N511SW

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 71,928 hrs · 68,010 cycles

RIGHT OVERWING EXIT LIGHT ASSEMBLY INOPERATIVE. R & R POWER SUPPLY IAW MM.

Part: STOP FITTING — CRACKED (L2 DOOR) · airframe 71,856 hrs · 67,935 cycles

L2 DOOR UPPER FWD STOP PIN FITTING CRACKED. R & R DOOR IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,511 hrs · 67,519 cycles

FUSELAGE SKIN CRACKED AT STATION 445, STRINGER 16R. REPAIRED SKIN IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 71,205 hrs · 67,186 cycles

RIGHT EMER LIGHT LENS LOOSE AT ROW 16. SECURED LENS IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 71,205 hrs · 67,186 cycles

LEFT OVERWING EMER LIGHT LENS LOOSE. SECURED LIGHT IAW MM.

Part: LENS — MISSING (CABIN) · airframe 70,995 hrs · 66,959 cycles

RIGHT OVERWING EMER EXIT LIGHT LENS COVER MISSING. INSTALLED COVER IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,922 hrs · 66,884 cycles

FORWARD SERVICE DOOR LOWER EMER EXIT LIGHT BULB INOPERATIVE. RE-LAMPED LIGHT IAW AMM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 70,922 hrs · 66,884 cycles

BRACKET CRACKED AT BS 986.5 STRINGER 3L. R & R BRACKET IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 70,922 hrs · 66,884 cycles

RIGHT WING UPPER TE PANEL JUST OTBD OF THE PYLON AFT ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,922 hrs · 66,884 cycles

FUSELAGE SKIN CRACKED AT BS 987 STRINGER 7L. REPAIRED SKIN IAW SRM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 70,922 hrs · 66,884 cycles

BULKHEAD PRESS WEB CORRODED AT BS 1017 LBL 8. REPAIRED WEB IAW EA.

Part: SPOILER — DELAMINATED (RT WING) · airframe 70,822 hrs · 66,767 cycles

RIGHT WING NR 8 SPOILER DELAMINATED. R & R SPOILER IAW MM.

Part: ANGLE — CRACKED (RT AILERON) · airframe 70,822 hrs · 66,767 cycles

RIGHT WING AILERON DRY BAY STATION 534, VERTICAL ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 70,455 hrs · 66,374 cycles

DIVERSION, DECLARED EMERGENCY AT FL320 OVER PMD FWD LAVATORY SMOKE DETECTOR WENT OFF. R & R LAVATORY SMOKE DETECTOR IAW AMM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 70,198 hrs · 66,106 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 69,909 hrs · 65,802 cycles

RT OVERWING EXIT EMERGENCY LIGHT LENS LOOSE. SECURED LENS IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,535 hrs · 65,406 cycles

FUSELAGE SKIN CRACKED AT BS 404 STRINGER 16R. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,230 hrs · 65,092 cycles

RT OVERWING DOOR EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: ANGLE — CRACKED (RT WING) · airframe 69,230 hrs · 65,092 cycles

NR 6 CANOE FAIRING THE OTBD ANGLE AT THE FORE FLAP CRACKED. R & R ANGLE IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,230 hrs · 65,092 cycles

AFT LAVATORY EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: WIRE — DAMAGED (COCKPIT) · airframe 69,230 hrs · 65,092 cycles

COCKPIT EMERGENCY LIGHT INOPERATIVE. REPAIRED R340 DIMMING LIGHT WIRING IAW MM.

Part: FRAME — CRACKED (FLAP CARRIAGE) · airframe 69,230 hrs · 65,092 cycles

RT OTBD MID FLAP INBD CARRIAGE A-FRAME ARM ASSEMBLY CRACKED. R & R FRAME ASSEMBLY IAW SOPM.

Part: WIRE — BROKEN (CABIN) · airframe 69,230 hrs · 65,092 cycles

EMERGENCY EXIT LIGHT IN CEILING PANEL ABOVE ENTRY DOOR WIRE BROKEN. REPAIRED WIRE IAW WDM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

CREASE BEAM INNER CHORD UPPER SURFACE CRACKED AT BS 616, RBL 65. REPAIRED CHORD IAW SRM.

Part: PANEL — CRACKED (RT HORIZ STAB) · airframe 69,230 hrs · 65,092 cycles

RT HORIZONTAL STAB GAP PANEL 9223R CRACKED FWD TRACK ASSEMBLY AT FUSELAGE. R & R PANEL IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

AFT CARGO BAY STRINGER CORRODED AT BS 910, STRINGER 25L. R & R STRINGER IAW SRM & DRAWING.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

AFT CARGO BAY ON STRINGER SPLICE CORRODED AT BS 907, STRINGER 25L. R & R SPLICE IAW SRM & DRAWING.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

STRINGER CRACKED AT BS 482B +10, STRINGER 15L. REPAIRED STRINGER IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

FRAME CRACKED AT BS 328, BETWEEN STRINGER 20R TO STRINGER 21R. REPAIRED FRAME IAW ER & EA.

