N502SW

Part: COVER — BROKEN (EXIT SIGN) · airframe 69,563 hrs · 65,836 cycles

FWD ENTRY LOWER EMERGENCY EXIT SIGN COVER BROKEN. REMOVED AND REPLACED FWD ENTRY LOWER EMERGENCY EXIT SIGN COVER IAW M/M, OPS CHECK OK.

Part: LIGHT — LOOSE (CABIN) · airframe 69,488 hrs · 65,760 cycles

EMERGENCY EXIT LIGHT ON BULL NOSE AT 11 ABC LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,163 hrs · 65,424 cycles

FRAME CRACKED AT BS 482, STR 21L. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,163 hrs · 65,424 cycles

L1 DOOR FUSELAGE SKIN CRACKED AT FWD UPPER CORNER, BS 312, STR 6L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,124 hrs · 65,386 cycles

FUSELAGE SKIN CRACKED AT BS 927, STR 4R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,124 hrs · 65,386 cycles

FUSELAGE SKIN CRACKED AT BS 927 + 5, STR 24R. REMOVED AND REPLACED SKIN IAW EA.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 67,877 hrs · 64,603 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT AT CASE, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE PER MT.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 67,877 hrs · 64,603 cycles

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

Part: WIRE — BROKEN (CABIN) · airframe 67,784 hrs · 64,541 cycles

AFT CARGO EMERGENCY LIGHT WIRE BROKEN BETWEEN BS 747 TO BS 767, BETWEEN STR 23L TO STR 24L. REPAIRED WIRE IAW BSWPM & AMM.

Part: WEB — CRACKED (NLG WW) · airframe 67,784 hrs · 64,541 cycles

NOSE LANDING GEAR LEFT SIDE INTERNAL SKIN WEB CRACKED AT BS 259, WL 174. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,784 hrs · 64,541 cycles

SKIN CRACKED AT BS 847, STR 18L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,784 hrs · 64,541 cycles

SKIN CRACKED AT BS 767, STR 19L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,784 hrs · 64,541 cycles

SKIN CRACKED BETWEEN BS 764 TO BS 765.25, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,784 hrs · 64,541 cycles

SKIN CRACKED AT BS 827 + 4, STR 19L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,784 hrs · 64,541 cycles

SKIN CRACKED AT BS 800, STR 18L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,784 hrs · 64,541 cycles

SKIN CRACKED AT BS 807, STR 23L. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,784 hrs · 64,541 cycles

FUSELAGE SKIN CRACKED AT BS 787-3, STR 23L. REPAIRED SKIN IAW REO AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,784 hrs · 64,541 cycles

FUSELAGE SKIN CRACKED BS 787-7, STR 19L. REPAIRED SKIN IAW REO AND EA.

Part: LIGHT — BROKEN (CABIN) · airframe 67,782 hrs · 64,540 cycles

LT EMERGENCY EXIT LIGHT BROKEN AT ROW 5. REMOVED AND REPLACED LIGHT PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,462 hrs · 63,667 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED BETWEEN BS 747+2 TO BS 747+15, BETWEEN STR 27L TO STR 27R.

Part: TRIM TAB — DELAMINATED (LT AILERON) · airframe 66,463 hrs · 63,667 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT WING AILERON TRIM TAB I/B T/E CORNER DELAMINATED. REMOVED AND REPLACED TAB IAW MM.

Part: SKIN — DELAMINATED (RT SPOILER) · airframe 66,463 hrs · 63,667 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 5 SPOILER DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED SPOILER IAW MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,463 hrs · 63,667 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT TEE CAP FLOOR SUPPORT UPPER SURFACE CORRODED AT ABS 986, BETWEEN BL 0 TO RBL 48. REMOVED AND REPLACED TEE CAP IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,463 hrs · 63,667 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,463 hrs · 63,667 cycles

