N682SW

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND FLOORBEAM CORRODED AT BS 967, BETWEEN RBL 0 TO RBL 45.5. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 705 TO BS 715, LBL 24.5. REPAIRED BEAM PER EO & EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND NR 3 L/E SLAT LOWER SKIN CRACKED. REMOVED AND REPLACED SLAT ASSY PER MM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 772, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STR TIE CLIP CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED CLIP PER SRM & BAC DRAWING.

Part: SKIN — CRACKED (LE SLAT) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND NR 1 L/E SLAT LOWER SKIN CRACKED. REMOVED AND REPLACED SLAT ASSY PER MM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 727C+605, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 753, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: SLAT — DELAMINATED (LT WING) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND NR 2 L/E SLAT DELAMINATED AT UPPER INBD EDGE. REMOVED AND REPLACED SLAT ASSY PER MM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 891, RBL 3.0. REPAIRED CHANNEL PER EA.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND EMERGENCY LIGHT BATTERY PACK INOP AT CABIN CEILING STA 380. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND FLOOR CHANNEL CORRODED AT BS 794, RBL 3. REPAIRED CHANNEL PER EA.

Part: FLAP — CRACKED (RT WING) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP CRACKED AT L/E. REPAIRED FLAP PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND NR 2 L/E SLAT DELAMINATED AT UPPER SKIN. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 500A, STR 28L TO STR 28R. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 21R TO STR 20R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 27L TO STR 27R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520 , STR 20L TO STR 21L. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 20L TO STR 21L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 26L TO STR 27L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 28L TO STR 28R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 20L TO STR 21L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20R TO STR 21R. REPAIRED FRAME PER EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND FLOOR CHANNEL CORRODED AT BS 859.7, RBL 13.8. REPAIRED CHANNEL PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, BETWEEN STR 20R AND STR 21R. REPAIRED FRAME PER EO & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 709 TO BS 716, BBL .07. REPAIRED BEAM PER EO & EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 706 TO BS 714, BBL .07. REPAIRED BEAM PER EO & EA.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED POWER SUPPLY PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, BETWEEN STR 20L AND STR 21L. REPAIRED FRAME PER EO & EA.

Part: SPOILER — DELAMINATED (LT WING) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND NR 3 SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: LENS — CRACKED (CABIN) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND FWD EMERGENCY EXIT LIGHT LENS ASSY CRACKED. REMOVED AND REPLACED LENS ASSY PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 793.5, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED CLIP PER SRM AND BAC DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 729.5E, LBL 12.5. REPAIRED CHANNEL PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 43. REPAIRED BEAM PER TI.

Part: FRAME — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CRACKED AT BS 500D, STR 21R. REPAIRED FRAME PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 19R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 1. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 78,111 hrs · 58,616 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED CLIP PER SI.

Part: LIGHT — BROKEN (CABIN) · airframe 77,905 hrs · 58,461 cycles

DURING SCHEDULED MV3 CHECK, FOUND R1 DOOR LOWER EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 77,905 hrs · 58,461 cycles

DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 77,793 hrs · 58,373 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,758 hrs · 58,342 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 793, STR 18L. REPAIRED SKIN PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,758 hrs · 58,342 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 308, STR 18R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,758 hrs · 58,342 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 810, STR 18L. REPAIRED SKIN PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,758 hrs · 58,342 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 502D, STR 18L. REPAIRED SKIN PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,758 hrs · 58,342 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 801, STR 18L. REPAIRED SKIN PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,758 hrs · 58,342 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 804, STR 18L. REPAIRED SKIN PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,758 hrs · 58,342 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 514D, STR 15L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,758 hrs · 58,342 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 787+14, STR 19L. REPAIRED SKIN PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,758 hrs · 58,342 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 814, STR 19L. REPAIRED SKIN PER MT.

Part: LIGHT — LOOSE (CABIN) · airframe 77,057 hrs · 57,780 cycles

L1 DOOR EMERGENCY EXIT LIGHT LOOSE. REPAIRED LIGHT PER MM.

Part: LENS — LOOSE (EXIT LIGHT) · airframe 76,826 hrs · 57,599 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EMERGENCY EXIT LINER AFT LIGHT LENS LOOSE. REMOVED AND REPLACED SIGN PER MM.

Part: LENS — BROKEN (CABIN) · airframe 76,730 hrs · 57,526 cycles

FWD F/A STA EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — BROKEN (CABIN) · airframe 76,399 hrs · 57,265 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD GALLEY OVERHEAD EMERGENCY EXIT LIGHT LENS COVER BROKEN. REMOVED AND REPLACED LENS COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 76,399 hrs · 57,265 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD GALLEY SIDEWALL EMERGENCY EXIT LIGHT LENS COVER MISSING. INSTALLED LENS COVER PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 76,172 hrs · 57,084 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,153 hrs · 57,073 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 76,108 hrs · 57,042 cycles

PRESSURE AUTO FAIL LIGHT ON AT 9000 FEET STANDBY GREEN ILLUMINATED, PRESSURIZED, NONE UNDER CONTROL. WENT TO STANDBY, NO CONTROL. CABIN ALT SHOWING 40-50K. PRESSURE DIFF 6-7. CABIN RATE AT 4000 F/M. CONTROLLER IN MANUAL, WAS ABLE TO CONTROL PRESSURIZATION NORMALLY. AFTER OUTFLOW VALVE OPENED RATE 1500 F/M CLIMB. PRIOR TO OUTFLOW VALVE OPENING VALVE WAS FULLY CLOSED. FOUND OUTFLOW VALVE STICKING. REMOVED AND REPLACED OUTFLOW VALVE AND CABIN PRESSURE CONTROLLER PER MM.

