SRM AND BAC DWG.

Part: FITTING — CRACKED (R1 DOOR) · airframe 73,443 hrs · 65,380 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR UPPER HINGE HOUSING CRACKED AT BS 296, RBL 55.36. REMOVED AND REPLACED FITTING PER SRM AND BAC DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 73,443 hrs · 65,380 cycles

DURING SCHEDULED SPV CHECK, FOUND SUBFRAME CRACKED AT LOWER SIDE OF R1 DOOR. REMOVED AND REPLACED SUBFRAME PER SRM AND BAC DWG.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 73,443 hrs · 65,380 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 297, STR 17R. REMOVED AND REPLACED WEB PER SRM AND BAC DWG.

Part: LENS — BROKEN (CABIN) · airframe 72,496 hrs · 64,678 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 72,496 hrs · 64,678 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS DAMAGED AT ROW 22. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 72,496 hrs · 64,678 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS DAMAGED BETWEEN ROW 8 TO ROW 9. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 72,024 hrs · 64,307 cycles

DURING SCHEDULED MV3 CHECK, FOUND AFT I/B EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: LENS — MISSING (CABIN) · airframe 72,000 hrs · 64,290 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,968 hrs · 64,263 cycles

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

Part: FLAP — DAMAGED (RT WING) · airframe 71,637 hrs · 64,016 cycles

RT WING UPPER T/E AFT FLAP DAMAGED. REMOVED AND REPLACED O/B AFT FLAP PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 70,206 hrs · 62,935 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 360, BETWEEN STR 19R TO STR 20R. REPAIRED FRAME PER ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 706 TO BS 714, BBL 0.07. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 20R TO STR 21R. REPAIRED FRAME PER SRM & EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND RT KEEL BEAM CORRODED AT BS 525. REPAIRED KEEL BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16R. REPAIRED FRAME PER ACO.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING INBOARD T/E FORE FLAP LOWER SKIN PUNCTURED. REPAIRED FLAP PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM ANGLE CRACKED AT BS 694, LBL 0.07. REPAIRED ANGLE PER SRM AND ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 13R. REPAIRED FRAME PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, LBL 24.8. REPAIRED FLOORBEAM PER SRM AND ACO.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 365, STR 21R. REPAIRED STRINGER PER SRM AND ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 707, LBL 24.8. REPAIRED FLOORBEAM PER SRM AND ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 20R TO STR 21R. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 13R. REPAIRED FRAME PER EA.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 25L DAMAGED AT BS 400. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP DAMAGED AT BS 500C, STR 23R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 2L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 6L TO STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND LT CREASE BEAM CORRODED AT BS 500B+7. REPAIRED CREASE BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 8L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 15R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 15L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 4R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

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

Part: BRACKET — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM BRACKET CRACKED AT BS 727B, LBL 45.5. REMOVED AND REPLACED BRACKET PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 1L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 2R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 948, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,724 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED BETWEEN BS 380 TO BS 400, STR 15R. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,734 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 807, STR 18L. REPAIRED SKIN PER ACO 7833.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,939 hrs · 62,734 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 807, STR 19L. REPAIRED SKIN PER ACO 7833.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,936 hrs · 62,723 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 943, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,834 hrs · 62,651 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 755, STR 20L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,174 hrs · 62,160 cycles

DURING SCHEDULED CV CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 68,473 hrs · 61,655 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR LOWER FWD EMERGENCY EXIT LIGHT INOP. REPAIRED WIRE PER WDM.

Part: LENS — LOOSE (CABIN) · airframe 68,355 hrs · 61,566 cycles

RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,275 hrs · 61,510 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER CUTOUT, BS 291.5, WL 260. REPAIRED SKIN PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,275 hrs · 61,510 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 291.5, WL 260. REPAIRED FRAME PER AAR EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 68,294 hrs · 61,522 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING O/B T/E FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 68,294 hrs · 61,522 cycles

DURING SCHEDULED HC2 CHECK, FOUND EMERGENCY EXIT LIGHT INOP ABOVE L1 DOOR. REMOVED AND REPLACED BATTERY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,275 hrs · 61,510 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 290, BETWEEN STR 9R TO STR 10R, WL 258. REPAIRED FRAME PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,275 hrs · 61,510 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,275 hrs · 61,510 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BS 291, BETWEEN WL 233 TO WL 234. REPAIRED SKIN PER AAR EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,275 hrs · 61,510 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 348, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,275 hrs · 61,510 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,275 hrs · 61,510 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14L TO STR 13L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,275 hrs · 61,510 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,275 hrs · 61,510 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 290, STR 10L. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,275 hrs · 61,510 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,275 hrs · 61,510 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,275 hrs · 61,510 cycles

DURING SCHEDULED SPV CHECK, FOUND RT SIDE EMERGENCY EXIT DOOR SIDEWALL LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,294 hrs · 60,090 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 933, STR 25R. REPAIRED SKIN PER SRM.