DURING SCHEDULED 22Y CHECK FOUND, SKIN CRACKED AT BS 527-5, STR 17L. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,463 hrs · 63,667 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 727A, WL 208. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: LENS — MISSING (CABIN) · airframe 66,463 hrs · 63,667 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD LAV EMERGENCY EXIT SIGN LENS MISSING. REMOVED AND REPLACED SIGN IAW MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,463 hrs · 63,667 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 665, LBL 24. REPAIRED CHORD IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 66,463 hrs · 63,667 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 669, LBL 24. REPAIRED CHORD IAW EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 66,463 hrs · 63,667 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 277, BETWEEN STR 8L TO STR 9L. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,463 hrs · 63,667 cycles

DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM INNER CHORD CORRODED BETWEEN BS 954 TO BS 986, RBL 50. REMOVED AND REPLACED CHORD PER SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (HORIZ STAB) · airframe 66,463 hrs · 63,667 cycles

DURING SCHEDULED 22Y CHECK, FOUND HORIZONTAL STABILIZER CENTER SECTION BEAM ATTACH ANGLE CRACKED AT BS 1119. REMOVED AND REPLACED ANGLE IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 66,463 hrs · 63,667 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 520, BETWEEN STR 21L TO STR 22L. REPAIRED SHEAR TIE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,364 hrs · 663,596 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 767+7, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,364 hrs · 663,596 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 767+16, STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,364 hrs · 663,596 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 767+12, STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,243 hrs · 63,511 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 434, STR 1. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,832 hrs · 63,242 cycles

DURING SCHEDULED MV3 CHECK FOUND, SKIN CRACKED AT BS 348, STR 2L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,832 hrs · 63,242 cycles

DURING SCHEDULED MV3 CHECK FOUND, FUSELAGE SKIN CRACKED AT UPPER HINGE CUTOUT LOWER CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,684 hrs · 63,140 cycles

DURING SCHEDULED OTS CHECK FOUND FSLG SKIN CRACK AT FS 893, STR 25R. REPAIRED PER DOC.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,684 hrs · 63,140 cycles

DURING SCHEDULED OTS CHECK FOUND CORROSION ON SHEAR TIE BS 867 STR 26 - 27 RT. REMOVED CORROSION ON SHEAR TIE PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 65,478 hrs · 63,005 cycles

DURING SCHEDULED OTS CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,478 hrs · 63,005 cycles

DURING SCHEDULED OTS CHECK, FOUND CRACK RT SIDE FRAME FWD PIT STA 482. REPAIRED FRAME PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 65,478 hrs · 63,005 cycles

DURING SCHEDULED OTS CHECK, FOUND CRACKED WEB AT STA 178, LBL 5.7, WL 178. REPAIRED WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,478 hrs · 63,005 cycles

DURING SCHEDULED OTS CHECK, FOUND CRACK LT SIDE FRAME REINFORCEMENT FWD PIT STA 482A. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,446 hrs · 62,255 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 842, STR 16L. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 64,401 hrs · 62,224 cycles

L2 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM & MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,957 hrs · 61,921 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 482B + 15, STR 16R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,693 hrs · 61,057 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 540, STR 8R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,578 hrs · 60,978 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 306, STR 18R. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,578 hrs · 60,978 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 890, STR 22R. REPAIRED SKIN PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 61,791 hrs · 60,464 cycles

R1 DOOR LOWER EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 61,598 hrs · 60,342 cycles

L1 COCKPIT WINDSHIELD ARCING ON DESCENT AND CRACKED UPON PARKING AT GATE. REMOVED AND REPLACED L1 WINDOW PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,130 hrs · 60,061 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 372, STR 26R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,130 hrs · 60,061 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 802, STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

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

Part: FITTING — LOOSE (GIRT BAR) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR UPPER STUB FRAME CRACKED. REMOVED AND REPLACED FRAME SECTION PER BAC DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR UPPER STUB FRAME CRACKED. REMOVED AND REPLACED FRAME SECTION PER BAC DWG.

Part: LIGHT — MISSING (CABIN) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD GALLEY EMERGENCY EXIT LIGHT MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND FWD GALLEY EMERGENCY EXIT LIGHT MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: STRINGER CLIP — CRACKED (BS 987 S24L) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 987, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 987, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 967, STR 19L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE BELLY SKIN CORRODED AT BS 304, RBL 6. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CRACKED AT BS 980, STR 21L. REPAIRED STRINGER PER SRM.

