N509SW

Part: RETAINER — LOOSE (LT SPOILER) · airframe 71,563 hrs · 67,575 cycles

LT WING INBD GND SPOILER LOWER SKIN PANEL SEAL RETAINER LOOSE FROM PANEL DUE TO INSERTS FAILING. R & R SPOILER IAW AMM.

Part: SKIN — DAMAGED (TE FLAP) · airframe 71,563 hrs · 67,575 cycles

LT WING INBD FORE FLAP DAMAGED UPPER SKIN CUT BY LOOSE SHELF SCREW. R & R FORE FLAP IAW AMM.

Part: FLAP — DELAMINATED (RT WING) · airframe 70,711 hrs · 66,633 cycles

RT WING INBD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,711 hrs · 66,633 cycles

SKIN CRACKED AT STATION 362, STRINGER 6R. REPAIRED SKIN IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 70,711 hrs · 66,633 cycles

LT WING INBD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 70,711 hrs · 66,633 cycles

OBSERVED STRONG ACID HOT ELECTRICAL SMELL, NO SMOKE FROM A/C SYSTEM, WENT AWAY WHEN GASPER FAN TURNED OFF. R&R GASPER FAN & HEPA FILTER IAW MM.

Part: UNKNOWN — FAULTY (COCKPIT) · airframe 70,647 hrs · 66,564 cycles

OPC VERY WARM WITH ELECTRIC ODOR. R&R OPC IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,264 hrs · 66,139 cycles

AFT FUSELAGE SKIN CRACKED AT BS 787 + 17, STR 19L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,264 hrs · 66,139 cycles

FUSELAGE UPPER CROWN SKIN CRACKED AT STA 410 + 4, STR 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,264 hrs · 66,139 cycles

FUSELAGE SKIN CRACKED AT BS 410 - 2, STR 16R. REPAIRED SKIN IAW EA.

Part: RIB — CRACKED (LT WING K FLAP) · airframe 70,261 hrs · 66,138 cycles

LEFT WING OTBD KRUEGER FLAP OUTBD STIFFENER RIB CRACKED. R & R RIB IAW AMM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 70,137 hrs · 66,018 cycles

L2 DOOR SLIDE IS LOOSE. REMOVED AND REPLACED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,910 hrs · 65,802 cycles

FUSELAGE SKIN CRACKED AT BS 927, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,910 hrs · 65,802 cycles

FUSELAGE SKIN CRACKED AT BS 927+13, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,910 hrs · 65,802 cycles

FUSELAGE SKIN CRACKED AT BS 927+5, STR 23R. REPAIRED SKIN PER SRM.

Part: FAN — FAULTY (AC BAY) · airframe 69,694 hrs · 65,576 cycles

UNUSUAL SMELL IN CABIN, WENT AWAY WHEN GASPER & RECIRC FANS TURNED OFF. REMOVED AND REPLACED RECIRC AND GASPER FANS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,021 hrs · 64,069 cycles

SKIN CRACKED AT BS 787+3, STR 18L. REPAIRED SKIN IAW ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

SKIN CRACKED AT BS 482B+16, STR 16R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

SKIN CRACKED AT BS 380+5, STR 15L. REPAIR SKIN IAW SRM.

Part: SPAR — CRACKED (RT HORIZ STAB) · airframe 67,528 hrs · 63,737 cycles

RT HORIZONTAL STABILIZER REAR SPAR WEB CRACKED AT BS 1146, RBL 14. REPAIRED WEB IAW EO AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

FRAME CRACKED AT BS 460, STR 14L. REPAIRED FRAME IAW EO.