Part: SKIN — CHAFED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

FUSELAGE SKIN CHAFED UNDER DORSAL FIN AT SEAL CONTACT POINT, BS 862 TO BS 887, STRINGER 2L TO STRINGER 2R. REPAIRED SKIN IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

FRAME CRACKED AT BS 947.5, STRINGER 18R. R & R FRAME IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

FRAME CRACKED AT BS 380, STRINGER 19R. REPAIRED FRAME IAW ER & EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

STRINGER CRACKED AT BS 463, STRINGER 2L. REPAIRED STRINGER IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

STRINGER CLIP CRACKED AT BS 663.75, STRINGER 4L. R & R CLIP IAW SRM & DRAWING.

Part: SKIN — CRACKED (R1 DOOR) · airframe 69,230 hrs · 65,092 cycles

R1 DOOR INNER SKIN CRACKED AT CUTOUT CORNER BELOW CONTROL ROD FWD ATTACH POINT. REPAIRED SKIN IAW SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

CHORD CORRODED AT BS 270, BETWEEN LBL 10 TO RBL10. R & R CHORD IAW SRM & DRAWING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

SEAT TRACK CORRODED BETWEEN BS 727B TO BS 947, RBL 45. R & R SEAT TRACK IAW SRM & DRAWING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

SEAT TRACK CORRODED BETWEEN BS 727B TO BS 947, LBL 25. R & R SEAT TRACK IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

NLG INSPECTION WINDOW INTERCOSTAL CORRODED. R & R INTERCOSTAL IAW SRM & DRAWING.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

SEAT TRACK CORRODED BETWEEN BS 727B TO BS 947, LBL 45. R & R SEAT TRACK IAW SRM & DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

STRINGER CLIP CRACKED AT STATION 360, STRINGER 15L. R & R CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

FUSELAGE FRAME CRACKED AT BS 348, STRINGER 16L. REPAIRED FRAME IAW SWA EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

FRAME SHEAR WEB CRACKED AT BS 348, STRINGER 16L. R & R INTERCOSTAL IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

FUSELAGE SKIN CRACKED AT L1 DOOR AFT LOWER CUTOUT. REPAIRED SKIN IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

FRAME CRACKED AT BS 482, STRINGER 14L. REPAIRED FRAME IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

L1 DOOR UPPER HINGE H STRAP CRACKED AFT LOWER END IN RADIUS. R & R STRAP IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

SKIN CRACKED BETWEEN BS 933 TO 934.4, STRINGER 22R. REPAIRED SKIN IAW SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 69,230 hrs · 65,092 cycles

MAIN WW PRESSURE DECK CRACKED BETWEEN BS 672.5 TO BS 673, RBL41. REPAIRED DECK IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

SKIN CRACKED AT BS 908, STRINGER 4L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

SKIN CRACKED BETWEEN BS 942.3 TO BS 944, STRINGER 22L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

SKIN CRACKED BETWEEN BS 783.4 TO BS 784.5, STRINGER 21L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

FUSELAGE SKIN CRACKED TA BS 392.5 TO BS 396, STRINGER 1. REPAIRED SKIN IAW SWA EA.

Part: LENS — CRACKED (CABIN) · airframe 69,230 hrs · 65,092 cycles

AFT LAVATORY EMERGENCY EXIT LIGHT LENS COVER BROKEN. R & R LENS IAW MM.

Part: SKIN — CRACKED (LT WING) · airframe 69,230 hrs · 65,092 cycles

LT WING NR 3 SLAT ACTUATOR CUTOUT INNER SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

SKIN CRACKED BETWEEN BS 892 TO BS 894.5, STRINGER 24R. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

FUSELAGE FRAME CRACKED AT BS 520, STRINGER 20L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

FRAME FWD FLANGE CRACKED AT BS 727, STRINGER 18A LT. REPAIRED FLANGE IAW EA.

Part: SLIDE — CRACKED (L1 DOOR) · airframe 69,230 hrs · 65,092 cycles

L1 DOOR ESCAPE SLIDE GIRT HAS CRACKED PLASTIC SLEEVE AT AFT END. R & R SLIDE ASSEMBLY IAW MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

SKIN CRACKED AT BS 482B+14, STRINGER 16L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

FUSELAGE SKIN CRACKED AT BS 425, STRINGER 17R. REPAIRED SKIN IAW ER & SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

FRAME FWD FLANGE CRACKED AT BS 727, STRINGER 18A RT. REPAIRED FLANGE IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,230 hrs · 65,092 cycles

FUSELAGE SKIN CRACKED AT BS 482B+6, STRINGER 16R. REPAIRED SKIN IAW SWA EA.

Part: COVER — LOOSE (R1 DOOR) · airframe 69,230 hrs · 65,092 cycles

R1 DOOR EMERGENCY EVAC SLIDE COVER LOOSE. SECURED COVER IAW SRM.

Part: SENSOR — FAULTY (NR 2 ENGINE) · airframe 69,230 hrs · 65,092 cycles

NR 2 ENGINE WILL NOT GO TO IDLE IN DESCENT WITH THRUST LEVERS AT IDLE. R & R CIT SENSOR IAW AMM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 68,945 hrs · 64,801 cycles

LT OVERWING EXIT SIGN LOOSE. R&R LENS IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,848 hrs · 63,635 cycles

SKIN CRACKED AT BS 360, BETWEEN STR 1L AND STR 2L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,848 hrs · 63,635 cycles

SKIN CRACKED AT BS 360, BETWEEN STR 2R AND STR 3R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,848 hrs · 63,635 cycles

SKIN CRACKED AT BS 360, BETWEEN STR 1R AND STR 2R. REPAIRED SKIN IAW EA.

