N323SW

Part: STRIP — PEELING (CABIN) · airframe 81,172 hrs · 72,236 cycles

EMERGENCY LIGHTING STRIP F/O SIDE IS PEELING. REMOVED & REPLACED LUMINESCENT STRIP ON ROWS 7 8 9 DEF PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,826 hrs · 71,985 cycles

SKIN CRACKED AT BS 500B, STR 2L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,826 hrs · 71,985 cycles

SKIN CRACKED AT BS 500B+6, STR 2L. REPAIRED SKIN IAW SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 80,724 hrs · 71,916 cycles

EEPLS LOOSE AT ROW 8. SECURED EEPLS PER M/M.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 80,519 hrs · 71,768 cycles

OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER ASSY PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 80,519 hrs · 71,768 cycles

L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER ASSY PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 80,227 hrs · 71,531 cycles

LEFT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER M/M.

Part: SPINDLE — CORRODED (TE FLAP) · airframe 80,234 hrs · 71,538 cycles

LEFT WING O/B MID FLAP NR 1 SPINDLE CORRODED ON BOTTOM SIDE. REMOVED AND REPLACED NR 1 SPINDLE PER MT.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 80,223 hrs · 71,527 cycles

R2 DOOR LOWER EMERGENCY EXIT SIGN BULBS INOP. RELAMPED SIGN PER M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,216 hrs · 71,520 cycles

LEFT EEPLS INOP AT ROW 13. REPAIRED EEPLS IAW AMM AND SWPM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 80,216 hrs · 71,520 cycles

FORWARD EEPLS INOP. REMOVED AND REPLACED BATTERY PACK IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 80,216 hrs · 71,520 cycles

R1 DOOR LOWER EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN IAW WDM & AMM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 80,216 hrs · 71,520 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW MT.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 80,216 hrs · 71,520 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW MT.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 80,216 hrs · 71,520 cycles

RIGHT WING OUTBOARD FORE FLAP LOWER SURFACE PUNCTURED FROM OUTBOARD EDGE. REPAIRED FORE FLAP IAW SRM & AMM.

Part: STRUCTURE — CORRODED (NLG WW) · airframe 80,816 hrs · 71,976 cycles

LEFT NOSE LANDING GEAR TUNNEL LOWER CHORD BS 243 TO BS 251, LBL 26 CORRODED. REPAIRED CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,216 hrs · 71,520 cycles

FRAME WEB CRACKED AT BS 219, BETWEEN LBL 15 TO LBL 19. REPAIRED WEB IAW EA.

Part: PLATE — CORRODED (GIRT BAR) · airframe 80,216 hrs · 71,520 cycles

R1 DOOR FLOORBOARD FWD GIRT BAR FITTING MOUNTING PLATE CORRODED. REMOVED AND REPLACED PLATE IAW SRM.

Part: TEAR STRAP — CRACKED (FUSELAGE) · airframe 80,216 hrs · 71,520 cycles

BULKHEAD OUTER CIRCUMFERENTIAL TEAR STRAP CRACKED AT BS 1016, AT 2:30 O'CLOCK POSITION AT FASTENER HEAD. REPAIRED STRAP IAW EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 80,216 hrs · 71,520 cycles

T-CHORD WEB CORRODED AT BS 219, LBL 17. REPAIRED WEB IAW AAR EA AND EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 80,216 hrs · 71,520 cycles

STRINGER CLIP CORRODED AT BS 787, STR 26R. REMOVED AND REPLACED CLIP IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,216 hrs · 71,520 cycles

SKIN CRACKED BETWEEN BS 694 TO BS 700, STR 10R. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,216 hrs · 71,520 cycles

SKIN CRACKED AT BS 706, STR 10R. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 80,216 hrs · 71,520 cycles

FUSELAGE SKIN CRACKED AT BS 706, STR 10R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,943 hrs · 71,302 cycles

SKIN CRACKED AT BS 360 +15, STR 8L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 79,216 hrs · 70,721 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT OF COVER. RE-INSTALLED SLIDE ON TO COVER PER MT.

Part: FITTING — CRACKED (FUSELAGE) · airframe 79,003 hrs · 70,563 cycles

CLIP CRACKED AT BS 259, STR 15L. REMOVED AND REPLACED CLIP IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,003 hrs · 70,563 cycles

FUSELAGE SKIN CRACKED AT BS 259+12, STR 15L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (BS 259 S15L) · airframe 79,003 hrs · 70,563 cycles

FUSELAGE SKIN CRACKED AT BS 259 +12, STR 15L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 78,846 hrs · 70,445 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD EMERGENCY EXIT LIGHT SIGN BULB INOP. RELAMPED PER MM.

Part: O-RING — LEAKING (HYDRAULIC SYS) · airframe 78,743 hrs · 70,362 cycles

DECLARED EMERGENCY - AT ALT "B" SYS HYDRAULIC QUANTITY RAPIDLY FELL TO 1/3 FULL. SHORTLY AFTER B SYS ENGINE DRIVEN PUMP LOW PRESSURE LIGHT ILLUMINATED. PUMP SHUT DOWN IAW QRH. FOUND "B" SYS PRESSURE LINE TO LANDING GEAR TRANSFER VALVE LEAKED. REMOVED AND REPLACED O-RING, B SYS. RETURN FILTER, CASE DRAIN FILTER FOR EDP & EDMP PER MM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 78,561 hrs · 70,227 cycles

R2 DOOR SLIDE ASSEMBLY LOOSE. RE-INSTALLED SLIDE ASSEMBLY PER MM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 78,190 hrs · 69,951 cycles

DURING SCHEDULED OTS CHECK, FOUND RT MLG WHEEL WELL PRESSURE DECK CRACKED AT BS 668. REPAIRED DECK IAW ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,745 hrs · 68,814 cycles

DURING SCHEDULED 2HC2 CHECK FOUND, FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT. REMOVED AND REPLACED DOOR PER MM.

