N304SW

Part: SIGN — INOPERATIVE (CABIN) · airframe 77,351 hrs · 72,301 cycles

DURING SCHEDULED HC1 CHECK, FOUND AFT GALLEY EMERGENCY EXIT SIGN INOP. RELAMPED PER MM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 77,351 hrs · 72,301 cycles

DURING SCHEDULED HC1 CHECK, FOUND FWD GALLEY EMERGENCY EXIT SIGN INOP. RELAMPED PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,332 hrs · 72,289 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 76,912 hrs · 71,977 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,718 hrs · 71,837 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: LENS — MISSING (CABIN) · airframe 76,579 hrs · 71,737 cycles

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

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 76,509 hrs · 71,687 cycles

FWD LOWER EMERGENCY FLASHLIGHT DIM. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 76,416 hrs · 71,621 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,381 hrs · 71,592 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,735 hrs · 71,129 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 957, STR 5R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,735 hrs · 71,129 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 906, BETWEEN STR 4L STR 5L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,735 hrs · 71,129 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,735 hrs · 71,129 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 957, STR 5R. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 75,735 hrs · 71,129 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING I/B TRAILING EDGE FORE FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 75,735 hrs · 71,129 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING I/B TRAILING EDGE FORE FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 75,735 hrs · 71,129 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR SLIDE COVER FWD GIRT BAR CLIP LOOSE. REMOVED AND REPLACED CLIP PER SRM.

Part: COVER — MISSING (CABIN) · airframe 75,539 hrs · 70,990 cycles

RT EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,222 hrs · 70,762 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 272, STR 16R. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (R1 DOOR) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND R1 DOOR SKIN CRACKED AT UPPER HINGE CUTOUT, BS 290, BETWEEN WL 256 TO WL 259. REPAIRED SKIN PER ER.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 7,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND KEEL BEAM CORRODED AT BS 787, STR 27L. REPAIRED BEAM PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND MID CABIN FRAME CRACKED AT BS 639, WL 216 LT SIDE. REPAIRED FRAME PER DWG.

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING O/B FORE FLAP SKIN DELAMINATED AT 100" O/B OF I/B END. REPAIRED SKIN PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 7,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 769 TO BS 770, STR 25L. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 7,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 847, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FORE FLAP) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING O/B FORE FLAP SKIN CRACKED AT ATTACH FITTING CUTOUT. REPAIRED SKIN PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM INNER CHORD CRACKED AT BS 639, LBL 64. REPAIRED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 25L TO 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 25L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND MID CABIN LT FRAME WEB CRACKED AT BS 639, WL 215. REMOVED AND REPLACED WEB PER DWG.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT KEEL BEAM CORRODED BETWEEN BS 520 TO BS 530. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL CHORD CRACKED AT BS 666, RBL 24. REPAIRED CHORD PER ER.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM CHORD CRACKED AT BS 639, LBL 64. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CHORD CRACKED BETWEEN BS 666 TO BS 663, RBL 24. REPAIRED CHORD PER PAE ER.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 638, LBL 61. REPAIRED WEB PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727, RBL 24. REPAIRED CHORD PER ER.

Part: SKIN — CRACKED (FORE FLAP) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING O/B FORE FLAP SKIN CRACKED AT O/B TRACK ATTACH FITTING CUTOUT. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 786, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 794, BETWEEN STR 24R TO STR 25R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 24R. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 847, BETWEEN STR 27L TO 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BETWEEN BS 520 TO BS 530, STR 28R. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 22R. REMOVED AND REPLACED CLIP PER SRM.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND NR 2 L/E SLAT T/E WEDGE UPPER SURFACE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 25R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 74,925 hrs · 70,551 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP DAMAGED AT BS 420, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (LT WING) · airframe 74,103 hrs · 69,950 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT WING UPPER SKIN CRACKED AT STA 251. REPAIRED SKIN PER SWA EA.

Part: FAN — FAULTY (E&E BAY) · airframe 73,474 hrs · 69,480 cycles

GASPER FAN CIRCUIT BREAKER OPENED AND CABIN HAD A SMOKE ODOR. REMOVED AND REPLACED GASPER FAN PER MM.

Part: ENGINE — SHUTDOWN (NR 2) · airframe 73,227 hrs · 69,307 cycles

INFLIGHT SHUTDOWN/DIVERSION. NR 2 ENGINE FAILED DURING CLIMB THRU 33,000 FT. NO ABNORMAL INDICATIONS ON ANY ENGINE INSTRUMENT. FUEL WAS BEING TRANSFERRED FROM NR 1 TANK TO NR 2 TANK WHEN ENGINE FAILURE OCCURRED. PERFORMED VISUAL CHECK OF NR 2 ENGINE FUEL CONTROL NO DEFECTS NOTED. COMPLIED WITH ENGINE FUEL SUCTION FEED OPERATION TEST PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 71,671 hrs · 68,143 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CORRODED BETWEEN BS 951 AND BS 960, STR 27L. REPAIRED SKIN PER ER.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 71,671 hrs · 68,143 cycles

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

Part: SKIN — CRACKED (HORIZ STAB) · airframe 71,660 hrs · 68,134 cycles

DURING SCHEDULED C3 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 132. REPAIRED SKIN PER SRM.

