N501SW

Part: LIGHT — LOOSE (CABIN) · airframe 66,185 hrs · 63,321 cycles

RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LOOSE BETWEEN ROW 12 TO ROW 13. SECURED LIGHT PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 66,163 hrs · 63,307 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER ASSY IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,163 hrs · 63,307 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 947.5, STR 20R. REPAIRED FRAME IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,163 hrs · 63,307 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CORRODED AT BS 482A, BETWEEN STR 28R TO STR 28L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,163 hrs · 63,307 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 25L. REPAIRED FRAME IAW EO AND EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 66,163 hrs · 63,307 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907+1.5, STR 4R. REMOVED AND REPLACED SPLICE IAW EO.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 66,163 hrs · 63,307 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED SPLICE IAW EO.

Part: TAB — DELAMINATED (ELEVATOR) · airframe 66,163 hrs · 63,307 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT ELEVATOR TAB DELAMINATED. REMOVED AND REPLACED TAB IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,163 hrs · 63,307 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 947.5, STR 25R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,163 hrs · 63,307 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 947, STR 25R. REPAIRED FRAME IAW EO AND EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 66,163 hrs · 63,307 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT PRESSURE BULKHEAD DOME WEB CRACKED AT BS 1016, BL 0. REPAIRED WEB IAW EO AND EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 66,163 hrs · 63,307 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT PRESSURE BULKHEAD DOME WEB CRACKED AT BS 1016, STR 7R. REPAIRED WEB IAW EO AND EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 66,163 hrs · 63,307 cycles

DURING SCHEDULED 22Y CHECK, FOUND AFT PRESSURE BULKHEAD DOME WEB CRACKED AT BS 1016, STR 15R.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 66,163 hrs · 63,307 cycles

DURING SCHEDULED 22Y CHECK, FOUND SUPPORT ANGLE CRACKED BETWEEN BS 847 TO BS 867, STR 25R. REMOVED AND REPLACED SUPPORT ANGLE PER SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,163 hrs · 63,307 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 482B, BETWEEN STR 28R TO STR 28L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 66,163 hrs · 63,307 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 7L. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,163 hrs · 63,307 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 321, BETWEEN STR 17L TO STR 21L. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 66,163 hrs · 63,307 cycles

DURING SCHEDULED 22Y CHECK, FOUND SUPPORT FITTING CRACKED AT BS 332.1, STR 8R. REMOVED AND REPLACED FITTING IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,163 hrs · 63,307 cycles

DURING SCHEDULE 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,163 hrs · 63,307 cycles

DURING SCHEDULE 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 967, STR 26R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,163 hrs · 63,307 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: LENS — MISSING (CABIN) · airframe 65,696 hrs · 62,982 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT SIDEWALL LIGHT LENS MISSING. REMOVED AND REPLACED LENS ASSY PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,202 hrs · 62,639 cycles

DURING SCHEDULED OTS CHECK FOUND, SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26 AND 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,202 hrs · 62,639 cycles

DURING SCHEDULED OTS CHECK FOUND, SKIN CRACKED BETWEEN BS 474.4 TO BS 475.9, STR 17L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,202 hrs · 62,639 cycles

DURING SCHEDULED OTS CHECK FOUND, SKIN CRACKED AT BS 787 + 3.5, STR 18L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,202 hrs · 62,639 cycles

DURING SCHEDULED OTS CHECK FOUND, FUSELAGE SKIN CRACKED AT BS 476, STR 17R. REPAIRED SKIN PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,202 hrs · 62,639 cycles

DURING SCHEDULED OTS CHECK FOUND, SHEAR TIE CORRODED AT BS 727C, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 65,202 hrs · 62,639 cycles

DURING SCHEDULED OTS CHECK FOUND, RT WING I/B FORE FLAP DELAMINATED ON UPPER SURFACE. REPAIRED FORE FLAP PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,202 hrs · 62,639 cycles

DURING SCHEDULED OTS CHECK FOUND, SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,202 hrs · 62,639 cycles

