N325SW

Part: ROD END — CORRODED (ELEVATOR TAB) · airframe 75,956 hrs · 68,222 cycles

DURING SCHEDULED CV CHECK, FOUND LT ELEVATOR TAB I/B CONTROL ROD FWD ROD END CORRODED. REMOVED AND REPLACED ROD ASSY PER SI AND EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,672 hrs · 68,020 cycles

DURING SCHEDULED SPV CHECK, FOUND LT OVERHEAD EMERGENCY EXIT LIGHT INOP BETWEEN ROW 6 TO ROW 10. REMOVED AND REPLACED BULBS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,672 hrs · 68,020 cycles

DURING SCHEDULED SPV CHECK, FOUND RT OVERHEAD EMERGENCY EXIT LIGHT INOP BETWEEN ROW 1 TO ROW 8. REMOVED AND REPLACED BULBS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 75,672 hrs · 68,020 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 10. SECURED LENS PER MM.

Part: GROUND WIRE — DISCONNECTED (CABIN) · airframe 75,672 hrs · 68,020 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. FOUND GROUND WIRE DISCONNECTED. CONNECTED WIRE PER SWPM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,294 hrs · 67,727 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER CUTOUT CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (PYLON) · airframe 75,080 hrs · 67,559 cycles

DURING SCHEDULED OTS CHECK, FOUND 1 ENGINE PYLON SKIN CRACKED AT 6 O'CLOCK POSITION, APPROXIMATELY 0.125 INCHES AWAY FROM CROWN STRINGER TRIM-OUT EDGE. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (PYLON) · airframe 75,077 hrs · 67,558 cycles

DURING SCHEDULED OTS CHECK, FOUND NR 1 ENG PYLON SKIN CRACKED. REPAIRED SKIN PER ER AND EA.

Part: KEELBEAM — CRACKED (RT MLG WW) · airframe 75,077 hrs · 67,558 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WHEEL WELL AFT KEEL BEAM COVER CRACKED. REMOVED AND REPLACED BEAM PER MM.

Part: LENS — CRACKED (L1 DOOR) · airframe 75,077 hrs · 67,558 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE COVER LENS CRACKED. REMOVED AND REPLACED LENS PER MT.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 75,077 hrs · 67,558 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 4 SLAT AFT WEDGE DELAMINATED. REPAIRED SLAT PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,595 hrs · 67,177 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 505C, STR 15R. REPAIRED SKIN PER EA.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 74,715 hrs · 67,259 cycles

R2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 74,684 hrs · 67,240 cycles

RIGHT WING I/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER EA.

Part: HOUSING — DEFECTIVE (CABIN) · airframe 74,475 hrs · 67,079 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING LOWER EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY HOUSING PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,306 hrs · 66,961 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 989, STR 21L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,311 hrs · 66,962 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 989, STR 21L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,311 hrs · 66,962 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 979, STR 21L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,754 hrs · 65,779 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER AFT CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,754 hrs · 65,779 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 358, BETWEEN STR 4R TO STR 5R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,752 hrs · 65,778 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 362, BETWEEN STR 5R TO STR 6R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,752 hrs · 65,778 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 525, AT STR 5R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,752 hrs · 65,778 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 362, BETWEEN STR 8R TO STR 9R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,752 hrs · 65,778 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER AFT CORNER CUTOUT. REPAIRED SKIN PER EA.

Part: LIGHT — LOOSE (CABIN) · airframe 72,752 hrs · 65,778 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS LOOSE AT ROW 7. REMOVED AND REPLACED EEPLS PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 72,398 hrs · 65,519 cycles

DURING SCHEDULED MV2 CHECK, FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT ASSY PER MM.

Part: HOLDER — DEFECTIVE (FLASHLIGHT) · airframe 72,397 hrs · 65,519 cycles

FWD GALLEY EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED HOLDER ASSY PER MM.