Part: STRINGER — CORRODED (BS 947 S26L) · airframe 71,660 hrs · 68,134 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 26L CORRODED AT BS 947. REPAIRED STRINGER PER SRM.

Part: SKIN — CORRODED (BS 360 S24R) · airframe 71,660 hrs · 68,134 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 360, STR 24R. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (BS 402 S19L) · airframe 71,660 hrs · 68,134 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 19L CRACKED AT BS 402. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (BS 360 S22L) · airframe 71,660 hrs · 68,134 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 22L CORRODED AT BS 360. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CRACKED (BS 500C S23L) · airframe 71,660 hrs · 68,134 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500C, STR 23L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 847 S18L) · airframe 71,660 hrs · 68,134 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 18L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CRACKED (BS 480 S25L) · airframe 71,660 hrs · 68,134 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 480, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (BS 450 S26L) · airframe 71,660 hrs · 68,134 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 26L CORRODED AT BS 450. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 22L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 460, STR 17R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 25R CRACKED AT BS 505C. REPAIRED STRINGER PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 25R. REPAIRED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (BS 500B S22L) · airframe 71,660 hrs · 68,134 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,660 hrs · 68,134 cycles

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

Part: HANDLE — DIRTY (COCKPIT) · airframe 71,648 hrs · 68,122 cycles

LANDING GEAR EXTENDED 3 GREEN LIGHTS ILLUMINATED, 3 RED LIGHTS DID NOT EXTINGUISH. CYCLED LANDING GEAR ALL INDICATIONS NORMAL. INSPECTED AND FOUND LANDING GEAR HANDLE STAYS OUT. LUBED AND CLEANED LANDING GEAR HANDLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,018 hrs · 67,598 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 906, STR 6R. REPAIRED SKIN PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,007 hrs · 67,588 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,007 hrs · 67,588 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,007 hrs · 67,588 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,007 hrs · 67,588 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (BS 906 S4-7R) · airframe 70,777 hrs · 67,405 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 906, BETWEEN STR 4R AND STR 7R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 386 S19R) · airframe 70,777 hrs · 67,405 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 386, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 908 S4L) · airframe 70,777 hrs · 67,405 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 908, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 70,777 hrs · 67,405 cycles

DURING SCHEDULED HC1 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED INBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: STRIP — LOOSE (CABIN) · airframe 70,725 hrs · 67,368 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 1 ABC. REMOVED AND REPLACED STRIP PER MM.

Part: SKIN — CRACKED (BS 491 S26L) · airframe 70,515 hrs · 67,201 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 494, STR 26L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 941 S22R) · airframe 70,515 hrs · 67,201 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 941, STR 22R. REPAIRED SKIN PER SWA EA.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 70,181 hrs · 66,951 cycles

ALL LIGHTS ON CARGO FIRE PANEL ILLUMINATED WITH MASTER FIRE WARNING LIGHT AND BELL. CARGO FIRE PANEL LIGHTS STAYED ON FOR 15 MINUTES, THEN WENT OFF. REMOVED AND REPLACED CARGO FIRE PANEL CONTROL PANEL PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,976 hrs · 66,793 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 269 S15R) · airframe 69,976 hrs · 66,793 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 269, STR 15R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,929 hrs · 66,760 cycles

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505, STR 23R. REPAIRED SKIN PER SWA EA.

Part: WINDOW — ARCED (COCKPIT) · airframe 69,351 hrs · 66,338 cycles

PILOT'S L2 WINDOW ARCHING. REMOVED AND REPLACED L2 WINDOW PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 69,262 hrs · 66,273 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SHEAR TIE — CRACKED (BS 500A S14L) · airframe 69,218 hrs · 66,241 cycles

DURING SCHEDULED MV2 CHECK, FOUND SHEAR TIE CRACKED AT BS 500A, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SWA EA.

Part: SKIN — CRACKED (BS 500A S16L) · airframe 69,218 hrs · 66,241 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 780 S19L) · airframe 69,218 hrs · 66,241 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, STR 19L. REPAIRED SKIN PER SWA EA.

Part: CREASE BEAM — CRACKED (BS 445 S18R) · airframe 69,134 hrs · 66,169 cycles

DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 445, STR 18R. REPAIRED WEB SECTION PER SRM.

Part: SKIN — CRACKED (BS 514B S18R) · airframe 68,424 hrs · 65,584 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514B, STR 18R. REPAIRED SKIN PER SWA EA AND SRM.

