N300SW

Part: SKIN — CRACKED (FUSELAGE) · airframe 82,851 hrs · 77,096 cycles

DURING SCHEDULED CV CHECK, FOUND SKIN CRACKED AT BS 260, BETWEEN STR 4R TO STR 5R. REPAIRED SKIN PER EA.

Part: VALVE — FAULTY (MLG W/W) · airframe 82,524 hrs · 76,846 cycles

AFTER LANDING GEAR LEVER PLACED IN OFF POSITION, INDICATED RED LIGHTS. REMOVED AND REPLACED LANDING GEAR TRANSFER VALVE PER MM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 82,293 hrs · 76,674 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT WING NR 0 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: LENS — MISSING (CABIN) · airframe 81,729 hrs · 76,235 cycles

DURING SCHEDULED OTS CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN LENS MISSING. REMOVED AND REPLACED SIGN PER MM.

Part: LENS — MISSING (CABIN) · airframe 81,208 hrs · 75,855 cycles

LT OVERWING EMERGENCY EXIT SIGN MISSING LIGHT LENS. INSTALLED LENS PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 81,020 hrs · 75,716 cycles

DURING SCHEDULED CV CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 81,020 hrs · 75,716 cycles

DURING SCHEDULED CV CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 80,286 hrs · 75,182 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 80,286 hrs · 75,182 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,008 hrs · 74,959 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT AT BS 303, WL 234. REPAIRED SKIN PER AAR EA.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 79,410 hrs · 74,550 cycles

DURING SCHEDULED RON CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 78,798 hrs · 74,107 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,599 hrs · 73,965 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 78,494 hrs · 73,882 cycles

LEFT NR 1 COCKPIT WINDOW ARCED AT UPPER I/B CORNER. REMOVED AND REPLACED WINDOW PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,926 hrs · 73,486 cycles

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

Part: WINDOW — OVERHEATED (COCKPIT) · airframe 77,875 hrs · 73,450 cycles

DIVERSION / DECLARED EMERGENCY. IN CRUISE LARGE AMOUNT OF SMOKE APPEARED FROM R2 SLIDING WINDOW NEAR THE HANDLE. FOUND WINDOW TERMINAL HEAR CONNECTOR SHOWED SIGNS OF OVERHEAT. REMOVED AND REPLACED WINDOW AND HEAT CONTROLLER PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,782 hrs · 73,386 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 15L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,782 hrs · 73,386 cycles

DURING SCHEDULED 26Y CHECK, FOUND RT FUSELAGE FRAME CRACKED AT BS 559, STR 13R. REPAIRED FRAME PER EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 77,782 hrs · 73,386 cycles

DURING SCHEDULED 26Y CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 727 TO BS 727A. REPAIRED BEAM PER AAR EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 77,782 hrs · 73,386 cycles

DURING SCHEDULED 26Y CHECK, FOUND FUSELAGE FRAME CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BS 291, WL 231. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,782 hrs · 73,386 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 348, STR 17R. REPAIRED FRAME PER SRM AND EA.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 77,782 hrs · 73,386 cycles

DURING SCHEDULED 26Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 77,782 hrs · 73,386 cycles

DURING SCHEDULED 26Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,782 hrs · 73,386 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, RBL 12. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 77,782 hrs · 73,386 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 359, STR 15L. REMOVED AND REPLACED SPLICE PER SRM.

Part: DOOR FRAME — CRACKED (L2 DOOR) · airframe 77,782 hrs · 73,386 cycles

DURING SCHEDULED 26Y CHECK, FOUND L2 DOOR, FWD EDGE FRAME CRACKED AT UPPER CORNER UNDERNEATH DOOR SKIN. REMOVED AND REPLACED DOOR PER MM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 77,782 hrs · 73,386 cycles

DURING SCHEDULED 26Y CHECK, FOUND LT KEEL BEAM CRACKED BETWEEN BS 625 TO BS 727. REMOVED AND REPLACED BEAM SECTION PER SRM.

Part: LENS — CRACKED (CABIN) · airframe 77,782 hrs · 73,386 cycles

DURING SCHEDULED 26Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,782 hrs · 73,386 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, LBL 9. REPAIRED SHEAR TIE PER SRM.

Part: LENS — CRACKED (CABIN) · airframe 77,782 hrs · 73,386 cycles

DURING SCHEDULED 26Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT HOUSING CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,782 hrs · 73,386 cycles

DURING SCHEDULED 26Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 13L. REPAIRED FRAME PER SWA EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,782 hrs · 73,386 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CORRODED AT BS 964, STR 27L. REPAIRED STRINGER PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,782 hrs · 73,386 cycles

DURING SCHEDULED 26Y CHECK, FOUND SHEAR TIE CORRODED AT BS 847, RBL 4. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 77,782 hrs · 73,386 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 827, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 77,782 hrs · 73,386 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 827, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 77,782 hrs · 73,386 cycles

DURING SCHEDULED 26Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 77,782 hrs · 73,386 cycles

DURING SCHEDULED 26Y CHECK, FOUND RT WING NR 5 SLAT DELAMINATED AT O/B TRAILING EDGE WEDGE. REPAIRED WEDGE PER SRM.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 77,782 hrs · 73,386 cycles

DURING SCHEDULED 26Y CHECK, FOUND RT WING NR 5 SLAT DELAMINATED AT I/B TRAILING EDGE WEDGE. REPAIRED WEDGE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,782 hrs · 73,386 cycles

DURING SCHEDULED 26Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 265, STR 9L. REPAIRED SKIN PER SRM.