DURING SCHEDULED OTS CHECK FOUND, SHEAR TIE CORRODED AT BS 807, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,202 hrs · 62,639 cycles

DURING SCHEDULED OTS CHECK FOUND, SHEAR TIE CORRODED AT BS 827 BETWEEN STR 27L AND 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,202 hrs · 62,639 cycles

DURING SCHEDULED OTS CHECK FOUND, CREASE BEAM WEB CORRODED AT BS 450, LBL 65. REMOVED AND REPLACED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,202 hrs · 62,639 cycles

DURING SCHEDULED OTS CHECK FOUND, SKIN CRACKED AT BS 767 + 16, STR 24L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,202 hrs · 62,639 cycles

DURING SCHEDULED OTS CHECK FOUND, L2 DOOR FUSELAGE SKIN CRACKED AT BS 942, STR 24 LT. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,202 hrs · 62,639 cycles

DURING SCHEDULED OTS CHECK FOUND, SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 65,203 hrs · 62,639 cycles

DURING SCHEDULED OTS CHECK FOUND, FAIL SAFE CHORD AT STA 747 STR 26 - 27 LT IS CORRODED ON THE VERTICAL AND HORIZONTAL FLANGES. REPAIRED CHORD PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,203 hrs · 62,639 cycles

DURING SCHEDULED OTS CHECK FOUND, AFT FUSELAGE CRACKED AT BS 787+3." BELOW STR 18 LEFT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,203 hrs · 62,639 cycles

DURING SCHEDULED OTS CHECK FOUND, AFT FUSELAGE CRACK AT BS 767+16 ABOVE STR 24 LEFT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,202 hrs · 62,639 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACK AT BS 435.5, STR 17 LT. REPAIRED PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 65,203 hrs · 62,639 cycles

DURING SCHEDULED OTS CHECK, FOUND RT WING NR 6 SLAT LOWER SKIN CRACKED AT O/B END. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 65,203 hrs · 62,639 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 64,858 hrs · 62,408 cycles

DURING SCHEDULED OTS CHECK, FOUND EEPSL INOP. CHARGED BATTERY PER MM EEPLS.

Part: SLAT — CRACKED (LT WING) · airframe 64,858 hrs · 62,408 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING L/E NR 1 SLAT CRACKED. REPAIRED SLAT PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,858 hrs · 62,408 cycles

DURING SCHEDULED OTS CHECK, FOUND FRAME CRACKED AT BS 482, BETWEEN STR 20L TO STR 21L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,858 hrs · 62,408 cycles

DURING SCHEDULED OTS CHECK, FOUND FRAME CRACKED AT BS 520, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,858 hrs · 62,408 cycles

DURING SCHEDULED OTS CHECK, FOUND FRAME CRACKED AT BS 482A, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,856 hrs · 62,407 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER FWD CORNER. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,309 hrs · 61,997 cycles

DURING SCHEDULED MV3 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 64,225 hrs · 61,939 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 64,196 hrs · 61,921 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,045 hrs · 61,810 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 433.5, STR 1. REPAIRED SKIN PER EA.

Part: LIGHT — BROKEN (CABIN) · airframe 63,498 hrs · 61,433 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 62,991 hrs · 61,084 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 61,919 hrs · 60,321 cycles

AIR TURNBACK / DECLARED EMERGENCY. ON CLIMB PASSING FL 240 CABIN ALT WARN HORN SOUNDED. CABIN ALT CONTINUED DESCENT TO LANDING AT 500FT / MIN IN AUTO MAX CABIN ALT 10" STABILIZED AT 3" IN AUTO. REMOVED AND REPLACED OUTFLOW VALVE AND HEATER GASKET PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,398 hrs · 59,980 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 392, STR 15L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,398 hrs · 59,980 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 376, STR 15L. REPAIRED SKIN PER EA.