Part: BEAM — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

LT BEAM WEB CRACKED AT BS 1096, LBL 8. REPAIRED WEB IAW EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 663.75+2, RBL 24.5. REPAIRED BEAM IAW EA AND EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

FRAME CRACKED AT BS 947.5, AT STR 18L. REPAIRED FRAME IAW EO.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 67,528 hrs · 63,737 cycles

LT WING AFT FLAP LOWER SURFACE DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 67,528 hrs · 63,737 cycles

LEFT WING O/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

FRAME CRACKED AT BS 947.5, BETWEEN STR 24R TO STR 25R. REPAIRED FRAME IAW EO.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

FRAME BRACKET CRACKED AT BS 847, BETWEEN STR 1R AND STR 2R. REMOVED AND REPLACED BRACKET IAW SRM AND DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

FRAME BRACKET CRACKED AT BS 847, BETWEEN STR 1L AND STR 2L. REMOVED AND REPLACED BRACKET IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

TIE CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

TIE CLIP CRACKED AT BS 767, STR 16L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (TE FLAP) · airframe 67,528 hrs · 63,737 cycles

RT INBD FORE FLAP LOWER SURFACE CRACKED. REPAIRED FLAP PER SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

FRAME BRACKET CRACKED AT BS 827, BETWEEN STR 1R AND STR 2R. REMOVED AND REPLACED BRACKET IAW SRM AND DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

FRAME BRACKET CRACKED AT BS 827, BETWEEN STR 1L AND STR 2L. REMOVED AND REPLACED BRACKET IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

TIE CLIP CRACKED AT BS 747, STR 23L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

TIE CLIP CRACKED AT BS 520, STR 9L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

TIE CLIP CRACKED AT BS 727B, STR 21L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

TIE CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

TIE CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

TIE CLIP CRACKED AT BS 380, STR 20L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 67,528 hrs · 63,737 cycles

LT WING NR 3 SLAT DELAMINATED ON OUTBOARD END UPPER SURFACE. REPAIRED NR3 SLAT IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

TIE CLIP CRACKED AT BS 787, STR 20R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

CHORD CORRODED AT BS 227.8 BETWEEN LBL 7 TO RBL 12. REPAIRED CHORD IAW EO AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

FLOORBEAM WEB CRACKED AT BS 294.5, LBL 56. REPAIRED WEB IAW EO AND EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

TIE CLIP CRACKED AT BS 947.5, STR 26L. REPAIRED CLIP IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 294.5, LBL 56. REPAIRED CHORD IAW EO AND EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

CRACK ON ANGLE AT AFT CUTOUT OF L1 DOOR. REMOVED AND REPLACED ANGLE PER SRM & BAC DRAWING.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

Z-ANGLE CORRODED BETWEEN BS 947.5 TO BS 986.5, STR 17R. REMOVED AND REPLACED Z-ANGLE IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

STUB FRAME CRACKED AT BS 296.5, STR 7R. REPAIRED FRAME IAW EO AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

FRAME WEB CRACKED AT BS 277, STR 16L. REPAIRED WEB IAW EA AND EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

FLOORBEAM CRACKED AT BS 947.5, LBL 53.5. REPAIRED BEAM IAW EO AND EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

CLIP CRACKED AT BS 294.5, STR 11L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

TIE CLIP CRACKED AT BS 277, STR 10L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

FRAME CORRODED AT BS 827, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (CABIN) · airframe 67,528 hrs · 63,737 cycles

SKIN CRACKED AT BS 698, RBL 6.50. REPAIRED SKIN IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

TIE CLIP CRACKED AT BS 420, STR 28L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 67,528 hrs · 63,737 cycles

LT WING NR 1 SLAT CRACKED ON LOWER SURFACE LOCATED AT STA 531. REPAIRED SKIN IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 672.5, RBL 24.5. REPAIRED BEAM IAW EA AND EO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

FLOORBEAM CRACKED AT BS 727B, LBL 24.5. REPAIRED BEAM IAW RO AND EO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

SKIN CRACKED AT BS 482B + 16, STR 18R. REPAIRED SKIN IAW EO AND EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 24.8. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (L2 DOOR) · airframe 67,528 hrs · 63,737 cycles

L2 DOOR SKIN CRACKED BETWEEN BS 967+3 TO BS 992.8+7 BETWEEN STR 9L TO STR 5L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

L2 DOOR FUSELAGE SKIN CRACKED AT BS 951+10, STR 17L. REPAIRED SKIN PER MT.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

FLOORBEAM WEB CRACKED BETWEEN BS 706 TO BS 713, RBL 24.5. REPAIRED WEB IAW EA AND EO.