Part: STRIP — WORN (CABIN) · airframe 77,779 hrs · 73,385 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS STRIP WORN AT ROW 17. REMOVED AND REPLACED EEPLS PER MM.

Part: STRIP — WORN (CABIN) · airframe 77,779 hrs · 73,385 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS STRIP WORN AT ROW 20. REMOVED AND REPLACED EEPLS PER MM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 77,000 hrs · 72,835 cycles

DURING SCHEDULED MV4 CHECK, FOUND KEEL BEAM CRACKED FWD BS 727. REPAIRED SKIN PER SWA EA.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 76,570 hrs · 72,517 cycles

DURING SCHEDULED MV1 CHECK, FOUND KEEL BEAM CRACKED AT FWD BS 727. REPAIRED BEAM PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 76,477 hrs · 72,449 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 74,650 hrs · 71,098 cycles

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

Part: CONNECTOR — LOOSE (CABIN) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND EMERGENCY EXIT LIGHTS ILLUMINATED WITH SWITCH IN THE OFF POSITION. FOUND LOOSE CONNECTOR. SECURED CONNECTOR PER WDM.

Part: SLAT — DELAMINATED (RT WING) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND RT WING NR 4 L/E SLAT DELAMINATED AT OUTBOARD T/E. REPAIRED SLAT PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND TEE CHORD CORRODED AT BS 807, RBL 21. REMOVED AND REPLACED TEE CHORD PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 294, LBL 7. REPAIRED UPPER CHORD PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, 6 O'CLOCK POSITION. REPAIRED WEB PER ER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 26R CORRODED AT BS 356. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 22R. REPAIRED FRAME PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 23R CORRODED AT BS 500C. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 711, STR 10L. REPAIRED SKIN PER ER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 24L CORRODED BETWEEN BS 851 AND BS 867. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 18R CORRODED AT BS 326. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 22L CORRODED AT BS 737. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 23L CORRODED AT BS 375. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 380, STR 25L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (BS 845 S23L) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER 23L CORRODED AT BS 845. REPAIRED STRINGER PER SRM.

Part: FRAME — CORRODED (BS 1016) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD FITTING CHORD CORRODED AT BS 1016, RBL 29. REPAIRED CHORD PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 14R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 24L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, STR 12L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SLAT — CRACKED (LT WING) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 380, STR 13L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 500A, STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 360 S5L) · airframe 74,649 hrs · 71,097 cycles

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

Part: FRAME — CRACKED (BS 380 S8R) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500A S8L) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 597 S8L) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER SPLICE — CRACKED (BS 360 S11L) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727E S25L) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727E, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 847 S23L) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 847, STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727E S22L) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 727E, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 887 S24L) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 887, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 787 S20L) · airframe 74,649 hrs · 71,097 cycles

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

Part: SKIN — CRACKED (BS 988) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 988, AFT UPPER CORNER L2 DOOR CUTOUT. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (BS 767 S22L) · airframe 74,649 hrs · 71,097 cycles

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

Part: STRINGER CLIP — CRACKED (BS 767 S21L) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 767, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 420 S23L) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 420, STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727E S20L) · airframe 74,649 hrs · 71,097 cycles

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

Part: STRINGER CLIP — CRACKED (BS 400 S24L) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 400, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRIDGE CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED RIGHT WING OUTBOARD AFT FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 787 S21L) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 787, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 767 S25R) · airframe 74,649 hrs · 71,097 cycles

DURING SCHEDULED BRIDGE CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 767, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: FITTING — CORRODED (L1 DOOR GIRT BAR) · airframe 74,649 hrs · 71,097 cycles

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

Part: FITTING — CORRODED (L1 DOOR GIRT BAR) · airframe 74,649 hrs · 71,097 cycles

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

Part: SENSOR — FAULTY (NLG) · airframe 74,649 hrs · 71,097 cycles

EXTENDING LANDING GEAR NOSE GEAR RED LIGHT ILLUMINATED. REMOVED AND REPLACED NLG SENSOR PER MM.

Part: SKIN — CRACKED (BS 386 S17R) · airframe 74,365 hrs · 70,886 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 386, STR 17R. REPAIRED SKIN PER SWA EA.

Part: REPAIR — MISSING (FOREFLAP) · airframe 74,326 hrs · 70,854 cycles

RIGHT WING INBOARD FORE FLAP PREVIOUS REPAIR PATCH MISSING. REMOVED AND REPLACED FORE FLAP PER MM.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 74,180 hrs · 70,736 cycles

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

Part: LENS — MISSING (CABIN) · airframe 73,998 hrs · 70,587 cycles

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

Part: CASTING — CRACKED (NR 4 SPOILER) · airframe 73,670 hrs · 70,317 cycles

DURING SCHEDULED C3 CHECK, FOUND LEFT WING NR 4 GROUND SPOILER INBOARD ACTUATOR ATTACH CASTING CRACKED. REMOVED AND REPLACED NR 4 SPOILER PER MM.

Part: SLAT — CRACKED (RT WING) · airframe 73,670 hrs · 70,317 cycles

DURING SCHEDULED C3 CHECK, FOUND RIGHT WING NR 4 L/E SLAT CRACKED AT AFT INBOARD END. REPAIRED SLAT PER SWA EA.

Part: SPOILER — DELAMINATED (RT WING) · airframe 73,670 hrs · 70,317 cycles

DURING SCHEDULED C3 CHECK, FOUND RIGHT WING NR 5 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED NR 5 SPOILER PER MM.