Part: LIMIT SWITCH — FAULTY (T/E FLAP) · airframe 68,154 hrs · 65,355 cycles

DECLARED EMERGENCY, ON APPROACH FLAPS WOULD NOT EXTEND PAST 25 DEGREES. CYCLED FLAPS UP AND TO 30 DEGREES, FLAPS WOULD NOT EXTEND PAST 25 DEGREES. REMOVED AND REPLACED S560 FLAP LOAD LIMIT SWITCH PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,082 hrs · 65,304 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506, STR 26L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,082 hrs · 65,304 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504, STR 19R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,082 hrs · 65,304 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RIGHT FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,082 hrs · 65,304 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 832, STR 17L. REPAIRED SKIN PER SRM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,611 hrs · 64,951 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD RT EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 67,523 hrs · 64,876 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 67,523 hrs · 64,876 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 67,409 hrs · 64,787 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,147 hrs · 64,593 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — CRACKED (BS 500A) · airframe 67,137 hrs · 64,585 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A, STR 26R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 353) · airframe 67,137 hrs · 64,585 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 353, STR 25R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 315) · airframe 67,137 hrs · 64,585 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 315, STR 25R. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (BS 360) · airframe 67,137 hrs · 64,585 cycles

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,885 hrs · 64,407 cycles

DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,790 hrs · 64,333 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,790 hrs · 64,333 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 66,583 hrs · 64,173 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (BS 930) · airframe 66,583 hrs · 64,173 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 22R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 930) · airframe 66,583 hrs · 64,173 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, BETWEEN STR 24R TO STR 25R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 504-513) · airframe 65,985 hrs · 63,703 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 504B AND BS 513B, STR 16L AND STR 17L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 515A) · airframe 65,985 hrs · 63,703 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 505A AND BS 515A, STR 15L. REPAIRED SKIN PER SWA EA.

Part: STRINGER — CORRODED (BS 321) · airframe 65,663 hrs · 63,468 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 321, STR 29R. REMOVED AND REPLACED STRINGER PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 65,574 hrs · 63,387 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,228 hrs · 63,118 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 485, STR 16L. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,228 hrs · 63,118 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A + 4, STR 16R. REPAIRED SKIN PER SWA EA AND SRM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,062 hrs · 62,986 cycles

DURING SCHEDULED A1 CHECK, FOUND RT FWD CABIN EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 64,694 hrs · 62,697 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 & R1 DOOR LOWER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY & CHARGER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,415 hrs · 62,450 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 500A + 6, STR 17L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,011 hrs · 62,135 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,712 hrs · 61,894 cycles

DURING SCHEDULED C4 CHECK, FOUND FOUND FUSELAGE SKIN AT BS 1012, STRINGER 24R, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,712 hrs · 61,894 cycles

DURING SCHEDULED C4 CHECK, FOUND AT BS 500C + 4, STRINGER 17L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,614 hrs · 61,816 cycles

DURING SCHEDULED THRU CHECK, FOUND FUSELAGE SKIN AT BS 500A + 15, ABOVE STRINGER 16R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,773 hrs · 61,159 cycles

DURING SCHEDULED C3 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 273, STRINGER 16L AND BS 911, STRINGER 23R. REPAIRED SKIN SECTIONS PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,773 hrs · 61,159 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 482, STRINGER 17L, CRACKED. REPAIRED SKIN PER EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,773 hrs · 61,159 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD SERVICE DOOR FRAME CUTOUT BELOW UPPER HINGE STUB FRAME CRACKED. REPAIRED FRAME PER EA.

Part: SENSOR — FAULTY (RT MLG) · airframe 62,646 hrs · 61,041 cycles

AIR TURNBACK, RIGHT MLG RED WARNING LIGHT ILLUMINATED. CYCLED GEAR, NO HELP. REMOVED AND REPLACED RIGHT MLG UPLOCK SENSOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,523 hrs · 60,939 cycles

DURING SCHEDULED PM CHECK, FOUND 4 EACH FUSELAGE SKIN CRACKS BETWEEN BS 500C AND BS 500C + 17, STRINGER 15L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,666 hrs · 60,185 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 370, STRINGER 26L, CRACKED. REPAIRED SKIN PER EA AND SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 61,001 hrs · 59,690 cycles

DURING SCHEDULED D CHECK, FOUND KEEL BEAM CHORD AT BS 727 TO BS 727 + 15, RBL 8 TO LBL 8, CORRODED. REPAIRED KEEL BEAM CHORD PER ER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER 26L, BS 727 + 5, CORRODED. REPAIRED STRINGER PER SRM.

Part: FLOORBEAM — CRACKED (CARGO BAY) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOORBEAM AT BS 727 + 18, RBL 44, CRACKED. REPAIRED FLOORBEAM SECTION PER ER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 60,998 hrs · 56,687 cycles

DURING SCHEDULED D CHECK, FOUND BS 1016, AFT PRESSURE BULKHEAD WEB, AT DOME CAP RBL1, CRACKED. REPAIRED WEB PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,998 hrs · 56,687 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT BS 395, BETWEEN STRINGER 15L AND STRINGER 16L, CRACKED. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND 2 EACH BEAR STRAPS AT THE L1 DOOR UPPER AND LOWER HINGE CUTOUTS, CRACKED. REPAIRED BEAR STRAPS PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME AT BS 663, STRINGER 2L, CRACKED. REPAIRED FRAME SECTION PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 597, STRINGER 8R, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: WIRE — BROKEN (COCKPIT) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND L1 AND R1 DOOR EVAC SLIDE LIGHTS INOP. REPAIRED BROKEN WIRE AT OVERHEAD PANEL IN COCKPIT PER WDM AND MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND FRAME WEBS AT BS 951, STRINGER 11R AND STRINGER 10L, CRACKED. REMOVED AND REPLACED WEB SECTION PER SRM AND BAC DRAWING.