Part: LENS — MISSING (CABIN) · airframe 61,112 hrs · 59,802 cycles

FWD GALLEY OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: ACTUATOR — FAULTY (FUEL SYSTEM) · airframe 60,672 hrs · 59,526 cycles

DIVERSION - AFTER 1 + 30 OF FLIGHT TIME HAD 900LB IMBALANCE BETWEEN BOTH MAINS WITH 5000LBS REMAINING IN CENTER TANK - ALL PUMPS WERE "ON" FUEL FLOW BURNED FROM RT MAIN WITH CENTER PUMPS "ON". REMOVED AND REPLACED FUEL CROSSFEED VALVE ACTUATOR AND ACTUATOR GATE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,593 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: MOUNT — OUT OF POSITION (GIRT BAR) · airframe 60,606 hrs · 59,489 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR MOUNTS OUT OF POSITION. REPOSITIONED MOUNTS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,593 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,593 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,593 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,593 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,593 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: LIGHT — CORRODED (CABIN) · airframe 60,593 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND EEPLS CORRODED. REMOVED AND REPLACED EEPLS PER BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,593 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,593 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER EA.

Part: FLAP — CORRODED (LT WING) · airframe 60,593 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING I/B MIDFLAP I/B GIMBLE SHAFT YOKE CORRODED ON BEARING BORES. REMOVED AND REPLACED MIDFLAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,593 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER EA.

Part: CABLE — OUT OF POSITION (EVAC SLIDE) · airframe 60,593 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE OUT OF POSITION. REPOSITIONED CABLE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,593 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 747, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,593 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 45.5. REPAIRED BEAM PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,593 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 482, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,593 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,593 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,593 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,593 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 482A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,593 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 807, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,593 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,593 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,593 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 482A, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,593 hrs · 59,480 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 482, STR 8R. REPAIRED FRAME PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,370 hrs · 59,331 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,302 hrs · 59,283 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 59,937 hrs · 59,053 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: PANEL — LEAKING (RT WING) · airframe 59,858 hrs · 59,002 cycles

AIR TURNBACK / DECLARED EMERGENCY. FUEL LEAK TOP OF RT WING - VISIBLE IN FLIGHT. FUEL WAS SEEN STREAMING FROM PANEL ON TOP OF WING. FUEL COMING FROM PANEL 8817R. REMOVED AND REPLACED PANEL PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 59,723 hrs · 58,915 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,595 hrs · 58,834 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 421, STR 17L. REPAIRED SKIN PER SRM.

Part: SENSE LINE — PUNCTURED (NR 2 ENGINE) · airframe 58,821 hrs · 58,290 cycles

AIR TURNBACK / DECLARED EMERGENCY. ON TAKEOFF HAD 0 FAULT LIGHT ON FIRE DETECT SYS. THIS WAS FOLLOWED BY A NR 2 ENG OVERHEAT AND A NR 2 FIRE LIGHT. BOTH THE ENG OVERHEAT LIGHT AND FIRE LIGHT AS WELL AS THE FAULT LIGHT EXTINGUISHED WITHIN SECONDS. REMOVED AND REPLACED SENSE LINE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,046 hrs · 57,581 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 894, STR 25R. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 57,338 hrs · 57,077 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 3 STOP FITTING. REPAIRED FRAME PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,324 hrs · 57,062 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 759, STR 21L. REPAIRED SKIN PER SWA EA.

Part: LIGHT — BROKEN (CABIN) · airframe 57,261 hrs · 57,017 cycles

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

Part: LENS — DISLODGED (EMERGENCY LIGHT) · airframe 57,044 hrs · 56,860 cycles

L2 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,360 hrs · 56,342 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,360 hrs · 56,342 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 413, STR 16R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,360 hrs · 56,342 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,360 hrs · 56,342 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 489, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,360 hrs · 56,342 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 779, STR 18L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 55,797 hrs · 55,893 cycles

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

Part: LENS — MISSING (CABIN) · airframe 54,724 hrs · 54,927 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: KEELBEAM — CORRODED (BS 487) · airframe 54,691 hrs · 54,906 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT KEEL BEAM CORRODED AT BS 487. REPAIRED KEEL BEAM PER EA.

