N503SW

Part: LENS — CRACKED (EXIT SIGN) · airframe 67,104 hrs · 64,246 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD EMERGENCY EXIT SIGN ASSY CRACKED. REPAIRED LENS ASSY PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 67,104 hrs · 64,246 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 1013, STR 5R. REPAIRED STRINGER IAW SRM.

Part: BEAM — CORRODED (FUSELAGE) · airframe 67,104 hrs · 64,246 cycles

DURING SCHEDULED 22Y CHECK, FOUND CHORD BEAM CORRODED BETWEEN BS 927 TO BS 1016, RBL 37. REPAIRED BEAM IAW SRM.

Part: SKIN — PUNCTURED (FOREFLAP) · airframe 67,104 hrs · 64,246 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING I/B FORE FLAP LOWER SKIN PUNCTURED AT I/B END. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,104 hrs · 64,246 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME INNER CHORD CRACKED AT BS 616, WL 202. REPAIRED FRAME IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,104 hrs · 64,246 cycles

DURING SCHEDULED 22Y CHECK, FOUND CRACKS AROUND FLIGHT DECK FLOOR WEB BS 248, BETWEEN RBL 15 TO RBL 22. REPAIRED WEB PER ACO.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 66,963 hrs · 64,157 cycles

DURING SCHEDULED RON CHECK, FOUND SKIN HEAT DAMAGED ABOVE FWD LAV SERVICE PANEL. REPAIRED DOUBLE IAW EA AND EA.

Part: ATTACH ANGLE — DAMAGED (FUSELAGE) · airframe 66,963 hrs · 64,157 cycles

DURING SCHEUDLED RON CHECK, FOUND LONGITUDINAL ATTACHED ZEE HEAT DAMAGED AT BS 270. REMOVED AND REPLACED ZEE IAW EA AND AAR EA.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 66,963 hrs · 64,157 cycles

DURING SCHEDULED RON CHECK, FOUND FRAME HEAT DAMAGED AT BS 277, BETWEEN STR 17R TO STR 19R. REMOVED AND REPLACED FRAME IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,963 hrs · 64,157 cycles

DURING SCHEDULED OTS CHECK, FOUND AFT OF L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY IAW SRM.

Part: CREASE BEAM — DAMAGED (FUSELAGE) · airframe 66,963 hrs · 64,157 cycles

DURING SCHEDULED RON CHECK, FOUND CREASE BEAM WEB HEAT DAMAGED BETWEEN BS 259 TO BS 277, STR 17R. REMOVED AND REPLACED WEB IAW EA AND EA.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 66,963 hrs · 64,157 cycles

DURING SCHEDULED RON CHECK, FOUND FRAME I/B SPLICE CHORD HEAT DAMAGED AT BS 277, STR 18R. REMOVED AND REPLACED SPLICE CHORD IAW EA.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 66,963 hrs · 64,157 cycles

DURING SCHEDULED RON CHECK, FOUND STRINGER HEAT DAMAGED BETWEEN BS 259 TO BS 277, STR 19R. REMOVED AND REPLACED STRINGER SECTION IAW EA AND AAR EA.

Part: CREASE BEAM — DAMAGED (FUSELAGE) · airframe 66,963 hrs · 64,157 cycles

DURING SCHEDULED RON CHECK, FOUND RT CREASE BEAM WEB HEAT DAMAGED AT BS 277, STR 17R. REMOVED AND REPLACED WEB IAW EA AND AAR EA.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 66,963 hrs · 64,157 cycles

DURING SCHEDULED RON CHECK, FOUND FRAME HEAT DAMAGED AT BS 277, BETWEEN STR 18R TO STR 19R. REMOVED AND REPLACED FRAME IAW EA.