Part: SPAR — CRACKED (RT WING) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING FWD SPAR LOWER CHORD CRACKED AT NR 2 PYLON RT SKATE ANGLE, FWD FASTENER HOLE. REPAIRED SPAR PER SWA EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 767, STR 13L. REPAIRED SHEAR TIE PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT, BS 295, WL 271. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT, BS 288, WL 253. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT, BS 292, WL 261. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 827, STR 13L. REPAIRED SKIN PER SWA EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 590, STR 15R. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 294.5, STR 14R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT, BS 291.75, WL 258. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND BS 559 RT LWR FWD AND AFT FASTENER HOLES COMMON TO THE WING CHORD CRACKED. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BETWEEN BS 290 TO BS 291, BETWEEN WL 232 TO WL 234. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 13L. REPAIRED FRAME PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER CUTOUT, BS 301. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 397, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 380, STR 17L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 373.5, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BS 291, WL 232. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 500C, STR 13L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 932, STR 23L. REPAIRED SKIN PER SWA EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 495, STR 23R. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 907, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND NLG WHEEL WELL T-CHORD SKIN CRACKED AT BS 227.8, LBL 1. REPAIRED SKIN PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 698 TO BS 717, BBL 0.07. REPAIRED BEAM PER SI.

Part: SKIN — CRACKED (BS 502D-518D) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED BETWEEN BS 502D TO BS 518D, BETWEEN STR 12L TO STR 12R. REPAIRED SKIN PER SWA EA.

Part: FLOORBEAM — CRACKED (BS 708) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 708, BL 0, WL 204. REPAIRED BEAM PER SI.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 712, BL 0.07, WL 204. REPAIRED BEAM PER SI.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 20R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 20R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 13L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 807, STR 13L. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 708, LBL 24.5, WL 204. REPAIRED BEAM PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 827, BETWEEN STR 13R TO STR 14R WL 233. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 887, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 13R. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, LBL 45.5, WL 208. REPAIRED BEAM PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 827, BETWEEN STR 13R TO STR 14R WL 234. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND CENTER CABIN LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 45.5. REPAIRED FLOORBEAM PER SWA EA.

Part: FLAP — DEBONDED (RT WING) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING OUTBOARD AFT FLAP DISBONDED NEAR INBOARD END. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND CENTER CABIN LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 24.8. REPAIRED FLOOR BEAM PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 847, AT STR 13L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 500, STR 13L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 807, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 787, BETWEEN STR 13R TO STR 14R, WL 233.5. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 662, RBL 24.5, WL 204. REPAIRED BEAM PER SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 662, LBL 24.5, WL 204. REPAIRED BEAM PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT BETWEEN BS 289.75 TO BS 304, BETWEEN WL 257 TO WL 262. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 16L. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT BETWEEN BS 303 TO BS 304.5, BETWEEN WL 234 TO WL 238.2. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,760 hrs · 65,054 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT BS 290.88, BETWEEN WL 232.88 TO WL 229. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,479 hrs · 64,172 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 426, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,479 hrs · 64,172 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A, STR 17R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,479 hrs · 64,172 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 420, STR 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,479 hrs · 64,172 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 436, STR 16R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,149 hrs · 63,933 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,064 hrs · 63,861 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 405, STR 27L. REPAIRED SKIN PER SWA EA.

Part: HOOK — BROKEN (L2 DOOR) · airframe 70,021 hrs · 63,827 cycles

L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK BROKEN. REMOVED AND REPLACED HOOK PER MT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 67,481 hrs · 61,896 cycles

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

Part: SKIN — CRACKED (BS 259 S19-23L) · airframe 67,235 hrs · 61,807 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259.5, BETWEEN STR 19L AND STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT NACELLE) · airframe 67,140 hrs · 61,736 cycles

DURING SCHEDULED SPV CHECK, FOUND NR 1 ENGINE UPPER PYLON T-CROWN CRACKED. REPAIRED PYLON PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,140 hrs · 61,736 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,140 hrs · 61,736 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 24R. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 66,766 hrs · 61,447 cycles