Part: BATTERY — FAULTY (CABIN) · airframe 65,728 hrs · 59,698 cycles

AFT CABIN EMERGENCY EXIT LIGHTS WILL NOT TURN OFF. REMOVED AND REPLACED BATTERY PACK AND BATTERY CHARGER PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,694 hrs · 59,676 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR UPPER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,590 hrs · 59,592 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D, STR 13L. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 65,590 hrs · 59,592 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 65,045 hrs · 59,195 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT FWD CARGO DOOR CUTOUT LOWER CORNER BS 451. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,045 hrs · 59,195 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, LBL 3. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,045 hrs · 59,195 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 14R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,045 hrs · 59,195 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,045 hrs · 59,195 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,045 hrs · 59,195 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,045 hrs · 59,195 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,045 hrs · 59,195 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,045 hrs · 59,195 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,045 hrs · 59,195 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259, STR 19R. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,045 hrs · 59,195 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 10L CRACKED AT BS 296. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,045 hrs · 59,195 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,045 hrs · 59,195 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,045 hrs · 59,195 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 27L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,045 hrs · 59,195 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259.5, BETWEEN STR 21L AND STR 23L. REPAIRED SKIN PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,045 hrs · 59,195 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,045 hrs · 59,195 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 23L. REPAIRED SKIN PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,045 hrs · 59,195 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BS 661, LBL 25. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,045 hrs · 59,195 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BS 664, LBL 25. REPAIRED FLOORBEAM PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,054 hrs · 59,195 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CACKED AT BS 767, STR 23R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,054 hrs · 59,195 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,054 hrs · 59,195 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 24R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 65,054 hrs · 59,195 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 616, STR 17L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,045 hrs · 59,195 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,045 hrs · 59,195 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,933 hrs · 59,114 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504D, STR 15R. REPAIRED SKIN PER SWA EA.

Part: CONTROLLER — OVERHEATED (CABIN PRESSURE) · airframe 64,247 hrs · 58,576 cycles

AIR TURNBACK / DECLARED EMERGENCY. PASSING 10,000 MSL CREW REPORTED STRONG BURNING SMELL IN CABIN. SMELL INTENSIFIED AND REMAINED UNTIL AFTER LANDING AND SHUT DOWN. FOUND CABIN PRESSURE CONTROLLER OVERHEATING. REMOVED AND REPLACED PRESSURE CONTROLLER PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 63,366 hrs · 57,892 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: STRUCTURE — CRACKED (NR 2 SLAT) · airframe 63,109 hrs · 57,692 cycles

DURING SCHEDULED C3 CHECK, FOUND LEFT WING NR 2 L/E SLAT CRACKED AT OUTBOARD TRACK. REPAIRED SLAT PER SWA EA.

Part: SKIN — CRACKED (L/E SLAT) · airframe 62,273 hrs · 56,997 cycles

DURING SCHEDULED C2 CHECK, FOUND RIGHT WING NR 4 L/E SLAT LOWER T/E SKIN CRACKED. REPAIRED SLAT PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,703 hrs · 56,564 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 804, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,703 hrs · 56,564 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 784, STR 20L. REPAIRED SKIN PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,629 hrs · 55,737 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT BULL NOSE LIGHT INOP AT ROW 17 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: CABLE — WORN (NR 2 ENGINE) · airframe 60,512 hrs · 55,645 cycles

NR 2 ENGINE SLOW TO SPOOL UP ON ADVANCING TO TAKEOFF THRUST, APPROX 5 TO 8 SECONDS. ON LANDING AGAIN TOOK 5 TO 8 SECONDS TO SPOOL UP AND CAUSED DIRECTIONAL CONTROL PROBLEMS. REMOVED AND REPLACED NR 2 ENGINE VSV FEEDBACK CABLE PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,450 hrs · 55,592 cycles

DURING SCHEDULED SERVICE CHECK, AFT CABIN EMERGENCY EXIT LIGHTS INOP DURING TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 60,322 hrs · 55,489 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT AFT ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: BOLT — WORN (ELEVATOR TAB) · airframe 60,322 hrs · 55,489 cycles

DURING SCHEDULED C4 CHECK, RT ELEVATOR NR 1 TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB BOLT PER MM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 60,322 hrs · 55,489 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT LOWER AFT DOOR STOP. REMOVED AND REPLACED R1 DOOR PER MM.