Part: SKIN — CRACKED (NLG WW) · airframe 67,119 hrs · 58,008 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND NLG WHEEL WELL CEILING SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 663.75, RBL 24.5. REPAIRED BEAM PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 332, BETWEEN STR 5R TO STR 19R. REMOVED AND REPLACED FRAME PER SRM AND BAC DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 661, LBL 25. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 664, LBL 25. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 744A, LBL 25. REPAIRED BEAM PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 807, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME PER SRM AND BAC DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 744A, RBL 25. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 668, LBL 25. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 662, RBL 25. REPAIRED BEAM PER ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND STUB BEAM FRAME CRACKED AT BS 685, LBL 46. REPAIRED FRAME BEAM PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 45.5. REPAIRED BEAM PER ER AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND BULKHEAD CHORD CRACKED AT BS 540, BETWEEN STR 23R TO STR 24R. REPAIRED CHORD PER ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 952, WL 254. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 837, STR 25L. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 952, STR 11L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 616, STR 17L. REPAIRED FRAME PER TI.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 480, BETWEEN STR 27R TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 847, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOOR SUPPORT CHANNEL CORRODED AT BS 758, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND VERTICAL ANGLE CRACKED AT BS 272B, BL 0. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND HORIZONTAL STIFFENER CORRODED AT BS 550, BETWEEN LBL 6 TO RBL 6. REMOVED AND REPLACED STIFFENER PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND BULKHEAD CHORD SPLICE CRACKED AT BS 540, BETWEEN STR 21L TO STR 22L. REMOVED AND REPLACED SPLICE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 21R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 303.9, STR 16L. REPAIRED FRAME PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 24R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 18L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 795, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND LT Z-ANGLE CRACKED AT STA 198.40. REMOVED AND REPLACED Z-ANGLE PER BAC DWG.

Part: HINGE FITTING — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND L2 DOOR UPPER HINGE LOWER FITTING CRACKED. REMOVED AND REPLACED FITTING PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLOOR SUPPORT CHANNEL CORRODED AT BS 772, LBL 8.10. REPAIRED CHANNEL PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 23L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 75,264 hrs · 67,716 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: MEC — FAULTY (NR 1 ENGINE) · airframe 75,211 hrs · 67,673 cycles

INFLIGHT SHUTDOWN/ DECLARED EMERGENCY. UNUSUAL THROTTLE SPLITS & DIFFERING SPOOL UP TIMES. PMC'S OFF AT 32K WHEN THROTTLES PULLED TO IDLE, 2 COMPRESSOR STALLS AND LEFT ENGINE ROLLED BACK. REMOVED AND REPLACED MEC AND CIT SENSOR.

Part: HYDRAULIC LINE — LEAKING (RT MLG) · airframe 74,456 hrs · 67,080 cycles

AIR TURNBACK, "A" SYSTEM QUANTITY DROPPED TO 1/4 RT MLG WOULD NOT LOCK UP. REMOVED AND REPLACED RT MLG ACTUATOR HYDRAULIC HOSE ASSY PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 500D, STR 27R. REPAIRED STRINGER PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND WEB CORRODED AT BS 500D, STR 27R. REPAIRED WEB PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CORRODED AT BS 500B, STR 26L. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500D, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 20R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND FAIL-SAFE CHORD CORRODED AT BS 500D, STR 17R. REPAIRED CHORD PER SRM.

Part: WINDOW FRAME — CORRODED (EMERGENCY EXIT) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND LT OVERWING EMERGENCY EXIT WINDOW FRAME CORRODED. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND LT CREASE BEAM CORRODED AT BS 917, STR 17L. REMOVED AND REPLACED WEB PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 727E, BETWEEN STR 19L TO STR 20L. REMOVED AND REPLACED SHEAR TIE PER BAC DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, BETWEEN STR 19L TO STR 20L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 967, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME WEB CRACKED AT BS 727B, STR 17L. REPAIRED FRAME PER BAC DWG AND SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 793, STR 20L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED BETWEEN BS 967 TO BS 987, STR 25R. REPAIRED STRINGER PER ACO.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 967, STR 27L. REPAIRED STRINGER PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CORRODED AT BS 947, STR 25R. REPAIRED SKIN PER ACO.

Part: SKIN — CORRODED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CORRODED BETWEEN BS 909 TO BS 928, STR 25R. REPAIRED SKIN PER ACO.

Part: SKIN — CORRODED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CORRODED BETWEEN BS 957 TO BS 986, STR 25R. REPAIRED SKIN PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (BS 500B S13R) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500B, STR 13R. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 9L. REMOVED AND REPLACED CLIP PER SI.

Part: FRAME — CRACKED (BS 500B S20-21R) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500B, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 9L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 9L. REMOVED AND REPLACED CLIP PER SI.

Part: FRAME — CRACKED (BS 767 S14R) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 767, STR 14R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (BS 500C S20-21R) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 9L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 9L. REMOVED AND REPLACED CLIP PER SI.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500C, STR 13L. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 9L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 380 S7L) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 380 S2L) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (BS 967 S24-25R) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 967, BETWEEN STR 24R TO STR 25R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 867 S2L) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 685 S10L) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 767 S4L) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 887 S8L) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A S8L) · airframe 73,313 hrs · 66,233 cycles

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

Part: STRINGER CLIP — CRACKED (BS 663 S10L) · airframe 73,313 hrs · 66,233 cycles

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

Part: STRINGER CLIP — CRACKED (BS 706 S10L) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 73,313 hrs · 66,233 cycles

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

Part: SHEAR TIE — CORRODED (BS 986 S24-25R) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 986, BETWEEN STR 24R TO STR 25R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727D S6L) · airframe 73,313 hrs · 66,233 cycles

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

Part: STRINGER CLIP — CRACKED (BS 597 S9R) · airframe 73,313 hrs · 66,233 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727B S5R) · airframe 73,313 hrs · 66,233 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 10R. REMOVED AND REPLACED CLIP PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 867, STR 13L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500B, STR 13L. REPAIRED FRAME PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,313 hrs · 66,233 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 700, STR 10L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,147 hrs · 66,103 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 435, STR 16R. REPAIRED SKIN PER EA.

Part: CHECK VALVE — FAULTY (APU BLEED AIR) · airframe 72,992 hrs · 65,992 cycles

DECLARED EMERGENCY - AT 36,000 FT AIRCRAFT SLOWLY LOST PRESSURIZATION. NO LIGHT ON PRESS PANEL, OUTFLOW VALVE WAS FULLY CLOSED. PRESSURIZATION WAS REGAINED AT APPROX 14,000 FT IN DESCENT. NO POPS OR BANGS WERE NOTED. REMOVED AND REPLACED APU BLEED AIR CHECK VALVE PER MM.