Part: BEAM — CORRODED (RT MLG) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT MLG BEAM I/B SUPPORT LINK CORRODED. REMOVED AND REPLACED BEAM PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 291, BETWEEN STR 16R TO STR 17R. REPAIRED FRAME PER AAR EA.

Part: ATTACH FITTING — CRACKED (RT WING) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING I/B LOWER TRAILING EDGE PANEL SUPPORT ROD UPPER ATTACH FITTING CRACKED. REPAIRED FITTING PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

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

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING NR 3 SLAT O/B TRAILING EDGE WEDGE DELAMINATED. REPAIRED WEDGE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED BETWEEN BS 907 TO BS 908, STR 4R. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED BETWEEN BS 907 TO BS 908, STR 4L. REMOVED AND REPLACED SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 4 SLAT T/E WEDGE DELAMINATED. REPAIRED SLAT PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

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

Part: RIB — CRACKED (RT WING) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT STA 135.5, BETWEEN STR 2 AND STR 3. REPAIRED RIB PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND MID CABIN PRESSURE DECK CRACKED AT BS 663, LBL 32. REPAIRED SKIN PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y, FOUND RT WING NR 5 SLAT O/B LEADING EDGE I/B UPPER TRAILING EDGE WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING NR 2 SLAT I/B WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,091 hrs · 60,036 cycles

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

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING NR 2 SLAT O/B END OF WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 61,091 hrs · 60,036 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING NR 1 SLAT WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,750 hrs · 59,826 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 983.5, STR 20L. REPAIRED SKIN PER SWA EA.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 60,750 hrs · 59,826 cycles

FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 60,393 hrs · 59,596 cycles

EEPLS MISSING. INSTALLED EEPLS PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 60,393 hrs · 59,596 cycles

EEPLS STRIP MISSING NEAR ROW 5. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,190 hrs · 59,464 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 770, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,190 hrs · 59,464 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 767, STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,190 hrs · 59,464 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 930, STR 21R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,190 hrs · 59,464 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 739.5, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,190 hrs · 59,464 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 900, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,190 hrs · 59,464 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 880.5, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,190 hrs · 59,464 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 767, STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,190 hrs · 59,464 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 779, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,190 hrs · 59,464 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 930, STR 21R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,190 hrs · 59,464 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 900, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,190 hrs · 59,464 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 880, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,190 hrs · 59,464 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 770, STR 19L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 60,181 hrs · 59,457 cycles

L1 DOOR EMERGENCY EVAC SLIDE PULLED OUT OF CASE, DID NOT DEPLOY. INSTALLED SLIDE PER MT.

Part: LENS — OUT OF POSITION (CABIN) · airframe 59,404 hrs · 58,902 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,900 hrs · 58,453 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 257, WL 182. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,900 hrs · 58,453 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 257, WL 181. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 58,262 hrs · 57,952 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR FRAME CRACKED AT AFT LOWER CORNER. REMOVED AND REPLACED FRAME PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,262 hrs · 57,952 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 520, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,262 hrs · 57,952 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 380, STR 15R. REPAIRED SKIN PER SRM.

Part: LINK — CORRODED (RT MLG TRUNNION) · airframe 57,216 hrs · 57,182 cycles

DURING SCHEDULED SPV CHECK, FOUND RT MLG TRUNNION LINK CORRODED. REMOVED AND REPLACED LINK PER MM.

Part: PIN — CORRODED (RT MLG TRUNNION) · airframe 57,216 hrs · 57,182 cycles

DURING SCHEDULED SPV CHECK, FOUND RT MLG TRUNNION PIN CORRODED. REMOVED AND REPLACED PIN PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 57,131 hrs · 57,121 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: HEAT EXCHANGER — DEFECTIVE (NR 1 ENGINE) · airframe 56,664 hrs · 56,743 cycles

INFLIGHT SHUTDOWN / AIR TURNBACK / DECLARED EMERGENCY. NR 1 ENGINE OIL TEMP IN YELLOW BAND AFTER TAKEOFF, THEN TEMP WENT TO RED BAND. MAX OIL TEMP AT 190 DEGREES, SHUTDOWN ENGINE PER QRH. REMOVED AND REPLACED NR 1 ENGINE TEMP BULB AND FUEL OIL HEAT EXCHANGER PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 56,454 hrs · 56,576 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,917 hrs · 56,125 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 769, STR 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,551 hrs · 55,794 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 775 AND BS 786, STR 18L AND STR 19L. REPAIRED SKIN PER SRM.