Part: SKIN — CRACKED (BS 386 S17R) · airframe 73,477 hrs · 70,161 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 386, STR 17R. REPAIRED SKIN PER SWA EA.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 73,416 hrs · 70,118 cycles

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

Part: LENS — MISSING (CABIN) · airframe 73,346 hrs · 70,064 cycles

AFT CABIN EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — CORRODED (BS 967 S25L) · airframe 73,175 hrs · 69,935 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 967, STR 25L. REPAIRED SKIN PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,175 hrs · 69,935 cycles

DURING SCHEDULED SERVICE CHECK, FOUND STRINGER 26L CORRODED AT BS 968. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,175 hrs · 69,935 cycles

DURING SCHEDULED SERVICE CHECK, FOUND STRINGER 27R CORRODED AT BS 964. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (BS 767 S19L) · airframe 72,832 hrs · 69,671 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 19L. REPAIRED SKIN PER SWA EA.

Part: BOLT — WORN (LT ELEVATOR) · airframe 72,832 hrs · 69,671 cycles

DURING SCHEDULED C2 CHECK, LEFT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED INBOARD PUSHROD BOLT PER MM.

Part: SIGN — BROKEN (EMERGENCY EXIT) · airframe 72,821 hrs · 69,665 cycles

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

Part: SKIN — CRACKED (BS 691 S10L) · airframe 72,650 hrs · 69,528 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 691, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,165 hrs · 69,151 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 360, STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,165 hrs · 69,151 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 360, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 72,165 hrs · 69,151 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 27L CORRODED BETWEEN BS 360 AND BS 365. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,165 hrs · 69,151 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,165 hrs · 69,151 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 847, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,165 hrs · 69,151 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,165 hrs · 69,151 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 827, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 847) · airframe 72,165 hrs · 69,157 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME CRACKED BS 847, LOWER CORNER. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 72,165 hrs · 69,151 cycles

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

Part: SHEAR TIE — CORRODED (BS 460 S25L) · airframe 72,165 hrs · 69,151 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 460, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 440 S25L) · airframe 72,165 hrs · 69,151 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 440, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,886 hrs · 68,927 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 19L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 71,886 hrs · 68,927 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — DEPLOYED (R1 DOOR) · airframe 71,138 hrs · 68,325 cycles

DURING SCHEDULED SERVICE CHECK, R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 70,960 hrs · 68,191 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR FRAME CRACKED AT UPPER HINGE. REMOVED AND REPLACED R1 DOOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,960 hrs · 68,191 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, BL 0. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (L/E SLAT) · airframe 70,960 hrs · 68,191 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 4 L/E SLAT LOWER SKIN CRACKED AT AFT INBOARD END. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,960 hrs · 68,191 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730C, STR 14R. REPAIRED SKIN PER SWA EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 70,725 hrs · 68,020 cycles

DURING SCHEDULED A1 CHECK, FOUND EEPLS LIGHT INOP AT ROW 17 ABC. REMOVED AND REPLACED EEPLS LIGHT BULB PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 69,989 hrs · 67,433 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING T/E OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED T/E AFT FLAP PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,585 hrs · 67,125 cycles

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

Part: SKIN — CRACKED (BS 266) · airframe 68,960 hrs · 66,651 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 266, STR 15R. MX FERRY TO DAL FOR REPAIRS. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 308) · airframe 68,960 hrs · 66,651 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 308, STR 24L. MX FERRY TO DAL FOR REPAIRS. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,960 hrs · 66,651 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT, FWD LOWER CORNER. MX FERRY TO DAL FOR REPAIRS. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 500C) · airframe 68,960 hrs · 66,651 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 17L. MX FERRY TO DAL FOR REPAIRS. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (BS 373) · airframe 68,960 hrs · 66,651 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 373, STR 19R. MX FERRY TO DAL FOR REPAIRS. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 911) · airframe 68,960 hrs · 66,651 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 911, STR 21L. MX FERRY TO DAL FOR REPAIRS. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 67,611 hrs · 65,553 cycles

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

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 67,193 hrs · 65,227 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FUSELAGE KEELBEAM, RT SIDE, BS 727A. REPAIRED KEELBEAM PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,193 hrs · 65,227 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 18R. REPAIRED FRAME PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 67,193 hrs · 65,227 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 4 EA CRACKS AT BS 1016 PRESS BULKHEAD WEB, STR 1 TO STR 7R. REPAIRED WEB PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 807) · airframe 67,193 hrs · 65,227 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, BETWEEN STR 17L TO STR 19L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: PRESSURE PANEL — CRACKED (MLG WW) · airframe 67,193 hrs · 65,227 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESS WEB CRACKED AT BS 664, LBL 39. REPAIRED WEB PER SWA EA.

Part: PRESSURE PANEL — CRACKED (MLG WW) · airframe 67,193 hrs · 65,227 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESS WEB CRACKED AT BS 665, RBL 38 & RBL 40. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,193 hrs · 65,227 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 383, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,193 hrs · 65,227 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 3, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,193 hrs · 65,227 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 843, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,193 hrs · 65,227 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 18L. REPAIRED SKIN PER SWA EA.