Part: COVER — LOOSE (L1 DOOR) · airframe 75,947 hrs · 56,924 cycles

L1 DOOR EMERGENCY EVAC SLIDE COVER LOOSE. SECURED COVER PER MT.

Part: LIGHT — BROKEN (CABIN) · airframe 75,828 hrs · 56,839 cycles

FWD ENTRY EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 75,552 hrs · 56,634 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD EEPLS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,384 hrs · 56,516 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 864, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,384 hrs · 56,516 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 854, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,365 hrs · 56,502 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO BAY DOOR CUTOUT SKIN CRACKED IN BEAR STRAP AT AFT LOWER CORNER. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 75,384 hrs · 56,516 cycles

DURING SCHEDULED CV CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 75,108 hrs · 56,311 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 74,726 hrs · 56,030 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT BACKUP INTERCOSTAL CRACKED AT BS 333. REPAIRED INTERCOSTAL PER SWA EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 74,649 hrs · 55,962 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 74,649 hrs · 55,962 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 1 SLAT SKIN LOWER T/E CRACKED. REMOVED AND REPLACED SKIN PER MM.

Part: CONTAINER — CRACKED (EVAC SLIDE) · airframe 74,649 hrs · 55,962 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE CONTAINER CRACKED. REPAIRED CONTAINER PER SRM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 74,649 hrs · 55,962 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND AFT EMERGENCY EXIT LIGHT CHARGER INOP. REMOVED AND REPLACED CHARGER PER MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 74,621 hrs · 55,940 cycles

L2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: LIGHT — LOOSE (CABIN) · airframe 74,573 hrs · 55,909 cycles

OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,331 hrs · 55,721 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 867, STR 10L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 74,049 hrs · 55,504 cycles

FWD BULKHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — OUT OF POSITION (EXIT SIGN) · airframe 72,946 hrs · 54,715 cycles

FWD EMERGENCY EXIT SIGN FELL OFF. SECURED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,562 hrs · 54,452 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, BETWEEN STR 21L TO STR 22L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,562 hrs · 54,452 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 923, STR 21R. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,562 hrs · 54,452 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 312, BETWEEN STR 22R TO STR 23R. REPAIRED FRAME PER EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,562 hrs · 54,452 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CENTER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — BROKEN (CABIN) · airframe 72,562 hrs · 54,452 cycles

DURING SCHEDULED 24Y CHECK, FOUND R1 DOOR OVERHEAD EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 72,562 hrs · 54,452 cycles

DURING SCHEDULED 24Y CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 72,562 hrs · 54,452 cycles

DURING SCHEDULED 24Y CHECK, FOUND R1 DOOR LOWER EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 72,562 hrs · 54,452 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 3 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 72,562 hrs · 54,452 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING OTBD FORE FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (RT WING) · airframe 72,562 hrs · 54,452 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING INBD L/E SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 360-380) · airframe 72,562 hrs · 54,452 cycles

DURING SCHEDULED 24Y CHECK, FOUND E&E COMPARTMENT SKIN CRACKED BETWEEN BS 360 TO BS 380, BETWEEN STR. 28L TO STR 29R. REMOVED AND REPLACED SKIN PER SRM.

Part: FRAME — CORRODED (BS 500 S28L/R) · airframe 72,562 hrs · 54,452 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,562 hrs · 54,452 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE LOWER CUTOUT. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 72,562 hrs · 54,452 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 72,562 hrs · 54,452 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 500B, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,562 hrs · 54,452 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,562 hrs · 54,452 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 72,562 hrs · 54,452 cycles

DURING SCHEDULED 24Y CHECK, FWD CARGO COMPT FRAME CORRODED AT BS 500, BETWEEN STR 27L TO STR 28L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,562 hrs · 54,452 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 72,562 hrs · 54,452 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,562 hrs · 54,452 cycles

DURING SCHEDULED 24Y CHECK, FOUND E & E COMPARTMENT SKIN CRACKED BETWEEN BS 360 TO BS 380, STR 28L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 72,562 hrs · 54,452 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,562 hrs · 54,452 cycles

DURING SCHEDULED 24Y CHECK, FOUND E & E COMPARTMENT SKIN CRACKED BETWEEN BS 360 TO BS 380, STR 28R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,036 hrs · 54,073 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 769 19L TO BS 770, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,036 hrs · 54,073 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 729E TO BS 739E, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,036 hrs · 54,073 cycles

DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 780, STR 18L. REPAIRED SKIN PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,805 hrs · 53,900 cycles

L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,754 hrs · 53,859 cycles

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

Part: GLOWSTRIP — WORN (CABIN) · airframe 71,654 hrs · 53,785 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 11 ABC. R&R STRIP PER MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 71,654 hrs · 53,785 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED AT OUTBOARD T/E END. REPAIRED SLAT PER SRM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 71,654 hrs · 53,785 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING FORE FLAP UPPER SURFACE DELAMINATED. R&R FLAP PER MM.