Part: COFFEEMAKER — LEAKING (CABIN) · airframe 58,501 hrs · 54,060 cycles

SMOKE/STEAM IN AFT GALLEY. FOUND AFT COFFEEMAKER LEAKING CAUSING STEAM. REMOVED AND REPLACED AFT COFFEEMAKER PER MM.

Part: SKIN — CRACKED (BS 794) · airframe 55,084 hrs · 51,340 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 794, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 55,084 hrs · 51,340 cycles

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

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 55,084 hrs · 51,340 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING INBD MIDFLAP OUTBD T/E WEDGE DELAMINATED. REMOVED AND REPLACED MIDFLAP PER MM.

Part: RELIEF VALVE — FAULTY (CABIN PRESSURE) · airframe 57,756 hrs · 53,435 cycles

AIR TURNBACK, CABIN PRESSURE AUTO FAIL LIGHT ILLUMINATED. REMOVED AND REPLACED LT CABIN PRESSURE SAFETY RELIEF VALVE PER MM.

Part: FRAME — CRACKED (BS 494) · airframe 57,354 hrs · 53,106 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 494, FWD CARGO DOOR CUTOUT LOWER STOP FITTING. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500B) · airframe 57,354 hrs · 53,106 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SWA EA.

Part: BULKHEAD — CRACKED (BS 1016) · airframe 57,354 hrs · 53,106 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT DOME CAP, 4 O'CLOCK, 5 O'CLOCK & 7 O'CLOCK POSITIONS. REPAIRED WEB PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 787) · airframe 57,354 hrs · 53,106 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 787, STR 21R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (LT WING FOREFLAP) · airframe 57,354 hrs · 53,106 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT WING OUTBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: FLOORBEAM — CORRODED (BS 773) · airframe 57,354 hrs · 53,106 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 773, RBL 3 & RBL 14. REPAIRED FLOORBEAM PER SWA EA.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 57,354 hrs · 53,106 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR EXTERNAL EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER SRM.

Part: SHEAR TIE — CORRODED (BS 947.5) · airframe 57,334 hrs · 53,081 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 947.5, BETWEEN STR 23L TO STR 24L. REPAIRED SHEAR TIE PER SWA EA.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 57,228 hrs · 53,003 cycles

AFT OUTBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: TORQUE TUBE — WORN (LT WING TE FLAP) · airframe 57,141 hrs · 52,926 cycles

DURING SCHEDULED SERVICE CHECK, FOUND NR 4 T/E FLAP TRANSMISSION TORQUE TUBES WORN. REMOVED AND REPLACED TORQUE TUBES PER MM.

Part: TORQUE TUBE — WORN (RT WING TE FLAP) · airframe 57,141 hrs · 52,926 cycles

DURING SCHEDULED SERVICE CHECK, FOUND NR 5 T/E FLAP TRANSMISSION TORQUE TUBES WORN. REMOVED AND REPLACED TORQUE TUBES PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,760 hrs · 52,637 cycles

DURING SCHEDULED RON CHECK, FOUND AFT GALLEY OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 56,372 hrs · 52,326 cycles

DURING SCHEDULED C4 CHECK, FOUND RT AFT OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: PLATE — CRACKED (LT PYLON) · airframe 55,600 hrs · 51,739 cycles

DURING SCHEDULED SERVICE CHECK, FOUND NR 1 ENG PYLON UPPER PLATE CRACKED AT STA 234.5. REMOVED AND REPLACED PLATE PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 55,386 hrs · 51,572 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBOARD T/E AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,377 hrs · 51,565 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 19L, CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,377 hrs · 51,565 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD CARGO DOOR CUTOUT FRAME AT BS 440, UPPER SIDE OF LOWER STOP CRACKED. REPAIRED FRAME PER EA.

Part: SKIN — WORN (FUSELAGE) · airframe 55,229 hrs · 51,447 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN BETWEEN BS 875 AND BS 878, STRINGER 1, WORN. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,229 hrs · 51,447 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 943, STRINGER 25R, CRACKED. REPAIRED SKIN PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 54,454 hrs · 50,863 cycles

DURING SCHEDULED C2 CHECK, FOUND LT FWD KEEL BEAM AT BS 520, OUTBOARD LEG, CORRODED. REPAIRED KEEL BEAM PER SRM.

Part: CABLE — MISROUTED (R2 DOOR GIRT BAR) · airframe 54,445 hrs · 50,856 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE GIRT BAR CABLE MISROUTED. REROUTED R2 DOOR EVAC SLIDE CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,445 hrs · 50,856 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 957, STRINGER 21L, CRACKED. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 54,094 hrs · 50,585 cycles

R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 53,543 hrs · 50,134 cycles

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

Part: LOCK SENSOR — FAULTY (NLG) · airframe 56,017 hrs · 53,567 cycles

AFTER GEAR RETRACTION, THE RED AND GREEN NLG LIGHTS STAYED ILLUMINATED IN BOTH THE UP AND OFF POSITION. CYCLED GEAR, NO IMPROVEMENT. REMOVED AND REPLACED NLG LOCK SENSOR PER MM.