Part: WEB — CRACKED (LH MLG W/W) · airframe 67,193 hrs · 65,227 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 665, LBL 40. REPAIRED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,193 hrs · 65,227 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 907, LBL 3 TO RBL 3. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,193 hrs · 65,227 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BELTFRAME SHEAR TIE CORRODED AT BS 500D, BL 0. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: COVER — CRAZED (EMERGENCY LIGHT) · airframe 67,193 hrs · 65,227 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT EXTERIOR EMERGENCY EXIT DOOR LIGHT COVER CRAZED. REMOVED AND REPLACED COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,193 hrs · 65,227 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SCREW — WORN (R2 DOOR SLIDE) · airframe 67,066 hrs · 65,103 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE HARDWARE WORN. REMOVED AND REPLACED HARDWARE PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,956 hrs · 65,016 cycles

DURING SCHEDULED A1 CHECK, FOUND L1 & R1 DOOR LOWER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,834 hrs · 64,915 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE BELT FRAME CRACKED AT BS 400, STR 18R. REPAIRED BELT FRAME PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,824 hrs · 64,909 cycles

DURING WALK AROUND INSP, FOUND 2 SKIN CRACKS AT BS 390, STR 16R, & BS 470, STR 17R. REPAIRED SKIN PER SRM & SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,824 hrs · 64,909 cycles

DURING WALK AROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 18R. REPAIRED SKIN PER SRM & SWA EA.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 66,824 hrs · 64,909 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 66,813 hrs · 64,898 cycles

DURING SCHEDULED A2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,813 hrs · 64,898 cycles

DURING SCHEDULED A2 CHECK, FOUND EMERGENCY BULLNOSE LIGHT INOP AT ROW 17 ABC. RELAMPED LIGHT PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 66,130 hrs · 64,369 cycles

DURING SCHEDULED C3 CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT STR 16L. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,124 hrs · 64,366 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 375, STR 26L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,124 hrs · 64,366 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, BELOW STR 12R. REPAIRED SKIN PER SWA EA.

Part: FITTING — CORRODED (RT WING) · airframe 66,093 hrs · 64,344 cycles

DURING SCHEDULED RON CHECK, FOUND RT MLG STAB FITTING CORRODED. REPAIRED FITTING PER SWA EA.

Part: BEARING — WORN (NR 6 SLAT) · airframe 65,817 hrs · 64,134 cycles

MOVING FLAPS FROM 5 TO 10 DEGREES BOTH PILOTS HEARD A LOUD POP AND A THUMP, ALL INDICATIONS NORMAL. REMOVED AND REPLACED NR 6 L/E SLAT BEARINGS PER SERVICE LETTER AND MM.

Part: LENS — MISSING (CABIN) · airframe 65,301 hrs · 63,735 cycles

DURING SPV, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 65,232 hrs · 63,686 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED. REMOVED AND REPLACED LT NR 2 L/E SLAT PER MM.

Part: LIGHT — LOOSE (ROW 19 DEF) · airframe 65,232 hrs · 63,686 cycles

DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT AT ROW 19 DEF, LOOSE. SECURED LIGHT ASSEMBLY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,232 hrs · 63,686 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 500D, ABOVE STRINGER 12L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,232 hrs · 63,686 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 485, STRINGER 16R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,232 hrs · 63,686 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 271, STRINGER 16R, CRACKED. REPAIRED SKIN PER SRM.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 64,395 hrs · 63,019 cycles

AFT CENTER AISLE EMERGENCY EXIT LIGHTS ERRATIC. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,379 hrs · 63,007 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 964, STR 22L, BS 972, STR 24L, BS 942, STR 24L, CRACKED. REPAIRED SKIN SECTIONS PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,379 hrs · 63,007 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 812, STR 18L, CRACKED. REPAIRED SKIN PER EA, SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,379 hrs · 63,007 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 515, STR 14R, BS 563, STR 10L, BS 583, STR 10L, BS 520, BL 0, CRACKED. REPAIRED SKIN SECTIONS PER EA.

Part: DOOR FRAME — CRACKED (CARGO BAY) · airframe 64,379 hrs · 63,007 cycles

DURING SCHEDULED C-1 CHECK, FOUND FWD CARGO DOOR AFT FRAME AT AFT LOWER STOP, CRACKED. REPAIRED DOOR FRAME PER BAC DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,379 hrs · 63,007 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR LOWER HINGE BOX FUSELAGE SKIN CUTOUT AT LOWER RADIUS, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (E/E DOOR) · airframe 64,379 hrs · 63,007 cycles

DURING SCHEDULED C1 CHECK, FOUND E&E DOOR OUTER SKIN CRACKED. REMOVED AND REPLACED E&E DOOR PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 64,377 hrs · 63,003 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,481 hrs · 61,474 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 801, STRINGER 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,227 hrs · 61,283 cycles

DURING SCHEDULED SC, FOUND SKIN CRACKED AT BS 960, WL 185 LT SIDE. REPAIRED SKIN CRACK PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,695 hrs · 60,084 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) ABOVE STR 19R, BS 410 AND BS 735. REPAIRED SKIN PER SRM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 60,665 hrs · 60,062 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE) · airframe 60,076 hrs · 59,575 cycles

DURING SCHEDULED PM CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESS IND LOW. REMOVED AND REPLACED EVACUATION SLIDE PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,947 hrs · 59,463 cycles

DURING SCHEDULED A2 CHECK, FOUND FWD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — DELAMINATED (RT WING SPOILER) · airframe 59,760 hrs · 59,298 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 6 FLIGHT SPOILER DELAMINATED ABOVE ACTUATOR ATTACH POINT. REMOVED AND REPLACED NR 6 FLIGHT SPOILER PER MM.

Part: FLOORBEAM — CRACKED (MID CABIN) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727A +17, WL 208 AND RBL 44. REPAIRED FLOORBEAM PER BFG ER.

Part: FLOORBEAM — CRACKED (CABIN) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727A + 17, WL 208 AND RBL 27.5. REPAIRED FLOORBEAM PER BFG ER.

