N693SW

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 80,713 hrs · 65,596 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REMOVED AND REPLACED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 80,151 hrs · 65,163 cycles

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

Part: LENS — MISSING (CABIN) · airframe 79,750 hrs · 64,858 cycles

LEFT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 6. INSTALLED LENS PER MM.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 79,586 hrs · 64,730 cycles

DIVERSION/DECLARED EMERGENCY. CLIMBING THROUGH 29,000FT, THE CABIN ALTITUDE HIT 10,000 FEET AND ACTIVATED THE CABIN ALTITUDE HORN. AS WE DESCENDED THE CABIN ALTITUDE DESCENDED, IT WAS PRESSURIZING, BUT NOT HOLDING PRESSURIZATION WELL. FOUND BOTH OUTFLOW VALVES FAULTY. REMOVED AND REPLACED BOTH SUPPLY DUCT VALVES AND THE NR 2 ENGINE 115 VALVE FAULTY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,227 hrs · 64,458 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REPAIRED LIGHT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,225 hrs · 64,457 cycles

SKIN CRACKED AT BS 259.5+13.5, STR 15L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,225 hrs · 64,457 cycles

SKIN CRACKED AT BS 259.5 +13, STR 15L. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 79,168 hrs · 64,415 cycles

FWD OUTBOARD FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER AMM.

Part: SKIN — CRACKED (BS 581 S10L) · airframe 79,124 hrs · 64,384 cycles

SKIN CRACKED AT BS 581, STR 10L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (BS 524) · airframe 79,124 hrs · 64,384 cycles

SKIN CRACKED AT BS 524, STR 1. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,123 hrs · 64,383 cycles

LT OVERHEAD EMERGENCY EXIT LIGHTS INOP AT ROW 6. REPAIRED LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 78,130 hrs · 63,626 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND BULKHEAD LOWER CHORD SPLICE CRACKED AT BS 540, STR 21R. REPAIRED SPLICE IAW EA.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND CHORD CORRODED BETWEEN BS 235 TO BS 243, STR 27R. REPAIRED CHORD PER EA AND DWG.

Part: FAILSAFE — DAMAGED (BS 500 S25L) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND FAILSAFE DAMAGED ON I/B FLANGE AT BS 500, S25L. REPAIRED FLANGE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND SKIN CRACKED AT BS 1016, STR 23L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR AFT CORNER CUTOUT, BS 346, STR 17L. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND LT WNG I/B MID FLAP I/B UPPER SURFACE DELAMINATED. REPAIRED MID FLAP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 14R. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 669, LBL 24.5. REPAIRED BEAM PER EA.

Part: SKIN — DELAMINATED (HORIZ STAB) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND LT HORIZONTAL STABILIZER TOP SURFACE AFT SKIN DELAMINATED AT STA 237. REPAIRED HORIZONTAL STABILIZER PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 302, RBL 52. REPAIRED BEAM PER BAC DWG AND SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND FLOORBEAM CORRODED AT BS 294, LBL 37. REPAIRED FLOORBEAM PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 15R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND STRINGER CORRODED AT BS 947, STR 26R. REPAIRED STRINGER EPR SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND FRAME CRACKED AT BS 348, WL 209. REPAIRED FRAME EPR SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND STRINGER CORRODED AT BS 277, STR 25R. REPAIRED STRINGER EPR SRM.

Part: REPAIR — CORRODED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND FWD CARGO STRINGER REPAIR ANGLE CORRODED AT BS 500D-4, STR 27R. REPAIRED ANGLE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND FLOORBEAM CORRODED AT BS 312, BETWEEN LBL 13 TO RBL 40. REPAIRED BEAM PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 663, STR 7L. REPAIRED SPLICE PER EA.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND INTERNAL DOUBLER CRACKED AT BS 368, BETWEEN STR 28R TO STR 28L. REPAIRED DOUBLER PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND BULKHEAD CHORD SPLICE ANGLE CRACKED AT BS 540, BETWEEN STR 21L TO STR 22L. REPAIRED ANGLE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND STRINGER CORRODED AT BS 499, STR 27R. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, BL 0. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 500D TO BS 540. REPAIRED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND SHEAR TIE CORRODED AT BS 360, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 500B, STR 27R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK FOUND, STRINGER CORRODED AT BS 767, STR 26R. REPAIRED STRINGER PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND FLOORBEAM TEE CAP CORRODED AT BS 986.5, BETWEEN RBL 55 TO LBL 55. REPAIRED BEAM PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND RT KEEL BEAM CORRODED BETWEEN BS 727 TO BS 728. REPAIRED BEAM IAW EA.

Part: LENS — CRACKED (CABIN) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS CRACKED AT ROW 14. REMOVED AND REPLACED LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULE 28Y CHECK, FOUND FRAME WEB CRACKED AT BS 303.9, STR 16L. REPAIRED WEB PER ACO.

Part: LENS — CRACKED (CABIN) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 28Y CHECK, FOUND FRAME CRACKED AT BS 807, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

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

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED 26Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 727E, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED STRINGER CLIP CORRODED AT BS 727D, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED STRINGER CLIP CORRODED AT BS 727D, STR 25L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 77,855 hrs · 63,423 cycles

DURING SCHEDULED STRINGER CLIP CORRODED AT BS 727D, STR 26R. REMOVED AND REPLACED CLIP PER SRM.

Part: WEB — CRACKED (NLG WW) · airframe 77,659 hrs · 63,250 cycles

DURING SCHEDULED SPV CHECK, FOUND NLG WHEEL WELL RT FWD WEB CRACKED BETWEEN BS 235 TO BS 251. REPAIRED WEB IAW EA.

Part: WEB — CRACKED (NLG WW) · airframe 77,659 hrs · 63,250 cycles

DURING SCHEDULED SPV CHECK, FOUND NLG WHEEL WELL LT FWD WEB CRACKED BETWEEN BS 235 TO BS 251. REPAIRED WEB IAW EA.

Part: WEB — CRACKED (NLG WW) · airframe 77,657 hrs · 63,249 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND NLG WHEEL WELL LT FWD WEB CRACKED BETWEEN BS 235 TO BS 251. REPAIRED WEB PER SRM.