Part: CHECK VALVE — FAULTY (APU BLEED AIR) · airframe 72,992 hrs · 65,992 cycles

DECLARED EMERGENCY, AT 36,000 FT AIRCRAFT SLOWLY LOST PRESSURIZATION. NO LIGHT ON PRESS PANEL, OUTFLOW VALVE WAS FULLY CLOSED. PRESSURIZATION WAS REGAINED AT APPROX 14,000 FT IN DESCENT. NO POPS OR BANGS WERE NOTED. REMOVED AND REPLACED APU BLEED AIR CHECK VALVE PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 72,635 hrs · 65,726 cycles

DURING SCHEDULED SPV CHECK, FOUND LT AFT FLASHLIGHT BATTERY INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 72,635 hrs · 65,726 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,635 hrs · 65,726 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD GALLEY RT LOWER EMERGENCY EXIT LIGHT BULB INOP. REMOVED AND REPLACED BULB PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,635 hrs · 65,726 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 767, STR 19R. REPAIRED FRAME PER EA.

Part: LIGHT — BROKEN (CABIN) · airframe 72,635 hrs · 65,726 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REPAIRED LIGHT ASSY PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 72,635 hrs · 65,726 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING NR 1 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,392 hrs · 64,806 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 750 TO BS 760, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,392 hrs · 64,806 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 435 TO BS 441, BETWEEN STR 16L TO STR 17L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,392 hrs · 64,806 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 747 TO BS 750, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,392 hrs · 64,806 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 730E, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,392 hrs · 64,806 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 750, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,392 hrs · 64,806 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 435 TO BS 500C, BETWEEN STR 16R TO STR 17R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,392 hrs · 64,806 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 450, STR 14R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,392 hrs · 64,806 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 727 TO BS 747, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,392 hrs · 64,806 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED BETWEEN BS 727 TO BS 727B, STR 14L. REPAIRED SKIN PER SWA EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 70,644 hrs · 64,256 cycles

DURING SCHEDULED 22Y CHECK, FOUND LT MLG WHEEL WELL CEILING PRESSURE DECK, FWD BULKHEAD, CRACKED AT BS 665, LBL 40. REPAIRED BULKHEAD PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,411 hrs · 64,096 cycles

DURING SCHEDULED 22Y CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT LAMP INOP. REMOVED AND REPLACED BATTERY PACK PER WDM.

Part: LIGHT — WORN (CABIN) · airframe 70,411 hrs · 64,096 cycles

DURING SCHEDULED HC2 CHECK, FOUND EMERGENCY LIGHT STRIP WORN BETWEEN ROW 8 TO ROW 13. REMOVED AND REPLACED STRIP PER MM.

Part: SKIN — DELAMINATED (NR 2 SLAT) · airframe 70,411 hrs · 64,096 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT LOWER T/E WEDGE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: FITTING — CRACKED (NR 5 SPOILER) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 5 SPOILER FITTING CRACKED AT FWD ATTACH HOLE. REMOVED AND REPLACED FITTING PER SRM.

Part: MOUNT — DAMAGED (GIRT BAR) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR GIRT BAR FLOOR MOUNT DAMAGED. REMOVED AND REPLACED MOUNT PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,400 hrs · 64,091 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,548 hrs · 64,213 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 593, STR 9R. REPAIRED SKIN PER SWA EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,548 hrs · 64,213 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 573, STR 10L. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 5 SLAT UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 323, STR 20L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294, R1 DOOR MIDDLE CUTOUT. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 328, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 70,401 hrs · 64,091 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 335, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (NR 1 SPOILER) · airframe 70,050 hrs · 63,840 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT WING NR 1 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,745 hrs · 63,624 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 847, STR 17L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,745 hrs · 63,624 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,745 hrs · 63,624 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 814, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,873 hrs · 62,998 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 366, STR 26L. REPAIRED SKIN PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 68,873 hrs · 62,998 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 26R CORRODED AT BS 830 TO BS 840. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (R1 DOOR) · airframe 68,873 hrs · 62,998 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR SKIN CRACKED AFT OF WINDOW. REMOVED AND REPLACED DOOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,873 hrs · 62,998 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED BS 503D, STR 16L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,873 hrs · 62,998 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED BS 394, STR 17R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,873 hrs · 62,998 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,873 hrs · 62,998 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 450, BL 0. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,872 hrs · 62,997 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,872 hrs · 62,997 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,872 hrs · 62,997 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR CUTOUT UPPER AFT CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FWD CARGO DOOR) · airframe 68,872 hrs · 62,997 cycles

DURING SCHEDULED HC1 CHECK, FOUND FWD CARGO DOOR OUTER SKIN CRACKED AT DOOR HANDLE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,593 hrs · 62,789 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 16R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,241 hrs · 61,805 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 407 AND BS 414, STR 26L. REPAIRED SKIN PER SWA EA.

Part: WEB — CRACKED (NLG WW) · airframe 67,229 hrs · 61,797 cycles

DURING SCHEDULED HC2 CHECK, FOUND NOSE W/W UPPER RIGHT CEILING PANEL WEB CRACKED. REPAIRED CEILING PANEL PER ACO.

Part: WEB — CRACKED (NLG WW) · airframe 67,229 hrs · 61,797 cycles

DURING SCHEDULED HC2 CHECK, FOUND NOSE W/W UPPER CEILING PANEL WEB CRACKED AT BS 229, RBL 16. REPAIRED CEILING PANEL PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,684 hrs · 61,382 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 289, STR 15L. REPAIRED SKIN PER SWA EA.

Part: LENS — MISSING (CABIN) · airframe 66,656 hrs · 61,356 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,484 hrs · 61,220 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 460, STR 16R. REPAIRED SKIN PER SWA EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 66,373 hrs · 61,128 cycles

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

Part: WIRE — FRAYED (CABIN) · airframe 66,228 hrs · 61,012 cycles

DURING SCHEDULED MV2 CHECK, INTERIOR EMERGENCY EXIT LIGHTS ILLUMINATED INTERMITTENTLY. FOUND FRAYED WIRE AT AFT FLIGHT ATTENDANT SWITCH. REPAIRED WIRE PER MM.