Part: BEAM — CRACKED (CABIN) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED BETWEEN BS 716 - BS 706, BBL 0, WL 208. REPAIRED BEAM PER SRM AND BFG ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 490, RBL 11. REPAIRED SKIN PER SRM.

Part: BEAM — CRACKED (LT WING T/E) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND LT MLG BEAM REAR SPAR CHORD CRACKED. REPAIRED BEAM PER SWA ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 639, RBL 70, WL 209. REPAIRED FRAME PER SRM.

Part: SPAR — CRACKED (RT WING) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND RT MLG BEAM REAR SPAR CHORD CRACKED. REMOVED AND REPLACED RT MLG BEAM REAR SPAR CHORD PER BFG ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND AFT SVC DOOR LOWER HINGE CUTOUT SKIN CRACKED AT LOWER FWD CORNER. REPAIRED SKIN PER SRM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND NR 9 SPOILER DELAMINATED AT INBD EDGE LOWER SURFACE. REPAIRED SPOILER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, WL 209 & RBL 70. REPAIRED FRAME PER SRM.

Part: LENS — BROKEN (FWD CABIN) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND CENTER AISLE OVERHEAD EMERGENCY EXIT LIGHT FWD CABIN LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: ANGLE — CORRODED (VERT STAB) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL STAB LEFT AND RT DRAG ANGLES CORRODED. REMOVED AND REPLACED ANGLES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND BS 639 FRAME CRACKED AT WL 208, LT AND RT SIDES. REPAIRED FRAME PER SRM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL FIN LT FWD, RT FWD AND RT AFT CLEVIS LUG FACES CORRODED. REPAIRED THE VERTICAL FIN LUG FACES PER SWA ER.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND LOWER HOLE IN BEARSTRAP CRACKED AT BS 303.9 LBL 62, WL 238. REPAIRED CRACK IN BEARSTRAP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND CORROSION ON SHEAR TIE BS 360 STR 18R AND STR 28L. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND NR 6 LE SLAT LOWER SKIN CRACKED .5 INCHES. SLAT SKIN CRACK REPAIRED PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND 2 EA STRINGER CLIPS CRACKED, BS 663, STRINGERS 9L AND 9R. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: FRAME — CRACKED (CABIN) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BIN ATTACH BRACKET BS 440 BETWEEN STR 8L AND STR 9L. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (CABIN) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT BIN ATTACH BRACKETS BS 807 AND BS 827 BETWEEN STR 8L AND STR 9L AND FRAME CRACK AT BIN ATTACH BRACKET BS 807 BETWEEN STR 8R AND STR 9R. REPAIRED FRAMES PER ER.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND CORROSION ON STRINGER SPLICES BS 360 STR 28L AND STR 28R. REMOVED AND REPLACED STRINGER SPLICES PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 296, STR 10L. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 639, RBL 65, WL 208. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 400, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,068 hrs · 78,757 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT ANTENNA CUTOUT, BS 406 AND BS 446, BL 0. REPAIRED SKIN PER BOEING SERVICE BULLETIN.

Part: WEB — CRACKED (FUSELAGE) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND STUB BEAM WEB CRACKED AT BS 695, WL 206 AND RBL 62. REPAIRED STUB BEAM WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,058 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND LT AND RT FUSELAGE FRAMES CRACKED (2 EA) AT BS 188, WL 207 AND WL 208. REMOVED AND REPLACED FRAMES PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 59,068 hrs · 58,757 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 1012, STR 7L. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,013 hrs · 58,717 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 20L, BS 972 AND BS 978. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,758 hrs · 58,512 cycles

DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, ABOVE STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,758 hrs · 58,512 cycles

DURING SCHEDULED C3, FOUND FUSELAGE SKIN CRACKED AT BS 767, ABOVE STR 20L. REPAIRED SKIN PER SRM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 58,689 hrs · 58,452 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11139-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEVATOR TAB MAST FITTING OTBD BUSHING.

Part: SLIDE — LOOSE (FWD SVC DOOR) · airframe 58,215 hrs · 58,082 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (FWD CABIN DOORS) · airframe 57,723 hrs · 57,665 cycles

DURING SCHEDULED C2 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,125 hrs · 57,159 cycles

DURING SCHEDULED PM CHECK, FOUND BOTH OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 57,108 hrs · 57,142 cycles

DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT OVERWING EXIT. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,900 hrs · 56,981 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,890 hrs · 56,973 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 938, BETWEEN STR'S 21L AND 22L. REPAIRED SKIN PER SRM.

Part: SLIDE — UNSERVICEABLE (AFT ENTRY DOOR) · airframe 56,795 hrs · 56,890 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,724 hrs · 56,834 cycles

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

Part: LENS — MISSING (CABIN) · airframe 56,383 hrs · 56,541 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 10 DEF. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,992 hrs · 56,211 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 5 CRACKS AT FUSELAGE EXTERNAL SKIN, BS 500B TO BS 832, STRINGER 10R. REPAIRED SKIN PER SRM AND SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,981 hrs · 56,204 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED (11 EA), STRINGER 4R, BETWEEN BS 480 AND BS 600, (2 EA) CRACKS, STRINGER 4L, BS 520, AND (2 EA) CRACKS STRINGER 19L, BS 807. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (WING) · airframe 55,139 hrs · 55,512 cycles

DURING SCHEDULED C3 CHECK, FOUND RT INBD T/E AFTFLAP OUTBD LWR SURFACE DELAMINATED. R & R RT INBD AFTFLAP PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 55,139 hrs · 55,512 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,087 hrs · 55,472 cycles