MID CABIN EMERGENCY EXIT LIGHTS ILLUMINATED WITH SWITCH IN ARMED POSITION. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — FAULTY (CABIN) · airframe 66,375 hrs · 61,136 cycles

DURING SCHEDULED MV1 CHECK, MID CABIN EMERGENCY EXIT LIGHTS STAY ILLUMINATED WITH SWITCH IN ARMED POSITION. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FITTING — CORRODED (L1 DOOR) · airframe 65,437 hrs · 360,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: FITTING — CORRODED (R1 DOOR) · airframe 65,437 hrs · 360,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,437 hrs · 360,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 19L. REPAIRED FRAME PER SWA EA.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 65,437 hrs · 360,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR LOWER FRAME CRACKED AT LOWER FWD CORNER. REMOVED AND REPLACED L1 DOOR PER MM.

Part: FITTING — CORRODED (L1 DOOR) · airframe 65,437 hrs · 360,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: FITTING — CORRODED (R1 DOOR) · airframe 65,437 hrs · 360,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: STRINGER CLIP — CRACKED (BS 747 S19L) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 19L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: INTERCOSTAL — CORRODED (BS 787-794 S25R) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND INTERCOSTAL CORRODED AT BS 787 TO BS 794, STR 25R. REMOVED AND REPLACED INTERCOSTAL PER SRM.

Part: STRINGER SPLICE — CORRODED (BS 907 S23R) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, STR 23R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 620 S5R) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 620, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 807 S8R) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 500D S15R) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500B S21R) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 380 S8R) · airframe 65,437 hrs · 60,410 cycles

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

Part: FRAME — CRACKED (BS 847 S8L) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 440 S8R) · airframe 65,437 hrs · 60,410 cycles

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

Part: FRAME — CRACKED (BS 520 S8L) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 727A S8R) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CORRODED (BS 789 S25R) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN BEAR STRAP CORRODED AT BS 789, STR 25R. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (BS 867 S8L) · airframe 65,437 hrs · 60,410 cycles

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

Part: FRAME — CRACKED (BS 827 S8L) · airframe 65,437 hrs · 60,410 cycles

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

Part: FRAME — CRACKED (BS 787 S8R) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500A S8R) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 480 S8L) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 887 S8L) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 847 S8R) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 360 S8L) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 700 S4R) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 700, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 500B S19L) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 19L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 680 S6R) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 680, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 827 S8R) · airframe 65,437 hrs · 60,410 cycles

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

Part: FRAME — CRACKED (BS 887 S8R) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 480 S8R) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (BS 583 S10L) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 583, STR 10L. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 663 S10R) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (BS 800 S17L) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 800, STR 17L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (BS 767 S8L) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 807 S8L) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 706 S1) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706 S2R) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 706 S2L) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 500C S8L) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 907 S8L) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 294 S10L) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (BS 583 S10R) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 583, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 413 TO BS 433, LBL 3 TO RBL 3. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,437 hrs · 60,410 cycles

DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E+17, STR 20L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (BS 303 S17L) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 303.9, STR 17L. REMOVED AND REPLACED FRAME WEB PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727B S26R) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 270, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CRACKED (BS 344) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BS 344, LBL 10. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500C S25R) · airframe 65,437 hrs · 60,410 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 25R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: SKIN — CORRODED (BS 967 S27L-R) · airframe 64,475 hrs · 59,699 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 967, STR 27L AND STR 27R. REPAIRED SKIN PER SWA EA.

Part: SHEAR TIE — CORRODED (BS 967) · airframe 64,475 hrs · 59,699 cycles

DURING SCHEDULED C1 CHECK, FOUND SHEAR TIE CORRODED AT BS 967, BL 0. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CORRODED (BS 947 S27L) · airframe 64,475 hrs · 59,699 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 947, STR 27L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 63,477 hrs · 58,910 cycles

DURING SCHEDULED C4 CHECK, FOUND LT HORZONTAL STAB LOWER SKIN CRACKED AT STA 117. REPAIRED SKIN PER SRM.