Part: SENSOR — FAULTY (NR 2 ENGINE) · airframe 67,298 hrs · 63,058 cycles

ON DESCENT FROM FL 210, POWER REDUCED ON BOTH ENGINES, NR 2 ENGINE NOT RESPONSIVE TO THRUST LEVER POSITION FOR +1/-2 MINS AND MAINTAINED 80% N1 WHILE / THE LEVER AT 101E. SUBSEQUENTLY BEGAN RESPONDING TO THRUST LEVER AND OPERATED NORMALLY TO LANDING

Part: SENSOR — FAULTY (NR 2 ENGINE) · airframe 67,298 hrs · 63,058 cycles

POWER REDUCED ON BOTH ENGINE NR 2 ENGINE NOT RESPONSIVE TO THRUST LEVER POSITION. REMOVED AND REPLACED SENSORS IAW M/M.

Part: LENS — MISSING (EXIT SIGN) · airframe 67,080 hrs · 62,861 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN MISSING. INSTALLED LENS PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,756 hrs · 62,512 cycles

FUSELAGE SKIN CRACKED AT BS 498, STR 19R. REPAIRED SKIN PER EA.

Part: LENS — MISSING (CABIN) · airframe 65,851 hrs · 61,967 cycles

FWD EEPLS LENS MISSING. INSTALLED LENS IAW M/M.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 65,410 hrs · 61,682 cycles

L2 DOOR LOWER EMERGENCY LIGHT INOP. RECONNECTED LIGHT ASSY IAW MM.

Part: FRAME — BROKEN (FUSELAGE) · airframe 65,411 hrs · 61,682 cycles

FUSELAGE FRAME BROKEN AT BS 847, BETWEEN STRINGERS 17R AND 18R LOWER END IS BROKEN. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 65,411 hrs · 61,682 cycles

LT AFT INNER CHORD CORRODED AT BS 967, LBL 52 IAW SRM. REPAIRED CHORD IAW AMM.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 65,411 hrs · 61,682 cycles

LEFT WING I/B FORE FLAP LOWER SURFACE PUNCTURED. REPAIRED FORE FLAP IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 65,411 hrs · 61,682 cycles

R2 DOOR THRESHOLD CENTER FLOOR PAN WEB CORRODED AT STA 980. REMOVED AND REPLACED WEB PER BAC DWG & SRM.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 65,411 hrs · 61,682 cycles

LT WING INBD FORE FLAP LOWER SURFACE PUNCTURED. REPAIRED FLAP PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 65,411 hrs · 61,682 cycles

LEFT WING I/B FOREFLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 65,411 hrs · 61,682 cycles

SHEAR WEB ANGLE CRACKED BETWEEN BS 380 TO BS 400, BL 0. REMOVED AND REPLACED ANGLE PER BAC DWG AND SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,411 hrs · 61,682 cycles

FLOORBEAM WEB CRACKED AT BS 295.5, LBL 53. REPAIRED WEB IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 65,411 hrs · 61,682 cycles

FWD CARGO DOOR CUTOUT AREA AFT TORQUE BOX LOWER AFT CORNER INNER WEB CRACKED. REMOVED AND REPLACED WEB PER MM, SRM, & BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,411 hrs · 61,682 cycles

RT CREASE BEAM WEB CORRODED BETWEEN BS 847 TO BS 86.7. REMOVED & REPLACED WEB IAW BAC DWG, SRM, & AMM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,411 hrs · 61,682 cycles

MAIN CABIN FLOORBEAM T-CAP CRACKED AT BS 294.5, LBL 52. REMOVED T-CAP IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 65,410 hrs · 61,682 cycles

COCKPIT FLOOR WEB CRACKED AT BS 247, RBL 23. REMOVED AND REPLACED WEB PER ACO.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,411 hrs · 61,682 cycles

LT CABIN CREASE BEAM WEB CORRODED AT BS 370. REMOVED AND REPLACED WEB IAW BAC DWG AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,411 hrs · 61,682 cycles

L2 DOOR FUSELAGE SKIN FWD LOWER CORNER CRACKED AT UPPER RADIUS OF CORNER LOWEST FASTENER. REPAIRED SKIN PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 65,411 hrs · 61,682 cycles

RT FLOOR SUPPORT BS 986.5, RBL 16 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 65,411 hrs · 61,682 cycles

FORWARD CARGO PIT DOOR CUTOUT AREA LOWER TORQUE BOX CRACKED BETWEEN BS 420 TO BS 440, STR 26R. REPAIRED WEB PER EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 65,411 hrs · 61,682 cycles

LT CREASE BEAM CORRODED AT BS 867 TO BS 887. REPAIRED BEAM PER SRM AND BAC DRAWING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,411 hrs · 61,682 cycles

FLOORBEAM CORRODED AT BS 986, RBL 45. REPAIRED FLOORBEAM PER SRM AND EA.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 65,012 hrs · 61,431 cycles

EMERGENCY EXIT LIGHT ON G-4 GALLEY INOPERATIVE. REMOVED AND REPLACED WIRE IAW SWPM AND AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,012 hrs · 61,431 cycles

CRACK IN SKIN AT CHEM MILL AT BS 758.5, STR 23 LT. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (BS 787 S19-20L) · airframe 65,012 hrs · 61,431 cycles

SHEAR TIE CRACKED AT BS 787, BETWEEN STR 19 TO STR 20L. REMOVED AND REPLACED SHEAR TIE PER DWG, SRM AND AMM.