Part: FITTING — CORRODED (VERTICAL FIN) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL FIN RT LUG AFT FACE AND BORE CORRODED. REPAIRED VERTICAL FIN LUG PER ER.

Part: BEAM — CRACKED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL BEAM WEB AT BS 178, LBL 17.1, WL 182, CRACKED. REMOVED AND REPLACED WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND 2 EA CRACKS AT FLOOR WEB AT BS 188 TO BS 196, STRINGERS 17 L AND 17R. REMOVED AND REPLACED FLOOR WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIES AT BS 927, AND BS 887, BETWEEN STRINGERS 26L AND 27L, CORRODED. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND HORIZONTAL STAB CENTER SECTION LT HINGE FITTING ON BOTH FACES CORRODED. REPAIRED FITTING PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP AT BS 597, STRINGER 8L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND FRAMES AT BS 188, STRINGERS 17R AND 17L, CRACKED. REPAIRED FRAME SECTIONS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 639, STRINGER 15R, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 336, BETWEEN STRINGERS 20L AND 21L, CRACKED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND HORIZONTAL STAB RT AND LT, AFT SPAR CLEVIS FWD AND AFT LUGS CORRODED. REPAIRED HORIZONTAL STAB AFT SPAR CLEVIS PER ER.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB AT BS 639, RBL 68, CRACKED. REMOVED AND REPLACED WEB PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL BEAM WEBS AT BS 709, RBL 25, BS 706, BL 0, CRACKED. REMOVED AND REPLACED WEB SECTIONS PER SRM.

Part: FITTING — CORRODED (RT WING) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D-CHECK, FOUND RT MLG OUTBOARD STABILIZER FITTING CORRODED. REMOVED AND REPLACED RT MLG FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D-CHECK, FOUND FRAMES AT STRINGER 9L, BS 400, BS 787, BS 807, BS 847, BS 887, BS 907, CRACKED. REPAIRED FRAME SECTIONS PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT BS 951, STRINGER 11R, CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND FRAME AT BS 727E, STRINGER 9L, CRACKED. REPAIRED FRAME SECTION PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS AT STRINGER 10R, BS 663, STRINGER 7R, BS 597, STRINGER 5R, BS 616, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS AT STRINGER 11L, BS 706, BS 291.5, STRINGER 8L, BS 616, BS 578, STRINGER 7L, BS 597, CRACKED. REMOVED AND REPLACED STRINGER CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D-CHECK, FOUND FRAMES AT STRINGER 9R, BS 380, BS 480, BS 767, BS 787, BS 887, CRACKED. REPAIRED FRAME SECTIONS PER ER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAMS AT BS 312, BS 344, BS BS 986, LBL 65 TO RBL 42 CORRODED. REPAIRED FLOORBEAM SECTIONS PER SRM AND ER.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND HORIZONTAL STAB CENTER SECTION RT UPPER THRUST FITTING, UPPER AND LOWER ATTACH LUGS CORRODED. REPAIRED HORIZONTAL STAB PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE AT BS 500B, STRINGER 16R CRACKED. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT L2 DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN AT BS 500B, BETWEEN STRINGERS 27R AND 28R, CORRODED. REPAIRED SKIN PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE STRAP AT BS 487 TO BS 490, RBL 22, WL 156, CORRODED. REMOVED AND REPLACED STRAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND FWD CARGO DOOR FRAME WEB CUTOUT AT BS 492, STRINGER 24R, CRACKED. REPAIRED FRAME WEB PER ER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND BS 500 + 16, STRINGER 23R, CORRODED. REPAIRED STRINGER SECTION PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND BULKHEAD WEB AT BS 1016, STRINGER 6R, CRACKED. REPAIRED WEB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIES AT BS 500C, BL 0, STRINGER 28L AND BS 500, BETWEEN STRINGERS 26L AND 27L, CORRODED. REMOVED AND REPLACED SHEAR TIES PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND AFT CARGO COMPARTMENT BS 835, STRINGER 25L, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB AT BS 985, RBL 49, WL 207, CORRODED. REPAIRED CREASE BEAM WEB PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 60,998 hrs · 59,687 cycles

DURING SCHEDULED D CHECK, FOUND CREASE BEAM AT BS 992, RBL 47, WL 208, CORRODED. REPAIRED CREASE BEAM SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,709 hrs · 59,468 cycles

DURING SCHEDULED SC, FOUND SKIN CRACK AT BS 487, STRINGER 17R. REPAIRED SKIN CRACK PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,238 hrs · 59,108 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT DOOR SIDE WALLS EMERGENCY EXIT LIGHTS INOP. RELAMPED EXIT LIGHTS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,336 hrs · 58,396 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 19R. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 59,330 hrs · 58,389 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BS 1016 BULKHEAD WEB CORRODED BETWEEN STR 24L AND STR 24R ON FWD SIDE. REPAIRED BULKHEAD WEB PER SRM AND SWA ACO.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 59,330 hrs · 58,389 cycles