Part: SIGN — LOOSE (EMERGENCY LIGHTS) · airframe 55,268 hrs · 55,536 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 54,295 hrs · 55,210 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER 18R CRACKED AT BS 947. REPAIRED STRINGER PER SRM.

Part: FLAP — SEPARATED (MID FLAP) · airframe 54,925 hrs · 55,210 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT WING OUTBOARD MID FLAP T/E SKIN SEPARATED. REPAIRED FLAP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 54,925 hrs · 55,210 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 344, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,925 hrs · 55,210 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 947, STR 18L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,925 hrs · 55,210 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 320, STR 20L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,925 hrs · 55,210 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,925 hrs · 55,210 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,925 hrs · 55,210 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,925 hrs · 55,210 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,925 hrs · 55,210 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727C S9L) · airframe 54,952 hrs · 55,210 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 380 S16L) · airframe 54,925 hrs · 55,210 cycles

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

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 54,925 hrs · 55,210 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727C S9L) · airframe 54,925 hrs · 55,210 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727B) · airframe 54,925 hrs · 55,210 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (BS 380) · airframe 54,925 hrs · 55,210 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER 15L CRACKED AT BS 380. REPAIRED STRINGER PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 54,604 hrs · 54,904 cycles

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

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 54,338 hrs · 54,630 cycles

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

Part: SKIN — CRACKED (BS 747 S18L) · airframe 54,134 hrs · 54,432 cycles

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

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,299 hrs · 53,566 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK AND BATTERY CHARGER PER MM.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 52,829 hrs · 53,090 cycles

DURING SCHEDULED SPV CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 15 ABC. RESEATED D7274 PIN CONNECTOR PER MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 52,648 hrs · 52,897 cycles

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

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 52,200 hrs · 52,427 cycles

UPON LANDING, AFT CABIN EMERGENCY EXIT LIGHT STAYS ILLUMINATED. BATTERY BASE IAW MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,102 hrs · 52,326 cycles

AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 52,044 hrs · 52,264 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP MISSING AT RT OVERWING EXIT. REPLACED EEPLS PHOTOLUMINESCENT STRIP PER MM.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 52,044 hrs · 52,264 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP MISSING AT LT OVERWING EXIT. REPLACED EEPLS PHOTOLUMINESCENT STRIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,044 hrs · 52,264 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: FLAP — CRACKED (LT WING) · airframe 52,044 hrs · 52,264 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING NR 1 L/E KRUEGER FLAP CRACKED AT INBOARD ACTUATOR ROD END CUTOUT. REMOVED AND REPLACED KRUEGER FLAP PER MM.

Part: WEB — CRACKED (BS 251) · airframe 51,179 hrs · 51,315 cycles

DURING SCHEDULED C1 CHECK, FOUND NOSE GEAR WHEEL WELL PRESSURE WEB CRACKED AT BS 251.625, FROM LBL 7.75 TO RBL 7.75. REPAIRED PRESSURE WEB PER SWA EA.

Part: SKIN — CRACKED (BS 747 S25L) · airframe 51,155 hrs · 51,276 cycles

FUSELAGE SKIN CRACKED AT BS 747, STR 25L. REPAIRED SKIN PER SRM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 50,815 hrs · 50,922 cycles

EEPLS STRIP COVER MISSING BETWEEN ROW 12 TO ROW 17. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (BS 971) · airframe 50,342 hrs · 50,419 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 971, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 737D) · airframe 50,115 hrs · 50,187 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737D, STR 23L. REPAIRED SKIN PER SWA EA & SRM.

Part: FRAME — CRACKED (FWD CARGO) · airframe 49,743 hrs · 49,797 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, FWD FRAME AT STOP FITTING, STR 24R. REPAIRED FRAME PER BFG ER.