Part: LENS — MISSING (CABIN) · airframe 71,654 hrs · 53,785 cycles

DURING SCHEDULED HC2 CHECK, FOUND CENTER ISLE OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,654 hrs · 53,785 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 71,654 hrs · 53,785 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP UPPER SURFACE DELAMINATED. R&R FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,654 hrs · 53,785 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 923, STR 21R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,503 hrs · 53,687 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 941, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,424 hrs · 52,912 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 766, STR 20R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,182 hrs · 52,725 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506D, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,226 hrs · 52,753 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506D, STR 16R. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,159 hrs · 52,709 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,897 hrs · 52,518 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: FIRE LOOP — FAULTY (MLG W/W) · airframe 69,845 hrs · 52,482 cycles

AIR TURNBACK - MLG WHEEL WELL FIRE LIGHT ILLUMINATED DURING CLIMBOUT OF BWI. REMOVED AND REPLACED FIRE LOOP PER MM.

Part: LENS — MISSING (CABIN) · airframe 69,845 hrs · 52,482 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — DEBONDED (FORE FLAP) · airframe 69,629 hrs · 52,316 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING INBOARD FORE FLAP UPPER SURFACE DISBONDED. REPAIRED FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,629 hrs · 52,316 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, STR 23L. REPAIRED SKIN PER SWA EA.

Part: LIGHT — BROKEN (CABIN) · airframe 69,472 hrs · 52,192 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,908 hrs · 51,769 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 68,337 hrs · 51,342 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: ENGINE — FLAMED OUT (RIGHT) · airframe 68,284 hrs · 51,297 cycles

UPON LANDING AND DECELERATION IN PHX NR 2 ENGINE FLAMED OUT. REMOVED AND REPLACED NR 2 ENGINE PER MM.

Part: PRESSURE BLKHD — CRACKED (FUSELAGE) · airframe 68,191 hrs · 51,223 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 7L. REPAIRED BULKHEAD PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,191 hrs · 51,223 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,191 hrs · 51,223 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,191 hrs · 51,223 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,191 hrs · 51,223 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,191 hrs · 51,223 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 68,191 hrs · 51,223 cycles

DURING SCHEDULED BRDG CHECK, FOUND KEEL BEAM CORRODED BETWEEN BS 727 AND BS 727A, RBL 7 AND LBL 17. REPAIRED KEEL BEAM PER ER.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,191 hrs · 51,223 cycles

DURING SCHEDULED BRDG CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,191 hrs · 51,223 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,191 hrs · 51,223 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,191 hrs · 51,223 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 747, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,191 hrs · 51,223 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 847 S27R) · airframe 68,191 hrs · 51,223 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 847, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: TORQUE TUBE — WORN (RT ELEVATOR) · airframe 68,191 hrs · 51,223 cycles

DURING SCHEDULED BRDG CHECK, RIGHT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR OUTPUT TORQUE TUBE PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,191 hrs · 51,223 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 727A, STR 22L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (BS 867 S26R) · airframe 68,191 hrs · 51,223 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 26R CORRODED AT BS 867. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (BS 787 S27R) · airframe 68,191 hrs · 51,223 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,191 hrs · 51,223 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 328, STR 21R. REPAIRED FRAME PER SRM.

Part: FITTING — CORRODED (L1 DOOR) · airframe 68,191 hrs · 51,223 cycles

DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 68,191 hrs · 51,223 cycles

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

Part: BULKHEAD — CRACKED (BS 1016 S23L) · airframe 68,191 hrs · 51,223 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 23L. REPAIRED WEB PER SRM.

Part: FITTING — CORRODED (L1 DOOR) · airframe 68,191 hrs · 51,223 cycles

DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (ELEVATOR TAB) · airframe 68,191 hrs · 51,223 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT ELEVATOR TAB INBOARD FITTING CRACKED. REMOVED AND REPLACED ELEVATOR TAB PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 344 S11R) · airframe 68,191 hrs · 51,223 cycles

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

Part: STRINGER CLIP — CRACKED (BS 277 S10R) · airframe 68,191 hrs · 51,223 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 68,191 hrs · 51,223 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED STRINGER SPLICE PER ER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,468 hrs · 50,634 cycles

L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (R1 DOOR) · airframe 67,280 hrs · 50,490 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR SKIN CRACKED AT LOWER DOOR HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,131 hrs · 50,358 cycles

L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 65,755 hrs · 49,275 cycles

EMERGENCY EXIT OVERHEAD LIGHT LENS LOOSE AT ROW 2. SECURED LIGHT LENS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 65,554 hrs · 49,120 cycles

FWD CABIN OVERHEAD EMERGENCY EXIT SIGN COVER LOOSE. SECURED COVER PER MM.

Part: SKIN — DELAMINATED (LT FORE FLAP) · airframe 65,317 hrs · 48,939 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD FORE FLAP DELAMINATED AT WBL 150. REMOVED AND REPLACED FORE FLAP PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,317 hrs · 48,939 cycles

DURING SCHEDULED C4 CHECK, FOUND LOWER SIDEWALL EMERGENCY EXIT LIGHT INOP L1 DOOR. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 64,768 hrs · 48,502 cycles

FWD CABIN OVERHEAD EMERGENCY EXIT SIGN LENS FELL OFF. INSTALLED SIGN LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,351 hrs · 48,183 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 776, STR 19L. REPAIRED SKIN PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 64,351 hrs · 48,183 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER LOOSE AT ROW 15 ABC. SECURED EEPLS COVER PER MM.