Part: WEB — CRACKED (NLG WW) · airframe 77,657 hrs · 63,249 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND NLG WHEEL WELL RT FWD WEB CRACKED BETWEEN BS 235 TO BS 251. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,657 hrs · 63,249 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 685+3, STR 10R. REPAIRED SKIN PER SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 77,261 hrs · 62,928 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING NR 2 SLAT DELAMINATED AT AFT O/B EDGE OF SLAT. REMOVED AND REPLACED NR 2 SLAT ASSY PER MM.

Part: SKIN — PUNCTURED (ELEVATOR) · airframe 77,261 hrs · 62,928 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT ELEVATOR UPPER SURFACE PUNCTURED. REMOVED AND REPLACED ELEVATOR PER MM.

Part: SPAR — CORRODED (HORIZ STAB) · airframe 77,261 hrs · 62,928 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT HORIZONTAL STABILIZER REAR SPAR CORRODED. REMOVED AND REPLACED STABILIZER PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 77,261 hrs · 62,928 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING NR 4 L/E SLAT DELAMINATED. REMOVED AND REPLACED NR 4 SLAT PER MM.

Part: LENS — BROKEN (CABIN) · airframe 76,754 hrs · 62,547 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 76,184 hrs · 62,125 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT ABS 663, BBL 0.07. REPAIRED WEB PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,184 hrs · 62,125 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED BETWEEN BS 348 TO BS 368, STR 15L. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 76,184 hrs · 62,125 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 295, STR 11L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 76,184 hrs · 62,125 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOOR BEAM WEB CRACKED AT ABS 656, BBL 0.07. REPAIRED WEB PER EA.

Part: COVER — LOOSE (CABIN) · airframe 75,782 hrs · 61,826 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND FWD GALLEY CENTER EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 75,782 hrs · 61,826 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND RT AFT EMERGENCY FLASHLIGHT STRAPS BROKEN. REMOVED AND REPLACED STRAPS PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 75,824 hrs · 61,858 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,462 hrs · 61,582 cycles

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

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 75,173 hrs · 61,360 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,134 hrs · 60,528 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 520, STR 28R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,134 hrs · 60,528 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 520, STR 28L. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 74,134 hrs · 60,528 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 74,134 hrs · 60,528 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 73,794 hrs · 60,289 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 73,311 hrs · 59,903 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD LOWER CARGO DOOR INNER SKIN CRACKED. REMOVED AND REPLACED DOOR PER MM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 45,817 hrs · 37,555 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD LOWER CARGO DOOR INNER SKIN CRACKED. REPAIRED SKIN PER EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,122 hrs · 59,763 cycles

FWD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 72,999 hrs · 59,667 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EEPLS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 72,999 hrs · 59,667 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EEPLS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,721 hrs · 59,470 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,721 hrs · 59,470 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,721 hrs · 59,470 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 20L. REPAIRED FRAME PER SRM AND ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,721 hrs · 59,470 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 20R. REPAIRED FRAME PER SRM AND ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,679 hrs · 59,437 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 294+13, STR 20R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,679 hrs · 59,437 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 18R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,679 hrs · 59,437 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 271, STR 16R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,679 hrs · 59,437 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 271, STR 16R. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 72,484 hrs · 59,291 cycles

L1 DOOR LOWER EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 72,420 hrs · 59,241 cycles

DURING SCHEDULED 26Y CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT LOWER STOP FITTING. REPAIRED FRAME PER SRM.

Part: SIGN — LOOSE (CABIN) · airframe 72,420 hrs · 59,241 cycles

DURING SCHEDULED 26Y CHECK, FOUND FWD EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,420 hrs · 59,241 cycles

DURING SCHEDULED 26Y CHECK, FOUND SKIN CRACKED A FWD LOWER CORNER OF R2 COCKPIT WINDOW CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,420 hrs · 59,241 cycles

DURING SCHEDULED 26Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 72,420 hrs · 59,241 cycles

DURING SCHEDULED 26Y CHECK, FOUND R1 DOOR LOWER FRAME CRACKED AT LOWER STOP FITTING. REPAIRED FRAME PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 72,420 hrs · 59,241 cycles

DURING SCHEDULED 26Y CHECK, FOUND R2 DOOR FWD FRAME CRACKED. REPAIRED FRAME PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 72,420 hrs · 59,241 cycles

DURING SCHEDULED 26Y CHECK, FOUND R1 DOOR AFT FRAME CRACKED. REPAIRED FRAME PER SRM.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 72,420 hrs · 59,241 cycles

DURING SCHEDULED 26Y CHECK, FOUND LT WING I/B MIDFLAP WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE ASSY PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 72,420 hrs · 59,241 cycles

DURING SCHEDULED 26Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.

Part: CAP — CRACKED (FUSELAGE) · airframe 72,420 hrs · 59,241 cycles

DURING SCHEDULED 26Y CHECK, FOUND AFT PRESSURE BULKHEAD CENTER DOME CAP CRACKED. REPAIRED DOME CAP PER AAR EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 72,419 hrs · 59,241 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,420 hrs · 59,241 cycles

DURING SCHEDULED 26Y CHECK, FOUND LONGITUDINAL FLOORBEAM CENTER WEB CRACKED BETWEEN BS 708 TO BS 712, LBL 0.07. REMOVED AND REPLACED WEB SECTION PER SI.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,314 hrs · 58,412 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 251.6, STR 24L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,314 hrs · 58,412 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED FWD AND AFT OF LOWER AFT R1 PAX WINDOW, BS 358. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,314 hrs · 58,412 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 707, STR 10R. REPAIRED SKIN PER ER.

Part: LIGHT — BROKEN (CABIN) · airframe 71,314 hrs · 58,412 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 71,314 hrs · 58,412 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: DOOR FRAME — CRACKED (FWD CARGO DOOR) · airframe 71,314 hrs · 58,412 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR LOWER FWD FRAME CRACKED. REMOVED AND REPLACED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,314 hrs · 58,412 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 251.6, STR 24L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,314 hrs · 58,412 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 251.6, STR 24L. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,314 hrs · 58,412 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 707.3, STR 10R. REPAIRED SKIN PER ER.