Part: FRAME — CRACKED (AFT CARGO) · airframe 49,743 hrs · 49,797 cycles

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

Part: BUTTSTRAP — CRACKED (BS 360) · airframe 49,742 hrs · 49,796 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME BUTT STRAP CRACKED AT BS 360, BETWEEN STR 14R TO STR 15R. REMOVED AND REPLACED BUTT STRAP PER BFG ER.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 49,742 hrs · 49,796 cycles

DURING SCHEDULED MAINTENANCE, FOUND FUSELAGE STRINGER DAMAGED AT BS 482, STR 3R. REPAIRED STRINGER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,509 hrs · 48,511 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 790, STR 17L. REPAIRED SKIN PER SWA EA & SRM.

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,992 hrs · 47,957 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST ASSY PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,850 hrs · 47,810 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP AT BS 287,STR 16L CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,850 hrs · 47,810 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 287,STR 16L CRACKED. REPAIRED FRAME SECTION PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,850 hrs · 47,810 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM TEE CAP AT BS 986, FROM RBL 48 TO BL 0, CORRODED. REPAIRED TEE CAP PER EA.

Part: TEE FITTING — CRACKED (AFT CARGO DOOR) · airframe 47,850 hrs · 47,810 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR AFT LOWER TEE CHORD, CRACKED. REMOVED AND REPLACED TEE CHORD PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 47,850 hrs · 47,810 cycles

DURING SCHEDULED 1/2D CHECK, FOUND 4 EACH CRACKS ON FLOORBEAM UPPER CHORD BETWEEN BS 659 AND BS 668, RBL 24.82. REPAIRED FLOORBEAM CHORD PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 47,850 hrs · 47,810 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 664, RBL 24.75, CRACKED. REPAIRED FLOORBEAM CHORD PER EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 47,850 hrs · 47,810 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT WING OUTBOARD FOREFLAP DELAMINATED. REPAIRED FOREFLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 47,850 hrs · 47,810 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO COMPARTMENT STRINGER CLIP AT BS 807, STRINGER 25L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 47,850 hrs · 47,810 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER WEB AT BS 295, STRINGER 16L, CRACKED. REMOVED AND REPLACED STRINGER WEB SECTION PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 47,850 hrs · 47,810 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 25L AT BS 970, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: HOOK — CORRODED (GIRT BAR) · airframe 47,850 hrs · 47,810 cycles

DURING SCHEDULED 1/2D CHECK, FOUND GIRT BAR FLOOR FITTING ASSY AT BS 344, LBL 59, CORRODED. REMOVED AND REPLACED GIRT BAR FITTING ASSY PER SRM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 47,775 hrs · 47,737 cycles

DURING SCHEDULED C1 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING T/E AFT FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 47,723 hrs · 47,675 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 47,679 hrs · 47,614 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,894 hrs · 46,839 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN AT BS 967, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,439 hrs · 46,340 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 525, STR 10R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,064 hrs · 45,979 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 935, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM.

Part: CABLE — MISROUTED (ESCAPE SLIDE) · airframe 45,125 hrs · 45,050 cycles

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

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 45,125 hrs · 45,050 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED FWD LIGHT LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,053 hrs · 44,064 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND .75 LONG CRACK AT VERTICAL CHORD, BS 178, WL 184. REPAIRED VERTICAL CHORD PER SRM.

Part: SKIN — DELAMINATED (L/E SLAT) · airframe 43,294 hrs · 43,346 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 2 L/E SLAT DELAMINATED ON OUTBD UPPER SURFACE. REMOVED AND REPLACED NR 2 L/E SLAT PER MM.

Part: TRUNNION — CORRODED (LT MLG W/W) · airframe 42,085 hrs · 42,225 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT MLG TRUNNION PIN CORRODED. REMOVED AND REPLACED LT MLG TRUNNION PIN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,016 hrs · 42,159 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 799, STR 24L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 41,490 hrs · 41,667 cycles

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

Part: FLOORBEAM — CRACKED (MID CABIN) · airframe 40,024 hrs · 40,278 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 663, BL 0. REPAIRED FLOORBEAM PER SWA EA.

