N346SW

Part: CAM — CRACKED (TE FLAP) · airframe 79,067 hrs · 68,735 cycles

LT WING INBD AFT FLAP DRIVE MECHANISM BOOM CABLE CLUTCH CAM ARM ASSEMBLY CRACKED. R & R CAM ARM ASSEMBLY IAW CMM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 79,067 hrs · 68,735 cycles

AFT CARGO COMPARTMENT CHANNEL CRACKED BETWEEN BS 787 TO BS 792.5 RBL 17.48. R & R CHANNEL IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 79,067 hrs · 68,735 cycles

FITTING CRACKED BETWEEN BS 291.5 TO BS 294.5 STRINGER 8R. R & R FITTING IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 79,067 hrs · 68,735 cycles

STRAP CRACKED BETWEEN BS 312 TO BS 344 LBL 46. R & R STRAP IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 79,067 hrs · 68,735 cycles

STRAP CRACKED BETWEEN BS 312 TO BS 344, LBL 10. REPAIRED STRAP IAW SRM & DRAWING.

Part: ACCESS PANEL — CRACKED (RT PYLON) · airframe 79,067 hrs · 68,735 cycles

RT PYLON ACCESS PANEL CRACKED AT BS 235. REPAIRED PANEL IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 79,067 hrs · 68,735 cycles

STIFFENER CRACKED AT BS 1016 RBL 10. R & R STIFFENER IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 79,067 hrs · 68,735 cycles

SUPPORT ANGLE CRACKED AT BS 540 STRINGER 4R. R & R ANGLE IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 79,067 hrs · 68,735 cycles

SUPPORT ANGLE CRACKED AT BS 540 STRINGER 24L. R & R ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,067 hrs · 68,735 cycles

FRAME CRACKED AT BS 520 BETWEEN STRINGER 20R TO STRINGER 21R. REPAIRED FRAME IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 79,067 hrs · 68,735 cycles

DOME CAP WEB CRACKED AT BS 1016 RBL 4. REPAIRED WEB IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 79,067 hrs · 68,735 cycles

DOME CAP WEB CRACKED AT BS 1016 RBL 3.5. REPAIRED WEB IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FLAP TRACK) · airframe 79,067 hrs · 68,735 cycles

RT WING 36 FAIRING FLAP TRACK SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (RT PYLON) · airframe 79,067 hrs · 68,735 cycles

RT WING AFT PYLON ANGLE CRACKED AT WBL 183.40. R & R ANGLE IAW SRM & DRAWING.

Part: SPOILER — DELAMINATED (RT WING) · airframe 79,067 hrs · 68,735 cycles

RT WING NR 8 SPOILER DELAMINATED. R & R NR 8 SPOILER IAW AMM

Part: ANGLE — CRACKED (LT WING) · airframe 79,067 hrs · 68,735 cycles

LT WING ANGLE CRACKED AT WBL 183.40. R & R ANGLE IAW SRM & DRAWING.

Part: WEB — CRACKED (NLG WW) · airframe 79,067 hrs · 68,735 cycles

LT NLG WW WEB CRACKED AT BS 235.8+3 WL 169.1. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 79,067 hrs · 68,735 cycles

LT NLG WW WEB CRACKED AT BS 235.8+4 WL 169.1. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 79,067 hrs · 68,735 cycles

LT NLG WW WEB CRACKED AT BS 243.7+4.5 WL 169.1. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 79,067 hrs · 68,735 cycles

LT NLG WW WEB CRACKED AT BS 243.7+2.5 WL 169.1. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 79,067 hrs · 68,735 cycles

LT NLG WW WEB CRACKED AT BS 243.7+3.5 WL 169.1. REPAIRED WEB IAW SRM.

Part: DOUBLER — CRACKED (NLG WW) · airframe 79,067 hrs · 68,735 cycles

RT NLG WW ALONG THE DOUBLER EDGE CRACKED AT BS 258.6 WL 169.1+ 6. REPAIRED DOUBLER IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 79,067 hrs · 68,735 cycles

BULKHEAD WEB CRACKED AT BS 1016 STRINGER 18R. REPAIRED WEB IAW EA.

Part: DOUBLER — CRACKED (NLG WW) · airframe 79,067 hrs · 68,735 cycles

LT NLG WW ALONG THE DOUBLER CRACKED AT BS 258.6 WL 169.1+ 5. REPAIRED DOUBLER IAW SRM.