Part: BATTERY — FAULTY (CABIN) · airframe 65,960 hrs · 60,805 cycles

MID CABIN EMERGENCY EXIT LIGHTS STAY ON WITH SWITCH IN ARM POSITION. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,467 hrs · 60,427 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515, STR 16L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,467 hrs · 60,427 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 943, STR 23R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 572 S10L) · airframe 65,176 hrs · 60,200 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 572, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 563 S10L) · airframe 65,176 hrs · 60,200 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 563, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 582 S10L) · airframe 65,176 hrs · 60,200 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 582, STR 10L. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,731 hrs · 59,052 cycles

DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,731 hrs · 59,052 cycles

DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 63,731 hrs · 59,052 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CABIN EMERGENCY EXIT SIGN INOP. REPAIRED BROKEN WIRE PER MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 63,731 hrs · 59,052 cycles

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

Part: CONNECTOR — LOOSE (CABIN) · airframe 63,731 hrs · 59,052 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. SECURED LOOSE CONNECTOR PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,731 hrs · 57,052 cycles

DURING SCHEDULED 20Y CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 13 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 63,731 hrs · 57,052 cycles

DURING SCHEDULED 20Y CHECK, FOUND OVERHEAD FWD CABIN EMERGENCY EXIT SIGN INOP. SECURED LOOSE CONNECTOR PER MM.

Part: FLOORBEAM — CRACKED (BS 663) · airframe 63,731 hrs · 59,052 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CRACKED AT BS 663, BL 0. REMOVED AND REPLACED FLOORBEAM SECTION PER SRM.

Part: FRAME — CRACKED (BS 360 S20R) · airframe 63,731 hrs · 59,052 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 20R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FITTING — CORRODED (R2 DOOR GIRT BAR) · airframe 63,731 hrs · 59,052 cycles

DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED AFT GIRT BAR FITTING PER SRM.

Part: FRAME — CRACKED (BS 294 S17R) · airframe 63,731 hrs · 59,052 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 294, STR 17R. REPAIRED FRAME SECTION PER SRM.

Part: FITTING — CORRODED (R1 DOOR GIRT BAR) · airframe 63,731 hrs · 59,052 cycles

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

Part: FITTING — CORRODED (R1 DOOR GIRT BAR) · airframe 63,731 hrs · 59,052 cycles

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

Part: FITTING — CORRODED (L2 DOOR GIRT BAR) · airframe 63,731 hrs · 59,052 cycles

DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM.

Part: FRAME — CORRODED (BS 747 S26R) · airframe 63,731 hrs · 59,052 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 747, STR 26R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,731 hrs · 59,052 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 20L. REPAIRED FRAME SECTION PER SRM.

Part: AILERON — DELAMINATED (RT WING) · airframe 63,731 hrs · 59,052 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING AILERON DELAMINATED ON INBOARD END. REPAIRED AILERON PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,731 hrs · 59,052 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 20L. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (BS 294 S10L) · airframe 63,731 hrs · 59,052 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 10L. REMOVED AND REPLACED STRINGER CLIP IAW SRM.

Part: FLOORBEAM — CRACKED (BS 328) · airframe 63,731 hrs · 59,052 cycles

DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CRACKED AT BS 328, LBL 12. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CORRODED (BS 747 S26R) · airframe 63,731 hrs · 59,052 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 747, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — DELAMINATED (FORE FLAP) · airframe 63,671 hrs · 59,052 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING OUTBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: FITTING — CORRODED (LT MLG BEAM) · airframe 63,731 hrs · 59,052 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT MLG BEAM INBOARD AFT ATTACH FITTING CORRODED. REMOVED AND REPLACED LT MLG ATTACH FITTING PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 63,731 hrs · 59,052 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP LOWER SURFACE DELAMINATED. REPAIRED FLAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,731 hrs · 59,052 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: BULKHEAD — CRACKED (BS 1016) · airframe 63,692 hrs · 59,020 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED AT BS 1016, STR 6L. REPAIRED BULKHEAD PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,395 hrs · 58,789 cycles

DURING SCHEDULED PM CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT FWD ENTRY DOOR. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: GUSSET — CRACKED (NLG W/W) · airframe 63,329 hrs · 58,744 cycles

DURING SCHEDULED A1 CHECK, FOUND NLG ACTUATOR ATTACH FITTING GUSSETT CRACKED IN RADIUS. REMOVED AND REPLACED GUSSETT FITTING PER SRM.

Part: BOLT — WORN (LT ELEVATOR TAB) · airframe 63,174 hrs · 58,623 cycles

DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB BOLTS PER MM.

Part: FITTING — BROKEN (RT WING SPOILER) · airframe 68,899 hrs · 58,420 cycles

RIGHT WING INBOARD GROUND SPOILER OUTBOARD FITTING BROKEN AT LOWER ATTACH LUG. REPAIRED SPOILER FITTING PER SWA EA.

Part: BOLT — WORN (LT ELEVATOR) · airframe 62,753 hrs · 58,311 cycles

DURING SCHEDULED C4 CHECK, LT ELEVATOR INBOARD TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR INBOARD TAB BOLTS PER MM.

Part: SKIN — CRACKED (BS 507A) · airframe 62,306 hrs · 57,985 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 507A, STR 26R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 769-782) · airframe 61,715 hrs · 57,548 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 769 AND BS 782, STR 18L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 520) · airframe 61,715 hrs · 57,548 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT AIR COND, GROUND SERVICE DOOR CUTOUT, RT FWD CORNER, BS 520, STR 28R. REPAIRED SKIN PER SWA EA.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 61,360 hrs · 57,277 cycles

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,322 hrs · 57,250 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L2 DOOR UPPER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,034 hrs · 57,016 cycles

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

Part: SLIDE — DEPLOYED (L1 DOOR) · airframe 60,983 hrs · 56,979 cycles

L1 DOOR EVACUATION SLIDE INADVERTANTLY DEPLOYED. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,883 hrs · 56,904 cycles

DURING SCHEDULED RON CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: ROD END — WORN (RT ELEVATOR) · airframe 60,724 hrs · 56,760 cycles

DURING SCHEDULED C2 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB ROD ENDS PER MM.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT) · airframe 60,643 hrs · 56,692 cycles