Part: SLAT — CRACKED (LT WING) · airframe 40,024 hrs · 40,278 cycles

DURING SCHEDULED D CHECK, FOUND NR 1 SLAT CRACKED BELOW INBD AUX TRACK CUTOUT. REPAIRED NR 1 SLAT PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 39,326 hrs · 39,546 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER WHEN DOOR WAS OPENED. REINSTALLED SLIDE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 39,804 hrs · 40,071 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS LOOSE AT ROW NR 17. SECURED EEPLS PER MM.

Part: SLIDE — UNSERVICEABLE (AFT ENTRY DOOR) · airframe 39,738 hrs · 40,009 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 38,896 hrs · 39,184 cycles

EEPLS COVER LOOSE. SECURED COVER PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 37,848 hrs · 38,170 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND WEB CRACKED AT BS 178, WL 234 AND LBL 10. REPAIRED WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 37,848 hrs · 38,170 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, WL 226 AND RBL 17.1. REMOVED AND REPLACED WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 37,848 hrs · 38,170 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND HORIZONTAL WEBS CRACKED (2 EA) AT BS 179, WL 207, LBL 27.0 AND RBL 27.0. REMOVED AND REPLACED WEBS PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 37,180 hrs · 37,538 cycles

DURING SCHEDULED C1 CHECK, FOUND CENTER EMERGENCY OVERHEAD EXIT LIGHT WIRES BROKEN. REPAIRED BROKEN WIRES PER MM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 36,721 hrs · 37,097 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: COVER — LOOSE (CABIN) · airframe 36,258 hrs · 36,640 cycles

EEPLS TRACK COVER LOOSE AT MID CABIN. INSTALLED EEPLS TRACK COVER PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 35,668 hrs · 36,060 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT AFT 7 ROWS. REMOVED AND REPLACED EEPLS CHARGER ASSY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 35,221 hrs · 35,637 cycles

EEPLS BROKEN AT OVERWING EXIT. REPLACED LIGHT ASSY PER MM.

Part: COVER — MISSING (CABIN) · airframe 33,784 hrs · 34,198 cycles

EEPLS TRACK COVER MISSING AT ROW 14. INSTALLED COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 33,329 hrs · 33,750 cycles

EEPLS TRACKS LOOSE. RE-INSTALLED TRACKS PER MM.

Part: SKIN — CRACKED (NR 1 SLAT) · airframe 32,939 hrs · 33,363 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 1 L/E SLAT LOWER SKIN CRACKED NEAR AFT RIVET ROW OF MID O/B AUX TRACK. REPAIRED SLAT PER SWA RA NR 1-A57-001.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 32,939 hrs · 33,363 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM.

Part: WARNING LIGHT — ILLUMINATED (E/E BAY) · airframe 32,543 hrs · 32,967 cycles

ABORTED TAKEOFF, NR 1 ENG T/R OVERHEAD LIGHT ILLUMINATED DURING TAKEOFF. RESEATED NR 1 ENG T/R FAULT BOX. OPERATED T/R. NO DEFECT NOTED.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 32,256 hrs · 32,680 cycles

DURING SCHEDULED SERVICE CHECK, F OUND RT ELEVATOR LOWER SKIN DELAMINATED IN 2 AREAS, APPROX STA 94.1, 8.5 INCHES AFT OF FRONT SPAR. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (BS 452)

DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR CUTOUT LOWER FRAME CRACKED, BS 452 AT LOWER DOOR STOP. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 400 - 482A)

DURING SCHEDULED D CHECK, FOUND 5 FUSELAGE FRAMES CRACKED, BS 400, STRINGERS 8L-9L AND 8R-9R, BS 440, BS 482, AND BS 482A, BETWEEN STRINGERS 8R-9R. REPAIRED FRAMES PER ER NR 00-210A AND SRM.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED D CHECK, FOUND BS 986 FLOORBEAM UPPER SURFACE CORRODED, LBL 53-RBL 53. REPAIRED BEAM PER ER NR OO-0212 AND SRM.

Part: FRAME — CRACKED (BS 727 - 907)

DURING SCHEDULED D CHECK, FOUND 5 FUSELAGE FRAMES CRACKED, BS 827, BS 907, STRINGER 8L, BS 727B, BS 747, BS 787, STRINGER 8R. REPAIRED FRAMES PER ER NR 00-210A AND SRM.