Part: KEELBEAM — CORRODED (BS 482) · airframe 54,691 hrs · 54,906 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT KEEL BEAM CORRODED AT BS 482. REPAIRED KEEL BEAM PER EA.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 54,691 hrs · 54,906 cycles

DURING SCHEDULED 18Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: FRAME — CRACKED (BS 277 S16L) · airframe 54,960 hrs · 54,905 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER EA.

Part: FLOORBEAM — CRACKED (BS 706) · airframe 54,690 hrs · 54,905 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CRACKED AT BS 706, LBL 49. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (BS 578 S14R) · airframe 54,690 hrs · 54,905 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 578, STR 14R. REPAIRED FRAME PER EA.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 54,690 hrs · 54,905 cycles

DURING SCHEDULED 18Y CHECK, FOUND VERTICAL STABILIZER FITTING FWD AND AFT LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: SKIN — CORRODED (BS 468) · airframe 54,690 hrs · 54,905 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 468, BL 0. REPAIRED SKIN PER EA.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 54,690 hrs · 54,905 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT WING INBOARD FOREFLAP DELAMINATED AT UPPER SURFACE. REMOVED AND REPLACED FOREFLAP PER MM.

Part: FRAME — CRACKED (BS 380 S16R) · airframe 54,690 hrs · 54,905 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16R. REPAIRED FRAME PER EA.

Part: WEDGE — DELAMINATED (T/E FLAP) · airframe 54,690 hrs · 54,905 cycles

DURING SCHEDULED 18Y CHECK, FOUND RIGHT WING INBOARD MID FLAP T/E WEDGE LOWER SURFACE DELAMINATED. REMOVED AND REPLACED WEDGE PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 54,690 hrs · 54,905 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,690 hrs · 54,905 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,690 hrs · 54,905 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 867 S6R) · airframe 54,609 hrs · 54,905 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 578 S10R) · airframe 54,609 hrs · 54,905 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 520 S14R) · airframe 54,609 hrs · 54,905 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 14R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 440 S21L) · airframe 54,960 hrs · 54,905 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 400 S14L) · airframe 54,960 hrs · 54,905 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 440 S21L) · airframe 54,960 hrs · 54,905 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 400 S14L) · airframe 54,690 hrs · 54,905 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,646 hrs · 54,863 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,454 hrs · 54,683 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 374, STR 26R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 787 S23L) · airframe 53,918 hrs · 54,172 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 23L. REPAIRED SKIN PER SWA EA.

Part: BEARING — WORN (RT ELEVATOR) · airframe 53,672 hrs · 53,945 cycles

DURING SCHEDULED C4 CHECK, RIGHT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD BEARING PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,672 hrs · 53,945 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 446, STR 16R. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,588 hrs · 53,862 cycles

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

Part: SKIN — CRACKED (BS 757 S18L) · airframe 53,402 hrs · 53,677 cycles

FUSELAGE SKIN CRACKED AT BS 757, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 767 S22L) · airframe 53,137 hrs · 53,416 cycles

FUSELAGE SKIN CRACKED AT BS 767, STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,960 hrs · 53,231 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 52,915 hrs · 53,187 cycles

DURING SCHEDULED THRU CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,893 hrs · 53,169 cycles

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

Part: SKIN — CRACKED (BS 872 S25R) · airframe 52,486 hrs · 52,737 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 872, STR 25R. REPAIRED SKIN PER SRM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 52,278 hrs · 52,529 cycles

DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: LIGHT — LOOSE (RT OVERWING) · airframe 52,066 hrs · 52,312 cycles

RT OVERWING EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM.