DURING SCHEDULED SERVICE CHECK, FOUND CHANNEL STIFFENERS CRACKED (2 EA) BS 1016 PRESS BULKHEAD AT BL O BELOW WL 200 AND WL 204. REPAIRED BULKHEAD PER BOEING DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,330 hrs · 58,369 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) BS 760 AT STR 19R, BS 932 AT STR 23R AND BS 940 AT STR 24L. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 59,328 hrs · 58,388 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT PRESS BULKHEAD CRACKED AT BS 1016, BETWEEN STR 4L AND STR 7L AT THE Y CHORD. REPAIRED AFT PRESS BULKHEAD PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,211 hrs · 58,284 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED (4 EA) AT BS 344 AT STR 25R, BS 475 AT STR 17R, BS 747 AT STR 20L AND BS 830 AT STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,515 hrs · 57,702 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 798, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,478 hrs · 57,676 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 384, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,478 hrs · 57,676 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT BS 384 AT STR 15R, BS 450 AT STR 17R & BS 460 AT STR 26L. REPAIRED SKIN PER SRM & SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,516 hrs · 56,903 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 530, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,516 hrs · 56,903 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 17L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,516 hrs · 56,903 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 807, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,516 hrs · 56,903 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 271, STR 15L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,637 hrs · 56,179 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 917, STR 25R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (FWD CABIN DOORS) · airframe 56,584 hrs · 56,128 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH FWD CABIN DOOR EMERGENCY EVAC SLIDE GIRT ASSY'S OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 56,384 hrs · 55,956 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND TIE CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED TIE CLIP PER SRM.

Part: BRACKET — CORRODED (FWD ENTRY) · airframe 56,384 hrs · 55,956 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR MOUNT SUPPORT BRACKET CORRODED. REMOVED AND REPLACED BRACKET PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,384 hrs · 55,956 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIE CRACKED AT BS 380, BETWEEN STR 14L AND STR 15L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,384 hrs · 55,956 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND SHEAR TIES CRACKED (3 EA) AT BS 360, BETWEEN STR 13L AND STR 15L. REPAIRED SHEAR TIES PER SRM.

Part: LENS — LOOSE (FUSELAGE) · airframe 56,384 hrs · 55,956 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT EXTERIOR EMERGENCY EXIT LIGHT LENS LOOSE AT BS 727D. SECURED LENS PER MM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,384 hrs · 55,956 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STR SPLICE PER MM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,384 hrs · 55,956 cycles

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

Part: LIGHT — INOPERATIVE (AFT ENTRY DOOR) · airframe 55,900 hrs · 55,569 cycles

DURING SCHEDULED RON, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,387 hrs · 55,163 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED (3 EA) AT BS 450R, BS 385R AND BS 380L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,387 hrs · 55,163 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518, WL 216 R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,763 hrs · 54,631 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR LOWER AND UPPER HINGE CUTOUTS FUSELAGE SKIN CRACKED IN CORNER RADIUS. REPAIRED SKIN PER SRM.

Part: BOLT — WORN (LT INBD T/E FLAP) · airframe 54,719 hrs · 54,595 cycles

DURING WALK AROUND INSPECTION, FOUND LT INBD T/E FLAP EXTENDED 4 INCHES. REMOVED AND REPLACED BOLT FOR T/E INBD AFT FLAP LOAD ROLLERS PER MM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 53,860 hrs · 53,902 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,560 hrs · 53,647 cycles

FUSELAGE SKIN CRACKED AT APPROX BS 787, STR 10R. REPAIRED SKIN PER SWA RA 1-A53-2545.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,486 hrs · 53,582 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BOTH LH & RH COCKPIT UPPER WINDOW POST SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: TAB — DELAMINATED (RH ELEVATOR.) · airframe 53,486 hrs · 53,582 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RH ELEVATOR TAB DELAMINATED NEAR OTBD HINGE ON LOWER SIDE. R&R TAB PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,486 hrs · 53,582 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAMS CORRODED AT BS 770, LBL 3 TO LBL 12, BS 793, RBL 3 TO LBL 8 & BS 857, LBL 17. REPAIRED FLOORBEAMS PER SRM & SWA RA 1-A53-2021.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 53,486 hrs · 53,582 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CLIPS CORRODED (2 EA) AT BS 767, STR 26R & BS 787, STR 26R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STIFFENER — CRACKED (RH W/W) · airframe 53,486 hrs · 53,582 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL STIFFENER CRACKED .25 INCH AT BS 663, RBL 6.0. REPAIRED STIFFENER PER SWA RA 1-357-2673.

Part: STRINGER — CORRODED (FWD CARGO) · airframe 53,486 hrs · 53,582 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CORRODED AT BS 500D, STR 28L. REPAIRED STR PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,486 hrs · 53,582 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 830, STR 20L. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (LH W/W) · airframe 53,486 hrs · 53,582 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESS WEB CRACKED AT BS 663, LBL 32. REPAIRED WEB PER SWA TI-353-046.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 53,486 hrs · 53,582 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CORRODED BETWEEN BS 847 & BS 857, BETWEEN STR 27R & STR 27L.