Part: LENS — DAMAGED (CABIN) · airframe 64,351 hrs · 48,183 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR LOWER EMERGENCY EXIT LIGHT LENS DAMAGED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 63,888 hrs · 47,822 cycles

R1 DOOR LOWER EMERGENCY EXIT SIGN LENS COVER BROKEN. R&R LIGHT ASSY PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 62,661 hrs · 46,893 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,567 hrs · 46,820 cycles

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

Part: CABLE ASSY — MISROUTED (L2 DOOR) · airframe 62,409 hrs · 46,693 cycles

DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY IAW MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,236 hrs · 46,544 cycles

DURING SCHEDULED A2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — INOPERATIVE (ROW 5 DEF) · airframe 61,989 hrs · 46,342 cycles

DURING SCHEDULED SERVICE CHECK, FOUND SEVERAL CABIN EEPLS LIGHTS INOP BETWEEN FWD GALLEY & ROW 5 DEF. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 61,569 hrs · 46,018 cycles

DURING SCHEDULED SERVICE CHECK, FOUND NLG WW LEFT UPPER ACCESS CUTOUT, AFT INBOARD CORNER CRACKED AT BS 249, LBL 2. REPAIRED WEB PER SWA EA.

Part: PANEL — CRACKED (LT MLG WW) · airframe 61,569 hrs · 46,018 cycles

DURING SCHEDULED C4 CHECK, FOUND LEFT MLG W/W UPPER FWD CEILING PANEL CRACKED AT BS 664, LBL 39. MX FERRY TO DAL, REPAIRED PANEL PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 60,626 hrs · 45,278 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,421 hrs · 45,136 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, STR 24R. REPAIRED FRAME PER PAE ER.

Part: MODULE — FAULTY (E&E BAY) · airframe 59,706 hrs · 44,604 cycles

ATB / DECLARED EMERGENCY. NLG RED UNSAFE LIGHT ILLUMINATED IN FLIGHT. NLG GREEN DOWN AND LOCKED LIGHT ILLUMINATED INTERMITTENTLY. REMOVED AND REPLACED M1214, PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND LOGITUDINAL FLOORBEAM UPPER CHORD AT BS 663, BL 0, CRACKED. REPAIRED CHORD PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 59,591 hrs · 44,156 cycles

DURING SCHEDULED D-CHECK, FOUND 3 EACH SHEAR TIES CRACKED FROM BS 360, STRINGER 13L AND BS 400, STRINGER 14L. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND FWD RT EMERGENCY EXIT DOOR SLIDE LIGHT INOP. RELAMPED PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 460, STRINGER 13L, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — WORN (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN FROM BS 862 TO BS 887, BL 0 TO RBL 5, WORN. REPAIRED SKIN SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EACH FRAMES CRACKED AT BS 787, STRINGER 9R AND BS 827, STRINGER 9. REPAIRED FRAME SECTIONS PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 360, STRINGER 14R, CRACKED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND 5 EACH CRACKS ON LONGITUDINAL FLOORBEAM AT BS 727B, FROM LBL 43 TO RBL 47. REPAIRED FLOORBEAM PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 986, BETWEEN LBL 47 AND RBL 47, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 727E, STRINGER 9R, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND FWD CARGO COMPARTMENT FRAME AT BS 492, STRINGER 24R, CRACKED. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 663, STRINGER 2R, CRACKED. REPAIRED SKIN PER SRM.

Part: SPAR — CORRODED (VERTICAL STAB) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB AFT SPAR LT AND RT PRIMARY CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED STAB PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EACH FRAMES CRACKED BETWEEN BS 827 AND BS 867, STRINGER 9R. REPAIRED FRAME SECTIONS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 5,951 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 787, STRINGER 9L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 639, STRINGER 16R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FITTING — CORRODED (L1 GIRT BAR) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND L1 DOOR EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED AFT GIRT BAR FITTING PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE AT BS 360, STRINGER 4L, CRACKED. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND ZEE CHORD AT BS 270, FROM LBL 11 TO RBL 11, CORRODED. REMOVED AND REPLACED ZEE CHORD PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 500, STRINGER 26R, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 967, RBL 28, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 1016, LBL 6, CORRODED. REMOVED AND REPLACED FLOORBEAM CHORD SECTION PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EACH STRINGER SPLICES CRACKED AT BS 907, STRINGER 4R AND STRINGER 4L. REMOVED AND REPLACED STRINGER SPLICES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 344, STRINGER 22L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND 3 EACH STRINGER CLIPS CRACKED AT BS 400, STRINGER 4R AND STRINGER 4L, BS 520, STRINGER 16L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER 17L AT BS 195, CRACKED. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 767, STRINGER 9L, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EACH STRINGER CLIPS CRACKED AT BS 380 STRINGER 9L AND BS BS 500A, STRINGER 16R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EA FUSELAGE FRAMES CRACKED AT BS 807 & BS 867, STR 9L. REPAIRED BOTH FRAMES PER SRM.