Part: SKIN — CRACKED (L2 DOOR) · airframe 67,528 hrs · 63,737 cycles

L2 DOOR SKIN CRACKED AT BS 986.5 + 2.5, STR 7L. REPAIRED SKIN IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

FLOORBEAM CRACKED AT BS 727B, LBL 45.5. REPAIRED BEAM IAW EA AND EO.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,528 hrs · 63,737 cycles

WEB CRACKED BETWEEN BS 706 TO BS 711, LBL 24.5. REPAIRED WEB IAW EA AND EO.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 67,126 hrs · 63,505 cycles

RIGHT WING I/B AFT FLAP O/B CORNER DELAMINATED FROM BOTH SURFACES. REMOVED AND REPLACED FLAP PER MM. (SUBMITTED AS A SUPPLEMENT, COULDN`T FIND ORIGINAL CONTROL NUMBER.)

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,294 hrs · 62,955 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 764, STR 21L. REPAIRED SKIN IAW ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,294 hrs · 62,955 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 803, STR 21L. REPAIRED SKIN IAW ER AND EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 66,294 hrs · 62,955 cycles

DURING SCHEDULED OTS CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 65,640 hrs · 62,520 cycles

AIR TURNBACK - INTERMITTENT RADAR PAINTS WEATHER EVERY OTHER SWEEP AND ERASES WEATHER EVERY OTHER SWEEP. REMOVED AND REPLACED WEATHER RADAR INDICATOR.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,559 hrs · 62,464 cycles

DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,417 hrs · 62,363 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 1. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,417 hrs · 62,363 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 6. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,369 hrs · 62,326 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 867+14, STR 23R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,369 hrs · 62,326 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 945, STR 24R. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 65,369 hrs · 62,326 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 64,602 hrs · 61,811 cycles

FWD EMERGENCY EXIT LIGHT INOP. SECURED CONNECTOR ON BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,554 hrs · 61,776 cycles

DURING SCHEDULED SPV CHECK, FOUND RT OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 1. RELAMPED LIGHT PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,529 hrs · 61,754 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,529 hrs · 61,754 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 787, STR 8R. REMOVED AND REPLACED STRINGER PER SI.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,529 hrs · 61,754 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED STRINGER PER SI.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,529 hrs · 61,754 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,529 hrs · 61,754 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 727C, STR 9R. REMOVED AND REPLACED STRINGER PER SI.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,529 hrs · 61,754 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED STRINGER PER SI.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,529 hrs · 61,754 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 597, STR 9R. REMOVED AND REPLACED STRINGER PER SI.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,529 hrs · 61,754 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 727A, STR 4R. REMOVED AND REPLACED STRINGER PER SI.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,529 hrs · 61,754 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,529 hrs · 61,754 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,529 hrs · 61,754 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 380, STR 8R. REMOVED AND REPLACED STRINGER PER SI.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,529 hrs · 61,754 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 727C, STR 6L. REMOVED AND REPLACED STRINGER PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 64,529 hrs · 61,754 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,529 hrs · 61,754 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 727C, STR 8R. REMOVED AND REPLACED STRINGER PER SI.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,529 hrs · 61,754 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 520, STR 9R. REMOVED AND REPLACED STRINGER PER SI.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,529 hrs · 61,754 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 639, STR 1. REMOVED AND REPLACED STRINGER PER SI.

Part: WINDOW — ARCED (COCKPIT) · airframe 64,504 hrs · 61,741 cycles

L1 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,992 hrs · 61,378 cycles

DURING SCHEDULED RON CHECK, FOUND R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RECHARGED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,992 hrs · 61,378 cycles

DURING SCHEDULED RON CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 1. RECHARGED BATTERY PER MM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 63,506 hrs · 61,041 cycles

DURING SCHEDULED HC2 CHECK, FOUND NOSE LANDING GEAR WHEEL WELL WEB CRACKED AT BS 259.5, WL 174. REPAIRED WEB PER EA.