Part: CIRCUIT CARD — FAULTY (E/E BAY) · airframe 52,284 hrs · 49,102 cycles

DIVERSION, RED AND GREEN NOSE GEAR LIGHTS STAY ON WITH HANDLE IN THE UP AND OFF POSITION. REMOVED AND REPLACED M983 CARD AND ADJUSTED NOSE GEAR LOCK SENSOR PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 51,086 hrs · 48,153 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME SHEAR TIE CRACKED AT BS 887, STRINGER 14R. REPAIRED SHEAR TIE PER SRM.

Part: SPLICE — CRACKED (STRINGER) · airframe 51,086 hrs · 48,153 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE 10R CRACKED AT BS 540. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,086 hrs · 48,153 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER 15L CRACKED AT BS 509. REPAIRED STR PER SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 51,086 hrs · 48,153 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN ATTACH ANGLE CRACKED AT BS 360, BETWEEN STR 14R AND STR 15R. REPAIRED ATTACH ANGLE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,741 hrs · 47,880 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 23L. REPAIRED SKIN PER SRM.

Part: SLIDE — DISLODGED (FWD ENTRY DOOR) · airframe 50,595 hrs · 47,770 cycles

DURING SCHEDULED RON, FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER WHEN OPENING DOOR. REINSTALLED SLIDE PER MM.

Part: DOOR LATCH — INOPERATIVE (COCKPIT) · airframe 50,048 hrs · 47,313 cycles

FO'S ESCAPE ROPE DOOR LATCH INOP. REMOVED AND REPLACED DOOR LATCH ASSY PER MM.

Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 49,731 hrs · 47,050 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND UPPER NLG W/W SKIN CRACKED AT AFT OUTBOARD LT CORNER OF NOSE TIRE BRAKE PAD. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 49,731 hrs · 47,050 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT OUTBOARD AFT T/E FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED LT OUTBOARD AFT T/E FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,731 hrs · 47,050 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT ENTRY DOOR FUSELAGE SKIN CRACKED AT LOWER FWD CORNER, BS 955 AT STR 20L. REPAIRED SKIN PER SWA EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 49,731 hrs · 47,050 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 1006 & BS 1016, RT SIDE. REPAIRED CREASE BEAM WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,731 hrs · 47,050 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 947.5, RBL 15. REPAIRED FLOORBEAM PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,731 hrs · 47,050 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 1006, STR 17R. REPAIRED FUSELAGE FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 49,731 hrs · 47,050 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM CORRODED FROM BS 380 TO BS 420, LT SIDE. REPAIRED CREASE BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,731 hrs · 47,050 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 872, ABOVE STR 20L. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 49,731 hrs · 47,050 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 996.5, LBL 21. REPAIRED FLOOR BEAM PER SWA EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 49,731 hrs · 47,050 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 500C & BS 500D, LT SIDE. REPAIRED CREASE BEAM PER SRM.

Part: SKIN — CRACKED (NR 6 SLAT) · airframe 49,731 hrs · 47,050 cycles

DURING SCHEDULED 1/2D CHECK, FOUND NR 6 L/E SLAT LOWER SKIN CRACKED AT MIDDLE AUX TRACK. REPAIRED NR 6 L/E SLAT PER SRM.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 49,731 hrs · 47,050 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAMS CORRODED AT RBL 8, BS 813, BS 827, BS 825, BS 845 & BS 847. REPAIRED FLOOR BEAMS PER SWA EA.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 49,731 hrs · 47,050 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BEADED WEB CRACKED AT BS 665, LBL 33. REPAIRED BEADED WEB PER SRM.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 49,731 hrs · 47,050 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAMS CORRODED AT BS 727D + 5, RBL 3 & BS 727B + 3, LBL 3. REPAIRED FLOORBEAMS PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,731 hrs · 47,050 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 21L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 47,785 hrs · 45,494 cycles

FWD INBD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,723 hrs · 45,434 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 525, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,723 hrs · 45,434 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,723 hrs · 45,434 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 24L. REPAIRED SKIN PER SRM.