Part: PRESSURE PANEL — CRACKED (MLG WW) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND MAIN LANDING GEAR W/W BEADED PRESS WEB CRACKED AT BS 665, RBL 42. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND BS 188 STUB FRAMES CRACKED AT STR 17L & STR 17R. REMOVED AND REPLACED FRAMES PER SRM.

Part: ANGLE — CRACKED (BULKHEAD) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD ANGLE CRACKED AT LBL 5.8, WL 196. REMOVED AND REPLACED ANGLE SECTION PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND FLOOR WEBS CRACKED AT BS 188 TO BS 196, STR 17L & STR 17R. REPAIRED WEBS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND 2 EACH STRINGER CLIPS CRACKED FROM BS 727E TO BS 727D AND BETWEEN STRINGERS 5R AND 6R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 727D, STRINGER 5R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,591 hrs · 44,516 cycles

DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 847, STRINGER 8L, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 59,523 hrs · 44,464 cycles

FWD ENTRY DOOR LOWER EMERGENCY EXIT LIGHT NEXT TO FLIGHT ATTENDANT SEAT BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,302 hrs · 44,295 cycles

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,142 hrs · 44,162 cycles

DURING SCHEDULED A1 CHECK, FOUND LOWER EMERGENCY EXIT LIGHTS ON AFT SERVICE AND ENTRY DOORS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: ACTUATOR — LEAKING (RT MLG) · airframe 58,940 hrs · 43,998 cycles

ON CLIMBOUT FROM LAX AT FL 238 THE RT MLG EXTENDED WITH THE HANDLE IN THE OFF POSITION. BOTH RED AND GREEN LIGHTS ILLUMINATED, SLOWED AIRCRAFT, GEAR RETRACTED. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR PER MM.

Part: CIRCUIT CARD — FAULTY (E&E BAY) · airframe 58,773 hrs · 43,855 cycles

RIGHT MLG UNSAFE LIGHT INDICATION. AFTER CYCLING LANDING GEARS AND USING MANUAL EXTENSION WARNING INDICATION PERSISTED. REMOVED AND REPLACED M981 CIRCUIT CARD PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,355 hrs · 43,528 cycles

DURING SCHEDULED PM CHECK, FOUND LOW LEVEL EMERGENCY EXIT LIGHTS AT FWD ENTRY AND FWD SERVICE DOORS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 57,786 hrs · 43,062 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR SKIN AT UPPER AFT CUTOUT FOR HANDLE, CRACKED. REPAIRED CARGO DOOR SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,786 hrs · 43,062 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 747, STRINGER 18 R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,786 hrs · 43,062 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 747, STRINGER 18R, CRACKED. REPAIRED SKIN PER SRM.

Part: CIRCUIT CARD — FAILED (E/E BAY) · airframe 57,740 hrs · 43,027 cycles

AFTER TAKEOFF AND MOVING GEAR LEVER TO OFF POSITION BOTH RED AND RT MLG LIGHT ILLUMINATED. MOVED GEAR LEVER TO UP THEN OFF, LIGHTS EXTINGUISHED. REMOVED AND REPLACED RT MLG DOWNLOCK LOGIC CARD, ADJUSTED UPLOCK SENSOR, PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,625 hrs · 42,930 cycles

DURING THRU FLIGHT CHECK, FOUND FUSELAGE SKIN AT BS 750, STRINGER 18R, CRACKED. REPAIRED SKIN PER SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,534 hrs · 42,850 cycles

DURING SCHEDULED PM CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 57,093 hrs · 42,510 cycles

L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,102 hrs · 41,739 cycles

DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP NEXT TO FWD GALLEY AND ENTRY DOORS. REMOVED AND REPLACED BATTERY PACK.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 55,944 hrs · 41,609 cycles

DURING SCHEDULED C2 CHECK, FOUND KEEL BEAM CORRODED AT BS 500D + 10, STR 28R. REPAIRED KEEL BEAM PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,944 hrs · 41,609 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS SECTION INOP IN CABIN. REPAIRED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,944 hrs · 41,609 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR LOWER HINGE CUT OUT. REPAIRED SKIN PER SRM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 55,908 hrs · 41,580 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 55,504 hrs · 41,255 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR LOWER EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,378 hrs · 41,166 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 948, STR 24L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 55,171 hrs · 40,994 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT WHEN OPENING THE DOOR. REINSTALLED SLIDE PER MM.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 55,011 hrs · 40,855 cycles

OVERWING EMERGENCY EXIT LIGHTS ILLUMINATE INTERMITTANTLY. REMOVED AND REPLACED OVERWING BATTERY PACKS (2 EA).

Part: CHARGER — INOPERATIVE (CABIN) · airframe 54,835 hrs · 40,699 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD CABIN DOORS LOWER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER BASE PER MM.

Part: LIGHT — BROKEN (FWD ENTRY DOOR) · airframe 54,639 hrs · 40,530 cycles

FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PER MM.

Part: FASTENER — WORN (GIRT BAR FITTNG) · airframe 54,131 hrs · 40,136 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTING LOOSE. REMOVED AND REPLACED FASTENER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,207 hrs · 39,396 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518, STR 12L. REPAIRED SKIN PER MM.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 53,207 hrs · 39,396 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 53,207 hrs · 39,396 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT CABIN OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 53,207 hrs · 39,396 cycles

DURING SCHEDULED C3 CHECK, FOUND BOTH FWD ENTRY AND FWD SVC DOOR LOWER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: BRACKET — WORN (RT ELEVATOR) · airframe 52,271 hrs · 38,629 cycles

DURING SCHEDULED C2 CHECK, SWA SI 11139-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB CONTROL BRACKET PER MM.