Part: BUSHING — WORN (RH ELEVATOR) · airframe 53,133 hrs · 53,275 cycles

DURING SCHEDULED BC4 CHECK, RH ELEVATOR TAB FAILED FREE PLAY INSPECTION. R&R # 1 TAB HINGE BUSHING PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 54,693 hrs · 55,377 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,895 hrs · 53,074 cycles

EEPLS LOOSE AT FWD SECTION. SECURED EEPLS, REPAIRED WIRING, REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,825 hrs · 53,006 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 410, STR 10R. REPAIRED SKIN PER SRM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 52,144 hrs · 52,412 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,042 hrs · 52,327 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 3 LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 440, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,034 hrs · 52,317 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 2 LONG EXTERNAL FUSELAGE SKIN CRACK AT BS 540, BETWEEN STR 15L & 16L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,893 hrs · 52,190 cycles

DURING SCHEDULED A1 CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 400, STR 4L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,711 hrs · 52,039 cycles

DURING SCHEDULED A2 CHECK, FOUND 3 EXTERNAL FUSELAGE SKIN CRACK AT BS 483, STR 16R. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 51,375 hrs · 51,749 cycles

EEPLS LOOSE IN FWD SECTION. SECURED EEPLS PER MM.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 51,142 hrs · 51,562 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 2 L/E SLAT AFT OUTBOARD EDGE DELAMINATED. REPAIRED SLAT PER RA 1-357-0946.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,138 hrs · 51,555 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 500B, STR 9R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,138 hrs · 51,555 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 500C, ABOVE STR 15R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,213 hrs · 50,784 cycles

DURING SCHEDULED C1 CHECK, FOUND 4 EXTERNAL FUSELAGE SKIN CRACKS AT STR 10R BETWEEN BS 480 & BS 500. REPAIRED FUSELAGE SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,213 hrs · 50,784 cycles

DURING SCHEDULED C4 CHECK, FOUND 2 INCH LONG FUSELAGE EXTERNAL SKIN CRACK AT BS 500, STR 10R. REPAIRED FUSELAGE SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,213 hrs · 50,784 cycles

DURING SCHEDULED C1 CHECK, FOUND 3 FUSELAGE EXTERNAL SKIN CRACKS AT STR 18R, BETWEEN BS 727D & 727E. REPAIRED FUSELAGE SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,213 hrs · 50,784 cycles

DURING SCHEDULED C1 CHECK, FOUND CRACKS EXTENDING FROM THREE FASTENERS AT BS 1016 BULKHEAD, BL 0, APPROX 6 INCHES ABOVE AND BELOW CENTER. REPAIRED BULKHEAD PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,205 hrs · 50,778 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 807 STR 18L & BS 767 STR 19L. REPAIRED FUSELAGE SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,205 hrs · 50,778 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 520 STR 12R, BS 380 STR 10R & BS 460 STR 10R. REPAIRED FUSELAGE SKIN PER SRM.

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 50,144 hrs · 50,715 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD STIFFENERS CRACKED AT LBL 17, WL 227 AND RBL 17, WL 232. REMOVED AND REPLACED STIFFENERS PER SRM.

Part: FRAME — CRACKED (BULKHEAD) · airframe 50,144 hrs · 50,715 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD LT SIDE CHORD CRACKED AT WL 207 - WL 208. REMOVED AND REPLACED SIDE LT CHORD PER ACO.

Part: STRAP — CRACKED (BULKHEAD) · airframe 50,144 hrs · 50,715 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 VERTICAL STRAP CRACKED BL 0, WL 223. REMOVED AND REPLACED VERTICAL STRAP PER ACO 7154-53.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,144 hrs · 50,715 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD CRACKS AT LBL 1, WL 213 - WL 216 AND RBL 12 TO RBL 14, WL 226. REPAIRED BULKEAD PER ACO 7154-53.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,039 hrs · 50,634 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 947, STRINGER 21L - 22L, BS 440, STRINGER 10R, AND BS 747, STRINGER 18R. REPAIRED CRACKS PER SRM.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 50,039 hrs · 50,634 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,472 hrs · 50,133 cycles

DURING SCHEDULED BC4 CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 414, STRINGER 17L. REPAIRED SKIN PER SRM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 49,472 hrs · 50,133 cycles

DURING SCHEDULED BC4 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUSTMENT. REINSTALLED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,472 hrs · 50,133 cycles

DURING SCHEDULED BC4 CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 500A - 500B, STRINGER 10R. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 48,557 hrs · 49,368 cycles

DURING SCHEDULED C3 CHECK, FOUND RT OVERWING EXIT LIGHT ASY LOOSE. SECURED LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 48,557 hrs · 49,368 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD EEPLS LOOSE. SECURED FWD EEPLS SECTION PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 48,542 hrs · 49,356 cycles

DURING SCHEDULED PM CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE LIGHT INOPERATIVE. R&R BATTERY PACK PER MM.