Part: CRANK ASSY — WORN (ELEVATOR TAB) · airframe 63,477 hrs · 58,910 cycles

DURING SCHEDULED C4 CHECK, FOUND LT ELEVATOR TAB CONTROL MACHANISM WITH EXCESSIVE PLAY AT OUTBOARD TAB CONTROL ROD. REMOVED AND REPLACED TAB CRANK ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 63,477 hrs · 58,910 cycles

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

Part: SKIN — CRACKED (L1 DOOR) · airframe 63,477 hrs · 58,910 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR LOWER GATE SKIN CRACKED AT AFT LOWER CORNER. REPAIRED L1 DOOR PER MM.

Part: FIRE DETECTOR — FAULTY (AFT CARGO BAY) · airframe 62,953 hrs · 58,487 cycles

AIR TURNBACK / DECLARED EMERGENCY. AFT CARGO COMPARTMENT FIRE WARNING LIGHT ILLUMINATED AND WARNING HORN SOUNDED. DEPLOYED FIRE EXTINGUISHER. REMOVED AND REPLACED AFT CARGO COMPARTMENT FIRE DETECTORS PER MM.

Part: FITTING — CRACKED (NLG W/W) · airframe 62,920 hrs · 58,460 cycles

DURING SCHEDULED SERVICE CHECK, FOUND NLG ACTUATOR SUPPORT FITTING GUSSETT CRACKED IN RADIUS. REMOVED AND REPLACED GUSSETT FITTING PER SRM.

Part: WEDGE — CRACKED (RT WING TE FLAP) · airframe 62,753 hrs · 58,329 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING T/E MID FLAP T/E WEDGE CRACKED. REMOVED AND REPLACED T/E WEDGE PER MM AND SRM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,753 hrs · 58,329 cycles

DURING SCHEDULED SPV CHECK, FOUND EMERGENCY EXIT LIGHTS INOP FROM ROW 2 TO ROW 5. RELAMPED LIGHTS PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,573 hrs · 58,329 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 61,901 hrs · 57,698 cycles

MID CABIN EEPLS TRACK LOOSE. REMOVED AND REPLACED EEPLS PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 61,713 hrs · 57,550 cycles

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

Part: SKIN — CRACKED (BS 511D) · airframe 61,671 hrs · 57,522 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 511D, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 500C) · airframe 61,671 hrs · 57,522 cycles

DURING WALKAROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 520) · airframe 61,517 hrs · 57,402 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 16L. REPAIRED SKIN PER SRM.

Part: CABLE — MISROUTED (L2 DOOR SLIDE) · airframe 61,517 hrs · 57,402 cycles

DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY PER MM.

Part: SKIN — CRACKED (BS 934) · airframe 60,540 hrs · 56,612 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 934, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 465-485) · airframe 60,540 hrs · 56,612 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 465 TO BS 485, STR 16R TO STR 17R. REPAIRED SKIN PER SWA EA & SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 60,225 hrs · 56,379 cycles

EMERGENCY EXIT INTERIOR & EXTERIOR LIGHTS FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — LOOSE (EMERGENCY LIGHT) · airframe 59,923 hrs · 56,157 cycles

DURING SCHEDULED RON CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT ILLUMINATED WITH SWITCH IN ARMED POSITION. RESEATED CONNECTOR TO BATTERY PACK PER MM.

Part: BUSHING — WORN (LT ELEVATOR TAB) · airframe 59,561 hrs · 55,861 cycles

DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB NR 1 HINGE BUSHING & HARDWARE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,086 hrs · 55,491 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 968, STR 21L. REPAIRED SKIN PER SWA EA.