Part: COVER — LOOSE (AFT GALLEY) · airframe 52,271 hrs · 38,629 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER LOOSE NEXT TO NR 3 GALLEY. SECURED COVER PER MM.

Part: RECEPTACLE — DAMAGED (SERVICE DOOR) · airframe 51,587 hrs · 38,036 cycles

DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED INNER RECEPTACLE PER MM.

Part: CAP — MISSING (CABIN) · airframe 51,445 hrs · 37,923 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS END CAP MISSING IN FWD CABIN. INSTALLED END CAP PER MM.

Part: CABLE — MISROUTED (FWD SVC DOOR) · airframe 51,445 hrs · 37,923 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,216 hrs · 37,729 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR FUSELAGE SKIN CRACKED AT BS 950, UPPER HINGE CUT OUT. REPAIRED SKIN PER SRM.

Part: COVER — CRACKED (CABIN) · airframe 51,216 hrs · 37,729 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EEPLS COVERS CRACKED AT FWD END. REMOVED AND REPLACED COVERS PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,216 hrs · 37,729 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAMES CORRODED (2 EA) BETWEEN STR'S 27L AND 27R, BS'S 807 AND 827. REPAIRED FRAMES PER SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 50,287 hrs · 36,962 cycles

DURING SCHEDULED RON, FOUND EMERGENCY FLASHLIGHT INOP IN AFT CABIN TOP POSITION. REMOVED AND REPLACED BATTERY PER MM.

Part: INDICATOR — FAILED (COCKPIT) · airframe 49,922 hrs · 36,666 cycles

AIR TURNBACK, AFTER T/O TRAILING EDGE FLAPS WOULD NOT RETRACT BEYOND ABOUT 2 DEG. FLAPS WERE LOWERED USING ALT FLAPS. REMOVED AND REPLACED TRAILING EDGE FLAP POSITION INDICATOR PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 49,692 hrs · 36,486 cycles

DURING SCHEDULED PM CHECK, FOUND BOTH FWD ENTRY AND FWD SVC DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,577 hrs · 36,383 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND LT & RT SIDE CHORDS CRACKED AT BS 178, WL 207. REPAIRED CHORDS PER SWA ACO 7342-53.

Part: WEB — CRACKED (FUSELAGE) · airframe 49,577 hrs · 36,383 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED ( 8 EA ) AT BS 178. REPAIRED BULKHEAD WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 49,577 hrs · 36,383 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND ( 2 EA ) VERTICAL BEAM WEBS CRACKED AT BS 178, WL 227 & WL 232, LBL 17.1 & RBL 17.1. R&R WEBS PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 49,114 hrs · 35,985 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY AND SVC DOORS EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LENS — MISSING (CABIN) · airframe 48,857 hrs · 35,775 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW 9 DEF. INSTALLED LENS PER MM.

Part: TAB — WORN (ELEVATOR) · airframe 48,816 hrs · 35,737 cycles

DURING SCHEDULED C2 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 48,816 hrs · 35,737 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM.

Part: GIRT BAR — OUT OF POSITION (AFT SVC DOOR) · airframe 48,816 hrs · 35,737 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. REPOSITIONED SLIDE ASSY PER MM.

Part: SHUTOFF VALVE — FAILED (NR 2 ENGINE) · airframe 48,544 hrs · 35,518 cycles

DECLARED EMERGENCY AFTER APPROX 20 MIN AT FL 350, CABIN WARNING HORN SOUNDED, CABIN ALTITUDE WAS AT 11,000 FT AND CLIMBING. INITIATED DESCENT. CABIN ALTITUDE CONTINUED TO CLIMB TO APPROX 20,000 FT. PASSENGER OXYGEN MASKS DEPLOYED. ON DESCENT NOTICED RIGHT PACK DUCT SHOWING ZERO PRESSURE. AIRCRAFT WAS UNABLE TO HOLD CABIN PRESSURE ON ONE PACK. NO ASSOCIATED BLEED OR PACK LIGHTS. F/A FWD ENTRY DOOR HAD LOUD PRESSURIZATION SQUEAL DURING DESCENT. FOUND NR 2 ENG PRSOV INOP. DEFERRED PER MEL & MX FERRY TO PHX FOR REPAIR. AT PHX REMOVED AND REPLACED NR 2 ENG PRSOV & 2 EA PNEU BLEED LINES, REMOVED AND REPLACED OUTFLOW VALVE AND RESEATED FWD ENTRY DOOR PRESS. SEAL PER MM OPS

Part: RETAINER — LOOSE (FWD ENTRY DOOR) · airframe 48,238 hrs · 35,271 cycles

FED ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 48,165 hrs · 32,210 cycles

VIBRATION FELT ABOVE 250 KTS IN REAR OF AIRCRAFT, NOT ENG RELATED. Removed and replaced Rt ELEVATOR TAB BUSHING. REPAIRED ELEVATOR TAB PER MM.