Part: GATE — CRACKED (L2 DOOR) · airframe 62,635 hrs · 60,446 cycles

DURING SCHEDULED CV CHECK, FOUND L2 DOOR LOWER WASTE GATE AFT UPPER EDGE CRACKED. REMOVED AND REPLACED DOOR PER MM.

Part: LENS — BROKEN (CABIN) · airframe 62,130 hrs · 60,081 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 62,130 hrs · 60,081 cycles

RIGHT WING NR 9 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT KEEL BEAM CORRODED BETWEEN BS 718 TO BS 727. REPAIRED BEAM PER ER.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REMOVED AND REPLACED STABILIZER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LOOSE. REMOVED AND REPLACED LIGHT PER MM.

Part: LUG — CORRODED (VERTICAL STAB) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT PRIMARY VERTICAL FIN LUG FACES CORRODED. REPAIRED LUGS PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 854, STR 24L. REPAIRED SKIN PER ER.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 770, LBL 8. REPAIRED SUPPORT PER EA.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING O/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM AND EO.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 860, LBL 3. REPAIRED SUPPORT PER EA.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 750, LBL 8. REPAIRED SUPPORT PER EA.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 770, LBL 3. REPAIRED SUPPORT PER EA.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 860, RBL 8. REPAIRED SUPPORT PER EA.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 860, LBL 8. REPAIRED SUPPORT PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 847, STR 26R TO STR 27R. REMOVED AND REPLACED FRAME SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, STR 26R TO STR 27R. REMOVED AND REPLACED FRAME SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 986, BETWEEN STR 25R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 13R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT BS FWD OF REAR SPAR STAB STA 117. REMOVED AND REPLACED SKIN PER EA.

Part: ANGLE — CRACKED (RT WING) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND ZEE ANGLE CRACKED AT RT WING FRONT SPAR LWR CHORD, FSS 243. REMOVED AND REPLACED ZEE ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 709 TO BS 711, BBL 0.07. REPAIRED WEB PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 708, BBL 0.07. REPAIRED BEAM PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 19R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR UPPER FWD HINGE CUTOUT IS CRACKED ON H-STRAP. REMOVED AND REPLACED STRAP PER SRM AND BAC DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 61,834 hrs · 59,860 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR LOWER FWD HINGE CUTOUT IS CRACKED ON H-STRAP. REMOVED AND REPLACED STRAP PER SRM AND BAC DWG.

Part: FLAP — DELAMINATED (LT WING) · airframe 61,701 hrs · 59,764 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING T/E INBOARD FORE FLAP DELAMINATED NEAR INBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,050 hrs · 59,321 cycles

DURING SCHEDULED MV4 CHECK, FOUND SKIN CRACKED AT BS 782, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,050 hrs · 59,321 cycles

DURING SCHEDULED MV4 CHECK, FOUND SKIN CRACKED AT BS 767, STR 24L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,050 hrs · 59,321 cycles

DURING SCHEDULED MV4 CHECK, FOUND SKIN CRACKED AT BS 777, STR 19L. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 59,696 hrs · 58,467 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,613 hrs · 57,768 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 824 TO BS 825, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,613 hrs · 57,768 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 782.5 TO BS 785, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,613 hrs · 57,768 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 920 TO BS 921, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,613 hrs · 57,768 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 799 TO BS 801, STR 23L. REPAIRED SKIN PER SRM.

Part: WIRE — CHAFED (OUTFLOW VALVE) · airframe 58,688 hrs · 57,819 cycles

DECLARED EMERGENCY. PRESSURIZATION LOST AT 36,000FT, CABIN AT 10,000FT INITIALLY. QRH FOLLOWED & DESCENT INITIATED. CABIN CONTROLLABLE ONLY IN MANUAL DESCENT. MASKS DEPLOYED AUTOMATICALLY. FOUND OUTFLOW VALVE WIRE CHAFED AT AFT CARGO COMPT. REPAIRED PER WDM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,613 hrs · 57,768 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 972 TO BS 973, ABOVE STR 24L. REPAIRED SKIN PER SRM.