Part: SKIN — NICKED (FUSELAGE) · airframe 79,067 hrs · 68,735 cycles

SKIN NICKED AT BS 178+8.5" LBL 4. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,067 hrs · 68,735 cycles

FUSELAGE SKIN CRACKED AT BS 360 STRINGER 3R. REPAIRED SKIN IAW EO & EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 79,067 hrs · 68,735 cycles

MAIN WW PRESS DECK CRACKED BETWEEN BS 664 TO BS 675 BETWEEN LBL 24.5 TO LBL 45.50. REPAIRED DECK IAW EA.

Part: PLATE — CRACKED (FUSELAGE) · airframe 79,067 hrs · 68,735 cycles

PLATE CRACKED BETWEEN BS 1137 TO BS 1156 STRINGER 9L. R & R PLATE IAW SRM & DRAWING.

Part: LANYARD — LOOSE (OVERWING EXIT) · airframe 78,326 hrs · 68,206 cycles

RT OVERWING EMERGENCY EXIT LANYARD LOOSE. SECURED LANYARD IAW MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 78,140 hrs · 68,049 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,812 hrs · 67,083 cycles

EMERGENCY EXIT LIGHT AFT OF L2 DOOR INOP. RELAMPED PER AMM.

Part: SLAT — CRACKED (LT WING) · airframe 76,640 hrs · 66,965 cycles

NR 2 SLAT O/B AUX TRACK FIXED L/E CUTOUT CRACKED. REPAIRED PER EA.

Part: SLAT — CRACKED (LT WING) · airframe 76,640 hrs · 66,965 cycles

NR 2 SLAT O/B AUX TRACK FIXED 4 CUTOUT CRACKED. REPAIRED NR 2 SLAT O/B AUX TRACK PER EA.

Part: CURTAIN — CRACKED (LE SLAT) · airframe 76,640 hrs · 66,965 cycles

RIGHT WING NR 6 SLAT ACTUATOR CUTOUT CURTAIN CRACKED. REMOVED AND REPLACED PER MM.

Part: ANGLE — CRACKED (LT WING) · airframe 76,640 hrs · 66,965 cycles

LEFT WING I/B UPPER SHELF PANEL L-ANGLE CRACKED. REPAIRED ANGLE PER AMM.

Part: COVER — OUT OF POSITION (L1 DOOR) · airframe 76,606 hrs · 66,942 cycles

FWD ENTRY DOOR EMERGENCY EVACUATION SLIDE- MANUAL INFLATION HANDLE FLAP COVER NOT POSITIONED PROPERLY. REPOSITIONED MANUAL INFLATION HANDLE FLAP COVER ON FWD ENTRY & FWD SERVICE DOOR EMERGENCY EVAC SLIDES PER MM.

Part: COVER — OUT OF POSITION (R1 DOOR) · airframe 76,606 hrs · 66,942 cycles

SERVICE ENTRY DOOR EMERGENCY EVACUATION SLIDE- MANUAL INFLATION HANDLE FLPA COVER NOT POSITIONED PROPERLY. REPOSITIONED MANUAL INFLATION HANDLE FLAP COVER ON FWD ENTRY & FWD SERVICE DOOR EMERGENCY EVAC SLIDES PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,821 hrs · 66,368 cycles

LEFT AFT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK IAW AMM.

Part: SKIN — CRACKED (TE FLAP) · airframe 75,821 hrs · 66,368 cycles

RIGHT WING O/B FOREFLAP LOWER SKIN CRACKED AT WBL 396. REPAIRED FOREFLAP IAW SRM.

Part: LIGHT — FAILED (CABIN) · airframe 75,821 hrs · 66,368 cycles

LEFT EMERGENCY EXIT LIGHT AFT OF MLG W/W FAILED CHECK. REMOVED AND REPLACED LAMP IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,766 hrs · 66,326 cycles

FUSELAGE SKIN CRACKED AT BS 360, STR 5R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,766 hrs · 66,326 cycles

FUSELAGE SKIN CRACKED AT BS 360, STR 6R. REPAIRED SKIN IAW SRM.