Part: SLAT — DELAMINATED (LT WING) · airframe 71,314 hrs · 58,412 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING NR 3 SLAT DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,314 hrs · 58,412 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 358, BETWEEN STR 10R TO STR 14R. REPAIRED SKIN PER ER.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 71,310 hrs · 58,411 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: HINGE — BROKEN (SPOILER) · airframe 71,313 hrs · 58,412 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 5 GROUND SPOILER O/B ACTUATOR HINGE BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: RIB — CRACKED (RT WING) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT HORIZONTAL WING FLANGE RIB CRACKED AT WBL 135, BETWEEN STR 2R TO STR 3R. REPAIRED RIB PER ACO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL BEAM WEB CRACKED BETWEEN BS 705 TO BS 711, LBL 24. REPAIRED BEAM PER ER.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CORRODED AT BS 617, BETWEEN LBL 6 TO RBL 6. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 27L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND KEEL BEAM CORRODED AT BS 767, STR 27L. REPAIRED BEAM PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: WIRE — DAMAGED (CABIN) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REPAIRED WIRE PER WDM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 559, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 45. REPAIRED BEAM PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500A, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT, BS 292, WL 259. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 380, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 380, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN STR 27L TO 27R. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL BEAM CRACKED AT BS 727B, RBL 45. REPAIRED BEAM PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 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 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, BETWEEN STR 27L TO 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 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 70,541 hrs · 57,863 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26L TO STR 25L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 927, STR 25L. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 25R TO STR 26R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 27R TO STR 26R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 927, STR 26R. REPAIRED STRINGER PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 887, BETWEEN STR 27L TO 27R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 907, BETWEEN STR 27L TO 26L. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CORRODED AT BS 887, BETWEEN STR 27R TO STR 27L. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 27R TO STR 26R. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BS 292, WL 233. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 305, WL 262. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 305, WL 258. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 305, WL 261. REPAIRED SKIN PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL BEAM CRACKED AT BS 727B, RBL 24. REPAIRED BEAM PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 927, STR 9R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 663, LBL 24. REPAIRED BEAM PER ER.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 380 TO BS 400. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME STUB BEAM CRACKED AT BS 616, RBL 65, WL 207. REMOVED AND REPLACED FRAME PER SRM.

Part: FITTING — CRACKED (RT ELEVATOR TAB) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT ELEVATOR TAB MAST FITTING CRACKED. REMOVED AND REPLACED RT ELEV TAB ASSY PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 21R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CRACKED AT BS 395, STR 22R. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 705,741 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 947, BETWEEN STR 25L TO STR 26L. R&R SHEAR TIE PER SRM.

Part: CABLE — BROKEN (EVAC SLIDE) · airframe 705,741 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EMERGENCY EVACUATION SLIDE SHROUD CABLE BROKEN. REMOVED AND REPLACED CABLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 20L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 807, STR 26L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 887, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 22L. REMOVED AND REPLACED CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 400, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (BS 480 S27-28R) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO BAY FRAME CORRODED AT BS 480, BETWEEN STR 27R TO STR 28R. REPAIRED FRAME PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WHEEL WELL KEELBEAM CORRODED AT BETWEEN BS 673 TO BS 707, RBL 6. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (BS 400 S28L) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 70,541 hrs · 57,863 cycles

DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO BAY FRAME CORRODED AT BS 767, RBL 22. REPAIRED FRAME PER SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 70,367 hrs · 57,748 cycles

FOUND AFT FLASHLIGHT INOP. R&R BATTERY PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 69,713 hrs · 57,267 cycles

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,646 hrs · 57,222 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CHARGER — FAULTY (CABIN) · airframe 69,528 hrs · 57,134 cycles

DURING SCHEDULED MV2 CHECK, LT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: CHARGER — FAULTY (CABIN) · airframe 69,528 hrs · 57,134 cycles

DURING SCHEDULED MV2 CHECK, RT AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 69,273 hrs · 56,964 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 69,136 hrs · 56,864 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 69,136 hrs · 56,864 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: TERMINAL — CRACKED (RT MLG) · airframe 68,872 hrs · 56,688 cycles

ON CLIMBOUT, RIGHT MLG UNSAFE LIGHT AND GEAR DOWN LIGHT ILLUMINATED. CYCLED GEAR, ALL INDICATIONS NORMAL. INSPECTED GEAR, FOUND RIGHT MLG UPLOCK SENSOR TERMINAL CRACKED. REMOVED AND REPLACED TERMINAL END PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,409 hrs · 56,342 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CARRIAGE — WORN (T/E FLAP) · airframe 68,351 hrs · 56,301 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING NR 2 MID FLAP CARRIAGE ASSY BEARING SUPPORT WORN. REMOVED AND REPLACED FLAP CARRIAGE PER MM.

Part: CARRIAGE — WORN (T/E FLAP) · airframe 68,351 hrs · 56,301 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING NR 1 MID FLAP CARRIAGE ASSY BEARING SUPPORT WORN. REMOVED AND REPLACED FLAP CARRIAGE PER MM.

Part: CARRIAGE — WORN (T/E FLAP) · airframe 68,351 hrs · 56,301 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING NR 7 MID FLAP CARRIAGE ASSY BEARING SUPPORT WORN. REMOVED AND REPLACED FLAP CARRIAGE PER MM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 68,175 hrs · 56,171 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT KEEL BEAM CORRODED AT BS 527, RBL 7. REPAIRED KEEL BEAM PER SRM.

Part: LUG — CRACKED (NR 5 SPOILER) · airframe 68,174 hrs · 56,170 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SPOILER INBOARD ATTACH LUG CRACKED. REMOVED AND REPLACED ATTACH LUG PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 68,174 hrs · 56,170 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 67,650 hrs · 55,770 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 67,138 hrs · 55,392 cycles

L1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 67,138 hrs · 55,392 cycles

FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,479 hrs · 54,879 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 969, STR 25R. REPAIRED SKIN PER ER.