Part: CHARGER — INOPERATIVE (COCKPIT) · airframe 5,813 hrs · 57,768 cycles

EMERGENCY EXIT LIGHTS CAME ON WITH THE EMERGENCY EXIT LIGHT SWITCH IN THE ARMED POSITION. ALL C/B'S CHECK, ALL ELECTRICAL BUSSES POWERED NORMALLY. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,613 hrs · 57,768 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 360, STR 1L. REPAIRED SKIN PER SRM.

Part: COVER — MISSING (CABIN) · airframe 58,370 hrs · 57,595 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED COVER PER MM.

Part: STRIP — DAMAGED (CABIN) · airframe 57,960 hrs · 57,274 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS STRIP DAMAGED BETWEEN ROW 11 TO ROW 17. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,960 hrs · 57,274 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 57,805 hrs · 57,134 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,597 hrs · 56,953 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 258, BETWEEN STR 22L TO STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,162 hrs · 56,561 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BETWEEN BS 431 TO BS 434, STR 1L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,770 hrs · 56,284 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACK AT FWD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,770 hrs · 56,284 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT AT BS 450, BL 0. REPAIRED SKIN PER ER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 56,770 hrs · 56,284 cycles

DURING SCHEDULED 18Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7, WL 183. REPAIRED WEB PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,770 hrs · 56,284 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,770 hrs · 56,284 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,770 hrs · 56,284 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,770 hrs · 56,284 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — DELAMINATED (NR 1 SLAT) · airframe 56,770 hrs · 56,284 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING NR 1 L/E SLAT AFT INBOARD CORNER DELAMINATED. REPAIRED SLAT PER SRM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 56,770 hrs · 56,284 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP INBOARD END DELAMINATED. REPAIRED FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,770 hrs · 56,284 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 907 S8L) · airframe 56,770 hrs · 56,824 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,585 hrs · 55,394 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 840, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,574 hrs · 55,386 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 499, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,574 hrs · 55,386 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 840, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,404 hrs · 55,240 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 907, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,404 hrs · 55,240 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,314 hrs · 55,166 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 22L. REPAIRED SKIN PER SRM.

Part: WINDOW — ARCED (COCKPIT) · airframe 54,253 hrs · 54,285 cycles

FLIGHT DECK R2 WINDOW ARCED. REMOVED AND REPLACED WINDOW AND CONTROLLER PER MM.

Part: SKIN — CRACKED (BS 769 S18L) · airframe 54,105 hrs · 54,146 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 769, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,045 hrs · 54,076 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 17R. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,908 hrs · 53,931 cycles

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

Part: ROD — WORN (ELEVATOR TAB) · airframe 53,908 hrs · 53,931 cycles

DURING SCHEDULED BRDG CHECK, LEFT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED INPUT ROD PER MM.

Part: BEARING — WORN (ELEVATOR TAB) · airframe 53,908 hrs · 53,931 cycles

DURING SCHEDULED BRDG CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED INPUT ROD BEARING PER MM.

Part: STRINGER — CRACKED (BS 440 S13R) · airframe 53,908 hrs · 53,931 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 13R CRACKED AT BS 440. REPAIRED STRINGER PER SRM.

Part: STRINGER — CRACKED (BS 1006 S7L) · airframe 53,908 hrs · 53,931 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 7L CRACKED AT BS 1006. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (BS 887 S25R) · airframe 53,908 hrs · 53,931 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 767 S22L) · airframe 53,908 hrs · 53,931 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 277 S15L) · airframe 53,908 hrs · 53,931 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 927 S26R) · airframe 53,908 hrs · 53,931 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (BS 380 S16L) · airframe 53,908 hrs · 53,931 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 16L CRACKED AT BS 380. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,908 hrs · 53,931 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 380 S15L) · airframe 53,908 hrs · 53,931 cycles

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

Part: STRINGER CLIP — CRACKED (BS 277 S16R) · airframe 53,908 hrs · 53,931 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 539 S28L) · airframe 53,908 hrs · 53,931 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 539, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 947 S26R) · airframe 53,908 hrs · 53,931 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 380 S18L) · airframe 53,908 hrs · 53,931 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 18L. REPAIRED FRAME PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 53,908 hrs · 53,931 cycles

DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: STRINGER CLIP — CRACKED (BS 277 S11R) · airframe 53,908 hrs · 53,931 cycles

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

Part: STRINGER CLIP — CRACKED (BS 328 S20L) · airframe 53,908 hrs · 53,931 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 20L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 277 S12R) · airframe 53,908 hrs · 53,931 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 12R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 53,908 hrs · 53,931 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 294 S13R) · airframe 53,905 hrs · 53,931 cycles

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

Part: STRINGER CLIP — CRACKED (BS 344 S11R) · airframe 53,905 hrs · 53,931 cycles

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

Part: LOGIC CARD — FAULTY (NLG INDICATOR) · airframe 53,731 hrs · 53,755 cycles

THIRTY MINUTES PRIOR TO DESCENT NLG RED LIGHT ILLUMINATED. WHEN GEAR HANDLE SELECTED TO DOWN POSITION NLG INDICATED UNSAFE. CYCLED GEAR TWICE BEFORE SAFE INDICATION. REMOVED AND REPLACED NLG M983 LOGIC CARD PER MM.

Part: ROD END — WORN (RT ELEVATOR TAB) · airframe 53,280 hrs · 53,290 cycles

DURING SCHEDULED C4 CHECK, FOUND RT ELEVATOR TAB CONTROL ROD TO ELEVATOR TAB MAST FITTING EXCESSIVE PLAY. REMOVED AND REPLACED TAB CONTROL ROD ENDS PER MM.

Part: TAB — CRACKED (LT ELEVATOR) · airframe 53,280 hrs · 53,290 cycles

DURING SCHEDULED C4 CHECK, FOUND LT ELEVATOR TAB CRACKED AT UPPER OUTBOARD END. REMOVED AND REPLACED ELEVATOR TAB PER MM.

Part: HINGE — WORN (RT ELEVATOR TAB) · airframe 53,280 hrs · 53,290 cycles

DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REPAIRED NR 1 HINGE PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 53,280 hrs · 53,290 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 53,280 hrs · 53,290 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,103 hrs · 53,117 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING DUCT CUTOUT BS 380, BETWEEN LBL 2.8 AND BL 0. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 52,581 hrs · 52,606 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 52,572 hrs · 52,599 cycles

R2 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 52,572 hrs · 52,599 cycles

L2 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 52,293 hrs · 52,319 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,779 hrs · 51,801 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 762, STR 22L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,779 hrs · 51,801 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 764, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 887 S25R) · airframe 51,374 hrs · 51,393 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 887, STR 25R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 931 S25L) · airframe 51,374 hrs · 51,393 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 931, STR 25L. REPAIRED SKIN PER SWA EA.

Part: PRESSURE PANEL — CRACKED (CABIN) · airframe 50,100 hrs · 49,999 cycles

DURING SCHEDULED C4 CHECK, FOUND NLG W/W CEILING PANELS CRACKED AT RT BS 250 AND LT BS 250. REPAIRED CEILING PANELS PER SWA EA.

Part: SKIN — CRACKED (BS 882 S25R) · airframe 49,866 hrs · 49,738 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 882, STR 25R. REPAIRED SKIN PER SWA EA AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,504 hrs · 49,354 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, AFT FRAME NR 5 STOP FITTING. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 303) · airframe 49,504 hrs · 49,354 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT BS 303, STR 16L. REPAIRED FRAME PER ER.

Part: STRINGER CLIP — CRACKED (BS 350) · airframe 49,504 hrs · 49,354 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 350, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (BS 747-767) · airframe 48,583 hrs · 48,422 cycles

FOUND FUSELAGE SKIN CRACKED AT BS 747 TO BS 767, BETWEEN STR 18L TO STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,721 hrs · 47,462 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 23L. REPAIRED SKIN PER SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 47,219 hrs · 46,931 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO FWD SKIN STRAP CRACKED AT BS 794.3, STR 22R TO STR 23R. REPAIRED SKIN STRAP PER SWA EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 47,219 hrs · 46,931 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON AFT CARGO FWD STUB FRAME AT BS 794.3, STR 24R TO STR 25R. REPAIRED STUB FRAME PER SWA EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 47,219 hrs · 46,931 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 3 EA WEB CRACKS AT BS 1016 PRESSURE BULKHEAD DOME CAP 11, 12 & 2 O'CLOCK POSITIONS. REPAIRED WEB PER SWA EA.