Part: SKIN — CRACKED (BS 976 S21L) · airframe 51,991 hrs · 52,233 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 976, STR 21L. REPAIRED SKIN PER SWA EA.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,619 hrs · 50,717 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT BULL NOSE LIGHT INOP AT ROW 3 ABC. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (BS 312) · airframe 50,429 hrs · 50,508 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, WL 208 RT SIDE. REPAIRED SKIN PER SRM AND SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,574 hrs · 49,570 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,574 hrs · 49,570 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,574 hrs · 49,570 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD FRAME NR 5 STOP FITTING. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SHEAR TIE — CRACKED (BS 360) · airframe 49,574 hrs · 49,570 cycles

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

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 49,574 hrs · 49,570 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN BEAR STRAP CORRODED AT FWD CARGO DOOR CUTOUT UPPER CORNERS. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 49,574 hrs · 49,570 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE BULKHEAD WEB CRACKED AT BS 178, RBL 5.7, WL 187. REPAIRED BULKHEAD WEB PER SRM.

Part: SKIN — CRACKED (BS 890) · airframe 49,282 hrs · 49,265 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 890, STR 17L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,393 hrs · 48,349 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,393 hrs · 48,349 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,206 hrs · 48,167 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520 + 6, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,206 hrs · 48,167 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 400, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,206 hrs · 48,167 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 870, STR 23R. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 47,599 hrs · 47,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE AT FWD GALLEY. SECURED LENS PER MM.

Part: PANEL — CRACKED (NLG W/W) · airframe 47,599 hrs · 47,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND NLG W/W CEILING PANEL CRACKED AT LT & RT BRAKE MOUNT PADS. REPAIRED PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,599 hrs · 47,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT CARGO DOOR CUTOUT, FWD LOWER CORNER. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,599 hrs · 47,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM UPPER T-CAP AT BS 986, BETWEEN RBL 45 TO LBL 45. REMOVED AND REPLACED UPPER T-CAP PER TYPICAL REPAIR MANUAL.

Part: FRAME — CRACKED (E/E BAY) · airframe 47,599 hrs · 47,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, BL 0. REPAIRED FRAME PER SRM.

Part: GUSSET — CRACKED (R1 DOOR) · airframe 47,599 hrs · 47,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND R1 DOOR AFT LOWER GUSSET CRACKED. REMOVED AND REPLACED GUSSET PER SRM & BAC DRAWING.

Part: SKIN — CRACKED (R1 DOOR) · airframe 47,599 hrs · 47,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT, AFT LOWER CORNER. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,599 hrs · 47,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (R1 DOOR) · airframe 47,599 hrs · 47,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND R1 DOOR LOWER AFT FRAME CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 47,599 hrs · 47,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE CREASE BEAM WEB CRACKED AT BS 616, RBL 64. REPAIRED WEB PER SWA EA & SRM.

Part: STRINGER CLIP — CRACKED (AFT CARGO) · airframe 47,599 hrs · 47,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727 B, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,599 hrs · 47,551 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED AT BS 638, RBL 65. REPAIRED WEB PER SWA EA & SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 46,981 hrs · 46,909 cycles

DURING SCHEDULED C4 CHECK, FOUND RT HORIZONTAL STAB, LOWER SKIN AT STA 140, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,762 hrs · 46,681 cycles

FUSELAGE SKIN AT BS 517, STRINGER 17R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 46,154 hrs · 46,092 cycles

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

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 46,109 hrs · 46,036 cycles

R1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED R1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 46,053 hrs · 45,874 cycles

L1 DOOR EVACV SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM.

Part: STRIP — WORN (ROWS 10 - 13 ABC) · airframe 45,303 hrs · 45,217 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS FLOOR STRIP AT ROW 10 ABC TO ROW 13 ABC, WORN. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 45,303 hrs · 45,217 cycles

DURING SCHEDULED C2 CHECK, FOUND L2 AND R2 DOOR EVAC SLIDE CABLES MISROUTED. REROUTED L2 AND R2 DOOR EVAC SLIDE CABLES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,357 hrs · 44,273 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BS 482B + 17, STRINGER 12R. REPAIRED SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 43,559 hrs · 43,544 cycles

DURING SCHEDULED PM CHECK, FOUND A 3.5 LONG CRACK AT NLG W/W SIDE WEB, BS 258. REPAIRED WEB PER SWA EA.