Part: ACM — MALFUNCTIONED (A/C BAY) · airframe 59,023 hrs · 55,437 cycles

AIR TURNBACK / DECLARED EMERGENCY. BURNING SMELL IN CABIN & COCKPIT. REMOVED AND REPLACED RT AIR CYCLE MACHINE PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,548 hrs · 55,101 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 & R1 DOOR EMERGENCY EXIT SIGNS INOP. RELAMPED L1 & R1 EXIT SIGNS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,565 hrs · 54,359 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 937, STRINGER 14L, CRACKED. REPAIRED SKIN PER SRM.

Part: LENS — CRACKED (FUSELAGE) · airframe 57,565 hrs · 54,359 cycles

DURING SCHEDULED C2 CHECK, FOUND SIDEWALL EMERGENCY EXIT LIGHT LENS AT ROW 11 ABC, CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: DUCT — RESTRICTED (COCKPIT) · airframe 57,431 hrs · 54,258 cycles

EQUIPMENT COOLING LIGHT ILLUMINATED. AUTOPILOT SYS DISCONNECTED AND FUMES ENTERED COCKPIT. FOUND INSTRUMENT COOLING AIRFLOW TO CAPT'S & F/O'S INSTRUMENT PANELS RESTRICTED. CLEANED DISTRIBUTION DUCT AND OPS CK GOOD PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,797 hrs · 53,751 cycles

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

Part: FITTING — LOOSE (L2 DOOR GIRT BAR) · airframe 56,797 hrs · 53,751 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L2 DOOR EVAC SLIDE FWD GIRT BAR FLOOR FITTING LOOSE. SECURED L2 DOOR EVAC SLIDE FITTING PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,797 hrs · 53,751 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 500D, RBL 13, CORRODED. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 56,674 hrs · 53,652 cycles

DURING SCHEDULED C1 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 ELEVATOR TAB HINGE BUSHING AND HARDWARE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,448 hrs · 53,461 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 961, STRINGER 21L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,285 hrs · 53,335 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN AT BS 740, STRINGER 18L, BS 792, STRINGER 19L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,044 hrs · 53,150 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 727E + 16, STRINGER 19L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,810 hrs · 52,981 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 275, BETWEEN STRINGERS 15L AND 16L, CRACKED. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 55,810 hrs · 52,981 cycles

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

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 53,865 hrs · 51,446 cycles

DURING SCHEDULED C2 CHECK, FOUND LT OUTBD TE FORE FLAP DELAMINATED AT T/E. REMOVED AND REPLACED LT OUTBD T/E FORE FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,865 hrs · 51,446 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR CUTOUT LOWER FWD CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 53,865 hrs · 51,446 cycles

DURING SCHEDULED C2 CHECK, FOUND LT INBOARD AFT T/E FLAP DELAMINATED AT LOWER INBD CORNER. REMOVED AND REPLACED LT INBD AFT T/E FLAP PER MM.

Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE) · airframe 53,865 hrs · 51,446 cycles

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

Part: SLIDE — DEPLOYED (SERVICE DOOR) · airframe 53,784 hrs · 51,389 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,275 hrs · 50,960 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 807, STR 17L. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 52,950 hrs · 50,690 cycles

DURING SCHEDULED C1 CHECK, FOUND BS 1016 BULKHEAD CRACKED AT STR 7L. REPAIRED BULKHEAD PER SRM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 51,898 hrs · 49,873 cycles

DURING SCHEDULED C4 CHECK, SWA SI 11139-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB MAST HARDWARE AND BUSHING AND NR 1 TAB HINGE BUSHING PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,835 hrs · 49,818 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER 5R CRACKED AT BS 827+12. REPAIRED STRINGER PER SRM