Part: SENSOR — ERRATIC (LT MLG) · airframe 47,423 hrs · 45,181 cycles

LEFT MLG DOWN (RED) LIGHT REMAINED ILLUMINATED AFTER GEAR WAS RETRACTED, RECYCLED GEAR AND LIGHT WENT OUT, BUT ILLUMINATED TWICE DURING FLIGHT. REMOVED AND REPLACED LT MLG UPLOCK SENSOR PER MM.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 47,217 hrs · 44,995 cycles

AFT GALLEY COFFEEMAKER ARCHING AND BURNING ELECTRICAL SMELL WAS NOTED. REMOVED AND REPLACED COFFEEMAKER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,105 hrs · 44,900 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 12R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (NLG W/W) · airframe 46,359 hrs · 44,266 cycles

DURING SCHEDULED C1 CHECK, FOUND NLG W/W SKIN CRACKED AT AFT OTBD CORNER OF LT NOSE TIRE BRAKE PAD ATTACH POINT. REPAIRED SKIN PER SWA RA.

Part: BRACKET — CRACKED (AFT SVC DOOR) · airframe 46,353 hrs · 44,259 cycles

DURING SCHEDULED BC1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE FWD SUPPORT BRACKET CRACKED. REPAIRED BRACKET PER SRM.

Part: TAB — WORN (RT ELEVATOR) · airframe 46,173 hrs · 44,129 cycles

DURING SCHEDULED RON,(SI-11111-55) RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB PER MM.

Part: WIRE — BROKEN (TAIL) · airframe 45,530 hrs · 43,620 cycles

AIR TURNBACK, APU FIRE WARNING BELL AND LIGHT ACTIVATED AT FL 110. DISCHARGE APU FIRE BOTTLE AND LIGHT WENT OUT. 2 MINUTES LATER, LIGHT AND BELL CAME BACK ON AGAIN. FOUND BROKEN WIRE AT APU WIRE BUNDLE SI NR 2491548. REMOVED AND REPLACED WIRE AND OPS CK GOOD PER MM.

Part: FIRE LOOP — ERRATIC (APU) · airframe 45,522 hrs · 43,611 cycles

AIR TURNBACK, AFTER APU SHUT DOWN, APU FIRE WARNING BELL ACTIVATED, CK LIST WAS C/W AND WARNING WENT OFF, THEN CAME ON SEVERAL TIMES BEFORE LANDING. C/W APU COMPT INSPECTION, NO DEFECTS FOUND, DEFERRED APU PER MEL. LATER DURING RON AT OAK, APU FIRE DETECT MX FAULT TEST FAILED. REMOVED AND REPLACED APU FIRE CONTROL PANEL AND FIRE DETECT UNIT WITH NO HELP. REINSTALLED ORIGINAL EQUIPMENT, TESTED APU FIRE DETECT LOOP AND CLEANED LOOP CONNECTOR. OPS CK GOOD PER MM.

Part: LENS — MISSING (CABIN) · airframe 42,775 hrs · 41,283 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 41,512 hrs · 40,191 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 663 STIFFENER CRACKED AT LBL 6.5. REPAIRED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 41,512 hrs · 40,191 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 727 BLKHD HORIZ STIFFENER CRACKED AT LBL 52. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 41,512 hrs · 40,191 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 663 BLKHD STIFFENER CRACKED AT RBL 7.0. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STRUCTURE — DAMAGED (LT WING TE FLAP) · airframe 41,512 hrs · 40,191 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT WING O/B MIDFLAP DAMAGED AT INBOARD T/E. REPAIRED MIDFLAP PER RA 1-357-0902.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,512 hrs · 40,191 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 515, STR 10R. REPAIRED SKIN PER SRM.

Part: LIGHT — WORN (GALLEY) · airframe 41,512 hrs · 40,191 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD GALLEY EMERGENCY EXIT LIGHT LENS GASKET WORN. REMOVED AND REPLACED LENS GASKET PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 41,512 hrs · 40,191 cycles

DURING SCHEDULED 1/4 CHECK, FOUND EEPLS LOOSE AT VERT AFT CABIN. REMOVED AND REPLACED EEPLS SYSTEM PER ACO 7160-33.

Part: FRAME — CRACKED (PAX DOOR) · airframe 41,512 hrs · 40,191 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR FRAME CRACKED AT 5TH STOP FROM BOTTOM AFT SIDE. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (SERVICE DOOR) · airframe 41,512 hrs · 40,191 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR FRAME CRACKED AT 3RD STOP CUTOUT FROM TOP AND 3RD STOP CUTOUT FROM BOTTOM, AFT SIDE. REPAIRED DOOR PER T1-152-003.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,512 hrs · 40,191 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 1 EXTERNAL FUSELAGE SKIN CRACKED, AT BS 867, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,512 hrs · 40,191 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACKED AT BS 947, STR 23L. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 41,512 hrs · 40,191 cycles

DURING SCHEDULED 1/4D CHECK, FOUND WEB CRACKED AT BS 178 BULKHEAD, RBL 11, WL 234. REPAIRED BULKHEAD PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 41,512 hrs · 40,191 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT LBL 11 & LBL 12, WL 234. REPAIRED BULKHEAD PER SRM.