Part: CLAMP — BROKEN (AIR DUCT) · airframe 43,019 hrs · 43,030 cycles

DECLARED EMERGENCY, CABIN ALTITUDE WARNING HORN SOUNDED AT CRUISE. FOUND, KEELBEAM DUCT CLAMP BROKEN. REMOVED AND REPLACED DUCT CLAMP AND SEAL PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,705 hrs · 42,738 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) BS 502 AT STR 10R AND BS 878 AT STR 25R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 42,483 hrs · 42,532 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,870 hrs · 41,952 cycles

DURING SCHEDULED PM CHECK, FOUND 2.5 INCH LONG CRACK, BS 727D, STRINGER 18L. REPAIRED SKIN PER SRM.

Part: TRACK — CRACKED (CABIN) · airframe 41,870 hrs · 41,952 cycles

DURING SCHEDULED C2 CHECK, FOUND SEVERAL EEPLS PHOTOLUMINESCENT SECTIONS CRACKED BETWEEN ROW 10 DEF & ROW 19 DEF. REMOVED AND REPLACED EEPLS STRIPS PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 41,392 hrs · 41,492 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER WHEN CLOSING DOOR. REINSTALLED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,087 hrs · 41,228 cycles

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

Part: STRIP — LOOSE (CABIN FLOOR) · airframe 40,928 hrs · 41,079 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 11 DEF. SECURED STRIP PER MM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 40,122 hrs · 40,303 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 665, RBL 32. REPAIRED WEB PER SRM.

Part: COVER — CRACKED (CABIN) · airframe 40,068 hrs · 40,250 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 1. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 39,486 hrs · 39,699 cycles

DURING SCHEDULED PM CHECK, FOUND EEPLS COVERS LOOSE (7 EA) IN CABIN. SECURED EEPLS COVERS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 39,441 hrs · 39,659 cycles

EEPLS LOOSE AND DISCONNECTED AT ROW NR 12. SECURED AND CONNECTED EEPLS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 39,420 hrs · 39,639 cycles

EEPLS LOOSE AT ROW NR 13. SECURED EEPLS PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 39,411 hrs · 39,629 cycles

EEPLS DAMAGED AT MID CABIN. REPAIRED EEPLS PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 39,392 hrs · 39,610 cycles

EEPLS LOOSE AT ROW'S NR 12 AND NR 13. REPAIRED WIRES AND INSTALLED MISSING COVERS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 39,373 hrs · 39,591 cycles

EEPLS LOOSE AT ROW NR 12. REMOVED AND REPLACED EEPLS AT ROW NR 12 PER MM.

Part: COVER — LOOSE (CABIN) · airframe 39,326 hrs · 39,546 cycles

EEPLS WIRES EXPOSED AT ROW NR 7. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 39,315 hrs · 39,536 cycles

SEVERAL EEPLS INOP IN CABIN. RECONNECTED WIRE PER MM.

Part: WIRE — LOOSE (CABIN) · airframe 38,822 hrs · 39,055 cycles

EEPLS WIRES LOOSE ON CABIN FLOOR. SECURED WIRES PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,804 hrs · 39,036 cycles

EEPLS INOP BETWEEN ROW'S 10 AND 13. REPAIRED EEPLS PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 38,567 hrs · 38,812 cycles

EEPLS DAMAGED AT ROW 13. REMOVED AND REPLACED EEPLS AT ROW 13 PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 38,486 hrs · 38,737 cycles

EEPLS BROKEN AT MID CABIN. REMOVED AND REPLACED EEPLS SECTION PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 38,249 hrs · 38,528 cycles

DURING SCHEDULED C2 CHECK, FOUND KEEL BEAM CORRODED AT BS 482. REPAIRED KEEL BEAM PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 38,249 hrs · 38,528 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS LOOSE AT ROW NR 12. SECURED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,989 hrs · 37,289 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 23L. REPAIRED SKIN PER SRM.