Part: CREASE BEAM — DAMAGED (FUSELAGE) · airframe 66,963 hrs · 64,157 cycles

DURING SCHEDULED RON CHECK, FOUND CREASE BEAM OUTER CHORD HEAT DAMAGED BETWEEN BS 259 TO BS 277, STR 17R. REMOVED AND REPLACED SECTION OF CHORD IAW EA AND EA.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 66,963 hrs · 64,157 cycles

DURING SCHEDULED RON CHECK, FOUND STRINGER HEAT DAMAGED BETWEEN BS 259 TO BS 277, STR 18R. REMOVED AND REPLACED STRINGER SECTION IAW EA AND AAR EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 66,963 hrs · 64,157 cycles

DURING SCHEDULED SPV CHECK, FOUND WEB CORRODED BETWEEN BS 440 TO BS 460, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,658 hrs · 63,292 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 913, STR 25R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,658 hrs · 63,292 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 274, STR 15R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,658 hrs · 63,292 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 371.5, STR 26L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,658 hrs · 63,292 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 386, STR 15R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,660 hrs · 63,293 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 371.5, STR 26L. REPAIRED SKIN PER EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 65,660 hrs · 63,293 cycles

DURING SCHEDULED OTS CHECK, FOUND L1 DOOR COCKPIT ENTRY EMERGENCY EXIT LIGHTS INOP. CHARGED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 65,660 hrs · 63,293 cycles

DURING SCHEDULED OTS CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY EXIT LIGHTS INOP. CHARGED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,243 hrs · 62,276 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,243 hrs · 62,276 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 790, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 63,813 hrs · 61,959 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT HANDLE CUTOUT UPPER AFT RADIUS. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,267 hrs · 61,558 cycles

DURING SCHEDULED OTS CHECK, FOUND RT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 13. REMOVED AND REPLACED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,267 hrs · 61,558 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 445, STR 1. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,267 hrs · 61,558 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 445, STR 1. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,959 hrs · 61,344 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 760, STR 18L. REPAIRED SKIN PER AAR EA.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND BULKHEAD CHORD CORRODED AT BS 227, RBL 1 TO RBL 6. REPAIRED CHORD PER EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM OUTER CHORD CRACKED BETWEEN BS 431 TO BS 435. REMOVED AND REPLACED BEAM PER AAR EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 662, LBL 24.5. REMOVED AND REPLACED BEAM PER AAR EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND LOWER LT EXTERIOR EMERGENCY EXIT LIGHTS INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD EEPLS INOP AT ROW 1. RELAMPED PER MM.

Part: SPOILER — CRACKED (RT WING) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 5 SPOILER O/B LUG CRACKED. REMOVED AND REPLACED SPOILER PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHTS INOP AT R2 DOOR. RELAMPED PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND EEPLS BROKEN. REMOVED AND REPLACED EEPLS PER DRAWING.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 706 TO BS 709, BBL 0.07. REMOVED AND REPLACED WEB PER SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 6 SLAT SKIN LOWER SURFACE CRACKED. REPAIRED SKIN PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND KEEL BEAM CORRODED BETWEEN BS 482B TO 484B, STR 28R. REPAIRED BEAM PER SRM.

Part: FITTING — CRACKED (RT MLG) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT MLG GEAR BEAM FITTING CRACKED. REMOVED AND REPLACED FITTING PER ACO.

Part: TORQUE TUBE — CORRODED (TE FLAP) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING I/B TRAILING EDGE FORE FLAP TORQUE TUBE ASSY CORRODED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 1L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT HORIZONTAL STABILIZER SKIN CRACKED. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482A, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 772.60, RBL 8.10. REPAIRED BEAM PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,730 hrs · 60,561 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,370 hrs · 60,336 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,370 hrs · 60,336 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,370 hrs · 60,336 cycles

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

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 61,370 hrs · 60,336 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING NR 3 SLAT T/E WEDGE UPPER SURFACE DELAMINATED. REMOVED AND REPLACED WEDGE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,231 hrs · 60,246 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 482, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,230 hrs · 60,246 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED BETWEEN BS 801 TO BS 819, BETWEEN STR 21L TO STR 22L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,559 hrs · 59,827 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,382 hrs · 59,706 cycles

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

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 60,256 hrs · 59,621 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 60,256 hrs · 59,621 cycles

R2 DOOR EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MM.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 59,836 hrs · 59,301 cycles

FWD I/B EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,474 hrs · 58,979 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 24R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,877 hrs · 58,446 cycles

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

Part: FAN — FAULTY (E&E BAY) · airframe 58,331 hrs · 58,046 cycles

DIVERSION - FLIGHT CREW REPORTED STRONG BURNING ODOR IN CABIN. BURNING ODOR DISSIPATED AFTER GASPER FAN TURNED OFF. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,663 hrs · 57,523 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 420 AND BS 440, STR 1. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,663 hrs · 57,523 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 57,222 hrs · 57,183 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 57,157 hrs · 57,133 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 57,148 hrs · 57,126 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 56,899 hrs · 56,922 cycles