DURING WALKAROUND INSPECTION FOUND ( 2 EA ) FUSELAGE SKIN CRACKS AT BS 420 & 500B, STR 10R. REPAIRED SKINS PER SWA RA 1-A53-2545 & SWA RA 1-353-2645.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 54,693 hrs · 55,127 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 54,312 hrs · 54,798 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 54,163 hrs · 54,679 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,302 hrs · 53,955 cycles

DURING SCHEDULED C1 CHECK, FOUND 1.75 EXTERNAL FUSELAGE SKIN CRACK AT BS 494, STR 10R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJ (AFT SVC DOOR) · airframe 53,302 hrs · 53,955 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 53,302 hrs · 53,955 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED EVAC SLIDE ASSY PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 53,234 hrs · 53,898 cycles

AFT ENTRY DOOR EVACUATION SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 53,005 hrs · 53,707 cycles

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

Part: STIFFENER — CRACKED (MLG W/W) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 663 STIFFENER CRACKED AT LBL 3. REPAIRED STIFFENER PER SRM.

Part: SKIN — CRACKED (NR2 SLAT) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND NR 2 L/E SLAT LOWER SKIN CRACKED NEAR OUTBOARD END. REPAIRED SKIN PER SRM.

Part: SLAT — CRACKED (LT WING) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND NR 1 L/E SLAT CRACKED AT TWO ADJOINING RIVET HOLES, INBOARD OF INBOARD MAIN TRACK AND OUTBOARD OF INBOARD AUX TRACK. REPAIRED SLAT PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT PREVIOUS REPAIR. REMOVED AND REPLACED AFT FLAP ASSY PER MM.

Part: SLIDE — LOOSE (AFT ENTRY) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR VIEW LENS LOOSE AND INDICATOR NOT VISIBLE. SECURED VIEW LENS PER MM.

Part: PANEL — CRACKED (NLG WW) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 2 CRACKS IN NLG W/W BELOW FWD RECESS PANEL, BS 244 & BS 245. REPAIRED NLG W/W BOX ASSY PER SRM.

Part: FITTING — CRACKED (LT WING) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT MLG WALKING BEAM FWD OUTBOARD ATTACH LINK CRACKED. REPAIRED FITTING PER SRM.

Part: FITTING — CRACKED (LT WING) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT MLG WALKING BEAM FWD OUTBOARD ATTACH LINK CRACKED. REPAIRED FITTING PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT LBL 1, WL 189. REPAIRED BULKHEAD WEB PER SRM.

Part: FLOORBEAM — CORRODED (AFT CARGO BAY) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 772, LBL 12.5. REPAIRED FLOORBEAM PER RA 1-A53-2021.

Part: FLOORBEAM — CORRODED (AFT CARGO BAY) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM CORRODED AT BS 772, LBL 12.5. REPAIRED FLOORBEAM PER RA 1-A53-2021.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT LBL 1, WL 189. REPAIRED BULKHEAD WEB PER SRM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BULKHEAD WEB CORRODED AT 6 O''CLOCK POSITION. REPAIRED BULKHEAD WEB PER SRM.

Part: STRUCTURE — CRACKED (LT WING SLAT) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND NR 2 L/E SLAT CRACKED AT RIVET HOLES OUTBOARD OF ACTUATOR. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (FWD FUSELAGE) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CAPTAINS LT UPPER WINDOW POST SKIN CRACKED. REPAIRED POST SKIN PER SRM.

Part: DOOR FRAME — CRACKED (SERVICE DOORWAY) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR CRACKED AT LWR AFT FRAME. REPAIRED DOOR FRAME PER BAC DWG 69-69854.

Part: STIFFENER — CRACKED (MLG WW) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 663 VERTICAL STIFFENER CRACKED AT WL 185, LBL 6. REMOVED AND REPLACED STIFFENER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 937, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 2 EA. EXTERNAL FUSELAGE SKIN CRACKS BETWEEN BS 727E & BS 747, STR 18R. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD WEB CRACKS AT RBL 7, WL 199 & RBL 1, WL 189. REPAIRED BULKHEAD PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 795, STR 18L. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT LBL 7, WL 199. REPAIRED WEB PER SRM.

Part: DOOR FRAME — CRACKED (SERVICE DOOR) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR FRAME CRACKED AT AFT 3RD STOP FITTING CUTOUT. REPAIRED DOOR FRAME PER T1-152-003.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOOR BEAM CORRODED, BS 771, RBL 8 TO LBL 8. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOOR BEAMS CORRODED AT RBL 13.8, BS 787, 827 & 867. REPAIRED FLOOR BEAMS PER SRM.

Part: BRACKET — LOOSE (ENTRY DOOR) · airframe 52,857 hrs · 53,581 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY RETAINER BRACKET RIVETS LOOSE. R&R BRACKET RIVETS PER SRM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 52,290 hrs · 53,069 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 4 SLAT I/B END DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — DELAMINATED (RT WING SPOILER) · airframe 52,290 hrs · 53,069 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 5 GROUND SPOILER IS DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 51,608 hrs · 52,499 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,375 hrs · 52,314 cycles

DURING SCHEDULED BC3 CHECK, FOUND AFT SERVICE DOOR AFT LOWER FUSELAGE SKIN DOUBLER CUTOUT CRACKED. REPAIRED SKIN PER SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,365 hrs · 52,306 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 927 AND BS 947.5, APPROX 10 ABOVE WATER SERVICE DOOR. REPAIRED SKIN PER SRM.