Part: STRINGER CLIP — CRACKED (BS 767 S22L) · airframe 65,012 hrs · 61,431 cycles

STRINGER CLIP CRACKED AT BS 767, STR 22 L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,012 hrs · 61,431 cycles

CRACK IN FUSELAGE SKIN AT CHEM-MILL BS 769.5 BELOW STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,012 hrs · 61,431 cycles

CRACK IN FUSELAGE SKIN AT CHEM-MILL AT BS 764 ABOVE STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,012 hrs · 61,431 cycles

CRACK IN FUSELAGE SKIN AT CHEM-MILL BS 841.75 ABOVE STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,012 hrs · 61,431 cycles

CRACK IN FUSELAGE SKIN AT BS 832.25, STR 17L. REMOVED SKIN IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 65,012 hrs · 61,431 cycles

FUSELAGE SKIN IS CORRODED AROUND FASTENERS AT THE LWR AFT CORNER OF THE FWD LAV SERVICING DOOR CUTOUT. REPAIRED SKIN IAW ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,012 hrs · 61,431 cycles

FUSELAGE SKIN CRACK (CHEM-MILL) BELOW S 19L AT BS 807+3" CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,012 hrs · 61,431 cycles

SKIN CRACKED AT BS 867, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,012 hrs · 61,431 cycles

FUSELAGE SKIN (CHEM-MILL) CRACKED ABOVE S 24R AT BS 867+6". REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 65,012 hrs · 61,431 cycles

LT WING I/B FORE FLAP DELAMINATED AT UPPER SURFACE. REPAIRED FORE FLAP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,012 hrs · 61,431 cycles

SKIN CRACKED AT BS 867, STR 23R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,012 hrs · 61,431 cycles

FUSELAGE SKIN CRACK (CHEM-MILL) S19L, AT BS 787+6 CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 807) · airframe 65,012 hrs · 61,431 cycles

SKIN CRACKED AT BS 807+3, STR 17L. REPAIRED SKIN IAW ER AND EA.

Part: SKIN — CRACKED (BS 867 S23R) · airframe 65,012 hrs · 61,431 cycles

SKIN CRACKED AT BS 867+3, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 867 S24R) · airframe 65,012 hrs · 61,431 cycles

SKIN CRACKED AT BS 867+3, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,012 hrs · 61,431 cycles

SKIN CRACKED AT BS. 809+3, STR 17R. REPAIRED SKIN PER SRM.

Part: SLAT — DAMAGED (RT WING) · airframe 64,246 hrs · 60,944 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 6 SLAT I/B CAN DAMAGED. REMOVED AND REPLACED SLAT CAN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,246 hrs · 60,944 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED BETWEEN BS 435 TO BS 436, STR 1. REPAIRED SKIN PER EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 63,529 hrs · 60,490 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,358 hrs · 60,376 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED BETWEEN BS 765 TO BS 767.5, STR 22L. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 62,557 hrs · 59,827 cycles

DURING SCHEDULED MV2 CHECK FOUND DELAMINATION LT OUTBD AFT FLAP. REMOVED AND REPLACED FLAP PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,406 hrs · 59,717 cycles

DURING SCHEDULED SPV CHECK, FOUND RT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,406 hrs · 59,717 cycles

DURING SCHEDULED SPV CHECK, FOUND LT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,406 hrs · 59,717 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,406 hrs · 59,717 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 62,406 hrs · 59,717 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,406 hrs · 59,717 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT BS 440 AT UPPER STOP FITTING. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,406 hrs · 59,717 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CHORD CRACKED AT BS 616, WL 208. REMOVED AND REPLACED CHORD PER EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 62,406 hrs · 59,717 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,405 hrs · 59,717 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 400+12, STR 1. REPAIRED SKIN PER EA.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 61,751 hrs · 59,298 cycles

STRONG ODOR COMING FROM ENVIRONMENTAL SYSTEM. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,548 hrs · 58,432 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 791, STR 19L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,548 hrs · 58,432 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 780, STR 19L. REPAIRED SKIN PER EA.

Part: SUPPORT FITTING — CRACKED (CARGO DOOR) · airframe 60,548 hrs · 58,432 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND AFT CARGO DOOR FWD AND AFT DOOR STOP T-CAP WEB SUPPORT FITTING CRACKED. REMOVED AND REPLACED DOOR PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 60,198 hrs · 58,186 cycles

LT EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 60,064 hrs · 58,097 cycles

DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SIGN — DAMAGED (CABIN) · airframe 60,064 hrs · 58,097 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD ENTRY EMERGENCY EXIT SIGN DAMAGED. REMOVED AND REPLACED SIGN PER MM.