BULLNOSE EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 56,343 hrs · 54,472 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,101 hrs · 56,258 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 487B, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 55,997 hrs · 56,169 cycles

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

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 55,905 hrs · 56,081 cycles

DURING SCHEDULED MV1 CHECK, FOUND AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SIGN — MISSING (EMERGENCY EXIT) · airframe 55,669 hrs · 55,838 cycles

L1 DOOR EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN PER MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 55,563 hrs · 55,741 cycles

DURING SCHEDULED 18Y CHECK, FOUND RIGHT WING INBOARD FOREFLAP DELAMINATED AT UPPER SURFACE. REPAIRED FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,474 hrs · 55,658 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 471, STR 17R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 421 S17R) · airframe 55,466 hrs · 55,647 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 421, STR 17R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 421 S17R) · airframe 55,407 hrs · 55,582 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 421, STR 17R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 803 S18L) · airframe 55,407 hrs · 55,582 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 803, STR 18L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 55,151 hrs · 55,346 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663.75, STR 1. REPAIRED FRAME PER SWA EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED 8Y CHECK, FOUND STRINGER 1 CRACKED BETWEEN BS 661 AND BS 667. REPAIRED STRINGER PER SRM.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 812, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 758, STR 22L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 782, STR 23L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

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

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

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

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 482A, STR 20R. REPAIRED FRAME PER SWA EA.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 294, STR 12L. REPAIRED FRAME PER SWA EA.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 294, STR 13L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 951, STR 24R. REPAIRED SKIN PER SRM.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 294, STR 11L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294, STR 13L. REPAIRED FRAME PER SWA EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 7L CRACKED AT BS 295. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 20L. REPAIRED FRAME PER SWA EA.

Part: WIRE — BROKEN (CABIN) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. FOUND BROKEN WIRE ON CONNECTOR, REPAIRED WIRE PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 9L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 11L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 907 S8L) · airframe 54,566 hrs · 54,750 cycles

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

Part: FRAME — CRACKED (BS 440 S8L) · airframe 54,566 hrs · 54,750 cycles

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

Part: STRINGER CLIP — CRACKED (BS 380 S4L) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727B S7R) · airframe 54,566 hrs · 54,750 cycles

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

Part: STRINGER CLIP — CRACKED (BS 400 S4R) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A S7R) · airframe 54,566 hrs · 54,750 cycles

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

Part: STRINGER CLIP — CRACKED (BS 639 S4L) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360 S5L) · airframe 54,566 hrs · 54,750 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 27L CRACKED AT BS 1036. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

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

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 482, STR 20L. REPAIRED FRAME PER SWA EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, 3 O'CLOCK POSITION. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 12L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 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 (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 24R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,566 hrs · 54,750 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 53,625 hrs · 63,860 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 53,625 hrs · 63,860 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 53,625 hrs · 63,860 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LENS — MISSING (CABIN) · airframe 53,555 hrs · 53,734 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD RT EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM.

Part: SKIN — CRACKED (BS 427) · airframe 53,445 hrs · 53,622 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 427, LBL 3. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (BS 496 S15L) · airframe 53,353 hrs · 53,528 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 496, STR 15L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 497 S15R) · airframe 53,353 hrs · 53,528 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 497, STR 15R. REPAIRED SKIN PER SRM.

Part: ATTACH FITTING — BROKEN (LT WING SPOILER) · airframe 52,802 hrs · 52,963 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING NR 5 GROUND SPOILER CENTER HINGE LUG BROKEN. REMOVED AND REPLACED SPOILER IAW MM.

Part: HINGE — BROKEN (NR 5 SPOILER) · airframe 52,717 hrs · 52,859 cycles

DURING SCHEDULED A2 CHECK, FOUND RT WING NR 5 SPOILER HINGE BROKEN. REMOVED AND REPLACED NR 5 SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,682 hrs · 52,821 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 403, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,968 hrs · 52,047 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 882, STR 25R. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,964 hrs · 52,040 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 882, STR 25R. REPAIRED SKIN PER SWA EA AND SRM.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 51,964 hrs · 52,040 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 51,280 hrs · 51,304 cycles

EEPLS STRIP LOOSE AT FWD END. REMOVED AND REPLACED STRIP PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 51,195 hrs · 51,216 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (BS 304) · airframe 50,269 hrs · 50,253 cycles

DURING WALKAROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 304, STR 19R. REPAIRED SKIN PER SWA EA AND SRM.