Part: BEAM — CORRODED (BS 727B - 727C)

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CORRODED, BS 727B-727C, BBL 70. REPAIRED BEAM PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD 10 CRACKS, LBL 5 TO RBL 7. REPAIRED BULKHEAD PER SRM.

Part: LIGHT — MISSING (CABIN)

DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK CAP END MISSING AT FWD END. REPLACED CAP END PER MM.

Part: LENS — CRACKED (CABIN)

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT LENS CRACKED AT MID CABIN. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — BROKEN (ROW 1)

DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK COVER BROKEN AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: LENS — MISSING (CABIN)

DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK LENS MISSING AT FWD AND AFT ENDS. REPLACED LENSES PER MM.

Part: BALLAST — FAILED (ROW 11)

ON TAXI OUT, THE FLIGHT ATTENDANTS REPORTED A SMELL IN THE CABIN LIKE BURNING INSULATION (ELEC). CEILING LIGHT INOPERATIVE-ROW 11. REMOVED AND REPLACED LIGHT BALLAST PER BOEING MM. OPS CHECK GOOD.

Part: WIRE — EXPOSED (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY TRACK LIGHTING AT ROW 5 HAS EXPOSED WIRES. REPAIRED PER BOEING MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT INOP AT MID CABIN. RECONNECTED EMERGENCY FLOOR TRACK LIGHT PER BOEING MM.

Part: LIGHT — LOOSE (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT ROW TRACK LIGHTING LOOSE. SECURED FLOOR TRACK LIGHTING PER BOEING MM.

Part: LIGHT — LOOSE (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT ROW TRACK LIGHTING LOOSE. SECURED FLOOR TRACK LIGHTING PER BOEING MM.

Part: WIRE — EXPOSED (CABIN)

DURING WALKAROUND CHECK, FOUND WIRES EXPOSED ON FLOOR TRACK LIGHTING. REPAIRED AND SECURED WIRING PER BOEING M/M.

Part: WIRE — BROKEN (CABIN)

DURING SCHEDULED RON CHECK, FOUND A SECTION OF FLOOR TRACK LIGHTING INOP. REPAIRED A BROKEN WIRE PER BOEING M/M.

Part: ACM — FAILED (RIGHT)

AFTER PUSHBACK FROM GATE, EXPERIENCED SMOKE IN CABIN. RETURNED TO GATE. INSPECTED, REPLACED RIGHT AIR CYCLE MACHINE AND AIR CONDITION RELAY MODULE PER BOEING M/M.

Part: SENSOR — MALFUNCTION (NR 2 LE FLAP)

AFTER TAKEOFF, NR 2 KRUGER FLAP INDICATED NO RETRACTION. AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. INSPECTED AREA. REPLACED FLAP FULL UP PROXIMITY SENSOR PER BOEING M/M.

Part: SKIN — CRACKED (RT FUSELAGE)

DURING SCHEDULED 1/2 D CHECK, FOUND RIGHT FUSELAGE SKIN CRACKED AT STRINGER S16R AT WING SCANNING LIGHT CUTOUT, AT AFT END OF FWD SECTION. REPAIRED PER SWA ACO 6405-53.

Part: BELTFRAME — CRACKED (BS 482)

DURING SCHEDULED 1/2 D CHECK, FOUND BELTFRAME CRACKED .125 INCHES AT RIVET HOLE, BS 482, RBL 1. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: WEB — CRACKED (BS 460)

DURING SCHEDULED 1/2 D CHECK, FOUND FWD CARGO DOOR CUTOUT WEB CRACKED AT BS 460, LWR AFT CORNER. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FLOOR BEAM — CRACKED (BS 400)

DURING SCHEDULED 1/2 D CHECK, FOUND FWD CARGO FLOOR BEAM CRACKED AT BS 400, LBL 21.0. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: DOOR FRAME — CRACKED (CARGO COMPT)

DURING SCHEDULED 1/2 D-CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT FWD LWR SIDE NEXT TO RELEASE UPLOCK HOOK. REPAIRED PER SWA ACO 3194-52.