Part: BRACKET — LOOSE (SLIDE GIRT BAR) · airframe 51,365 hrs · 52,306 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT BAR ATTACH BRACKETS LOOSE ON CONTAINER. SECURED BRACKETS PER MM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 50,891 hrs · 51,917 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND LT MLG WHEEL WELL PRESSURE DECK WEB CRACKED NEXT TO AILERON TOWER SHAFT ASSY. REPAIRED PRESS WEB PER ER NR 00-0578.

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 50,844 hrs · 51,872 cycles

FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER WHILE ACFT WAS BEING PROVISIONED. INSTALLED SLIDE ASSY PER MM.

Part: INDICATOR — DISLODGED (ESCAPE SLIDE) · airframe 50,516 hrs · 51,595 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: STRINGER — CRACKED (BS 500D & BS 480)

DURING SCHEDULED C1 CHECK, FOUND STRINGERS CRACKED, BS 500D, STRINGER 10L AND BS 480, STRINGER 10R. REPAIRED STRINGER PER SRM.

Part: PCU — INOP (RUDDER)

ABORTED TAKEOFF, DURING TAKEOFF, RUDDER WAS HARD TO OPERATE. REMOVED AND REPLACED RUDDER PCU AND RUDDER CENTERING AND FIELD ASSY.

Part: SKIN — DELAMINATED (RT TE FLAP)

DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD CORNER. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: STRAPS — BROKEN (CABIN)

EMERGENCY FLASHLIGHT STRAPS BROKEN. REMOVED AND REPLACED STRAPS PER MM.

Part: SKIN — CRACKED (BS 727)

FUSELAGE SKIN CRACKED 2 INCHES LONG AT APPROX BS, 727A - 727B, STRINGER 11R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 510)

DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH CRACKS ON FUSELAGE SKIN BS 510, STRINGER 16R, AND BS 930, STRINGER 23L.

Part: VBV DOOR — MALFUNCTIONED (NR 2 ENGINE)

ABORTED TAKEOFF---- NR 2 ENG THRUST WOULD NOT ADVANCE ON TAKEOFF ROLL. REMOVED AND REPLACED NR 2 ENG VBV DOOR ASSY AT 5 O'CLOCK POSITION PER MM.

Part: SLIDE — DETACHED (SERVICE DOOR)

FWD SERVICE DOOR EMERGENCY EVACUATION SLIDE FELL OUT OF CONTAINER. RESTOWED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (BS 440-460)

DURING WALK AROUND CHECK, FOUND A 4 INCH LONG CRACK AT FUSELAGE EXTERNAL SKIN, APPORX BS 440-460, STRINGER 10R. REPAIRED SKIN PER SRM.

Part: SLIDE — PRESSURE LOW (R1 DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (BS 815)

DURING WALKAROUND INSPECTION, FOUND APPROX A 2.5 INCH LONG CRACK AT FUSELAGE SKIN, BS 815 STRINGERS 14-15L. REPAIRED SKIN PER SRM.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED SC CHECK, FOUND LAST BULLNOSE EMERGENCY LIGHT ON RT SIDE INOP. RELAMPED PER BOEING M/M.

Part: SKIN — CRACKED (BS 500)

DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACK AT BS 500, STRINGER 10R. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 1028)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED CLOSET WALL ATTACH ANGLE WEB AT BS 1028 BL 0. REMOVED AND REPLACED PER BOEING SRM.

Part: WEB — CORRODED (BS 1012-1020)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOOR WEB AT BS 1012 TO BS 1020, LBL 2. REPAIRED PER BOEING SRM.

Part: WEB — CORRODED (BS 1016)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOOR WEB AT BS 1016 LBL 13. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — OUT OF LIMITS (BS 1016)

DURING SCHEDULED 1/2 D-CHECK, FOUND 4 FASTENER HOLES ALONG THE FLOORBEAM AT BS 1016 OUT OF LIMITS. REPAIRED PER BOEING TI-A53-014.

Part: INTERCOSTAL — CORRODED (BS 1013)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED LOWER SURFACE OF UPPER FLANGE OF INTERCOSTAL AT BL 0, BS 1013. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CRACKED (BS 947.5)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED BS 947.5 FLOORBEAM UPPER CHORD FROM SCREW HOLE AT LBL 54. REPAIRED PER SWA RA NR 1-353-1834.

Part: INTERCOSTAL — CORRODED (BS 1006-1016)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED DIAGONAL INTERCOSTAL AT BS 1006 TO 1016, LBL 7. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 1016)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOORBEAM AT BS 1016, FLOOR PANEL HOLE LBL 6, BS 1016 FLOOR PANEL HOLE LBL 10, BS 1016 FLOOR PANEL HOLE LBL 15 AND BS 1016 FLOOR PANEL HOLE LBL 16. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 270)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED ZEE ANGLE AT BS 270. REPAIRED PER SWA RA NR 1-353-1840.

Part: INTERCOSTAL — CORRODED (BS 294-312)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED SURFACE ON INTERCOSTAL BETWEEN BS 294 AND 312, RBL 11. REMOVED AND REPLACED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 360)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED STRINGER 14L AT BS 360. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 986.5-1006)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED INTERCOSTAL AT BS 986.5 TO 1006 AT PANEL HOLES, BL 0. REMOVED AND REPLACED PER BOEING SRM.

Part: CHANNEL — CORRODED (BS 994)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED HAT CHANNEL AT PANEL HOLES BS 994, LBL 14 TO LBL 44. REMOVED AND REPLACED PER BOEING SRM.