Part: COVER — BROKEN (CABIN) · airframe 36,902 hrs · 37,215 cycles

EEPLS COVER BROKEN AT ROW 15. R&R COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 36,734 hrs · 387,049 cycles

EEPLS COVER LOOSE AT ROW 1. SECURED COVER PER MM.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 34,667 hrs · 34,618 cycles

DURING SCHEDULED RON CHECK, FOUND WINDOW POST CRACKED AT CAPT'S #1 WINDOW, UPPER LH CORNER. REPAIRED WINDOW POST PER SRM.

Part: BRACKET — BROKEN (WINDOW) · airframe 35,823 hrs · 36,156 cycles

DECLARED EMERGENCY, TOXIC FUMES IN COCKPIT. SOURCE OF ODOR AT, F/O'S NR 5 EYEBROW WINDOW. SENSOR SPRING BRACKET BROKEN, SPRING SHORTED OUT SENSOR WIRES. CONT PER MEL 30-11. ON 16 JUN AT DAL REMOVED AND REPLACED SPRING BRACKET PER MM.

Part: SLIDE — OUT OF ADJ (AFT SVC DOOR) · airframe 34,780 hrs · 35,164 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM.

Part: ENGINE — BIRD STRIKE (NR 1) · airframe 33,209 hrs · 33,634 cycles

AIR TURNBACK. SMOKE SMELL IN CABIN AFTER TAKEOFF. EVIDENCE OF BIRD STRIKE FOUND AT NR 1 ENGINE. C/W BIRD STRIKE INSPECTION AND NR 1 ENG BORESCOPE INSPECTION. NO DEFECT NOTED.

Part: WIRE — EXPOSED (CABIN FLOOR) · airframe 32,951 hrs · 33,373 cycles

EEPLS WIRES EXPOSED AT MID CABIN. SECURED WIRES AND REPLACED COVERS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,045 hrs · 32,447 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED, BS 440, BETWEEN STRINGERS 8 - 9 RT AND BS 787, BETWEEN STRINGERS 8 -9 LT. REPAIRED FRAMES PER SRM AND ER 00-0361.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,045 hrs · 32,447 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED, BS 727B, BS 827, BS 520, BETWEEN STRINGERS 8 -9 RT AND BS 907, BS 827. BETWEEN STRINGERS 8 -9 LT. REPAIRED FRAMES PER SRM AND EO 00-00361.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,045 hrs · 32,447 cycles

DURING SCHEDULED D CHECK, FOUND BS 360 FUSELAGE FRAME CRACKED, STRINGER 8L. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,045 hrs · 32,447 cycles

DURING SCHEDULED D CHECK, FOUND BS 947 FLOOR BEAM UPPER SURFACE CORRODED, RBL 5 AND RBL 48. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,045 hrs · 32,447 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 188. WL 208. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 32,045 hrs · 32,447 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE 4 LT CRACKED, BS 907. R&R STRINGER SPLICE SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,045 hrs · 32,447 cycles

DURING SCHEDULED D CHECK, FOUND 2 EACH FUSELAGE FRAMES CRACKED, BS 787 BETWEEN STRINGERS 8 - 9 RT, AND BS 867, BETWEEN STRINGERS 8 LT AND 9 LT. REPAIRED FRAMES PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,045 hrs · 32,447 cycles

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 5 TO RBL 1. R&R BULKHEAD WEB PER ACO 7154-53.

Part: COVER — CRACKED (CABIN)

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVERS CRACKED, LOOSE AT ROWS 21 AND ROW 1. REPLACED TRACK COVERS PER MM.

Part: LIGHT — INOPERATIVE (ROW 14)

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT ROW 14. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: KEEL BEAM — CRACKED (BS 717)

DURING SCHEDULED C2 CHECK, FOUND KEEL BEAM CRACKED AT LOWER SKIN, BS 717. REPAIRED BEAM PER SRM.