Part: CSD — MALFUNCTIONED (NR 2 ENGINE) · airframe 41,431 hrs · 40,123 cycles

AIR TURNBACK, NR 2 ENGINE CSD LOW PRESSURE LIGHT ILLUMINATED ON TAKEOFF. SERVICED CSD AND ACCOMPLISHED ENG RUN PER MM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 41,004 hrs · 39,727 cycles

DURING SCHEDULED C3 CHECK, FOUND BOTH FWD EVACUATION SLIDE GIRT ASSY''S OUT OF ADJUST. ADJUSTED BOTH SLIDES PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 39,646 hrs · 38,571 cycles

AFT CABIN EMERGENCY FLASHLIGHT INOPERATIVE. R&R FLASHLIGHT ASSY PER MM.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 39,626 hrs · 38,555 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOPERTIVE. R&R BATTERY AND LIGHT HOUSING ASSY PER MM.

Part: BEAM — CRACKED (CARGO DOOR)

DURING SCHEDULED C1 CHECK, FOUND AFT CARGO DOOR UPPER T-BEAM CRACKED. REPAIRED BEAM PER SWA RA NR 1-352-0350.

Part: SLIDE — LOW PRESSURE (L2 DOOR)

DURING SCHEDULED SC CHECK, FOUND L2 DOOR EMERGENCY SLIDE PRESSURE LOW. REPLACED SLIDE PER BOEING M/M.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED D-CHECK, FOUND RIGHT REAR EMERGENCY EXIT LIGHT AT RIGHT REAR SERVICE DOOR INOP. REMOVED AND REPLACED BULB, CLEANED CONTACTS, AND OP CK GOOD PER BOEING MM.

Part: WEB — DENTED (BS 866)

DURING SCHEDULED D-CHECK, FOUND DENTED WEB AT BS 866, RBL 29, WL 170. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — DAMAGED (BS 791)

DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 791, RBL 60, WL 190 HAS DOUBLE DRILLED HOLE. REMOVED AND REPLACED PER BOEING SRM.

Part: COWL — PUNCTURE (NR 1 ENGINE)

DURING SCHEDULED D-CHECK, FOUND 1 X .5 PUNCTURE ON INNER SKIN OF NR 1 O/B ENG COWL 8.5 FROM L/E AND 29 FROM LOWER EDGE. REPAIRED PER BOEING SRM.

Part: BUSHING — CORRODED (NR 2 LE FLAP ACT)

DURING SCHEDULED D-CHECK, FOUND CORRODED NR 2 K-FLAP ACTUATOR ROD END FITTING BUSHINGS. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (RT WING)

DURING SCHEDULED D-CHECK, FOUND SMALL CRACK AT FIXED L/E SKIN LOWER PANEL. REPAIRED PER BOEING SRM.

Part: SPAR CHORD — CRACKED (WS 224)

DURING SCHEDULED D-CHECK, FOUND CRACK INDICATION ON TOP MOST INBOARD FASTENER HOLE COMMON TO MAIN LANDING GEAR BEAM FITTING (RIGHT SIDE) RSS 224 (CRACK ON SPAR CHORD UPPER). REPAIRED PER BOEING SRM.

Part: FRAME — DENTED (BS 867)

DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 867, RBL 21, WL 166. REMOVED AND REPLACED PER BOEING SRM.

Part: DOOR FRAME — CORRODED (BS 493-496)

DURING SCHEDULED D-CHECK, FOUND CORRODED DOOR FRAME COVER PLATE AT BS 493-496, RBL 25-30, WL 157. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 181)

DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 181, RBL 17.5, WL 182. REMOVED AND REPLACED PER BOEING SRM.

Part: SKATE ANGLE — CHAFED (VERT STAB)

DURING SCHEDULED D-CHECK, FOUND CHAFED RIGHT VERTICAL STAB CLOSURE SKATE ANGLE. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — GOUGED (BS 500)

DURING SCHEDULED D-CHECK, FOUND GOUGED INNER SURFACE OF SKIN UNDER VHF ANTENNA AT BS 500 PLUS 5, WL 149, LBL 01. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (BS 318)

DURING SCHEDULED D-CHECK, FOUND SKIN GOUGED ABOVE FWD ENTRY DOOR CUTOUT AT BS 318, WL 296 YTO WL 291, LBL 40. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 727-947)

DURING SCHEDULED D CHECK, FOUND CORRODED CARGO FLOORBEAM AT BS 727 PLUS 4, 947, LBL 12, WL 155; AND BS 727 PLUS 4 TO 947, RBL 7.5, WL 155. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 519)

DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 519, ABOVE STR 22 RT. REPAIRED PER BOEING SRM.