Part: STRINGER — CORRODED (BS 350 S25R) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 25R CORRODED AT BS 350. REPAIRED STRINGER PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND NLG W/W CEILING PANEL CRACKED AT LBL 7.75. REPAIRED CEILING PANEL PER ACO.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 20R CORRODED AT BS 500C. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

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

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 23R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 21L CORRODED AT BS 500A. REPAIRED STRINGER PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 25R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 25R CORRODED AT BS 350. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 21L CORRODED AT BS 370. REPAIRED STRINGER PER SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 26R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND NLG W/W CEILING PANEL CRACKED AT RBL 7.75. REPAIRED CEILING PANEL PER ACO.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 23L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 380, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

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

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 22L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 18R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 14L. REPAIRED FRAME PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 23L CORRODED AT BS 370. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,478 hrs · 64,878 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,478 hrs · 64,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 66,478 hrs · 64,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER 23L CORRODED AT BS 370. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,478 hrs · 64,878 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,478 hrs · 64,878 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 66,478 hrs · 64,878 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,478 hrs · 64,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — BROKEN (FUSELAGE) · airframe 66,478 hrs · 64,878 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE BROKEN AT BS 520, STR 16L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,478 hrs · 64,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

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

Part: FRAME — CRACKED (BS 380 S8R) · airframe 66,478 hrs · 54,878 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

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

Part: FRAME — CRACKED (BS 440 S8-8LR) · airframe 66,478 hrs · 54,878 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,478 hrs · 54,878 cycles

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

Part: STRINGER CLIP — CRACKED (BS 360 S9L) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 578 S2L) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500A S4R) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500C S4R) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360 S8L) · airframe 66,478 hrs · 54,878 cycles

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

Part: STRINGER CLIP — CRACKED (BS 500D S7L) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 420 S4R) · airframe 66,478 hrs · 54,878 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 597 S9R) · airframe 66,478 hrs · 54,878 cycles

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

Part: FRAME — CRACKED (BS 520 S8R) · airframe 66,478 hrs · 54,898 cycles

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

Part: FRAME — CRACKED (BS 827 S8R) · airframe 66,478 hrs · 54,898 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,427 hrs · 54,842 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 734D, STR 21R. REPAIRED SKIN PER SWA EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 66,427 hrs · 54,842 cycles

DURING SCHEDULED MV1 CHECK, FOUND STRINGER 21R CORRODED AT BS 727D. REPAIRED STRINGER PER SRM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 66,322 hrs · 54,757 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 4 ABC. REMOVED AND REPLACED STRIP PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,659 hrs · 54,234 cycles

DURING SCHEDULED MV2 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,223 hrs · 53,910 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 907, STR 25L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,223 hrs · 53,910 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 982, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,223 hrs · 53,910 cycles

DURING SCHEDULED MV2 CHECK, FOUND SHEAR TIE CORRODED AT BS 987, STR 23L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,223 hrs · 53,910 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 765, STR 23L. REPAIRED SKIN PER SWA EA.

Part: BRACKET — CORRODED (L1 ENTRY) · airframe 64,720 hrs · 535,521 cycles

DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR FWD GIRT BAR FLOOR BRACKET CORRODED. REMOVED AND REPLACED BRACKET PER SRM.

Part: BRACKET — CORRODED (L1 ENTRY) · airframe 64,720 hrs · 535,521 cycles

DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR AFT GIRT BAR FLOOR BRACKET CORRODED. REMOVED AND REPLACED BRACKET PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,720 hrs · 535,521 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT OVERWING DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,720 hrs · 535,521 cycles

DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 64,720 hrs · 535,521 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER 27L CORRODED AT BS 360. REPAIRED STRINGER SECTION PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,720 hrs · 535,521 cycles

DURING SCHEDULED 22Y CHECK, FOUND RT OVERWING DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 64,720 hrs · 535,521 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER 26L CORRODED AT BS 360. REPAIRED STRINGER SECTION PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,714 hrs · 53,514 cycles

DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FRAME — CRACKED (BS 986 S2L) · airframe 64,714 hrs · 53,514 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 986.5, S2L. REPAIRED FRAME SECTION PER EA.

Part: STRINGER SPLICE — CORRODED (BS 907 S25R) · airframe 64,714 hrs · 53,514 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, STR 25R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,714 hrs · 53,514 cycles

DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FRAME — CRACKED (BS 639 S17-17L-R) · airframe 64,714 hrs · 53,514 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 17R AND STR 17L. REPAIRED FRAME SECTION PER EA.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 64,714 hrs · 53,514 cycles

DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. RESEATED CONNECTOR D2972 PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,714 hrs · 53,514 cycles

DURING SCHEDULED 22Y CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FITTING — LOOSE (L2 DOOR SLIDE) · airframe 64,714 hrs · 53,514 cycles

DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM.

Part: STRINGER — CORRODED (BS 515B S20R) · airframe 64,714 hrs · 53,514 cycles

DURING SCHEDULED 22Y CHECK, FOUND STRINGER 20R CORRODED AT BS 515B. REPAIRED STRINGER PER SRM.

Part: FITTING — LOOSE (L2 DOOR GIRT BAR) · airframe 64,714 hrs · 53,514 cycles

DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM.

Part: FRAME — CRACKED (BS 986) · airframe 64,714 hrs · 53,514 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 986.5, STR 7L. REPAIRED FRAME SECTION PER SRM.

Part: FRAME — CORRODED (BS 847 S26R) · airframe 64,714 hrs · 53,514 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, STR 26R. REPAIRED FRAME SECTION PER SRM.

Part: DOOR FRAME — CORRODED (BS 996 S17R) · airframe 64,714 hrs · 53,514 cycles

DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR CUTOUT AFT FRAME CORRODED AT BS 993, STR 17R. REPAIRED FRAME SECTION PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 64,714 hrs · 53,514 cycles

DURING SCHEDULED 22Y CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME SECTION PER SRM.

Part: SKIN — CORRODED (BS 845-847) · airframe 64,714 hrs · 53,514 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 845 TO BS 847, STR 26R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,714 hrs · 53,514 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, BL 0. REPAIRED SKIN PER SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,714 hrs · 53,514 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, BL 0. REPAIRED SKIN PER SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,714 hrs · 53,514 cycles

DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 450, BL 0. REPAIRED SKIN PER SB.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 64,714 hrs · 53,514 cycles

DURING SCHEDULED 22Y CHECK, RIGHT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED INBOARD HINGE TAB BUSHING PER MM.

Part: BOLT — WORN (ELEVATOR TAB) · airframe 64,714 hrs · 53,514 cycles

DURING SCHEDULED 22Y CHECK, LEFT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED INBOARD HINGE TAB BOLT PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 64,678 hrs · 53,480 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD LOWER L/E. REMOVED AND REPLACED AFT FLAP PER MM.