Part: RIB — CRACKED (LT WING) · airframe 47,219 hrs · 46,931 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 & STR 3. REPAIRED RIB PER SWA ACO.

Part: RIB — CRACKED (RT WING) · airframe 47,219 hrs · 46,931 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 & STR 3. REPAIRED RIB PER SWA ACO.

Part: SKIN — DELAMINATED (RT WING FOREFLAP) · airframe 47,219 hrs · 46,931 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT WING OUTBOARD T/E FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: FITTING — CORRODED (L1 DOOR) · airframe 47,219 hrs · 46,931 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON L1 DOOR EMERGENCY EVAC SLIDE FWD & AFT GIRT BAR FLOOR FITTINGS. REMOVED AND REPLACED FITTINGS PER MM.

Part: FRAME — CRACKED (MID CABIN) · airframe 47,219 hrs · 46,931 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 2 EA FUSELAGE BELT FRAME CRACKS AT INBOARD LOWER ATTACH CASTINGS, BS 616, LBL 64 & RBL 64. REPAIRED FRAMES PER SRM AND BOEING SB.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 47,219 hrs · 46,931 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT DOME CAP, STR 15R. REPAIRED BULKHEAD PER SWA EA.

Part: FITTING — OUT OF ADJUST (AFT CARGO DOOR) · airframe 47,198 hrs · 46,902 cycles

AIR TURNBACK. AFTER TAKEOFF, AFT CARGO DOOR LIGHT ILLUMINATED. ACFT WOULD NOT PRESSURIZE. ADJUSTED AFT CARGO DOOR AFT ROLLER LOCK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,144 hrs · 45,828 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 797, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM.

Part: GUIDE VANE — CRACKED (NR 1 ENGINE) · airframe 45,777 hrs · 45,508 cycles

DURING SCHEDULED C3 CHECK, FOUND NR 1 ENG 1ST STAGE LPT NGV CRACKED AT L/E. REMOVED AND REPLACED NR 1 ENG PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,527 hrs · 45,240 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 749, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 44,883 hrs · 44,589 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER AT ROW 7 ABC, DAMAGED. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,766 hrs · 44,467 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 946, STRINGER 24L. REPAIRED SKIN PER SWS EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,914 hrs · 43,635 cycles

DURING SCHEDULED SPV, FOUND 3 EACH CRACKS AT BS 178 BULKHEAD WEB, LBL .57 TO RBL 17.1, WL 178 TO WL 230. REPAIRED BULKHEAD WEB PER SRM.

Part: ACM — OVERHEATED (A/C BAY) · airframe 39,895 hrs · 39,911 cycles

SMOKE IN CABIN, RT A/C PACK TRIP OFF LIGHT ILLUMINATED. SHUT RT A/C PACK OFF AND SMOKE DISSIPATED. REMOVED AND REPLACED RT AIR CYCLE MACHINE AND TURBO FAN PER MM.

Part: CABLE — MISROUTED (AFT SVC DOOR) · airframe 39,503 hrs · 39,545 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,438 hrs · 39,485 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT FWD AND AFT LOWER CORNERS OF THE AFT SVC DOOR CUTOUT. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FWD CARGO DOOR) · airframe 39,438 hrs · 39,485 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO DOOR LOWER FRAME AND T-CHORD CRACKED. REPAIRED DOOR PER SRM AND CCO.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 39,438 hrs · 39,485 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESS WEB CRACKED BETWEEN BS 664 AND BS 665, LBL 31 TO LBL 32. REPAIRED BEADED PRESS WEB PER SWA T1.