Part: SKIN — CORRODED (LT WING) · airframe 60,064 hrs · 58,097 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING WING ROOT I/B SKIN CORRODED. REPAIRED SKIN PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,064 hrs · 58,097 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME WEB CRACKED AT BS 303.9, STR 16L. REPAIRED WEB PER ACO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 60,064 hrs · 58,097 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT BULKHEAD FITTING CRACKED BS 727, RBL 6.5. REMOVED AND REPLACED FITTING PER SRM BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 6,064 hrs · 58,097 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,064 hrs · 58,097 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 522, RBL 4.5. REPAIRED SKIN PER AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,064 hrs · 58,097 cycles

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

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 60,064 hrs · 58,097 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 6 SLAT I/B WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,064 hrs · 58,097 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED CLIP PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 60,064 hrs · 58,097 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 5 SLAT O/B WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,064 hrs · 58,097 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 59,162 hrs · 57,489 cycles

DURING SCHEDULED OTS CHECK, FOUND LT WING NR 2 SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 2 SLAT PER MM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 59,158 hrs · 57,488 cycles

DURING SCHEDULED OTS CHECK, FOUND WHEEL WELL KEEL BEAM WEB CRACKED AT BS 711. REMOVED AND REPLACED WEB PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 59,158 hrs · 57,488 cycles

DURING SCHEDULED OTS CHECK, FOUND LT KEEL BEAM Z-ANGLE CRACKED AT BS 711. REPAIRED Z-ANGLE PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 59,158 hrs · 57,488 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND RT EEPLS LENS LOOSE AT ROW 5. SECURED LENS PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 58,938 hrs · 57,351 cycles

L1 DOOR EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED SIGN PER MM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 58,523 hrs · 57,079 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MAIN WHEEL WELL BULKHEAD SUPPORT STIFFENER CRACKED AT BS 633, LBL 6. REPAIRED STIFFENER PER EA.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 58,367 hrs · 56,986 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,045 hrs · 56,773 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 310, STR 4R. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 58,045 hrs · 56,773 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED AT BS 1016, STR 15R. REPAIRED BULKHEAD PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 57,839 hrs · 56,632 cycles

RIGHT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT LOOSE AT ROW 1. SECURED LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 57,580 hrs · 56,459 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 57,580 hrs · 56,459 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 57,577 hrs · 56,455 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 57,529 hrs · 56,423 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MT.

Part: LENS — LOOSE (CABIN) · airframe 56,657 hrs · 55,881 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT LOOSE AT ROW 15. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — LOOSE (ROW 15) · airframe 56,656 hrs · 55,881 cycles

BULLNOSE EMERGENCY EXIT LIGHT LOOSE AT ROW 15. REMOVED AND REPLACED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,073 hrs · 55,445 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 794.2, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,066 hrs · 55,437 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727C+16 TO 727D, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,066 hrs · 55,437 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 800, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,219 hrs · 54,630 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 1. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (NR 3 SLAT) · airframe 54,179 hrs · 53,876 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING NR 3 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM.

Part: LIGHT — DEBONDED (CABIN) · airframe 54,179 hrs · 53,876 cycles

DURING SCHEDULED 18Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT ASSY DISBONDED AT ROW 14 DEF. REPAIRED LIGHT ASSY PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,179 hrs · 53,876 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 344, STR 9R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,179 hrs · 53,876 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 986.5, STR 2L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,179 hrs · 53,876 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 11R. R&R STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,179 hrs · 53,876 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,179 hrs · 53,876 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 54,179 hrs · 53,876 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,179 hrs · 53,876 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,179 hrs · 53,876 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,179 hrs · 53,876 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, BL 0. REPAIRED SKIN PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 54,179 hrs · 53,876 cycles

DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 54,179 hrs · 53,876 cycles

DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM.

Part: BULB — FAULTY (NR 1 ENGINE) · airframe 54,082 hrs · 53,805 cycles

NR 1 ENGINE OIL TEMP CLIMBED INTO RED BAND. NR 1 ENGINE WAS SHUTDOWN PER QRH. REMOVED AND REPLACED OIL TEMP BULB PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 53,871 hrs · 53,649 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT SIGN LOOSE. SECURED SIGN PER MM.

Part: BEARING — WORN (LT ELEVATOR TAB) · airframe 53,460 hrs · 53,314 cycles

DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BUSHING AND BEARING PER SWA EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 53,460 hrs · 53,314 cycles

DURING SCHEDULED C4 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SRM.

Part: BUSHING — WORN (RT ELEVATOR TAB) · airframe 53,460 hrs · 53,314 cycles

DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BUSHING AND BEARING PER SWA EA.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 53,460 hrs · 53,314 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 53,460 hrs · 53,314 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD FOREFLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,460 hrs · 53,314 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, STR 24L. REPAIRED SKIN PER SWA EA.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 53,147 hrs · 55,059 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT AFT CARGO DOOR LOWER FWD CUTOUT BS 798. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,859 hrs · 52,818 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 21R. REPAIRED SKIN PER SRM.