Part: SLIDE — LOW (L1 DOOR) · airframe 75,136 hrs · 65,837 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 74,966 hrs · 65,706 cycles

R2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 74,846 hrs · 65,610 cycles

FUSELAGE SKIN CRACKED AT BS 500D+2, STR 8R. REPAIRED SKIN CRACK PER EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 73,767 hrs · 64,800 cycles

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

Part: CHARGER — INOPERATIVE (CABIN) · airframe 73,733 hrs · 64,779 cycles

LT SIDEWALL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,733 hrs · 64,779 cycles

RT SIDEWALL EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,733 hrs · 64,779 cycles

L2 DOOR FUSELAGE SKIN CRACKED AT UPPER AFT CORNER. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,733 hrs · 64,779 cycles

FRAME CRACKED AT BS 460, STR 26L. REPAIRED FRAME PER EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 73,733 hrs · 64,779 cycles

ENTRY DOOR CREASE BEAM CORRODED AT BETWEEN BS 301 TO BS 345, BETWEEN LBL 55 TO 60. REPAIRED BEAM PER SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 73,733 hrs · 64,779 cycles

LONG FLOORBEAM LBL 45.5 STA 727A+19 CRACKED AT O/B ATTACH STRAP. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,733 hrs · 64,779 cycles

LONG FLOORBEAM LBL 45.5 STA 727A+19 CRACKED AT O/B ATTACH STRAP. REPAIRED BEAM PER EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 73,733 hrs · 64,779 cycles

ENTRY DOOR CREASE BEAM CORRODED AT BETWEEN BS 301 TO BS 345, BETWEEN LBL 55 TO 60. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 73,733 hrs · 64,779 cycles

FWD GALLEY FLOORBEAM CORRODED AT BS 328, BETWEEN LBL 25 TO RBL 65. REMOVED AND REPLACED T-CAP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 73,733 hrs · 64,779 cycles

FWD GALLEY FLOORBEAM AT BS 328, BETWEEN LBL 25 AND RBL 65 CORRODED. REMOVED AND REPLACED T-CAP PER SRM. (SUBMITTED AS A SUPPLEMENT, COULDN`T FIND ORIGINAL CONTROL NUMBER.)

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 73,733 hrs · 64,779 cycles

DURING SCHEDULED 24Y CHECK, FOUND DOUBLER CORRODED AT BS 727D, BL 0. REPAIRED DOUBLER PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,733 hrs · 64,779 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 727D+3, STR 27L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,733 hrs · 64,779 cycles

DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 727D+8, STR 27L. REPAIRED SKIN IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,733 hrs · 64,779 cycles

DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 867, BL 0. REPAIRED SHEAR TIE PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 73,733 hrs · 64,779 cycles

DURING SCHEDULED 24Y CHECK, FOUND FUEL TANK EXTERNAL STIFFENER CRACKED AT BS 548, LBL 57. REMOVED AND REPLACED STIFFENER PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 73,733 hrs · 64,779 cycles

DURING SCHEDULED 24Y CHECK, FOUND RT WING NR 5 SLAT I/B T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,733 hrs · 64,779 cycles

DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 815, STR 27R. REMOVED AND REPLACED STRINGER PER SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 73,733 hrs · 64,779 cycles

RT CENTER EMERGENCY EXIT LIGHT FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 73,733 hrs · 64,779 cycles

LT FWD EMERGENCY EXIT LIGHT FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BRACKET — FAULTY (FUSELAGE) · airframe 73,733 hrs · 64,779 cycles

DURING SCHEDULED 24Y CHECK, FOUND FLIGHT DECK FLOOR OPC CRADLE BRACKET FWD O/B MOUNTING HOLE CRACKED AT BS 247, RBL 23. REPAIRED WEB IAW ACO.

Part: BATTERY PACK — FAILED (CABIN) · airframe 73,733 hrs · 64,779 cycles

RT CENTER EMERGENCY EXIT LIGHT FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 73,733 hrs · 64,779 cycles

RT AFT EMERGENCY EXIT LIGHT FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 73,733 hrs · 64,779 cycles

RT AFT EMERGENCY EXIT LIGHT FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 73,733 hrs · 64,779 cycles

LT FWD EMERGENCY EXIT LIGHT FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 73,733 hrs · 64,779 cycles

DURING SCHEDULED 24Y CHECK, FOUND PRESSURE WEB CRACKED AT BS 663, RBL 39. REPAIRED WEB IAW SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 73,552 hrs · 64,634 cycles

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

Part: LIGHT — CRACKED (CABIN) · airframe 73,422 hrs · 64,531 cycles

LT LOWER EMERGENCY EXIT LIGHT CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,397 hrs · 64,503 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT BULB INOP. RELAMPED PER MM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 72,255 hrs · 63,639 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 72,256 hrs · 63,639 cycles

R2 DOOR EMERGENCY EVAC SLIDE GAUGE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: BEAM — CRACKED (FUSELAGE) · airframe 71,759 hrs · 63,282 cycles

DURING SCHEDULED SPV CHECK, FOUND LT STUB BEAM CRACKED AT BS 616. REPAIRED BEAM PER EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 71,759 hrs · 63,282 cycles

DURING SCHEDULED SPV CHECK FOUND, L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,759 hrs · 63,282 cycles

DURING SCHEDULED SPV CHECK FOUND, FORWARD ENTRY EMERGENCY LIGHT INOP. RELAMPED PER MM.