Part: RETAINER — LOOSE (ENTRY DOOR) · airframe 47,902 hrs · 35,004 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM.

Part: LENS — BROKEN (CABIN) · airframe 47,779 hrs · 34,902 cycles

BULLNOSE EMERGENCY EXIT LIGHT LENS BROKEN AT ROW 9 DEF. R&R LENS PER MM.

Part: DUCT — RUPTURED (CARGO BAY) · airframe 47,615 hrs · 34,767 cycles

DIVERTED, UNABLE TO MAINTAIN CABIN PRESSURE. FOUND CLAMP LOOSE ON LT WATER SEPERATOR & MUFFLER/DUCT ASSY RUPTURED IN FWD CARGO BAY, BEHIND AFT WALL. SECURED CLAMP AND R&R DUCT ASSY PER MM. OPS CHECK NORMAL PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,995 hrs · 34,280 cycles

DURING SCHEDULED RON CHECK, FOUND EEPLS INOP AT FWD HALF OF CABIN. REMOVED AND REPLACED FWD EEPLS BATTERY PACK PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 46,150 hrs · 33,578 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP IN AFT CABIN. REMOVED AND REPLACED AFT BATTERY PACK AND CHARGER PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 45,703 hrs · 33,222 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP 11 - 23. REMOVED AND REPLACED AFT POWER PACK AND BATTERY (P/N 65C27095).

Part: BATTERY PACK — INOPERATIVE (ROWS 11 - 23) · airframe 42,314 hrs · 31,255 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT ROWS 11D TO 23D. REMOVED AND REPLACED EEPLS BATTERY PACK PER MM.

Part: ACTUATOR — INOPERATIVE (LE FLAP)

AIR TURNBACK, NR 3 KRUGER FLAP WOULD NOT FULLY RETRACT, TRANSIT LIGHT ILLUMINATED. REMOVED AND REPLACED NR 3 KRUGER FLAP ACTUATOR.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FWD EMERGENCY AISLE EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY AND CHARGER PER MM.

Part: FRAME — CRACKED (BS 304)

DURING SCHEDULED 1/2D CHECK, FOUND BS 304 FRAME CRACKED, STRINGER 4L. REPAIRED FRAME PER SRM.

Part: BRACKETS — CORROSION (CABIN FLOOR)

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY AND SERVICE DOOR EVACUATION SLIDE GIRT BAR FLOOR ATTACH BRACKETS CORRODED. REMOVED AND REPLACED BRACKETS PER MM.

Part: BEAM — CORROSION (FWD GALLEY)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM UPPER SURFACE, BS 344. REMOVED AND REPLACED UPPER T-CAP FROM RBL 38 TO LBL 67 PER SRM.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM BS 312, LBL 1- RBL 21. REPAIRED BEAM PER TYPICAL REPAIR NR TI-353-007.

Part: WEB — CRACKED (BS 663)

DURING SCHEDULED 1/2D CHECK, FOUND PRESS WEB CRACKED, BS 663, LBL 32. REPAIRED WEB PER TI-353-046.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD HAS 3 EACH CRACKS, LBL 5- RBL 7. REPAIRED BULKHEAD PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 5. REPAIRED BULKHEAD PER SRM.

Part: SENSOR — INOPERATIVE (LT MLG)

AIR DIVERTION-- AT CRUISE ALTITUDE LT MAIN LANDING GEAR RED UNSAFE LIGHT ILLUMINATED AND REMAINED LIT UNTIL THE GEAR WAS LOWERED. REMOVED AND REPLACED LT MAIN GEAR UPLOCK SENSOR AND LOGIC CARD.

Part: HOUSING — CRACKED (SPOILER)

HOUSING ASSY IS CRACKED AT RETAINER NUT BOSS JUST BELOW THREADS RUNNING HALF WAY AROUND CIRCUMFERENCE OF BORE. POSSIBLE CAUSE, EXCESSIVE STRESS, FORCE AND/OR PRESSURE. RE: SOUTHWEST A/L, OPER CONTROL NR 0270131-63R.

Part: LIGHT — INOPERATIVE (R2 DOOR)

DURING SCHEDULED BC1 CHECK, FOUND FWD EMERGENCY LIGHT INOP AT R2 DOOR. REMOVED AND REPLACED EGRESS LIGHTING BATTERY PER MM.

Part: CSD SEAL — LEAKING (NR 1 ENGINE)

DIVERTED TO MSY DUE TO INFLT SHUTDOWN OF NR 1 ENGINE, WHEN OIL PRESSURE DROPPED BELOW RED LINE, DUE TO CSD CARBON SEAL LEAKING. LANDED WITHOUT INCIDENT. REMOVED THE CSD FOR ENGINEERING EVALUATION OF THE GEARBOX. REPLACED NR 1 ENGINE CSD GARLOC SEAL AND RETAINING RING PER BOEING MM.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED BC4 CHECK, FOUND AFT ENTRY DOOR LOWER FWD CORNER CRACKED FROM EDGE UNDER BEARSTRAP. REPAIRED PER SWA RA 1-A57-1744.

Part: FRAME — CRACKED (BS 500)

DURING SCHEDULED 1/4 D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, LBL1. REPAIRED PER BOEING SRM.

Part: CHARGER — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY AND FWD SERVICE DOORS LOWER EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY CHARGER PER BOEING M/M.