Part: MOUNT — WORN (LT WING) · airframe 52,818 hrs · 52,768 cycles

DURING SCHEDULED SERVICE CHECK, FOUND NR 1 ENGINE FWD OUTBOARD MOUNT WORN. REMOVED AND REPLACED MOUNT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,640 hrs · 52,582 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 751 AND BS 781, STR 18L AND STR 19L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 52,640 hrs · 52,582 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,278 hrs · 52,216 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,278 hrs · 52,216 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 51,983 hrs · 51,924 cycles

R1 DOOR EMERGENCY EXIT LIGHT ASSY LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (BS 885 S24-25R) · airframe 51,852 hrs · 51,796 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 885, BETWEEN STR 24R TO STR 25R. REPAIRED SKIN PER SWA EA.

Part: SIGN — MISSING (EMERGENCY EXIT) · airframe 51,848 hrs · 51,795 cycles

AFT CABIN EMERGENCY EXIT SIGN MISSING. INSTALLED EXIT SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,852 hrs · 51,796 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 51,044 hrs · 51,016 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 50,928 hrs · 50,904 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,801 hrs · 50,781 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 770, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,801 hrs · 50,781 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 972, STR 21L. REPAIRED SKIN PER SWA EA.

Part: BOTTLE — LOW PRESSURE (L1 DOOR SLIDE) · airframe 50,373 hrs · 50,390 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 49,767 hrs · 49,790 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SKIN — CORRODED (LT WING) · airframe 49,181 hrs · 49,168 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING UPPER SKIN CORRODED AT WING STA 75, STR 7. REPAIRED SKIN PER ER.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 49,181 hrs · 49,168 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 380 S8R) · airframe 49,181 hrs · 49,168 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME SECTION PER ER.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 49,181 hrs · 49,168 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 616 TO BS 639, STR 17L. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,181 hrs · 49,168 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L AND STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,181 hrs · 49,168 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,181 hrs · 49,168 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 49,181 hrs · 49,168 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,181 hrs · 49,168 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,181 hrs · 49,168 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,181 hrs · 49,168 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,181 hrs · 49,168 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,181 hrs · 49,168 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R AND STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,181 hrs · 49,168 cycles

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

Part: STRINGER SPLICE — CRACKED (BS 908 S4R) · airframe 49,181 hrs · 49,168 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,008 hrs · 48,983 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 24R. REPAIRED SKIN PER SWA EA.

Part: ACTUATOR — CRACKED (GRND SPOILERS) · airframe 48,592 hrs · 48,523 cycles

LT WING INBOARD NR 4 GROUND SPOILER OUTBOARD ACTUATOR HOUSING CRACKED. REMOVED AND REPLACED NR 4 OUTBOARD ACTUATOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,369 hrs · 48,297 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 931, STR 21L. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 48,345 hrs · 48,265 cycles

DURING SCHEDULED C2 CHECK, FOUND BULKHEAD WEB CRACKED AT BS 1016, STR 6L. REPAIRED WEB SECTION PER SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 47,553 hrs · 47,414 cycles

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

Part: WEB — CRACKED (CABIN FLOOR) · airframe 47,126 hrs · 46,956 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 664, LBL 42. REPAIRED WEB PER SWA EA.

Part: FRAME — CRACKED (FWD CARGO) · airframe 47,126 hrs · 46,956 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD FRAME LOWER STOP FITTING. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,126 hrs · 46,956 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT L1 DOOR CUTOUT, LOWER FWD CORNER. REPAIRED FRAME PER SRM.

Part: DOOR FRAME — CRACKED (AFT CARGO BAY) · airframe 47,126 hrs · 46,956 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR AFT FRAME CRACKED AT NR 5 STOP FITTING. REMOVED AND REPLACED AFT CARGO DOOR PER MM.

Part: FLOORBEAM — CORRODED (BS 1016) · airframe 47,126 hrs · 46,956 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 1016, RBL 30.5. REPAIRED FLOORBEAM PER SRM.

Part: SKIN — CRACKED (BS 385-387) · airframe 47,126 hrs · 46,956 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 385 TO BS 387, STR 4R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CHAFED (BS 889-919) · airframe 47,126 hrs · 46,956 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CHAFED AT DORSAL FIN BLADE SEAL, BETWEEN BS 889 TO BS 919, LBL 7. REPAIRED SKIN PER SWA EA.

Part: SKIN — CHAFED (BS 925-927) · airframe 47,126 hrs · 46,956 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CHAFED AT DORSAL FIN BLADE SEAL, BETWEEN BS 925 TO BS 927, LBL 9 & RBL 9. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 498A-500A) · airframe 47,126 hrs · 46,956 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 498A TO BS 500A, STR 12L. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (BS 482A) · airframe 47,126 hrs · 46,956 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 20L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 482) · airframe 47,126 hrs · 46,956 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 20R. REPAIRED FRAME PER SWA EA.

Part: RIB — CRACKED (RT WING) · airframe 47,126 hrs · 46,956 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 47,126 hrs · 46,956 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14R TO STR 15R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,126 hrs · 46,956 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 47,126 hrs · 46,956 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 664, LBL 32. REPAIRED BEADED WEB PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,126 hrs · 46,956 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 344, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,126 hrs · 46,956 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 615, STR 17R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 47,126 hrs · 46,956 cycles

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

Part: SKIN — CRACKED (BS 931) · airframe 47,126 hrs · 46,956 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 931, STR 25R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 47,126 hrs · 46,956 cycles

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

Part: STIFFENER — CORRODED (BS 1016) · airframe 47,126 hrs · 46,956 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 AFT PRESSURE BULKHEAD ANGLE STIFFENER CORRODED AT BL 0. REPAIRED ANGLE STIFFENER PER ACO & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,126 hrs · 46,956 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 328, STR 17R. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (BS 660) · airframe 47,126 hrs · 46,956 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 660, BL 0. REPAIRED FLOORBEAM PER SWA EA.