Part: GATE — LEAKING (PAX DOOR) · airframe 49,993 hrs · 49,925 cycles

AIR TURNBACK, AUTO FAIL LIGHT ILLUMINATED, SELECTED STANDBY, NO HELP. REMOVED AND REPLACED EXTERNAL GROUND AIR CONDITIONING FLAPPER DOOR PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 49,870 hrs · 49,795 cycles

EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW 3 ABC. INSTALLED LENS PER MM.

Part: FRAME — CRACKED (FWD CARGO) · airframe 49,778 hrs · 49,701 cycles

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

Part: SPLICE — CRACKED (BS 360) · airframe 49,778 hrs · 49,701 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SPLICE — CRACKED (BS 908) · airframe 49,778 hrs · 49,701 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,778 hrs · 49,701 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT AFT CARGO DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (COCKPIT FLOOR) · airframe 49,778 hrs · 49,701 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND COCKPIT FLOOR WEB CRACKED BETWEEN BS 188 TO BS 196, LBL 29 TO RBL 29, WL 208. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (COCKPIT FLOOR) · airframe 49,778 hrs · 49,701 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STUB FRAMES CRACKED AT BS 188, LT & RT SIDE, WL 208. REPAIRED STUB FRAMES PER SRM.

Part: FRAME — CRACKED (FWD CARGO) · airframe 49,778 hrs · 49,701 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 1 & NR 5 STOP FITTINGS. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 49,778 hrs · 49,701 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT AFT CARGO DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (COCKPIT FLOOR) · airframe 49,778 hrs · 49,701 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, LT SIDE, WL 208. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 49,778 hrs · 49,701 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: WEB — CRACKED (COCKPIT FLOOR) · airframe 49,778 hrs · 49,701 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND COCKPIT FLOOR WEB CRACKED BETWEEN BS 188 TO BS 196, LBL 29, WL 208. REPAIRED WEB PER SRM.

Part: FLOOR PANEL — CRACKED (COCKPIT FLOOR) · airframe 49,778 hrs · 49,701 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND COCKPIT FLOOR WEB CRACKED BETWEEN BS 188 TO BS 196, RBL 29, WL 208. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (COCKPIT FLOOR) · airframe 49,778 hrs · 49,701 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, RT SIDE, WL 208. REPAIRED STUB FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,764 hrs · 48,619 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 887, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,614 hrs · 48,488 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,614 hrs · 48,488 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER AFT CORNER SKIN CUTOUT. REPAIRED SKIN PER SWA EA & SRM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 48,614 hrs · 48,488 cycles

DURING SCHEDULED C2 CHECK, FOUND R1 DOOR FRAME CRACKED AT AFT LOWER STOP FITTING. REMOVED AND REPLACED DOOR PER MM.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 48,574 hrs · 48,441 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT FORWARD EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 48,304 hrs · 48,156 cycles

DURING SCHEDULED SERVICE CHECK, FOUND STRINGER AT BS 941, STRINGER 23R, CRACKED. REPAIRED STRINGER SECTION PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 47,888 hrs · 47,730 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2 EA CRACKS AT NLG W/W CEILING WEB, BS 259.5, LT & RT SIDES OF ACCESS PANEL. REPAIRED WEB PER SRM.

Part: RIB — CRACKED (LT WING) · airframe 47,490 hrs · 47,336 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT WING UPPER RIB CHORD CRACKED AT WBL 135.5, STR 2. REPAIRED RIB CHORD PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,490 hrs · 47,336 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 16L. REPAIRED FRAME PER SWA EA.