Part: SKIN — CRACKED (BS 770)

DURING WALKAROUND INSP, FOUND 2 INCHES LONG CRACK AT FUSELAGE EXTERNAL SKIN, BS 770, APPROX STRINGER 18L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (TE FLAP)

DURING SCHEDULED C2 CHECK, FOUND RT WING INBD AND OUTBD AFT FLAPS DELAMINATED. REMOVED AND REPLACED FLAP ASSY'S PER MM.

Part: SKIN — CRACKED (BS 400 - 420)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN HAS A 7.25 INCHES LONG CRACK, BS 400-420, JUST ABOVE SKIN LAP, STRINGER 26L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 500)

EXTERNAL FUSELAGE SKIN CRACKED, BS 500C, STRINGER 11L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 727)

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED, BS 727B, STRINGER 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED ON RT SIDE ABOVE WING SCANNING LIGHT. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT TE AFT FLAP)

DURING WALK ARROUND INSPECTION, FOUND LT WING INBD AFT T/E FLAP DELAMINATED ON OUTBD CORNER. REPAIRED FLAP PER SRM.

Part: LIGHT — INOPERATIVE (ROW 19)

DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EGRESS LIGHT INOP AT ROW 19 DEF. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: WIRE — CUT (SERVICE DOOR)

DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY SLIDE ESCAPE LIGHT AT FWD GALLEY DOOR INOP. FOUND WIRE ASSY TO LAMP CUT. SPLICED WIRE PER MM.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM UPPER CHORD, BS 328, LBL 28. REPAIRED BEAM PER SWA RA NR 1-353-2049.

Part: WEB — CRACKED (BS 663.75)

DURING SCHEDULED 1/2D CHECK, FOUND WEB CRACKED AT BS 663.75, RBL 52, WL 177, RT MAIN LANDING GEAR WHEEL WELL. REPAIRED WEB PER SWA RA NR 1-353-2052.

Part: ANGLE — CRACKED (BS 695)

DURING SCHEDULED 1/2D CHECK, FOUND BS 695, STRINGER 18A LT, ANGLE CRACKED. REPAIRED PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/2D CHECK, FOUND 11 CRACKS AT BS 178 BULKHEAD BETWEEN LBL 17.5-RBL 17.5. REPAIRED BULKHEAD PER SWA RA NR 1-353-2055.

Part: FLOORBEAM — CORRODED (CARGO COMPT)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT 4 FLOORBEAM SECTIONS BS 727E, BS 767, BS 845 AT RBL 8 AND BS 727D, RBL 14. REPAIRED BEAMS PER SRM.

Part: FRAME — CORRODED (BS 907)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FWD LOWER FACE OF BELTFRAME BS 907 RBL 8. REPAIRED PER SRM.

Part: FLOORBEAM — CRACKED (BS 663)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED AT BS 663, BL 0. REPAIRED PER SRM.

Part: FLOORBEAM — CRACKED (BS 947)

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CRACKED AT BS 947, LBL 45. REPAIRED PER SRM.

Part: FRAME — CRACKED (PAX DOORWAY)

DURING SCHEDULED 1/2D CHECK, FOUND UPPER FWD STUB FRAMES CRACKED ON FWD GALLEY AND AFT ENTRY DOOR CUTOUTS. REMOVED AND REPLACED FRAMES PER SRM.

Part: FLOORBEAM — CORRODED (BS 1006)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAM BS 1006, LBL 13-15. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (CARGO COMPT)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT FLOORBEAMS, BS 727E LBL3, BS 767, LBL8, BS 807, LBL18, AND BS 827, LBL 18. REPAIRED BEAMS PER SWA REPAIR AUTH 1-A53-2021.

Part: STRINGER — CRACKED (BS 290)

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 13R CRACKED AT BS 290. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR, AFT DOOR FRAME CRACKED IN TWO LOCATIONS; 3RD AND 4TH FRAME CUT OUTS. REPLACED DOOR ASSY PER MM.

Part: WEB — CRACKED (BS 665)

DURING SCHEDULED 1/2D CHECK, FOUND BEADED WEB CRACKED AT BS 665 RBL 40 AT WHEEL WELL. REPAIRED PER SWA RA NR 1-353-2048.

Part: KEEL BEAM — CORRODED (BS 500)

DURING SCHEDULED 1/2D CHECK, CORROSION AT KEEL BEAM RT SIDE BS 500D TO 515. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 312)

DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON NUT PLATE HOLES AT FLOORBEAM BS 312, LBL 20 - LBL 45. REPAIRED PER SRM.

Part: SKIN — CRACKED (BS 500)

DURING SCHEDULED 1/2D CHECK, FOUND THRU EDDY CURRENT INSPECTION TWO, 2.5 INCH LONG CRACKS AT FUSE SKIN BS 500C TO 500D STRINGER 10R. REPAIRED PER SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED SC CHECK, FOUND A 4 INCH CRACK IN FUSELAGE SKIN 27 INCHES FWD OF OUTFLOW VALVE, BETWEEN STRINGERS 27 AND 26R. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT LIGHT OVER AFT GALLEY AND DOOR INOP. REMOVED AND REPLACED BATTERY PACK PER BOEING M/M.