Part: SKIN — CRACKED (BS 320) · airframe 47,126 hrs · 46,956 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 320, R1 DOOR CUTOUT, AFT LOWER CORNER. REPAIRED SKIN PER SRM.

Part: STIFFENER — CORRODED (BS 1016) · airframe 47,126 hrs · 46,956 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 AFT PRESSURE BULKHEAD CHANNEL STIFFENER CORRODED AT BL 0. REPAIRED CHANNEL STIFFENER PER ACO & SRM.

Part: FLOORBEAM — CORRODED (BS 987) · airframe 47,126 hrs · 46,956 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 987, BETWEEN RBL 46.5 TO LBL 46.5. REMOVED AND REPLACED FLOORBEAM UPPER CAP PER SRM.

Part: BULKHEAD — CRACKED (BS 1016) · airframe 47,126 hrs · 46,956 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BS 1016 AFT PRESSURE BLKHD DOME WEB PANEL NR 6 CRACKED AT 9 O'CLOCK POSITION. REPAIRED DOME WEB PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,112 hrs · 44,765 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 18L. REPAIRED SKIN PER SRM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 43,817 hrs · 43,498 cycles

EEPLS LIGHT STRIP FROM ROW 1 ABC TO ROW 3 ABC, LOOSE. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: SKIN — CORRODED (LT WING) · airframe 43,323 hrs · 42,984 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING SKIN AT WING STATION 132, STRINGER 3, CORRODED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,554 hrs · 41,250 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STRINGER 24L. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 39,768 hrs · 39,571 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR AFT FRAME CRACKED AT NR 4 STOP FITTING. REPAIRED FRAME PER SRM.

Part: HOUSING — DEFECTIVE (CABIN) · airframe 38,672 hrs · 38,557 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT MID CABIN OVERHEAD. REMOVED AND REPLACED BATTERY PACK HOUSING PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 36,280 hrs · 36,291 cycles

DURING SCHEDULED C4 CHECK, FOUND RT OTBD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT OTBD AFT T/E FLAP PER MM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 34,032 hrs · 34,153 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 33,285 hrs · 33,412 cycles

EMERGENCY FLASHLIGHT INOP AT AFT UPPER POSITION. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: TRACK — LOOSE (CABIN) · airframe 32,688 hrs · 32,843 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK LOOSE AT ROWS 3 & 7. REPAIRED TRACK PER MM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 32,128 hrs · 32,292 cycles

AIR TURNBACK - DURING CLIMB, R2 COCKPIT WINDOW CRACKED. REMOVED AND REPLACED R2 WINDOW & WINDOW HEAT CONTROLLER PER MM. OPS CHECK GOOD PER MM.

Part: LIGHT — DEBONDED (CABIN FLOOR) · airframe 31,724 hrs · 31,909 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS STRIP (PHOTO-LUMINESCENT) DISBONDED AT ROW 7. SECURED LIGHTING STRIP PER MM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 31,673 hrs · 31,863 cycles

DURING SCHEDULED D-CHECK, FOUND 2 CRACKS AT STR 4L SPLICE, BS 908. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 31,673 hrs · 31,863 cycles

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

Part: LENS — DAMAGED (EVAC SLIDES) · airframe 31,673 hrs · 31,863 cycles

DURING SCHEDULED D CHECK, FOUND ALL FOUR EMERGENCY EVAC SLIDE PRESS INDICATORS DIFFICULT TO READ. REPAIRED VIEW PLATES PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 31,673 hrs · 31,863 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND 4 EA. BS 178 BULKHEAD WEB CRACKS AT RBL 5 TO LBL 5, WL 188 TO WL 201. REPAIRED BULKHEAD WEBS PER ACO 7154-53.

Part: BEAM — CRACKED (FUSELAGE) · airframe 31,673 hrs · 31,863 cycles

DURING SCHEDULED D CHECK, FOUND 14 EA. CRACKS AT BS 178 BULKHEAD VERTICAL BEAMS, WL 226 TO WL 231.75, RBL 17.1 & WL 226 TO WL 232.5, LBL 17.1. REPAIRED VERTICAL BEAMS PER RA 1-553-2403.

Part: FITTING — CRACKED (RT/LT MLG) · airframe 31,673 hrs · 31,863 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND RT & LT MLG AFT BEAM FITTINGS CRACKED. R&R BEAM FITTINGS PER ACO 6384-57.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,673 hrs · 31,863 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND FLOOR BEAM CORRODED AT BS 986.5, RBL 4.75. REPAIRED FLOOR BEAM PER SRM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 31,559 hrs · 31,743 cycles

DURING FWD ENTRY DOOR CLOSURE, EMERGENCY EVAC SLIDE ENGAGED FRAME AND FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: COVER — LOOSE (ROW 7) · airframe 31,249 hrs · 31,445 cycles

EEPLS TRACK COVER PULLED LOOSE AT ROW 7. INSTALLED TRACK COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 30,920 hrs · 31,119 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER CRACKED AT FWD END. REMOVED AND REPLACED TRACK COVER PER MM.