Part: BEAM — CRACKED (CENTER WING) · airframe 47,490 hrs · 47,336 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CENTER WING LONGITUDINAL BEAM CRACKED AT BS 616, LBL 45.57. REPAIRED BEAM PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,490 hrs · 47,336 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 2 EACH FRAMES CRACKED AT BS 663.75, STRINGER 14R AND STRINGER 14L. REPAIRED FRAME SECTIONS PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 47,490 hrs · 47,336 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM FWD FLANGE AT BS 946, LBL 54, CRACKED. REPAIRED FLOORBEAM PER EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 47,490 hrs · 47,336 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR AFT FRAME NEAR 4TH STOP FITTING FROM BOTTOM, CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: GUSSET — CRACKED (DOOR FRAME) · airframe 47,490 hrs · 47,336 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR LOWER FWD FRAME AT LOWER STOP FITTING GUSSET CRACKED. REMOVED AND REPLACED GUSSET PER SRM.

Part: RIB — CRACKED (RT WING) · airframe 47,490 hrs · 47,336 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT WING LOWER RIB CHORD AT WING STATION 135.5, BETWEEN STRINGER 2 AND STRINGER 3, CRACKED. REPAIRED RT WING RIB CHORD PER EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 47,490 hrs · 47,336 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR CUTOUT FWD LOWER FRAME WEB CRACKED. REMOVED AND REPLACED FRAME WEB SECTION PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 47,490 hrs · 47,336 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 663, BL 0, CRACKED. REPAIRED FLOORBEAM CHORD PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,490 hrs · 47,336 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AT BS 907 + 8, RBL 3, CORRODED. REPAIRED FLOORBEAM PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,490 hrs · 47,336 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 663.75, STRINGER 10L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (R1 DOOR) · airframe 47,490 hrs · 47,336 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR LOWER FRAME AT AFT INBOARD LOWER STOP CRACKED. REMOVED AND REPLACED SERVICE DOOR PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 46,469 hrs · 46,274 cycles

LEFT OVERWING EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS COVER PER MM.

Part: FRAME — CRACKED (FUSELAGE)

RT FS 718 BETWEEN STRINGERS 10R AND 12R IS CRACKED 1 INCH LONG IN RADIUS OF FRAME FLANGE. POSSIBLE STRESS RELIEF CRACK. REPAIR IAW MFG REO 601R5-53-61-193 REV A.

Part: FRAME — CRACKED (FUSELAGE)

LT FS 718 BETWEEN STRINGERS 10L AND 12L IS CRACKED 1 INCH LING IN RADIUS OF FRAME FLANGE. POSSIBLE STRESS RELIEF CRACK. REPAIR IAW REO 601R-53-61-193 REV A. (EA09200402463)

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,116 hrs · 44,955 cycles

DURING SCHEDULED C2 CHECK, FOUND SKIN CRACKED AT BS 823, STRINGER 23L. REPAIRED SKIN CRACK PER SRM.

Part: ENGINE — OVERTEMP (NR 2) · airframe 43,893 hrs · 43,795 cycles

ABORTED TAKEOFF, NR 2 ENGINE EGT EXCEEDED TAKEOFF LIMITS. REMOVED AND REPLACED NR 2 ENGINE PER MM.

Part: ACTUATOR — FAULTY (NR 2 ENGINE) · airframe 43,524 hrs · 43,446 cycles

DIVERSION, NR 2 ENGINE EGT EXCEEDANCE. FOUND, VBV MASTER ACTUATOR STUCK IN OPEN POSITION. REMOVED AND REPLACED VBV MASTER ACTUATOR AND VBV MOTOR PER MM.

Part: LIGHT — LOOSE (MID CABIN) · airframe 43,348 hrs · 43,276 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS STRIP LOOSE AT ROW NR 12. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 43,348 hrs · 43,276 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS STRIP INOP. RECONNECTED EEPLS WIRES PER MM.

Part: COVER — CRACKED (CABIN) · airframe 42,447 hrs · 42,422 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 4 & WIRES EXPOSED AT ROW NR 9. REMOVED AND REPLACED COVER AND SECURED WIRES PER MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 41,781 hrs · 41,791 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP BETWEEN ROW NR 10 AND ROW NR 13. RECONNECTED WIRE PER MM.

Part: HINGE PIN — DISLODGED (FWD ENTRY DOOR) · airframe 41,625 hrs · 41,647 cycles

ON ARRIVAL UNABLE TO OPEN FWD ENTRY DOOR. FOUND, UPPER HINGE PIN PARTIALLY DISLODGED. REINSERTED PIN AND INSTALLED CIRCLIP PER MM.