Part: WINDOW — CRACKED (RT COCKPIT)

IN FLIGHT, F/O'S NUMBER 1 WINDOW CRACKED, OBSTRUCTING HIS VIEW. AIRCRAFT RETURNED TO LAS AND MADE AN UNEVENTFUL LANDING. REPLACED WINDOW PER BOEING M/M.

Part: SUPPLY — INOPERATIVE (CABIN)

DURING SCHEDULED RON CHECK, FOUND FWD ENTRY EMERGENCY LIGHTING INOP. REPLACED BATTERY POWER SUPPLY AND OP CHECKED PER BOEING M/M.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED BC1 CHECK, FOUND A .5 INCH CRACK AT COOLING DUCT CUTOUT SKIN AFT END. REPAIRED PER BOEING SRM.

Part: CHARGER — INOPERATIVE (CABIN)

DURING SCHEDULED A1 CHECK, FOUND FWD TRACK LIGHTING INOP. REPLACED BATTERY CHARGER PER BOEING M/M.

Part: DOOR FRAME — CRACKED (FWD CARGO COMPT)

DURING SCHEDULED B/C1 CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT UPLOCK HOOK. REPAIRED PER TI NR T1-A52-003.

Part: CHARGER — INOP (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FORWARD DOOR LOWER EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK CHARGER PER BOEING M/M.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 312, LBL 1 TO RBL7, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: DOOR FRAME — CRACKED (AFT ENTRY DOOR)

DURING SCHEDULED D-CHECK, FOUND FORWARD UPPER FRAME OF AFT ENTRY DOOR CRACKED. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: STRINGER — CORRODED (BS 1088-1138)

DURING SCHEDULED D-CHECK, FOUND STRINGER CORRODED ON RIGHT SIDE OF APU TORQUE BOX FROM BS 1088 TO 1138, WL 230. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DENTED (NR 1 SPOILER)

DURING SCHEDULED D-CHECK, FOUND NUMBER 1 SPOILER SKIN DENTED 2 PLACES ON UPPER SURFACE. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN AT BS 500A PLUS 8, BETWEEN S21 AND 22L, AT BS 500, BETWEEN 23 AND 24L, AND AT BS 460, BETWEEN S23 AND 24L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SHEAR WEB — CRACKED (BS 312)

DURING SCHEDULED D-CHECK, FOUND SHEAR WEB CRACKED AT BS 312, BL 0, WL 207. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: BLKHD STIFFENER — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD VERTICAL STIFFENER CRACKED AT BS 178, LBL 5.7, WL 184. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FLOORBEAM — CORRODED (BS 947)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT UPPER FLANGE, BS 947, BL 0 TO LBL 10. REPAIRED PER TRAMCO EWO 95-0231 AND BOEING STRUCTURAL REPAIR MANUAL.

Part: DOOR FRAME — CRACKED (AFT SERV DOOR)

DURING SCHEDULED D-CHECK, FOUND AFT SERVICE DOOR UPPER FRAME CRACKED. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: DOOR SKIN — CRACKED (FWD GALLEY DOOR)

DURING SCHEDULED D-CHECK, FOUND FORWARD GALLEY DOOR LOWER HINGE CUTOUT CRACKED 2 PLACES. REPAIRED PER SWA ACO 3189-52.

Part: SKIN — DENTED (NR 5 SPOILER)

DURING SCHEDULED D-CHECK, FOUND NUMBER 5 GROUND SPOILER DENTED 2 PLACES ON LOWER SURFACE. REPAIRED PER TRAMCO EWO 95-0222.

Part: FLOORBEAM — CORRODED (BS 294)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 294, LBL 18.5 TO 23.5, WL 208. REPAIRED PER TRAMCO EWO 95-0231 AND BOEING STRUCTURAL REPAIR MANUAL.

Part: FRAME — MECH DAMAGE (BS 993)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME TO INTERCOSTAL STRAP AT BS 993, WL 247 DAMAGED. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FRAME — CRACKED (BS 294)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME AT BS 294, CRACKED AT RBL 54, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: ANGLE — CORRODED (BS 1121)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME SUPPORT ANGLE CORRODED AT BS 1121, RT SIDE, 10 INCHES ABOVE APU AIR INLET OPENING. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — CREASED (BS 1100)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CREASED AT BS 1100, AT S16L AND AT BS 1112, S17L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DENTED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTS AT BS 1012, AT S14-15L, AT BS 927 AND 947.5, BETWEEN S18 AND 19L, AT BS 887 AND 907, BETWEEN S17 AND 18L, AT BS 310 AND 326, S21 TO 22R, AT BS 1006, S12 TO 13L, AT 1004, S11 TO 12L, AT BS 351, BETWEEN S25 AND 26L, AT BS 366, AT S5L, AND AT BS 950, BL 0. REPAIRED ALL PER BOEING STRUCTURAL REPAIR MANUAL.

Part: CLIPS — CRACKED (BS 440)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 480, S2L, S3L, AT BS 500D, S3L, AT BS 616, S3L, AND AT BS 440, S16L. REPLACED ALL PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — CRACKED (NR 3 LE SLAT)

DURING SCHEDULED D-CHECK, FOUND NUMBER 3 SLAT SKIN CRACKED AT T/E. REPAIRED PER BOEING DRAWING BAC 65C30133.