Part: LAMP — FAILED (SERVICE DOOR)

DURING SCHEDULED BC2 CHECK, FOUND EMERGENCY EXIT LIGHT AT FWD SERVICE DOOR INOP. RELAMPED PER BOEING M/M.

Part: BULB — FAILED (SERVICE DOOR)

DURING SCHEDULED BC2 CHECK, FOUND 2 BURNED OUT BULBS AT EMERGENCY EXIT LIGHT AT FWD SERV DOOR. RELAMPED PER BOEING M/M.

Part: DUMP VALVE — CONTAMINATED (LAVATORY)

AIRCRAFT EN ROUTE FROM MCI TO OKC DIVERTED DUE TO INFLIGHT SHUTDOWN NR 2 ENGINE FLAMEOUT AT CRUISE POWER SETTING AT FL 310, M.755 (ACTUAL STATION COS). AFTER LANDING INSPECTION REVEALED 3-4 ADDITIONAL DENTS IN L/E RT WING JUST OUTBOARD OF TURNOFF/LANDING LIGHT. SUSPECT FWD LAV STILL LEAKING IN FLIGHT. C/W FOD BORESCOPE INSP PER SAM 451. NO OUT OF LIMIT DEFECTS NOTED. C/W TEST NR 5 POWER ASSURANCE CHECK PER BOEING MM. NO FAULTS NOTED. COCKPIT VOICE RECORDER REMOVED FOR MAINT CONVENIENCE. FOUND DUMP VALVE UNABLE TO SEAL DO TO EXCESSIVE PAPER TOWELS IN LAV TANK. REMOVED DUMP VALVE CLEANED AND REINSTALLED. REMOVED AND REPLACED FILL VALVE ASSY PER BOEING MM (P/N 16007-045). REPAIRED DENTS PER SRM.

Part: INTERCOSTAL — BROKEN (FUSELAGE)

DURING SCHEDULED C1 CHECK, FOUND INTERCOSTAL BROKEN AT SUPPORT UPLOCK LATCH. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 372)

DURING SCHEDULED TERMINAL CHECK, FOUND 4 INCH CRACK AT BS 372, 14 ABOVE FLOOR LINE ON LT SIDE OF A/C. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (RT WING)

DURING SCHEDULED SERVICE CHECK, FOUND .25 INCH CRACK AT L/E STATION 213, RT WING. REPAIRED PER SWA RA 1-357-0493.

Part: SKIN — CRACKED (WS 213)

DURING SCHEDULED SERVICE CHECK, FOUND 1/4 CRACK AT L/E STATION 213, LT WING. REPAIRED PER SWA RA 1-357-0493.

Part: SKIN — CRACKED (BS 372)

DURING SCHEDULED TERM CHECK, FOUND 4 INCH CRACK AT BS 372, 14 ABOVE FLOOR LINE ON LT SIDE OF A/C. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 790)

DURING SCHEDULED T-CHECK, FOUND SKIN CRACKS AT BS 790 STR 19 AND 20. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING WALKAROUND CHECK, FOUND I/B EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PER BOEING M/M.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED C4 CHECK, FOUND AFT SERVICE DOOR LOWER HINGE CUTOUT CRACKED 1.25, PROTRUDING FROM LOWER CORNER. REPAIRED PER SWA RA 1-353-1657.

Part: KEEL BEAM — CRACKED (FUSELAGE)

DURING SCHEDULED C-CHECK, FOUND KEEL BEAM PANEL BETWEEN WHEEL WELLS CRACKED APPROX 1 INCH FROM L/E. REPAIRED PER BOEING SRM.

Part: LOCK ACTUATOR — MALFUNCTIONED (NLG)

ON GEAR EXTENSION, NOSE GEAR DID NOT EXTEND. RECYCLED GEAR LEVER AND ALL THREE GEARS EXTENDED NORMALLY. MADE AN UNEVENTFUL LANDING AT OMA. INSPECTED, FERRIED AIRCRAFT TO MDW WHERE MAINT REPLACED NOSE GEAR LOCK ACTUATOR AND PERFORMED GEAR LUBE PER BOEING M/M.

Part: SKIN — SCRAPED (FUSELAGE)

DURING WALKAROUND CHECK, FOUND SCRAPED AREA ON LOWER FUSELAGE SKIN NEAR MAIN OUTFLOW VALVE. REPAIRED PER BOEING SRM.

Part: UPLOCK ACTUATOR — FAILED (NLG)

ON APPROACH, NOSE GEAR DID NOT EXTEND, SLOWED AND RETRIED. NOSE GEAR EXTENDED. AIRCRAFT LANDED NORMALLY IN PHX. REPLACED UPLOCK ACTUATOR, NOSE GEAR SEQUENCING VALVE AND OPS CHECKED PER BOEING M/M.

Part: STRAP — CRACKED (E/E BAY)

DURING SCHEDULED BC1 CHECK, FOUND FLOORBEAM STRAP CRACKED JUST O/B AND ABOVE BATTERY. REPAIRED PER BOEING SRM.