Part: CABLE — MISROUTED (AFT SVC DOOR) · airframe 41,583 hrs · 41,607 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 41,583 hrs · 41,607 cycles

DURING SCHEDULED C2 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED IN CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,362 hrs · 41,400 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, ABOVE STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,680 hrs · 40,761 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 23L. REPAIRED SKIN PER SRM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 40,375 hrs · 40,466 cycles

DURING SCHEDULED RON, FOUND BOTH SVC DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF LIMITS. REMOVED AND REPLACED BOTH SVC DOOR SLIDES PER MM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 40,351 hrs · 40,446 cycles

DURING SCHEDULED A1 CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, RBL 40. REPAIRED WEB PER SRM.

Part: SLIDE — DEPLOYED (FWD SVC DOOR) · airframe 40,245 hrs · 40,343 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 39,652 hrs · 39,772 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAMS CRACKED (2 EA) AT BS 180, LBL 5.7 AT WL 153 AND RBL 17.1 AT WL 230. REPAIRED VERTICAL BEAMS PER SRM.

Part: STIFFENER — CRACKED (LT MLG W/W) · airframe 39,652 hrs · 39,772 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 663, WL 190 AT LBL 54. REMOVED AND REPLACED STIFFENER PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 39,652 hrs · 39,772 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234 AT RBL 9.0. REPAIRED WEB PER SRM.

Part: LENS — LOOSE (MID CABIN) · airframe 38,701 hrs · 38,893 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 37,931 hrs · 38,177 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 1. R&R COVER PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 36,255 hrs · 36,486 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,255 hrs · 36,486 cycles

DURING SCHEDULED C4 CHECK, FOUND 3 INCH LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 947, STR 22R. REPAIRED SKIN PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 36,255 hrs · 36,486 cycles

DURING SCHEDULED C4 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT COVER LOOSE. SECURED LIGHT ASSY PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 35,218 hrs · 35,472 cycles

AFT LOWER EMERGENCY FLASHLIGHT INOP. R&R FLASHLIGHT BATTERY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,114 hrs · 35,360 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD LT & RT SIDE CHORDS CRACKED. REMOVED AND REPLACED SIDE CHORDS PER ACO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 35,114 hrs · 35,360 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND .5 INCH CRACK IN BS 178 BULKHEAD WEB, WL 198, RBL 5.0. REPAIRED BULKHEAD WEB PER SRM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 33,516 hrs · 33,758 cycles

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: PUMP — FAILED (HYD SYSTEM)

AIR TURNBACK, B-SYSTEM HYD PUMP LOW PRESS LIGHT ILLUMINATED DURING CLIMB. REMOVED AND REPLACED B-SYSTEM ELECTRIC HYD PUMP AND CASE DRAIN FILTER PER MM.

Part: FRAME — CRACKED (CARGO DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND FWD CARGO DOOR AFT LOWER T-FRAME CRACKED. REMOVED AND REPLACED CARGO DOOR ASSY PER MM.

Part: STRINGER — CRACKED (BS 907)

DURING SCHEDULED D CHECK, FOUND STRINGER 4R CRACKED, BS 907. REPAIRED STRINGER PER SRM.

Part: SKIN — DELAMINATED (NR 2 LE SLAT)

DURING SCHEDULED D CHECK, FOUND NR 2 L/E SLAT DELAMINATED ON OUTBOARD END. REPAIRED SLAT PER SRM.

Part: FRAME — CRACKED (BS 827,787&867)

DURING SCHEDULED D CHECK, FOUND 3 EACH FRAMES CRACKED, BS 827, BS 787, STRINGER 8L, AND BS 867, STRINGER 8R. REPAIRED FRAMES PER ER NR 99-6247.

Part: FRAME — CRACKED (BS 299)

DURING SCHEDULED D CHECK, FOUND DOORWAY FRAME CRACKED, BS 299, RBL 62. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 482,400&380)

DURING SCHEDULED D CHECK, FOUND 3 EACH FRAMES CRACKED, BS 482, BS 400, STRINGER 8L, AND BS 380, STRINGER 8R. REPAIRED FRAMES PER ER NR 99-6247.

Part: KEEL BEAM — CORRODED (BS 482)

DURING SCHEDULED D CHECK, FOUND KEEL BEAM LT LOWER CHORD CORRODED, BS 482B+4. REPAIRED BEAM PER SRM.