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 51,835 hrs · 49,818 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14L AND STR 15L. REPAIRED SHEAR TIE PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 51,835 hrs · 49,818 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 5L. REPAIRED STRINGER SPLICE PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 51,835 hrs · 49,818 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA STRINGER CLIPS CRACKED, BS 616, STR 5L AND BS 727A, STR 4L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,835 hrs · 49,818 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND TIE CLIPS CRACKED (2 EA) AT STR 4L, BS 727B AND BS 807. REMOVED AND REPLACED TIE CLIPS PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 51,835 hrs · 49,818 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICES CRACKED (3 EA) AT BS 360 AT STR 4L, BS 908 AT STR 4L AND BS 908 AT STR 4R. REMOVED AND REPLACED STRINGER SPLICES PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 51,835 hrs · 49,818 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA STRINGER CLIPS CRACKED, BS 727B, STR 4L AND BS 847, STR 4R. REMOVED AND REPLACED BOTH STRINGER CLIPS PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,534 hrs · 49,581 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,728 hrs · 48,957 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 26R. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (CARGO BAY) · airframe 50,293 hrs · 48,591 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,049 hrs · 48,384 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 10L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 50,049 hrs · 48,384 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,663 hrs · 47,272 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED .25 INCHES LONG AT POINT C ON RT C-D WINDOW POST. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,663 hrs · 47,272 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED .1 INCHES LONG AT POINT C ON LT C-D WINDOW POST. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,663 hrs · 47,272 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAMECRACKED, BS 639, STRINGER 15R. REPAIRED FRAME PER SWA RA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,663 hrs · 47,272 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED, BS 559, STRINGER 14L. REPAIRED FRAME PER SWA RA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,663 hrs · 47,272 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,663 hrs · 47,272 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME INNER CHORD CRACKED AT BS 559, STR 14R. REPAIRED FRAME CHORD PER SWA RA.

Part: FLAP — DELAMINATED (LT WING) · airframe 48,663 hrs · 47,272 cycles

DURING SCHEDULED 1/2 D CHECK, FOUND LT OUTBD T/E AFT FLAP DELAMINATED AT AFT EDGE CENTER. REMOVED AND REPLACED AFT T/E OTBD FLAP PER MM.

Part: BRACKET — CORRODED (PAX ENTRYWAY) · airframe 48,663 hrs · 47,272 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE FLOOR GIRT BAR BRACKETS (FWD AND AFT) CORRODED. REMOVED AND REPLACED BOTH BRACKETS PER SRM & MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,663 hrs · 47,272 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,663 hrs · 47,272 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 26R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 48,663 hrs · 47,272 cycles

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

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 48,663 hrs · 47,272 cycles

DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 616 BELOW FLOOR LEVEL LT SIDE. REPAIRED STIFFENER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,663 hrs · 47,272 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 773, STR 14L. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 48,140 hrs · 46,855 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS LOOSE AT BOTH FWD AND AFT CABIN. SECURED EEPLS PER MM.

Part: BEAM — WORN (LT MLG) · airframe 47,620 hrs · 46,422 cycles

DURING SCHEDULED A2 CHECK, FOUND LT MLG WALKING BEAM I/B BEARING MIGRATED 3/16. REMOVED AND REPLACED WALKING BEAM PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,306 hrs · 46,147 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS INOP AT MID AND AFT CABIN. RELAMPED EEPLS PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 47,292 hrs · 46,129 cycles

DURING SCHEDULED PM CHECK, FOUND RT T/E OUTBOARD AFT FLAP DELAMINATED ON INBOARD END, APPROX 11. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — LOOSE (AFT ENTRY DOOR) · airframe 47,236 hrs · 46,082 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE ASSY LOOSE. SECURED AFT ENTRY EVAC SLIDE ASSY PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 46,769 hrs · 45,681 cycles

AFT SVC DOOR EMERGENCY EXIT SIGN LOOSE. SECURED EXIT SIGN PER MM.