Part: PANEL — DELAMINATED (T/E FLAP) · airframe 34,254 hrs · 34,463 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD T/E FLAP WEDGE PANEL DELAMINATED. REMOVED AND REPLACED WEDGE PANEL PER MM.

Part: VALVE — VIBRATES (FWD FUSELAGE) · airframe 32,765 hrs · 3,298 cycles

AIR TURNBACK, FLUTTERING SOUND IN COCKPIT DURING CLIMBOUT. PACKS TURNED OFF AIRSPEED BELOW 200 KTS AND ENG POWER ADJ. STILL FLUTTERING. REMOVED AND REPLACED EQUIPMENT COOLING VALVE AND C/W AIRFRAME VIBRATION CONDITIONAL INSPECTION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,635 hrs · 31,834 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY LIGHT INOP. RELAMPED PER MM.

Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · airframe 31,617 hrs · 31,817 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB LT FWD, AFT AND RT AFT PRIMARY BODY ATTACH LUGS CORRODED. REPAIRED LUGS PER ER 00-5162.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,617 hrs · 31,817 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED, BS 867, WL 276, LBL 58. REPAIRED FRAME PER ER NR 00-5161 AND SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,617 hrs · 31,817 cycles

DURING SCHEDULED D-CHECK, FOUND BS 986 FLOORBEAM UPPER SURFACE CORRODED, LBL 55 TO RBL 45. REPAIRED BEAM PER SRM AND ER NR 00-5156.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 31,617 hrs · 31,817 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE 4L CRACKED, BS 907. REMOVED AND REPLACED STRINGER SPLICE SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,617 hrs · 31,817 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED, BS 482, WL 154, RT SIDE. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,617 hrs · 31,817 cycles

DURING SCHEDULED D-CHECK, FOUND BS 328 FLOORBEAM CORRODED ON UPPER SURFACE, RBL 13 TO RBL 51. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,617 hrs · 31,817 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED, BS 867, RBL 58, WL 276. REPAIRED FRAME PER PER T1-653-042.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 31,617 hrs · 31,817 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIPS CRACKED, BS 420, STR 4L, BS 787, STR 11R AND BS 727C, STR 4R. REMOVED AND REPLACED CLIPS PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,617 hrs · 31,817 cycles

DURING SCHEDULED D-CHECK, FOUND BS 294 FLOORBEAM CORRODED ON UPPER SURFACE, RBL 14 TO RBL 27. REPAIRED BEAM PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 31,617 hrs · 31,817 cycles

DURING SCHEDULED D-CHECK, FOUND EMERGENCY EXIT LIGHT RETAINER LOOSE BS 365 LT SIDE. SECURED LIGHT RETAINER PER MM.

Part: BLADE — BIRD STRIKE (NR 1 ENGINE)

ABORTED TAKEOFF, BIRD STRIKE ON NR 1 ENG INLET. FOUND 4 FAN BLADES DAMAGED. REMOVED AND REPLACED NR 1 ENG FAN BLADES PER MM.

Part: LIGHT — LOOSE (CABIN)

DURING SCHEDULED C4 CHECK, FOUND EEPLS LIGHT STRIPS LOOSE AND WIRES EXPOSED. RESECURED STRIPS, WIRES, AND REPLACED DAMAGED COVERS.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FWD EMERGENCY FLOOR TRACK LIGHT IS INOP. RELAMPED AND OP'S CK'D GOOD PER BOEING MM.

Part: SKIN — DENTED (CARGO DOOR)

DURING WALKAROUND CHECK, FOUND AFT CARGO DOOR HAS DEEP DENT WITH GOUGE SKIN AREA. REPAIRED PER BOEING SRM.

Part: SLIDE — LOW PRESS (CABIN)

DURING RON, FOUND AFT SERVICE DOOR ESCAPE SLIDE PRESS LOW. REPLACED PER BOEING M/M.

Part: RIB — GOUGED (WS 208)

DURING SCHEDULED C3 CHECK, FOUND LEFT WING RIB GOUGED AT SEAL RETAINER AT WING STA.208, PERPINDICULAR TO LOWER RIB FLANGE. REPAIRED PER SWA RA 1-357-0451.