Part: WIRE HARNESS — BURNED (COCKPIT) · airframe 64,565 hrs · 53,397 cycles

RIGHT ELEVATOR PITOT LIGHT ILLUMINATED ON CLIMBOUT, WITH ASSOCIATED C/B TRIPPED ON P-18-3 PANEL. FOUND WIRE BUNDLE W018 BEHIND P18-1 PANEL WITH NUMEROUS WIRES BURNT. REPAIRED WIRES PER WDM.

Part: SKIN — CRACKED (BS 750 S18R) · airframe 63,694 hrs · 52,692 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18R. REPAIRED SKIN PER SWA EA.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 63,694 hrs · 52,692 cycles

DURING SCHEDULED C3 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 5 DEF. SECURED LIGHT LENS PER MM.

Part: SKIN — CRACKED (BS 785 S19L) · airframe 63,694 hrs · 52,692 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 785, STR 19L. REPAIRED SKIN PER SWA EA.

Part: GLOWSTRIP — WORN (CABIN) · airframe 63,694 hrs · 52,692 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 8 ABC. REMOVED AND REPLACED EEPLS PHOTOLUMINESCENT STRIP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,286 hrs · 52,354 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD ENTRY DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 62,716 hrs · 51,905 cycles

L1 DOOR EMERGENCY EXIT LIGHT BROKEN. R&R SIGN ASSY PER WDM.

Part: BULB — INOPERATIVE (FUSELAGE) · airframe 58,781 hrs · 48,787 cycles

DURING SCHEDULED C1 CHECK, FOUND LT WING EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT IAW MM.

Part: LIGHT — LOOSE (ROW 8 ABC) · airframe 61,681 hrs · 51,083 cycles

EEPLS TRACK LOOSE AT ROW 8 ABC. SECURED EEPLS PER MM.

Part: ACTUATOR — FAULTY (RT MLG W/W) · airframe 61,212 hrs · 50,727 cycles

RT MLG EXTENDED WITH GEAR HANDLE IN "OFF" POSITION. RECYCLED GEAR HANDLE-GEAR RETRACTED. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR PER MM.

Part: FLASHLIGHT — ACTIVATED (AFT GALLEY) · airframe 61,062 hrs · 50,603 cycles

AFT GALLEY INBD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: CONTROL CABLE — BROKEN (LT WING TE FLAP) · airframe 60,991 hrs · 50,550 cycles

LT WING INBD T/E FLAP BOOM CABLE BROKEN. REMOVED AND REPLACED BOOM CABLES BC-3 AND BC-4 PER MM.

Part: SKIN — CRACKED (BS 806) · airframe 60,961 hrs · 50,529 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 806, STR 20L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 767) · airframe 60,961 hrs · 50,529 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 22L. REPAIRED SKIN PER SRM.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,942 hrs · 50,514 cycles

DURING SCHEDULED RON CHECK, FOUND FWD CABIN SIDEWALL EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: WHEEL — SEPARATED (MLG) · airframe 60,503 hrs · 50,151 cycles

NR 1 MAIN TIRE RETREAD SEPARATED. FOUND LT INBD T/E FOREFLAP AND GROUND SPOILER DAMAGED. REMOVED AND REPLACED NR 1 MAIN TIRE/WHEEL ASSY, LT INBD T/E FOREFLAP AND GROUND SPOILER PER MM.

Part: SLIDE — DISCHARGED (R2 DOOR) · airframe 60,374 hrs · 50,042 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,056 hrs · 49,819 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E + 14, STR 18L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,015 hrs · 49,784 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 2 STOP FITTING CUTOUT. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,075 hrs · 49,018 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CRACKED STUB FRAME AT BS 360, BETWEEN STR 14L & STR 15L. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 59,075 hrs · 49,018 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON LT FUSELAGE KEELBEAM AT BS 540. REPAIRED KEEL BEAM PER SRM & ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,075 hrs · 49,018 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CRACKED STRINGER CLIP AT BS 787, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,075 hrs · 49,018 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE BELT FRAME CRACKED AT BS 360, STR 14R. REPAIRED BELT FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500A) · airframe 59,075 hrs · 49,018 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIP CRACKED AT STR 9L, BS 500A. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 400) · airframe 59,075 hrs · 49,018 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CRACKED STRINGER CLIP AT STR 9L, BS 400. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 59,075 hrs · 49,018 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME TO SKIN ATTACH ANGLE CRACKED AT BS 400, STR 14L. REPAIRED FUSELAGE ATTACH ANGLE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,075 hrs · 49,018 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CRACKED STRINGER CLIP AT BS 807, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,075 hrs · 49,018 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND CRACKED STRINGER CLIP AT BS 807, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FITTING — CRACKED (GIRT BAR) · airframe 59,075 hrs · 49,018 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND R1 DOOR ESCAPE SLIDE GIRT BAR, AFT FLOOR FITTING CRACKED. REMOVED AND REPLACED R1 DOOR ESCAPE SLIDE FLOOR FITTING PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,073 hrs · 49,017 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 747, STRINGER 21R, CRACKED. REPAIRED SKIN PER SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,041 hrs · 48,989 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,625 hrs · 48,662 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 518, STRINGER 12R, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,625 hrs · 48,662 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 294.5 + 16, STRINGER 18R, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,578 hrs · 48,624 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 885, ABOVE STRINGER 24R, CRACKED. REPAIRED SKIN PER EA.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,803 hrs · 48,002 cycles

DURING SCHEDULED A1 CHECK, FOUND RT FWD SIDEWALL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,689 hrs · 47,913 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 20L, CRACKED. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,680 hrs · 47,904 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 20L, CRACKED. REPAIRED SKIN PER EA.