DURING SCHEDULED RON CHECK, RT AFT CABIN EMERGENCY LIGHTS BATTERY PACK WILL NOT HOLD CHARGE. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,624 hrs · 56,677 cycles

DURING SCHEDULED RON CHECK, FOUND RT AFT CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,608 hrs · 56,664 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 727E TO BS 747, STR 18R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 938) · airframe 60,608 hrs · 56,664 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 938, STR 21L. REPAIRED SKIN PER SWA EA & SRM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 60,227 hrs · 56,366 cycles

BULLNOSE LIGHT COVER MISSING AT ROW 6 ABC. INSTALLED COVER PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 59,745 hrs · 55,953 cycles

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

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 59,540 hrs · 55,773 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,540 hrs · 55,773 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 953, STR 21L. REPAIRED SKIN PER SWA EA.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 58,799 hrs · 55,189 cycles

DURING SCHEDULED C4 CHECK, FOUND EXCESSIVE PLAY ON RT ELEVATOR OUTBOARD HINGE FITTING. REPAIRED HINGE FITTING PER SWA EA.

Part: SKIN — CHAFED (FUSELAGE) · airframe 58,497 hrs · 54,972 cycles

DURING SPV, FOUND FUSELAGE SKIN CHAFED AT DORSAL FIN CONTACT AREA, FROM LT AND RT BS 863 TO 883, RT BS 911 TO 929, AND LT BS 964 TO BS 969. REPAIRED SKIN SECTIONS PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,497 hrs · 54,972 cycles

DURING SPV, FOUND STRINGER CLIP AT BS 887, STRINGER 2L, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,497 hrs · 54,972 cycles

DURING SPV, FOUND STRINGER CLIP AT BS 887, STRINGER 1, CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,497 hrs · 54,972 cycles

DURING SPV, FOUND FUSELAGE SKIN AT BS 759, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,497 hrs · 54,972 cycles

DURING SPV, FOUND FUSELAGE SKIN AT BS 911, STRINGER 25L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,497 hrs · 54,972 cycles

DURING SPV, FOUND FUSELAGE SKIN AT BS 751, STRINGER 18L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,952 hrs · 54,577 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 21R. REPAIRED SKIN PER SRM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 57,952 hrs · 54,577 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 57,952 hrs · 54,577 cycles

DURING SCHEDULED C3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,883 hrs · 54,519 cycles

TWO FUSELAGE SKIN CRACKS BETWEEN BS 445 AND BS 485, BETWEEN STRINGERS 18R AND 19R. REPAIRED SKIN SECTIONS PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 57,618 hrs · 54,293 cycles

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

Part: SENSOR — OUT OF TOLERANCE (NLG) · airframe 57,052 hrs · 53,815 cycles

AIR TURNBACK, AFTER TAKEOFF AND GEAR HANDLE UP, RED NOSE GEAR LIGHT REMAINED ILLUMINATED, CYCLED GEAR HANDLE DOWN AND UP. INDICATION NORMAL, APPROX 5 MINUTES LATER IN CLIMB, RED AND GREEN NOSE GEAR LIGHTS ILLUMINATED. REMOVED AND REPLACED SENSOR S845 PER MM.

Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 57,021 hrs · 53,791 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR, AFT DOOR FRAME, CRACKED. REMOVED AND REPLACED FWD ENTRY DOOR PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 57,021 hrs · 13,791 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD RT EMERGENCY EXIT LIGHT MISSING PLASTIC LENS. INSTALLED LIGHT LENS PER MM.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 57,013 hrs · 53,783 cycles

DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT FLOOR PATH PHOTOLUMINESCENT STRIPS AT ROW 9 DEF TO ROW 11 DEF, CRACKED. REMOVED & REPLACED PHOTOLUMINESCENT STRIPS PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 56,966 hrs · 53,739 cycles

AFT EMERGENCY FLASHLIGHT WEAK. REMOVED AND REPLACED BATTERY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,184 hrs · 53,118 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FRAME AT BS 492, RBL 45, CRACKED. REPAIRED FRAME PER ER.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 56,184 hrs · 53,118 cycles

DURING SCHEDULED C1 CHECK, FOUND KEEL BEAM CHORD AT RT BS 727 A, AND LT BS 727, CORRODED. REMOVED AND REPLACED KEEL BEAM CHORD PER SRM AND BAC DRAWING.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 56,184 hrs · 53,118 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO DOOR CUTOUT FRAME WEB AT BS 492, LOWER STOP FITTING, CRACKED. REPAIRED FRAME WEB PER SB AND ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,175 hrs · 53,110 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 500 D, STRINGER 12R, AND STRINGER 12L, CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,175 hrs · 53,109 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT FORWARD ENTRY DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,175 hrs · 53,109 cycles

DURING SCHEDULED C1 CHECK, FOUND SHEAR TIE AT BS 827, LBL 6 TO RBL 6, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,175 hrs · 53,109 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT AT BS 867 TO BS 907 STRINGER 26R, CORRODED. REPAIRED STRINGER PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,175 hrs · 53,109 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME AT BS 992, RBL 45, CORRODED. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,175 hrs · 53,109 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE AT BS 787, RBL 9, CORRODED. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,175 hrs · 53,109 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN AT BS 927, STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,175 hrs · 53,109 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE AT BS 500D, LBL 17, CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (LT WING) · airframe 56,175 hrs · 53,109 cycles

DURING SCHEDULED C1 CHECK, FOUND LT WING, NR 2 L/E SLAT LOWER SKIN AT AFT ROW OF RIVETS, CRACKED. REPAIRED NR 2 L/E SLAT SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,175 hrs · 53,109 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN AT BS 737, STRINGER 20R, BS 927, STRINGER 24R, CRACKED. REPAIRED SKIN PER SRM.

Part: ACTUATOR — BROKEN (LT SPOILER)

TPA - FLT 1817 - ON LANDING FELT VIBRATION COMING FROM LEFT WHEEL WELL AREA. REMOVED AND REPLACED SPOILER ACTUATOR AND SPOILER PANEL PER MM. (M)

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,238 hrs · 51,547 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505, STR 15R. REPAIRED SKIN PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 54,238 hrs · 51,547 cycles

DURING SCHEDULED C3 CHECK, FOUND STRINGER CRACKED AT BS 947, STR 24R. REPAIRED STRINGER PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 54,075 hrs · 51,416 cycles

DURING SCHEDULED RON, FOUND EEPLS LOOSE AT ROW NR 9. SECURED EEPLS PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 53,348 hrs · 50,801 cycles

DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 967, STR 27L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 53,348 hrs · 50,801 cycles

DURING SCHEDULED PM CHECK, FOUND STRINGER TIE CLIP CORRODED AT BS 967, STR 27L. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM.