Part: LIGHTS — INOPERATIVE (CABIN)

DURING SCHEDULED 1/2 D-CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT AFT OF FWD ENTRY DOOR HAS LOOSE LENS. REMOVED AND REPLACED LENS RETAINER ASSY PER BOEING MM.

Part: ANGLE — CRACKED (BS 360)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED ANGLE AT BS 360 STR 14 LT. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — WORN (RT WING)

DURING SCHEDULED 1/2 D-CHECK, FOUND I/B ANGLE WORN JUST I/B FROM I/B FOREFLAP. REMOVED AND REPLACED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED WEB AFT SIDE OF BLKHD LBL 27, WL 207. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 178)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED INDICATION UNDER ANGLE STIFFENER WL 218, LBL 11 AT BS 178. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 787)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED AND BROKEN CARGO TIE DOWN AT FLOOR SUPPORT BEAM AT BS 787, STR 26L, LBL 17.20. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — DAMAGED (BS 540)

DURING SCHEDULED 1/2 D-CHECK, FOUND SKIN ON TOP OF RT OUTBOARD SEAT TRACK FLOORBEAM DAMAGED/PEELING AT BS 540 JUST FWD OF CENTER. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 867)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOOR SUPPORT BEAM AT BS 867, RBL 8.10. REMOVED AND REPLACED PER BOEING SRM.

Part: CLIP — CRACKED (BS 663)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED CLIP AT BS 663R, STR 11 AND BS 663L, STR 11. REPAIRED PER BOEING SRM.

Part: SHEAR TIE — CORRODED (BS 927)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED BETWEEN SHEAR TIE AND SKIN AT BS 927 STR 23L TO 24L. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 344-360)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED INTERCOSTAL FLOORBOARD HOLES AT BS 344 TO 360, RBL 11. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 500)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FASTENER HOLES IN RIGHT TRANSITION ANGLE BETWEEN BS 500 AND 500B. REMOVED AND REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 827-787)

DURING SCHEDULED 1/2 D-CHECK, FOUND INTERGRANULAR CORROSION AT FLOOR SUPPORT BEAM BS 827 TO 787 ABOVE STR 26R. REPLACED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 747)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED CARGO TIE DOWN AT FLOOR SUPPORT BEAM BS 747, STR 26L. REMOVED AND REPLACED PER BOEING SRM.

Part: INTERCOSTAL — CORRODED (BS 967-986.5)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED INTERCOSTAL UPPER AND LOWER SURFACES AT PANEL HOLES RBL 18 FROM BS 967 TO 986.5. REMOVED AND REPLACED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 289)

DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED ANGLE ABOVE STR 12, BS 289. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (PAX DOORWAY)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED AFT ENTRY DOORWAY AT Z-ANGLE. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 1006)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOORBEAM BS 1006 AT FLOOR PANEL HOLE LBL 26. REPAIRED PER BOEING TYPICAL REPAIR TI NR A53-014.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED 1/2 D-CHECK, FOUND THAT ULTRA SONIC INSP SHOWS 100 PERCENT CRACK INDICATION UNDER STRAP LBL 6.5, WL 213 AT BS 178 BULKHEAD LBL 5, WL 210.5 (UNDER BRKT AND OR STRAP) AT BS 178 BULKHEAD AND LBL 6.5, WL 213 BS 178 BULKHEAD. REPAIRED PER BOEING SRM.

Part: BLKHD FASTENER — CRACKED (BS 178)

DURING SCHEDULED 1/2 D-CHECK, FOUND THAT EDDY CURRENT SHOWS CRACK AT FASTENER HEAD, FWD SIDE, WL 234, RBL 10 BS 178 BULKHEAD. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 787)

DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED CARGO TIE DOWNS AT BS 787, STR 26R. REMOVED AND REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED 1/2 D CHECK, FOUND FLOORBEAM CORRODED AT BS 312, BL0. REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (BS 500)

DURING SCHEDULED SERVICE CHECK, FOUND CRACKED FUSELAGE SKIN APPROX 2.75 AT BS 500 D AND S10R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (WS 213)

DURING TERMINAL CHECK, FOUND A .125 CRACK IN FIXED L/E AT KRUGER FLAP SEAL DOOR CUTOUT. REPAIRED PER SWA RA 1-A57-0503.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED C2 CHECK, FOUND A 4 INCH FUSELAGE SKIN CRACK, AT LOWER AFT CORNER OF FWD ENTRY DOOR FRAME. REPAIRED PER SWA RA 1-353-1625.

Part: LIGHT — BROKEN (CABIN)

DURING SCHEDULED A1 CHECK, FOUND NR 2 RT BULLNOSE EMERGENCY EXIT LIGHTS BROKEN AND LENS MISSING. REPLACED LIGHT ASSEMBLY PER BOEING M/M.

Part: SKIN — CRACKED (BS 310)

DURING SCHEDULED SERVICE CHECK, FOUND 3 INCHES FUSELAGE SKIN CRACK AT BS 310 AT S25L. REPAIRED PER BOEING SRM.

Part: COWL — DENTED (NR 1 ENGINE)

EXPERIENCED BIRDSTRIKE TO NUMBER 2 ENGINE. AIRCRAFT DIVERTED TO PHX AND MADE AN UNEVENTFUL LANDING. PERFORMED BIRDSTRIKE INSPECTION AND NOTED DAMAGE TO ENGINE INLET COWL. NO DAMAGE TO ENGINE INTERNALLY. PERFORMED TEMP REPAIR AND MAINTENANCE FERRIED AIRCRAFT TO DAL FOR REPAIRS. REPLACED ENGINE INLET COWL PER BOEING M/M.