Part: LAMP — INOPERATIVE (R2 DOOR) · airframe 57,311 hrs · 47,603 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,311 hrs · 47,603 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L1 & L2 & OVERWING EXIT LOWER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,294 hrs · 47,587 cycles

DURING SCHEDULED SERVICE CHECK, FOUND STRINGER 26R, BS 500A, CORRODED. REPAIRED STRINGER PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 56,714 hrs · 47,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND KEELBEAM CHORD AT BS 500D + 2, RBL 6, CORRODED. REPAIRED KEELBEAM CHORD PER EA.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 56,714 hrs · 47,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE DOUBLER AT BS 727D, BL 0, CORRODED. REMOVED AND REPLACED DOUBLER PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 56,714 hrs · 47,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER TIE CLIP AT BS 787, STRINGER 26R, CORRODED. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,714 hrs · 47,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 660, BL 0, CRACKED. REPAIRED FLOORBEAM PER EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 56,714 hrs · 47,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT MLG BEADED PRESSURE WEB AT BS 664, LBL 39.5, CRACKED. REPAIRED PRESSURE WEB PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,714 hrs · 47,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT FRAME CUTOUT AT UPPER STOP CRACKED. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,714 hrs · 47,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 727C + 7, LBL 8, CORRODED. REPAIRED FLOORBEAM PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,714 hrs · 47,125 cycles

DURING SCHEDULED 1/4D CHECK, BELT FRAME AT BS 827, RBL 9, CORRODED. REPAIRED BELT FRAME PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 56,714 hrs · 47,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED INBOARD AFT FLAP PER MM.

Part: SKIN — DELAMINATED (RT FORE FLAP) · airframe 56,714 hrs · 47,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED. REPAIRED RT WING INBOARD FORE FLAP PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 56,714 hrs · 47,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO KEELBEAM WEB AT BS 807 TO BS 827, RBL 7, CORRODED. REMOVED AND REPLACED KEEL BEAM WEB PER SRM.

Part: WEDGE — CRACKED (RT WING FLAP) · airframe 56,714 hrs · 47,125 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD MID FLAP WEDGE, CRACKED. REPAIRED RT WING MID FLAP WEDGE PER SRM.

Part: LENS — BROKEN (EMERGNECY LIGHT) · airframe 55,851 hrs · 46,425 cycles

FORWARD F/A STATION EMERGENCY LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,293 hrs · 45,269 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, ABOVE STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,065 hrs · 45,092 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (3 EA) BELOW STR 4L, BS 661, BS 648 AND BS 667. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,065 hrs · 45,092 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED (2 EA) AT BS 178, WL 234, LBL 7.7 AND WL 195, RBL 0.5. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,571 hrs · 44,675 cycles

DURING SCHEDULED A2 CHECK, FOUND 2 LONG FUSELAGE SKIN CRACK, BS 349, STRINGER 18R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 53,422 hrs · 44,563 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 6 L/E SLAT CRACKED AT LOWER T/E AFT ROW OF FASTENERS. REPAIRED NR 6 L/E SLAT PER SWA EA.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 53,422 hrs · 44,563 cycles

DURING SCHEDULED C4 CHECK, FOUND LEFT INBOARD T/E FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED LEFT INBOARD T/E FORE FLAP PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 53,422 hrs · 44,563 cycles

DURING SCHEDULED C4 CHECK, FOUND RIGHT OUTBOARD AFT T/E FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED RIGHT OUTBOARD AFT T/E FLAP PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 52,242 hrs · 43,641 cycles

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

Part: FITTING — CORRODED (RT MLG) · airframe 51,840 hrs · 43,338 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT MLG FWD WALKING BEAM HANGER ATTACH LUG CORRODED. REMOVED AND REPLACED HANGER FITTING PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,604 hrs · 43,155 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELSGE SKIN CRACKED 2.5 IN LONG, BS 747+7, STR 19R. REPAIRED SKIN PER SWA SAM FORM 326.

Part: WEB — GOUGED (FUSELAGE) · airframe 51,604 hrs · 43,155 cycles

DURING SCHEDULED C2 CHECK, FOUND KEEL BEAM WEB GOUGED ADJACENT TO LT A/C PACK VALVE. REPAIRED WEB PER SWA EA.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 51,585 hrs · 43,141 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 51,287 hrs · 42,889 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,164 hrs · 42,787 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 25L. REPAIRED SKIN PER SRM.

Part: MOTOR — FAILED (T/E FLAP) · airframe 50,889 hrs · 42,564 cycles

AIR TURNBACK, AFTER TAKEOFF T/E FLAPS WOULD NOT RETRACT HYDRAULICALLY. REMOVED AND REPLACED T/E FLAP HYDRAULIC MOTOR PER MM.

Part: RELAY — FAILED (E/E BAY) · airframe 50,854 hrs · 42,535 cycles

NOSE GEAR RED UNSAFE LIGHT DID NOT EXTINGUISH AFTER TAKEOFF. REMOVED AND REPLACED NOSE GEAR LATCHING RELAY R 374 PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,740 hrs · 42,438 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737, BETWEEN STR 20L AND 21L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 50,733 hrs · 42,430 cycles

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

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 50,405 hrs · 42,173 cycles

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

Part: SLIDE — LOOSE (SVC DOOR) · airframe 50,347 hrs · 42,123 cycles

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

Part: BUSHING — WORN (LT ELEVATOR) · airframe 49,893 hrs · 41,748 cycles

DURING SCHEDULED C4 CHECK, FOUND LT ELEVATOR TAB HAS EXCESSIVE AXIAL PLAY. REMOVED AND REPLACED TAB HINGE BUSHING PER MM.

Part: VALVE — DAMAGED (MLG W/W) · airframe 49,758 hrs · 41,647 cycles

AIR TURNBACK, AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. FOUND INNER STRUT SUPPORT VALVE DAMAGED, WOULD NOT LET STRUT FULLY EXTEND AND ACTUATE AIR SENSOR. REPACKED INNER STRUT AND REMOVED AND REPLACED SUPPORT VALVE PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 49,725 hrs · 41,619 cycles

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

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 49,589 hrs · 41,515 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,031 hrs · 41,055 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSE SKIN CRACKED (3 EA) AT BS 727E, STR 21R, BS 735, STR 18R AND BS 870, STR 24R. REPAIRED SKIN PER SRM.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 48,582 hrs · 40,693 cycles

DURING SCHEDULED D CHECK, FOUND VERTICAL FIN FRONT SPAR CRACKED AT SLING ATTACH POINT FASTENER HOLE. REPAIRED SPAR PER ER 01-5587.

Part: BEAM — CORRODED (LOWER FUSELAGE) · airframe 48,579 hrs · 40,691 cycles

DURING SCHEDULED D CHECK, FOUND KEEL BEAM CORRODED, BS 500D PLUS 6, LT SIDE, OUTBD FLANGE. REPAIRED KEEL BEAM PER SRM.