Part: STRAP — BROKEN (CABIN) · airframe 52,603 hrs · 50,200 cycles

EMERGENCY FLASHLIGHT STRAP BROKEN. R&R STRAP PER MM.

Part: WEB — CRACKED (NLG W/W) · airframe 52,452 hrs · 50,080 cycles

DURING SCHEDULED C1 CHECK, FOUND RT NLG W/W WEB CRACKED AT BS 246, WL 168.5. REPAIRED WEB PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,452 hrs · 50,080 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 797, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,452 hrs · 50,080 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT SECOND RADIO ALTIMETER ANTENNA CUTOUT, AT BS 410, LEFT OF BL 0. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,452 hrs · 50,080 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 797, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,452 hrs · 50,080 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 52,205 hrs · 49,884 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 52,205 hrs · 49,884 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND RT FWD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,205 hrs · 49,884 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 663 FRAME CRACKED AT STR 2R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,205 hrs · 49,884 cycles

DURING SCHEDULED SPV CHECK, FOUND CRACK AT MAIN FRAME BS 360 BETWEEN STR 14R AND STR 15R. REPAIRED FRAME PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 52,205 hrs · 49,884 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 180 FLOOR WEB CRACKED AT RBL 24, WL 207. REPAIRED FLOOR WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,804 hrs · 49,567 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D + 5, STR 15L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,554 hrs · 49,374 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 460, ABOVE STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,542 hrs · 48,536 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,542 hrs · 48,536 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKS (4 EA) 3 INCHES ABOVE STR 10R, AT BS'S 500, 500C PLUS 12, 500C PLUS 16 AND 500 PLUS 15. REPAIRED SKIN PER SWA RA AND ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,542 hrs · 48,536 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 500 PLUS 16, STR 10L. REPAIRED SKIN PER SWA RA AND ER.

Part: RECEPTACLE — LOOSE (CABIN) · airframe 50,445 hrs · 48,466 cycles

DURING LANDING F/A REPORTED SPARKS COMING FROM ELECTRICAL OUTLET IN FWD GALLEY. INSPECTED, CLEANED AND ADJUSTED RECEPTACLE PER MM.

Part: FRAME — CRACKED (AFT CARGO DOOR) · airframe 49,948 hrs · 48,067 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND AFT CARGO DOOR FRAME CRACKED (2 EA) AT FWD INBD LOWER STOP AREA AND FWD INBD PULLEY BRACKET. REMOVED AND REPLACED CARGO DOOR PER SWA ACO AND SWA RA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,947 hrs · 48,066 cycles

DURING SCHEDULED BC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 12R. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (AFT CARGO DOOR) · airframe 49,947 hrs · 48,066 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR FRAME CRACKED (2 EA) AT FWD INBD LOWER STOP AREA AND FWD INBD PULLY BRACKET. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,063 hrs · 47,341 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 16R. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (SERVICE DOOR) · airframe 48,924 hrs · 47,247 cycles

DURING SCHEDULED A2 CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT INOP. SECURED BULB INTO SOCKET PER MM.

Part: SPOILER — DELAMINATED (LH WING) · airframe 48,234 hrs · 46,693 cycles

DURING SCHEDULED 1/2D CHECK AT DALFORT, FOUND LH WING OUTBD SPOILER DELAMINATED. REPAIRED SPOILER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 48,234 hrs · 46,693 cycles

DURING SCHEDULED 1/2D CHECK AT DALFORT, FOUND STRINGER CORRODED AT BS 1006, STR 26R. REPAIRED STR PER SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 48,234 hrs · 46,693 cycles

DURING SCHEDULED 1/2D CHECK AT DALFORT, FOUND FLOOR BEAM CRACKED AT BS 744A, RBL 43.5. REPAIRED FLOOR BEAM PER DLF XEA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,234 hrs · 46,693 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LOWER CHORD BULGED AT 1016 BULKHEAD, BL 0. REMOVED AND REPLACED LOWER CHORD PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,234 hrs · 46,693 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 312, LBL 11.0. REPAIRED FLOORBEAM PER SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 48,234 hrs · 46,693 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE CORRODED AT BS 968, STR 25L. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: WEB — CORRODED (AFT CABIN) · airframe 48,234 hrs · 46,693 cycles

DURING SCHEDULED 1/2D CHECK AT DALFORT, FOUND WEB CORRODED AFT OF BS 1016 FLOOR BEAM, RBL 32 TO RBL 36. REPAIRED WEB PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 48,234 hrs · 46,693 cycles

DURING SCHEDULED 1/2D CHECK AT DALFORT, FOUND STRINGER TIE CLIP CRACKED AT BS 663, STR 10L R&R TIE CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,234 hrs · 46,693 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 334, BL 0.0 TO LBL 12.0. REPAIRED FLOORBEAM PER SRM.

Part: TIE CLIP — CRACKED (MID CABIN) · airframe 42,834 hrs · 46,693 cycles

DURING SCHEDULED 1/2D CHECK AT DALFORT, FOUND TIE CLIP CRACKED AT BS 663, STR 10R. R&R TIE CLIP PER SRM.

Part: FLAP — DEBONDED (LT WING) · airframe 48,121 hrs · 46,596 cycles

DURING SCHEDULED BC4 CHECK, FOUND LT WING OTBD AFT FLAP DISBONDED 4.0 INCH AT LOWER SURFACE INBD END. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,924 hrs · 45,562 cycles

DURING WALK-AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 25R. REPAIRED CRACK PER SRM.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 46,518 hrs · 45,235 cycles

DIVERSION, CABIN FAILED TO PRESSURIZE DURING FLIGHT. PRESS CONTROLLER AUTO MODE ALREADY ON MEL. REMOVED AND REPLACED CABIN PRESS CONTROLLER PER MM, OPS CHECK GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,314 hrs · 45,061 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 500C+2, STR 15L. REPAIRED SKIN PER SRM.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 44,515 hrs · 43,588 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,449 hrs · 43,530 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED, BS 742E, ABOVE STRINGER 19L. REPAIRED SKIN PER SRM.