Part: FRAME — CORRODED (BS 955)

DURING SCHEDULED D-CHECK, FOUND CORRODED LOWER STUB FRAME AT BS 955, RBL 54, WL 208. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 380/440/747)

DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH ANGLE BETWEEN STR 8 LT AND 9 LT AT BS 747; STR 8 LT AND 9 LT AT BS 440; AND STR 8 RT AND 9 RT AT BS 380. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 727)

DURING SCHEDULED D-CHECK, FOUND CORRODED CARGO FLOORBEAM AT BS 727 PLUS 8 = 947, LBL 3, WL 155. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (CARGO COMPT)

DURING SCHEDULED D-CHECK, FOUND CRACKED INTERCOSTAL. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 358)

DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 358, LBL 65, WL 216. REPAIRED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 295)

DURING SCHEDULED D-CHECK, FOUND CRACKED WEB INTERCOSTAL AT BS 295, LBL 59, WL 223; AND BS 295, LBL 58, WL 216. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 294.5)

DURING SCHEDULED D-CHECK, FOUND CRACKED STUB FRAME AT BS 294.5, WL 209, RBL 54. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (BS 327)

DURING SCHEDULED D-CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 327, RBL 66, WL 210.5. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 907)

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER SPLICE AT BS 907, STR 4 RT. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — DENTED (BS 827)

DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 827, LBL 45, WL 171. REPAIRED PER BOEING SRM.

Part: BEAM — DAMAGED (BS 947)

DURING SCHEDULED D-CHECK, FOUND DAMAGED CREASE BEAM WEB AND OUTBOARD CHORD AT BS 947, LBL 59, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: KEEL BEAM — CORRODED (BS 500)

DURING SCHEDULED D-CHECK, FOUND CORRODED KEEL BEAM OB FLANGE AT BS 500 D PLUS 500 D PLUS, LBL 6, WL 149. REPAIRED PER BOEING SRM.

Part: CHORD — CORRODED (BS 270)

DURING SCHEDULED D-CHECK, FOUND CORRODED Z CHORD AT BS 270, WL 207, RBL 5. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CORRODED (BS 967-986)

DURING SCHEDULED D CHECK, FOUND CORRODED WEB AT BS 967-986, RBL 46-48, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — DENTED (BS 727)

DURING SCHEDULED D CHECK, FOUND DENTED FRAME AT BS 727C, RBL 48, WL 169. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CORRODED (BS 1002)

DURING SCHEDULED D CHECK, FOUND CORRODED WEB AT BS 1002, RBL 45.5, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 302)

DURING SCHEDULED D CHECK, FOUND CRACKED INTERCOSTAL ATTACH ANGLE AT BS 302, WL 236, 6.5 ABOVE STR 14 LT. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD ANGLE — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND CRACKED SUPPORT ANGLE AT 178 BULKHEAD, LBL 27, WL 207. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — GOUGED (E/E DOOR)

DURING SCHEDULED D CHECK, FOUND E/E DOOR OUTER SKIN, HAS NUMEROUS GOUGES AND DENTS. REMOVED AND REPLACED PER BOEING SRM.

Part: BRACKET — CRACKED (BS 328)

DURING SCHEDULED D CHECK, FOUND CRACKED BRACKET AT BS 328, LBL 53, WL 181. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND CRACKED BS 178 BULKHEAD WEB AT LBL 6.7, WL 200 TO WL 198. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOOR WEB — CRACKED (BS 179-188)

DURING SCHEDULED D CHECK, FOUND CRACKED FLOOR WEB AT BS 179-188, RBL 25-29, WL 207; AND BS 179-188, LBL 25-29, WL 207. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 767-787)

DURING SCHEDULED D CHECK, FOUND CORRODED VERTICAL SUPPORT WEB AT BS 767-787, RBL 20, WL 156. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 277)

DURING SCHEDULED D CHECK, FOUND CORRODED FLOORBEAM AT BS 277, RBL 41, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 615)

DURING SCHEDULED D CHECK, FOUND CRACKED WEB AT BS 615 WL 221 LBL 65. REMOVED AND REPLACED PER BOEING SRM.