Part: SPAR — CORRODED (LT HORZ STAB) · airframe 48,579 hrs · 40,691 cycles

DURING SCHEDULED D CHECK, FOUND RT HORIZONTAL STAB UPPER REAR SPAR CHORD CORRODED BETWEEN STA 279 AND STA 305. REPAIRED SPAR PERSRM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 48,579 hrs · 40,691 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 767, LBL 3 TO LBL 5, WL 146 AND WL 147. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 48,579 hrs · 40,691 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CORRODED AT BS 767, RBL 7 TO RBL 10, WL 146. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (AFT CARGO COMPT) · airframe 48,579 hrs · 40,691 cycles

DURING SCHEDULED D CHECK, FOUND 2 EA AFT CARGO COMPT SHEAR TIES CORRODED, BS 747, RBL 1-7, AND BS 767, LBL 7-10. REPAIRED SHEAR TIES PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 48,579 hrs · 40,691 cycles

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

Part: SPLICE — CRACKED (FUSELAGE) · airframe 48,579 hrs · 40,691 cycles

DURING SCHEDULED D-CHECK, FOUND STR SPLICE'S CRACKED (2 EA) AT BS 908, STR 4L & 4R. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: STIFFENER — CRACKED (FWD CABIN) · airframe 48,579 hrs · 40,691 cycles

DURING SCHEDULED D CHECK, FOUND CRACKED STIFFENER AT BS 328, RBL 32 & WL 201. REPAIRED STIFFENER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,579 hrs · 40,691 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR UPPER HINGE UPPER CORNER OF CUTOUT. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,579 hrs · 40,691 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 328, WL 208 & RBL 20 TO RBL 49. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,579 hrs · 40,691 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (3 EA) AT BS 727A, STR 3R, BS 600, STR 8R & BS 560, STR 10R. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,533 hrs · 40,650 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED ( 2 EA ) AT BS 727, STR 20L, 3 INCHES LONG & BS 767, STR 19R, 2 INCHES LONG. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 48,088 hrs · 40,286 cycles

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

Part: BATTERY — ERRATIC (CABIN) · airframe 47,991 hrs · 40,201 cycles

EEPLS ILLUMINATING ERRATICALLY AFT OF ROW # 10. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,508 hrs · 39,793 cycles

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

Part: SCREW — LOOSE (PITOT TUBE) · airframe 47,358 hrs · 39,665 cycles

AIR TURNBACK. DURING CLIMB F/A HEARD LOUD POP and HIGH SQUEAL STARTED IN COCKPIT. FOUND CAPT AUX PITOT TUBE SCREWS LOOSE, TIGHTEN SCREWS PER MM.

Part: TRACK — LOOSE (CABIN) · airframe 47,182 hrs · 39,498 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK LIGHTING LOOSE AT ROW 24. SECURED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,074 hrs · 39,409 cycles

DURING SPECIAL VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 727E+17, STR 21L. REPAIRED SKIN PER SWA RA.

Part: FITTING — WORN (LT WING) · airframe 46,724 hrs · 39,118 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT MLG WALKING BEAM FWD ATTACH FITTING ON REAR SPAR WORN AT WBL 135.505. REMOVED AND REPLACED BEAM FITTING PER MM.

Part: SLIDE — LOOSE (SERVICE DOOR) · airframe 46,535 hrs · 38,957 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 46,405 hrs · 38,847 cycles

LEFT AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,216 hrs · 38,692 cycles

DURING SCHEDULED C4 CHECK, FOUND 2 EXTERNAL FUSELAGE SKIN CRACK AT BS 727D, BETWEEN STR 19R & STR 20R. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 46,216 hrs · 38,692 cycles

DURING SCHEDULED C4 CHECK, FOUND MID CABIN OVERHEAD EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT ASSY PER MM.

Part: CAP — MISSING (CABIN) · airframe 45,272 hrs · 37,925 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS AFT END CAP MISSING. INSTALLED END CAP PER MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 45,069 hrs · 3,774 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE LWR GIRT BAR BRACKET LOOSE. RE-SECURED BRACKET PER MM.

Part: SUPPORT BRACKET — BROKEN (PAX DOOR GIRT) · airframe 44,969 hrs · 37,644 cycles

FWD ENTRY DOOR EVACUATION SLIDE GIRT BAR SUPPORT BROKEN. REPAIRED GIRT BAR SUPPORT PER MM.

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE) · airframe 44,761 hrs · 37,488 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE PRESSURE INDICATOR LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,720 hrs · 36,584 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 760, STRINGERS 19R AND 25R AND BS 757, STRINGER 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 272D)

DURING WALKAROUND INSPECTION FOUND, FUSELAGE EXTERNAL SKIN CRACKS, BS 727D, STRINGER 23R, BS 887, STRINGER 25R, BS 775, STRINGER 20L, AND BS 737, STRINGER 22L. REPAIRED SKIN PER SRM.

Part: SKIN — DELAMINATED (LT ELEVATOR TAB)

DURING SCHEDULED 1/4D CHECK, FOUND LEFT ELEVATOR TAB DELAMINATED. REMOVED AND REPLACED ELEVATOR TAB PER MM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 8 -RBL 10. REPAIRED BULKHEAD PER SWA RA NR 1-353-2152.

Part: STRINGER — CORRODED (BS 500)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON STRINGER 26R, BS 500D. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (BS 872,500&804)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON STRINGER 25L, BS 827,BS 500B, BS 804. REPAIRED STRINGER PER SRM.

Part: FLOORBEAM — CORRODED (BS 727)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON BS 727D FLOORBEAM UPPER FLANGE, LBL 17- RBL 3. REPAIRED BEAM PER SWA RA NR 1-A53-2021.

Part: STRINGER — CORRODED (BS 500)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION ON STRINGER 22R, BS 500C. REPAIRED STRINGER PER SRM.

Part: SKIN — CORRODED (BS 907-1106)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION AT BELLY SKIN, BS 907 TO 1106, STRINGERS 25L-25R. REMOVED AND REPLACED BELLY SKIN SECTION PER SRM.

Part: WEB — CRACKED (BS 663)

DURING SCHEDULED 1/4D CHECK, FOUND BS 663 PRESSURE WEB CRACKED, LBL 32. REPAIRED PER SWA RA NR 1-353-2150.