Part: SLIDE — LOOSE (PAX DOOR) · airframe 43,539 hrs · 42,746 cycles

DURING SCHEDULED C3 CHECK, FOUND ALL FOUR ENTRY AND SERVICE DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUSTMENT. REINSTALLED SLIDE ASSY PER MM.

Part: ESCAPE ROPE — FRAYED (COCKPIT)

COCKPIT'S ESCAPE ROPE NOT BRAIDED AT TIP. REBRAIDED AND SECURED ROPE TIP PER MM.

Part: SKIN — CRACKED (BS 500D)

DURING SCHEDULED C2 CHECK, FOUND 2.5 INCH LONG CRACK AT FUSELAGE EXTERNAL SKIN, BS 500D, STRINGER 10R. REPAIRED SKIN PER SRM.

Part: FLEX BOOT — CRACKED (APU)

AT 37000 FT CABIN ALTITUDE INDICATED 9800 FT, OPERATED STAND BY MODE AND PACKS ON HIGH POSITION TO START CABIN DESCENDING. REMOVED AND REPLACED TORN APU PNEU MANIFOLD FLEX RUBBER BOOT AT KEEL BEAM AREA.

Part: GIRT — OUT OF POSITION (DOORS)

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY AND SERVICE DOOR EVACUATION SLIDE GIRT ASSY'S EXTENDING OUT OF LIMITS. ADJUSTED SLIDE ASSY'S PER MM.

Part: SLIDE — TORN (PAX DOORWAY)

DURING SCHEDULED RON, FOUND AFT ENTRY DOOR EVACUATION SLIDE TORN ON AFT SIDE. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SLIDE — DETACHED (PAX DOORWAY)

DURING SCHEDULED RON, FOUND BOTH FWD ENTRY AND SERVICE DOOR EVACUATION SLIDES COMING OUT OF COVER. INSTALLED SLIDES PER MM.

Part: NUT PLATE — STRIPPED (PAX DOOR)

FWD ENTRY DOOR EVACUATION SLIDE ATTACH FASTENER WILL NOT SECURE ASSY. REMOVED AND REPLACED NUTPLATE AND REINSTALLED FASTENER PER MM.

Part: BULKHEAD CHORD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 T-CHORD CRACKED AT LBL 5.7 , WL 184. REPAIRED CHORD PER SRM.

Part: POST — CRACKED (RT COCKPIT)

DURING SCHEDULED 1/4D CHECK, FOUND APPROX A .25 INCH LONG CRACK ON UPPER END OF RT OUTBD SLIDING WINDOW POST. REPAIRED POST PER SRM.

Part: FLOORBEAM — CORRODED (BS 860)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM, AFT CARGO AREA, BS 860, LBL 17. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 730)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM, AFT CARGO AREA, BS 730, RBL 3 - RBL 8. REPAIRED BEAM PER SWA RA NR 1-A53-2021.

Part: FLOORBEAM — CORRODED (BS 771)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON FLOORBEAM, AFT CARGO AREA, BS 771, LBL 12 - RBL2.5. REPAIRED BEAM PER SWA RA NR 1-A53-2021.

Part: BULKHEAD STRAP — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND CENTER SUPPORT STRAP CRACKED AT BS 178 BULKHEAD, WL 188. REPAIRED STRAP PER SRM.

Part: FLOORBEAM — CORRODED (BS 860)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION AT FLOORBEAM BS 860 LBL 12- RBL 2.5. REPAIRED BEAM PER SWA RA NR 1-A53-2021.

Part: STRAP — CRACKED (LT WING)

DURING SCHEDULED 1/4D CHECK, FOUND LT WING UPPER STRAP FWD OF AILERON CRACKED. REMOVED AND REPLACED STRAP PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND 2 CRACKS AT BS 178 BULKHEAD LBL 5 - RBL 5. REPAIRED BULKHEAD PER SRM.

Part: WEB — CRACKED (BS 665)

DURING SCHEDULED 1/4D CHECK, FOUND CRACK AT PRESSURE WEB, BS 665, LBL 34. REPAIRED WEB PER SWA RA NR 1-353-2072.

Part: MCP — INOP (COCKPIT)

AIR RETURN WHEN MCP WENT INTO THE TEST MODE. REMOVED AND REPLACED THE MCP AND THE SYSTEM CHECK OK.

Part: SKIN — CRACKED (BS 980)

DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED APPROX 3 INCHES LENGTH AT BS 980, STR 21L. REPAIRED SKIN PER BOEING SRM.

Part: INTERCOSTAL — CRACKED (CARGO COMPT)

DURING SCHEDULED C4 CHECK, FOUND CRACKED AFT CARGO DOOR HOLD OPEN LATCH INTERCOSTAL. REPAIRED PER BOEING SRM.

Part: SLIDE — MISSING (SERVICE DOOR)

DURING WALKAROUND CHECK, FOUND FWD SVC DOOR HAS NO EMERGENCY EXIT SLIDE. REMOVED AND REPLACED PER BOEING MM.

Part: SKIN — DAMAGED (BS 178)

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN DAMAGED AT BS 178 BLKHD 2 FT BELOW CAPT WINDOW AND RT FIXED L/E 4 FT FROM FUSELAGE. REPAIRED PER SWA MPM.

Part: BULKHEAD SKIN — DAMAGED (BS 178)

DURING SCHEDULED A1 CHECK, FOUND BS 178 BLKHD AND SKIN DAMAGED. REPAIRED PER BOEING SRM.

Part: SLIDE — LOOSE (FWD SERV DOOR)

DURING WALKAROUND CHECK, FOUND FWD SERVICE DOOR ESCAPE SLIDE WOULD NOT REMAIN SECURED IN CONTAINER. REPLACED PER BOEING M/M.

Part: SKIN — CRACKED (SERV DOORWAY)

DURING SCHEDULED C4 CHECK, FOUND AFT SERVICE DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED PER BOEING SRM.

Part: SKIN — CORRODED (BS 727)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN BULGING UNDER KEEL BEAM 27R AT BS 727+3. REPAIRED PER TRAMCO EWO 96-0722.