Part: RETAINER — LOOSE (ENTRY DOOR) · airframe 46,326 hrs · 45,301 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 45,863 hrs · 44,931 cycles

DURING SCHEDULED RON CHECK, AFT ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 45,565 hrs · 44,678 cycles

DURING SCHEDULED A1 CHECK, FOUND AFT LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,517 hrs · 44,640 cycles

OUTBOARD FWD EMERGENCY FLASHLIGHT RED LIGHT INDICATOR INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BULB — INOPERATIVE (CABIN FLOOR) · airframe 45,365 hrs · 44,515 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS BULB INOP IN AFT SECTION. REMOVED AND REPLACED BULB PER MM.

Part: SLIDE — OUT OF ADJ (PAX DOOR) · airframe 45,365 hrs · 44,515 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. REPOSITIONED EVAC SLIDE ASSY PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 44,361 hrs · 43,680 cycles

DURING SCHEDULED SPECIAL VISIT AT DALFORT, FOUND 3 CRACKS AT BS 178 BULKHEAD WEB LBL 15 & LBL 24, WL 207 & LBL 12, WL 218. REPAIRED BULKHEAD PER SRM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 43,018 hrs · 42,490 cycles

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

Part: SLIDE — DEPLOYED (SERVICE DOOR) · airframe 42,537 hrs · 42,090 cycles

FWD SERVICE DOOR EVACUATION SLIDE PARTIALLY DEPLOYED ON THE GROND. R&R SLIDE ASSY PER MM.

Part: SLIDE — DISLODGED (PAX DOOR)

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

Part: CLIP — LOOSE (EVAC SLIDE)

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT BAR RETENSION CLIPS LOOSE. REMOVED AND REPLACED CLIPS FASTENERS PER MM.

Part: SLIDE — LOOSE (CABIN)

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

Part: CABLE — FRAYED (PAX DOORWAY)

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY EVACUATON SLIDE RELEASE CABLE FRAYED. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: FIRE LOOP — OUT OF POSITION (NR 1 ENGINE)

ABORTED TAKEOFF, NR 1 ENG OVERHEAT MASTER CAUTION ILLUMINATED DURING TAKEOFF AT APPROX 50 KNOTS. REPOSITIONED NR 1 ENG FIRE DETECTION LOOP AT 6 O'CLOCK POSITION PER MM. OPS CHECKED NORMAL.

Part: LINES — MISINSTALLED (RT MLG)

RT BRAKES FEEL SPONGY AND INEFFECTIVE. REMOVED CAPS AND PLUGS LEFT ON BRAKE LINES AT RT MLG SWIVEL INBD AND OUTBD LINES. RECONNECTED LINES, BRAKES LEAK AND OPS CHECKED GOOD.

Part: BRAKE — MALFUNCTIONED (RT MLG)

DURING SCHEDULED 1/4D CHECK, TAXING ACFT FOUND RT BRAKE PRESS WEAK AND WITH ANTI-SKID SYSTEM ON INOP. REMOVED AND REPLACED RT BRAKE ASSY PER MM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND 8 CRACKS FROM 1 TO 4 INCHES LONG AT BS 178 BULKHEAD, LBL 24-RBL 24. REPAIRED BULKHEAD PER SWA RA NR 1-353-2124.

Part: WEB — CRACKED (BS 663)

DURING SCHEDULED 1/4D CHECK, FOUND BS 663 PRESS WEB CRACKED, LBL 32. REPAIRED WEB PER SWA RA NR 1-353-2121.

Part: BULKHEAD CHORD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND T-CHORD CRACKED, BS 178 BULKHEAD RBL 24 WL 207. REPAIRED T-CHORD PER SRM.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 947)

DURING SCHEDULED BC3 CHECK, FOUND A 1.5 INCH LONG CRACK ON FUSELAGE SKIN, BS 947, ABOVE STRINGER 24L. REPAIRED SKIN PER SRM.

Part: LINE — LOOSE (NR 1 ADC)

AIR TURNBACK - AFTER TAKEOFF, CAPTAIN'S AIR SPEED, ALTIMETER, AND IVSI GIVING ERRATIC INDICATIONS. FOUND NR 1 ADC PITOT LINE LOOSE. SECURED LINE PER MM.