Part: COVER — MISSING (CABIN)

EEPLS TRACK COVER MISSING ON ROWS 9-10. INSTALLED AND SECURED COVER PER MM.

Part: SKIN — DELAMINATED (NR 5 LE SLAT)

DURING SCHEDULED C2 CHECK, FOUND NR 5 L/E SLAT DELAMINATED ON UPPER AFT INBOARD CORNER. REPAIRED SLAT PER SRM.

Part: INTERCOSTAL — CRACKED (CARGO COMPT)

DURING SCHEDULED BC3 CHECK, FOUND DOOR UPLOCK INTERCOSTAL CRACKED. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DENTED (LT HORIZ STAB)

DURING SCHEDULED RON CHECK, FOUND DENTED LEADING EDGE OF LT HORIZONTAL STABILIZER (CENTER SEC) DENT CAUSE ELONGATION OF SOME RIVETS HOLES. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (GALLEY DOORWAY)

DURING SCHEDULED 1/4D CHECK, FOUND CORRODED RT Z ANGLE AT AFT SERVICE DOOR CUTOUT. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 460-520)

DURING SCHEDULED 1/4D CHECK, FOUND CORRODED TRANSITION ANGLE LT AT BS 460 TO 520, LBL 24. REPLACED PER BOEING SRM.

Part: DOME NUTS — CORRODED (CARGO COMPT)

DURING SCHEDULED 1/4D CHECK, FOUND CORRODED 3 DOME NUTS AT BS 468, BL 0 FUSELAGE. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CORRODED (CARGO DOORWAY)

DURING SCHEDULED 1/4D CHECK, FOUND CORRODED DOORWAY LOWER WEB. REMOVED AND REPLACED PER BOEING SRM.

Part: SPLICE — FAILED (CABIN)

DURING WALKAROUND CHECK, FOUND TWO OVERWING RED STRIP LIGHTS AND TWO WHITE STRIP LIGHTS INOP. REPAIRED WIRE SPLICE AND 8ABC PER BOEING MM.

Part: WIRE — INOPERATIVE (CABIN)

DURING WALKAROUND CHECK, FOUND TWO OVERWING RED STRIP LIGHTS AND TWO WHITE STRIP LIGHTS INOP. REPAIRED WIRE SPLICE 8ABC PER BOEING MM.

Part: RETRACT MECH — LACK OF LUBE (LANDING GEAR)

AFTER TAKEOFF GEAR WOULD NOT COME UP, PULLED TRIGGER LOCK OVERRIDE TO RISE AFTER GEAR RETRACTED, TAKEOFF WARNING HORN AND CDU STUCK. USED QRH PULLED P62 CB HORN OFF, AND CDU OK. AIR RETURN TO PHX, AND MADE AN UNEVENTFUL LANDING. ADJUSTED GROUND SENSE CABLE AIR SENSOR AND LUBE CABLE PER BOEING MM.

Part: SKIN — GOUGED (BS 784)

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 784, AT S28R. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (BS 970)

DURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 970, AT STRINGER 19L. REPAIRED SKIN PER SWA RA 1-553-1566.

Part: LIGHT — DISCHARGED (CABIN)

DURING SCHEDULED C2 CHECK, FOUND CABIN UPPER EMERGENCY FLASHLIGHT NOT TESTING. REPLACED BATTERY PACK PER BOEING M/M.

Part: SLIDE — DEPLOYED (R 1 DOOR)

INADVERTENT SLIDE DEPLOYMENT AT FWD SERVICE DOOR. REPLACED SLIDE ASSEMBLY PER BOEING M/M.

Part: WIRE — BROKEN (CABIN)

DURING WALK-AROUND, FOUND EMERGENCY EXIT LIGHTING WIRES BROKEN, 4 WHITE LIGHTS INOP AT ROW FWD OF OVERWING EXIT. REPAIRED AND OP CHECKED PER BOEING M/M.

Part: SKIN — GOUGED (FUSELAGE)

DURING SCHEDULED B/C1 CHECK, FOUND FUSELAGE SKIN GOUGED 14 INCHES BELOW AFT ENTRY. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (HORIZ STAB LE)

DURING SCHEDULED SV CHECK, FOUND LT HORIZ STAB L/E DENTED 2 PLACES. REPAIRED PER BOEING SRM.

Part: FLOOR BEAM — CORRODED (BS 312)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM AFT FLANGE CORRODED AT BS 312 LBL 15. REPAIRED PER BOEING SRM.

Part: FLOOR BEAM — CORRODED (BS 986.5)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM NUTPLATE HOLE CORRODED AT BS 986.5 RBL 30. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 294)

DURING SCHEDULED 1/2 D-CHECK, FOUND 3.3 INCH CRACK IN RADIUS OF RT CREASE BEAM I/B CHORD ANGLE AT BS 294, RBL 54. REPAIRED PER BOEING SRM AND TYPICAL REPAIR T1-A53-023.

Part: FLOOR BEAM — CORRODED (BS 986.5)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM NUTPLATE HOLE CORRODED AT BS 986.5. REPAIRED PER BOEING SRM.