Part: LENS — MISSING (CABIN)

DURING SCHEDULED RON, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING NEXT TO ROW 15. REPLACED LENS PER MM.

Part: LIGHT — INOP (ROW 20)

DURING SCHEDULED C1 CHECK, FOUND EEPLS LIGHT AT ROW 20 INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — MISSING (CABIN)

EMERGENCY EXIT TRACK LIGHT WIRING EXPOSED ON AFT SECTION. INSTALLED TRACK COVER PER MM.

Part: WIRE — OUT OF ADJ (ROW 15 & 18)

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOP BETWEEN SEAT ROWS 15 AND 18. READJUSTED FLOOR WIRING PER M/M.

Part: CIRCUIT BREAKER — MALFUNCTIONED (COCKPIT)

NR 1 ENGINE SHUTDOWN AFTER ENGINE START. RETURNED TO GATE. CYCLED NR 1 ENG, FUEL SHUT-OFF VALVE C/B, SYSTEM OP CKS NORMAL.

Part: AIR DIST — ODOR (CARGO COMPT)

AT GATE NOTED VERY CAUSTIC FUMES IN FWD B/B, BURNED EYES AND THROAT. INSPECTED FWD CARGO BIN FOR EVIDENCE OF A SPILL, NONE NOTED. CLEANED AREA FOR PRECAUTION, APPLIED VENTILATION AS REQUIRED FOR ODOR.

Part: SLIDE — DEPLOYED (SERV DOOR)

DURING WALKAROUND CHECK, FOUND FWD SERVICE DOOR ESCAPE SLIDE ACCIDENTALLY DEPLOYED AFTER ENGINES/SHUT DOWN. REPAIRED PER BOEING MM.

Part: GIRT BAR — WORN (SERVICE DOOR)

DURING SCHEDULED BC4 CHECK, FOUND FWD SERVICE DOOR EMERGENCY SLIDE GIRT BAR MATERIAL WORN/FRAYED. REMOVED AND REPLACED FWD SERVICE DOOR EMERGENCY SLIDE AS PER BOEING MM.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR UPPER HINGE CUTOUT CRACKED .25 INCH. REPAIRED PER BOEING SRM.

Part: WIRE — BROKEN (CABIN)

DURING SCHEDULED C1 CHECK, FOUND FLOOR TRACK LIGHTS INOP AT OVERWING EXIT 3 LIGHTS IN AFT CABIN. REPAIRED BROKEN WIRES PER BOEING M/M.

Part: FLOORBEAM — CORRODED (BS 947)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947 LBL 10 AND 5 AT BS 986.5 LBL 15 AND RBL 6. REPAIRED PER SWA RA 1-553-1329 AND BOEING STRUCTURAL REPAIR MANUAL.

Part: DOOR FRAME — DAMAGED (CARGO DOOR)

DURING SCHEDULED 1/2 D-CHECK, FOUND AFT CARGO DOOR FWD AND AFT LOWER FRAME WEBS DAMAGED. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: T-CHORD — CRACKED (BS 539)

DURING SCHEDULED 1/2 D-CHECK, FOUND A/C RAM AIR INLET WEB T-CHORD CRACKED JUST BELOW UPPER DRAG ANGLE AT BS 539. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: ANGLE — CRACKED (BS 727)

DURING SCHEDULED 1/2 D-CHECK, FOUND BULKHEAD SUPPORT ANGLE CRACKED AT BS 727 RBL 3. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FLOORBEAM — CORRODED (BS 294.5)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 294.5 RBL 42 AND 45. REPAIRED PER SWA RA 1-553-1325 AND BOEING STRUCTURAL REPAIR MANUAL.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 312 LBL 14. REPAIRED PER SWA RA 1-553-1327 AND BOEING STRUCTURAL REPAIR MANUAL.

Part: EEL BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN FLOOR TRACK LIGHTS AND RIGHT AFT EXTERIOR EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: EEL BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT EMERGENCY FLOOR TRACK LIGHTING AND RIGHT AFT EXTERIOR LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.