Part: SCREW — LOOSE (PASSENGER DOOR)

AFT ENTRY DOOR AFT GIRT BAR RETAINING FLOOR MOUNT LOOSE. REPLACED AND SECURED WITH NEW HARDWARE (ORIGINAL SCREWS TOO SHORT).

Part: RIB — DENTED (HORIZ STAB)

DURING SCHEDULED C4 CHECK, FOUND LT HORIZ STAB DENTED ON RIB APPROX 3.5 FT FROM INBD ROOT. REMOVED AND REPLACED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED C1 CHECK, FOUND A FUSELAGE SKIN CRACK AT AFT SERVICE DOOR UPPER HINGE CUTOUT UPPER FWD CORNER. REPAIRED PER SWA RA 1-353-1746.

Part: SKIN — CRACKED (SERV DOORWAY)

DURING SCHEDULED BC4 CHECK, FOUND AFT SERVICE DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED PER SWA RA 1-353-1700.

Part: SKIN — CRACKED (SERV DOORWAY)

DURING SCHEDULED BC4 CHECK, FOUND AFT SERVICE DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178 AT WL 212.5, LBL 4.7, AT WL 199, AND AT WL 201.5. REPAIRED PER BOEING SRM.

Part: BULKHEAD — DAMAGED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BULKHEAD AT BS 178 DAMAGED AT WL 187.5, LBL 11.5. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (SERV DOOR CUTOUT)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER AFT END OF FWD SERVICE DOOR. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 296)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACK AT BS 296, RBL 53, WL 209. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 286, BETWEEN S24 AND 25R, AT BS 994.5, 998, 1001, 1005 AT S14L, AND AT BS 282, BETWEEN S22 AND 23R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (AFT GALLEY DOOR)

DURING SCHEDULED D-CHECK, FOUND AFT GALLEY DOOR OUTER SKIN CRACKED AT LOWER HINGE CUTOUT, UPPER OUTER EDGE. REPAIRED PER BOEING SRM.

Part: FRAME — GOUGED (BS 867)

DURING SCHEDULED D-CHECK, FOUND FRAME GOUGED AT BS 867, RBL 44, WL 170. REPAIRED PER BOEING SRM.

Part: BULKHEAD CHORD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BULKHEAD LT VERTICAL CHORD CRACKED AT BS 178, WL 184.5, AND AT LT SIDE CHORD AT WL 195 TO 196. REPLACED PER BOEING SRM.

Part: SKIN — GOUGED (BS 936)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 936, BETWEEN S19 AND 20L. REPAIRED PER BOEING SRM.

Part: FRAME — DENTED (BS 1138)

DURING SCHEDULED D-CHECK, FOUND FRAME DENTED AT BS 1138, RBL 25, WL 268. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (BS 500)

DURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 500D, S19R. REPLACED SECTION PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 294.5/986.5)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 294.5, AT RBL 4, WL 208, AT BS 986.5, RBL 20 TO 45, RBL 5. REPAIRED PER BOEING SRM.

Part: MOPSILL — CORRODED (BS 301-341)

DURING SCHEDULED D-CHECK, FOUND MOPSILL CORRODED FROM BS 301 TO 341, RBL 55 AND 208. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 869)

DURING SCHEDULED C3 CHECK, FOUND FUSLAGE SKIN CRACKED AT BS 869, S24R. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (RT WING)

DURING SCHEDULED C3 CHECK, FOUND RT WING LOWER SKIN AT NR 6 SLAT CRACKED JUST O/B OF PREVIOUS REPAIR AND A CRACK AT EXTREME O/B END OF SLAT. REPAIRED PER SWA RA 1-357-259 AND BOEING DRAWING 65C30133.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED A1 CHECK, FOUND FWD I/B EMERGENCY FLASHLIGHT LOW BATTERY. REPLACED BATTERY PER BOEING M/M.