Part: STRINGER — CRACKED (BS 1140)

DURING SCHEDULED D CHECK, FOUND STRINGER 5A LT CRACKED AT BS 1140. REPAIRED STRINGER SECTION PER SRM AND ER NR 99-6236PI.

Part: BEAM — CRACKED (BS 663)

DURING SCHEDULED D CHECK, FOUND LONGITUDINAL CENTER WING BOX BEAM CRACKED, BS 663, RBL 25. REMOVED AND REPLACED BEAM SECTION PER BAC DRAWING AND SRM.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED D CHECK, FOUND BS 328 FLOORBEAM CORRODED ON UPPER FACE. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 967)

DURING SCHEDULED D CHECK, FOUND BS 967 FLOORBEAM CORRODED ON UPPER AND LOWER FACES, RBL 27. REPAIRED BEAM PER SRM.

Part: SLIDE — DETACHED (PAX DOOR)

FORWARD ENTRY SLIDE DROPPED OUT OF MOUNT. INSPECTED AND SECURED SLIDE PER MM.

Part: AIR DISTRIBUTION — ODOR (COCKPIT)

EN ROUTE, COCKPIT CREW DETECTED SMELL OF ELECTRICAL SMOKE ODOR, LASTED SEVERAL MINUTES, THEN DISSIPATED. RESET APU CONTROL CB APU OPS CK GOOD PER BOEING MM. RAN APU AT FULL LOAD AND INSPECTED APU CONTROL CIRCUIT WIRING IN COCKPIT NO ELECTRICAL SMOKE ODOR PRESENT.

Part: LIGHT — INOPERATIVE (CABIN)

DURING EMERGENCY ESCAPE SLIDE TEARDOWN IN SHOP, FOUND ONE LIGHT STRIP LAMP INOP. REMOVED AND REPLACED PER BOEING MM.

Part: BULKHEAD — CRACKED (BS 178)

DURING D CHECK, FOUND BS 178 BULKHEAD CRACK INDICATION AT LBL7.7 TO LBL 8.7, WL 219. REPAIRED PER TRAMCO EWO 97-0486.

Part: BULKHEAD — CRACKED (BS 178)

DURING D CHECK, FOUND BS 178 BULKHEAD CRACK INDICATION AT LBL4.7, WL 198-198.5. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING D CHECK, FOUND BS 178 BULKHEAD CRACK INDICATION AT RBL 1, WL 187.5-188.5. REPAIRED PER TRAMCO EWO 97-0487.

Part: BULKHEAD — CRACKED (BS 178)

DURING D CHECK, FOUND BS 178 BULKHEAD CRACK INDICATION AT RBL6.7, WL 212.5-213. REPAIRED PER TRAMCO EWO 97-0486.

Part: STRAP — CRACKED (LT FLOORBEAM)

DURING SCHEDULED BC1 CHECK, FOUND LEFT FLOORBEAM STRAP CRACKED. REPAIRED PER BOEING SRM.

Part: CIRCUIT BREAKER — TRIPPED (PRESS CONTL SYST)

AT 35,000 FT CABIN ALTITUDE BEGAN TO CLIMB AT 500 FPM TO 1800 FPM. AIRCRAFT INITIATED DESCENT AND CABIN PRESSURE STABILIZED AT 12.000. AIRCRAFT CONTINUED AND LANDED AT STL WITHOUT INCIDENT. RESET PRESSURE CONTROL SYSTEM CIRCUIT BREAKER AND OPERATION CHECKED PER BOEING M/M.

Part: WINDSHIELD — CRACKED (LT COCKPIT)

CAPTAIN'S WINDSHIELD CRACKED. AIRCRAFT DIVERTED TO OAK AND MADE AN UNEVENTFUL LANDING. REPLACED PER BOEING M/M.

Part: UPLOCK SENSOR — MALFUNCTION (LT MLG)

AFTER TAKEOFF, LEFT MAIN GEAR RED LIGHT REMAINED ILLUMINATED. RECYCLED GEAR AND LIGHT EXTINGUISHED. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED, TIGHTENED RED LIGHT BASE, AND OPERATION CHECKED PER BOEING M/M. ON NEXT FLIGHT EXPERIENCED RED LIGHT FLICKERING IN FLIGHT. REPLACED LEFT MAIN GEAR UPLOCK SENSOR PER BOEING M/M.