Part: WEB — CRACKED (BS 663)

DURING SCHEDULED 1/4D CHECK, FOUND BS 663 BEADED PRESS WEB CRACKED, LBL 30. REPAIRED WEB PER SWA RA NR 1-353-2150.

Part: STOPS — CRACKED (EMER EXIT DOOR)

DURING SCHEDULED 1/4D CHECK, FOUND RT EMERGENCY OVERWING EXIT DOOR LOWER STOPS CRACKED. REMOVED AND REPLACED STOPS PER MM.

Part: LIGHT — LOOSE (CABIN)

EMERGENCY EXIT ROW LIGHT (RT SIDE) IN OVERHEAD LUGGAGE BIN LOOSE. RESECURED LIGHT PER MM.

Part: SKIN — DAMAGED (BS 395-420)

DURING SCHEDULED D-CHECK, FOUND DAMAGED FWD CARGO DOORWAY HAS BIG HOLE IN FUSELAGE BETWEEN STR 25R AND 26R AT BS 395 TO 420. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED, AFT OF RT WING/BODY FAIRING. REPAIRED PER BOEING SRM.

Part: CSD — REQD SERVICE (NR 2 ENGINE)

IN FLIGHT, NR 2 ENGINE HAD A PERIOD OF UNRESPONSE WHEN NR 2 ENGINE GENERATOR TRIPPED OFF LINE. REMAINED OFF LINE UNTIL PASSING THROUGHT 10,000 FT, ENGINE RETURNED BACK TO SPEED. AIRCRAFT MADE AN UNEVENTFUL LANDING. INSPECTED AND SERVICED NR 2 CSD, GROUND OP CHECKED ENGINE. THROTTLE RESPONSE, BUSS TRANSFER AND ENGINE PARAMETERS, ALL NORMAL PER BOEING M/M.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED D-CHECK, FOUND AFT ENTRY DOORWAY OUTER SKIN CRACKED AT LOWER FWD CORNER. REPAIRED PER BOEING SRM.

Part: FRAME — CORRODED (BS 500)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500D, BETWEEN S26L AND 24L. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 616)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE INNER FRAME CHORD CRACKED AT BS 616, LBL 64. REPAIRED PER BOEING SRM.

Part: SHEAR TIE — CRACKED (BS 358)

DURING SCHEDULED D-CHECK, FOUND STRINGER SHEAR TIE CRACKED AT BS 358, AT S14L. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 1006)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1006, AT S12R. REPAIRED PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT RBL 4.7, WL 199 TO 197.75. REPAIRED PER TRAMCO EWO 97-0198.

Part: CLIP — DAMAGED (BS 460)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP DAMAGE AT BS 460, S28L. REPLACED PER BOEING SRM.

Part: FITTING — CRACKED (HORIZ STAB)

DURING SCHEDULED D-CHECK, FOUND A 2 INCH CRACK IN RADIUS OF SUPPORT FITTING MEMBER AT HORZ STAB CENTER SECTION UPPER SUPPORT, O/B SIDE OF BEAM, 25 AFT OF FWD SPAR, 20 I/B OF RT SIDE INTERNAL FUSE SKIN. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 500/727)

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 727E, AT S23R, AT 500C, LBL 24.74. REPAIRED PER BOEING SRM.

Part: FLOOR BEAM — CRACKED (BS 520)

DURING SCHEDULED C2 CHECK, FOUND FLOOR BEAM CRACKED AT BS 520, RBL 26. REPAIRED PER BOEING SRM.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING SCHEDULED C4 CHECK, FOUND CENTER AISLE AND LT EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK AND CONNECTOR PINS PER BOEING M/M.

Part: ENGINE — BIRD STRIKE (NR 2)

AFTER TAKEOFF, EXPERIENCED BIRD STRIKE TO NUMBER 2 ENGINE. AIRCRAFT RETURNED TO SMF AND MADE AN UNEVENTFUL LANDING. REPLACED NUMBER 2 ENGINE PER PER BOEING M/M.

Part: SKIN — DENTED (BS 328)

DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT BS 328, S21R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: DOOR — CRACKED (BS 298)

DURING SCHEDULED TRANSITION CHECK, FOUND CRACK ON FWD UPPER CORNER OF FWD GALLEY DOOR AT FASTENER HOLE. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FLOOR — CRACKED (BS 294)

DURING SCHEDULED TRANSITION CHECK, FOUND CRACK IN COCKPIT FLOOR AT BS 248, LBL 12, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: INTERCOSTAL — CORRODED (BS 294.5)

DURING SCHEDULED TRANSITION CHECK, FOUND INTERCOSTAL CORRODED BETWEEN BS 294.5 AND 312. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — CRACKED (NR 6 LE SLAT)

DURING SCHEDULED TRANSITION CHECK, FOUND NUMBER 6 SLAT CRACKED AT LOWER L/E OF SLAT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FRAME — DAMAGED (BS 787)

DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE FRAME DAMAGE AT BS 787, RBL 22, WL 156. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — OIL CANNING (BS 727)

DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN OIL CANNING AT BS 727E+3, BETWEEN S22 AND 23L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FLOOR BEAM — CORRODED (FUSELAGE)

DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM UPPER CHORD CORROSION AT BS 1112 TO 1121, RBL 22, WL 228, AT BS 986.5, LBL 55 TO RBL 55, WL 208 AND AT BS 1016, RBL 45 TO LBL 45, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — DENTED (FUSELAGE)

DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT FOLLOWING LOCATIONS: BS 1020, BETWEEN S12 AND 13L, AT BS 1000, WL 220, LEFT SIDE BEHIND AFT ENTRY DOOR, AT BS 356, BETWEEN S18 AND 19R, AT BS 193, WL 192, LEFT SIDE, AT BS 1040, LBL 188, BS 972, BETWEEN S22 AND 23L, AND AT BS 1000, LBL 4, WL 185. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FLOOR BEAM — CORRODED (FUSELAGE)

DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORRODED BS 328, WL 208, RBL 7 TO 56, AT BS 312, WL 208, LBL 15, AND AT BS 344, WL 208, LBL 60. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FLOOR BEAM — CORRODED (BS 1112-1121)

DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM LOWER HORIZONTAL CHORD CORRODED FROM BS 1112 TO 1121, RBL 22, WL 216. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.