Part: FRAME — GOUGED (BS 211.8)

DURING SCHEDULED D-CHECK, FOUND FRAME WEB GOUGED AT BS 211.8. INSTALLED REPAIR DOUBLER PER BOEING SRM.

Part: FRAME — CRACKED (BS 947.5)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 947.5, S11. REPLACED DAMAGED SECTION PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 987)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 987, WL 208, RBL 5, 15, 19, 28, 43, AND LBL 4, 5, 19, 40, AND 43. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 303)

DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACK AT FWD ENTRY DOOR CUTOUT AT BS 303, LBL 60. REPLACED PER BOEING SRM.

Part: SKIN — DAMAGED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND MECHANICAL DAMAGE TO FUSELAGE SKIN AT BS 312 S4L, AT BS 990 TO 1011 BETWEEN S13 AND 16L, AT BS 860 TO 886 BETWEEN S2L AND S2R, AND AT BS 363 TO 374 S4L TO 6L. REPAIRED PER BOEING SRM.

Part: BULKHEAD WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE BULKHEAD WEB CRACKED AT WL 218, RBL 9.5 AND AT WL 202, RBL 5. REPAIRED PER BOEING SRM.

Part: SKIN — CORRODED (BS 1008)

DURING SCHEDULED D-CHECK, FOUND SKIN BULGE AT BS 1008, AT S13L. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 721/386)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 721, AT S2L, AND AT BS 386 ABOVE S17L. REPAIRED PER BOEING SRM.

Part: CLIPS — DAMAGED (FUSELAGE)

DURING SCHEDULED D-CHECK, FOUND MECHANICAL DAMAGE TO STRINGER CLIPS, AT BS 344 S8R AND 11R, AND A CRACKED CLIPS AT BS 360 S10R, AT BS 787 S4R, AT BS 827 S13R AND AT BS 807 S4R. REPLACED PER BOEING SRM.

Part: SKIN — CRACK (SERV DOORWAY)

DURING SCHEDULED D-CHECK, FOUND CRACK IN FUSELAGE SKIN AT BOTTOM LT CORNER OF FORWARD SERVICE DOOR OPENING. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — DAMAGED (BS 344)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM DAMAGE AT BS 344, RBL 1 AND 8, WL 208. REPAIRED PER BOEING SRM.

Part: DOOR FRAME — CRACKED (BS 440)

DURING SCHEDULED D-CHECK, FOUND DOOR FRAME CRACKED AT BS 440, RBL 38, WL 159. REPAIRED PER BOEING SRM.

Part: STRAP — CORRODED (BS 774-858)

DURING SCHEDULED D-CHECK, FOUND AFT CARGO BAY DOOR CUTOUT LOWER BEAM STRAP CORRODED AT BS 774 TO 858, WL 162 TO 157. REPLACED PER BOEING SRM.

Part: WEB — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE WEBS CRACKED AT WL 198, LBL 4.7, AND AT WL 212.5, LBL 4 AND 7. REPAIRED PER BOEING SRM.

Part: WEB — DAMAGED (BS 440)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE WEB GOUGED AND DENTED AT BS 440, RBL 26, WL 156. REPLACED PER BOEING SRM.

Part: SKIN — DENTED (BS 500-515)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 500 PLUS 15, BELOW STRINGER 16L. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 344)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 344, 5 INCHES FROM E AND E COMPT DOOR, BELOW S26L. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 500)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 500B PLUS 6, BELOW S16R. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 211)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 211, 6 INCHES FROM NOSE GEAR DOOR CUTOUT. REPAIRED PER BOEING SRM.

Part: KEEL BEAM — CRACK/CORR (BS 724/721/713)

DURING SCHEDULED D-CHECK, FOUND CRACKING AND CORROSION ON CORRUGATED PLATES, ON TOP OF KEEL BEAM AT BS 724, 721, AND 713, BL 0, WL 155. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 420)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 420 PLUS 1, BELOW STRINGER 20R. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED RON CHECK, FOUND FWD CABIN EMERGENCY TRACK LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M.

Part: SKIN — PUNCTURED (FUSELAGE)

DURING SCHEDULED BC4 CHECK, FOUND PUNCTURE IN FUSELAGE SKIN 10 INCHES AFT EDGE AND 28 INCHES ABOVE CARGO DOOR HANDLE. REPAIRED PER BOEING SRM.

Part: EGT — OVERTEMP (NR 1 ENGINE)

ON CLIMB-OUT, NR 1 ENGINE INDICATED EGT OVERTEMP CONDITION FOR 3 SECONDS. AIRCRAFT RETURNED TO ABQ AND MADE AN UNEVENTFUL LANDING. PERFORMED ENGINE INLET AND EXHAUST INSPECTION PER BOEING M/M. NO DEFECTS NOTED.

Part: SKIN — DAMAGE (BS 807)

BAGGAGE CART STRIKE TO LEFT SIDE FUSELAGE WHILE PARKED AT GATE, BETWEEN BS 807 AND 827, AT S24L. REPAIRED PER BOEING SRM.

Part: TR SLEEVE — CAME LOOSE (NR 1 ENG)

ON DESCENT AT 24,000 FL, NUMBER 1 ENGINE O/B THRUST REVERSER SLEEVE PARTIALLY SEPARATED FROM AIRCRAFT. AIRCRAFT MADE AN UNEVENTFUL LANDING AT AUS. REINSTALLED NEW SLEEVE PER BOEING M/M.

Part: SKIN — CRACKED (BS 947.5)

DURING SCHEDULED SV-CHECK, FOUND FUSE SKIN CRACKED AT BS 947.5, ABOVE S25L AND FWD 4 INCHES. REPAIRED PER BOEING SRM.

Part: COMPRESSOR — STALLED (NR 2 ENGINE)

INITIATED AIR TURNBACK DUE TO NUMBER 2 ENGINE COMPRESSOR STALL. AIRCRAFT LANDED AT LAS WITHOUT INCIDENT. INSPECTED, ENGINE CHANGE UNDERWAY PER BOEING M/M.

Part: STRAP — CRACKED (BS 312)

DURING SCHEDULED BC1 CHECK, FOUND FLOOR BEAM SUPPORT STRAPS CRACKED AT BS 312, AT BL ZERO, RBL 46, AND RBL 28. REPAIRED PER BOEING SRM.