Part: CHANNEL — CORRODED (BS 334)

DURING SCHEDULED D CHECK, FOUND CORRODED U-CHANNEL AT BS 334, LBL 60 AND 354, LBL 61, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: CHORD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND RT CHORD CRACKED AT BS 178, WL 207, RBL 29 AND LBL 29. REPLACED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BULKHEAD 178 CRACKED AT RBL 4.7, WL 200.5 TO 201.25. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 332.1)

DURING SCHEDULED D-CHECK, FOUND ANGLE CRACKED AT BS 332.1 AT S8R. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BULKHEAD 178 CRACKED AT LBL 6.7, WL 211.5 TO 213.25. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 400/747/867)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 400, 747, AND 867. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BULKHEAD 178 CRACKED AT LBL 4.7, WL 198 TO 198.5. REPAIRED PER BOEING SRM.

Part: CLIP — CRACKED (BS 400)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 400 AND S27L, AND AT BS 663.75. REPLACED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BULKHEAD 178 CRACKED AT RBL 4.7, WL 198 198.5. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 294/986)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 294.5, 986.5. REPAIRED PER BOEING SRM.

Part: TIE STRAP — CORRODED (BS 787/774-858)

DURING SCHEDULED D CHECK, FOUND CORRODED TIE STRAP UNDERNEATH PRIMARY STILL WEB AT BS 787, RBL 21, WL 157; BS 774-858, RBL 19, WL 163. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 827)

DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH ANGLE BETWEEN STR 8 LT AND 9 LT; BS 827, STR 8 LT AND 9 LT; AND BS 787, STR 8 LT AND 9 LT. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CORRODED (BS 794-847)

DURING SCHEDULED D CHECK, FOUND CORRODED VERTICAL SUPPORT WEB AT BS 794-847, RBL 19, WL 160. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 787-794)

DURING SCHEDULED D CHECK, FOUND CORRODED INTERCOSTAL AT BS 787-794, RBL 23, WL 158. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 640)

DURING SCHEDULED D CHECK, FOUND CRACKED WEB AT BS 640, WL 221, LBL 65. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 520)

DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH ANGLE BETWEEN BS 520, STR 8 RT AND 9 RT; AND BS 727D, STR 8 RT AND 9 RT. REMOVED AND REPLACED PER BOEING SRM.

Part: BEAM — CRACKED (BS 179)

DURING SCHEDULED D CHECK, FOUND CRACKED CREASE BEAM AT BS 179, RBL 29, WL 207. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 500-520)

DURING SCHEDULED D CHECK, FOUND CRACKED INTERCOSTAL ANGLE AT BS 500D- 520, LBL 1, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 269)

DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 269, WL 207, RBL 11. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — DENTED (BS 747)

DURING SCHEDULED, D-CHECK, FOUND DENTED FRAME AT 747, LBL 35, WL 160. REMOVED AND REPLACED PER BOEING SRM.

Part: TIE STRAP — CORRODED (BS 781-802)

DURING SCHEDULED D CHECK, FOUND CORRODED TIE STRAP UNDERNEATH PRIMARY STILL WEB AT BS 781-802, RBL 19.5, WL 156; BS 839-855, RBL 19, WL162; AND 847, RBL 19, WL 161. REMOVED AND REPLACED PER BOEING SRM.

Part: FRAME — CRACKED (BS 400/867)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH ANGLE BETWEEN STR 8 LT AND 9 LT AT BS 867 AND BS 400, STR 8 RT AND 9 RT. REPAIRED PER BOEING MM.

Part: ANGLE — CRACKED (BS 348)

DURING SCHEDULED D-CHECK, FOUND CRACKED L-ANGLE AT DOOR STOP NR 9, BS 348 LBL 65 WL 223. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (BS 289/302/380)

DURING SCHEDULED D-CHECK, FOUND CRACKED INTERCOSTAL ATTACH ANGLE AT BS 289, WL 253, ABOVE STR 11 RT, BS 302 WL 256 ABOVE STR 10 L/H AND BS 380 TO 400 LBL 1 WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 271)

DURING SCHEDULED D-CHECK, FOUND CORRODED INTERCOSTAL AROUND NUT PLATE AT BS 271, RBL 1, WL 208. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 500)

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 500D, STR 19 RT. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOORWAY UPPER HINGE CUTOUT CRACKED. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED BC1 CHECK, FOUND FUSELAGE SKIN CRACK AT EXTERNAL POWER DOOR CUTOUT AT AFT FLANGE AT LATCH. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN FLOOR LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: SKIN — BIRD STRIKE (FWD FUSELAGE)

ON CLIMBOUT, EXPERIENCED BIRD STRIKE TO AREA ABOVE AND AFT OF F/O WINDOW. AIRCRAFT RETURNED TO SJC AND MADE AN UNEVENTFUL LANDING. PERFORMED BIRD STRIKE INSPECTION PER BOEING M/M, NO DAMAGE NOTED.