Part: GASPER FAN — FAULTY (CABIN) · airframe 71,601 hrs · 63,150 cycles

DECLARED EMERGENCY, STRONG ODOR OF SMOKE IN CABIN. REMOVED AND REPLACED GASPER FAN, RECIRCULATION FAN, HEPA FILTER AND COALESCER BAGS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 70,799 hrs · 62,543 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: ACTUATOR — BROKEN (SPOILER) · airframe 70,718 hrs · 62,489 cycles

ON LANDING, AFTER MAIN GEAR STRUT COMPRESS AND BEFORE NOSE GEAR TOUCH DOWN, THE AIRCRAFT ROLLS/ PULLS LEFT. REMOVED AND REPLACED BOTH NR 5 GROUND SPOILER ACTUATORS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,530 hrs · 61,588 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: UPLOCK ACTUATOR — FAULTY (LT MLG) · airframe 69,510 hrs · 61,572 cycles

LEFT MLG MOUNT INDICATED UNSAFE - RED. MANUALLY EXTENDED LANDING, ALL INDICATIONS AGREE - DOWN & LOCKED. REMOVED AND REPLACED UPLOCK AND DOWNLOCK ACTUATORS.

Part: FITTING — CORRODED (FUSELAGE) · airframe 68,939 hrs · 61,108 cycles

DURING SCHEDULED MV2 CHECK, FOUND STRINGER FITTING CORRODED AT BS 1016, STR 27R. REPAIRED FITTING PER SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 68,939 hrs · 61,108 cycles

DURING SCHEDULED MV2 CHECK, FOUND SPLICE ANGLE CORRODED AT BS 1016, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SPLICE PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 68,043 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING O/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: SPLICE — SHORTED (EVAC SLIDE) · airframe 68,043 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT SLIDE POWER WIRE SPLICE SHORTED TO GROUND. REMOVED AND REPLACED SPLICE PER WDM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,043 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 440, BETWEEN STR 13R TO STR 14R. REPAIRED FRAME PER ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, BETWEEN STR 23R TO STR 24R. REPAIRED SHEAR TIE PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 303.9 AT LOWER L1 DOOR STOP FITTING. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CORRODED AT BS 709, RBL 24.5. REPAIRED BEAM PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 380, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 5 TO RBL 45. REPAIRED BEAM PER ER.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 68,043 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 500D TO BS 540.6. REMOVED AND REPLACED BEAM PER SRM.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND BULKHEAD SUPPORT CHANNEL CRACKED AT BS 727, RBL 6. REMOVED AND REPLACED CHANNEL PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 1064, BETWEEN STR 20L TO STR 24L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BS 663, RBL 24.5. REPAIRED WEB PER ER.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 639, LBL 45. REMOVED AND REPLACED STIFFENER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 706 TO BS 716, LBL 24.5. REPAIRED WEB PER ER.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 639, RBL 45. REMOVED AND REPLACED STIFFENER PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO BULKHEAD T-ANGLE CRACKED AT BS 727, RBL 6. REMOVED AND REPLACED T-ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 907, STR 8R. REMOVED AND REPLACED FRAME SECTION PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 1040, BETWEEN STR 23RL TO STR 24L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 986.5, BETWEEN STR 2L TO STR 3L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND WEB CRACKED BETWEEN BS 928 TO BS 948, BETWEEN STR 25R TO STR 26R. REPAIRED WEB PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CORRODED AT BS 360, BETWEEN BL 0 TO LBL 5. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CHORD CRACKED AT BS 294, LBL 54. REPAIRED CHORD PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 10. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 6L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 10L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED BETWEEN BS 375 TO BS 377, STR 8L. REPAIRED SKIN PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 420, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 10R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 9R. REMOVED AND REPLACED CLIP PER SI.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 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 68,044 hrs · 60,426 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 970, STR 27L. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 500B, STR 8L. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 500A, STR 8L. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 500, STR 8L. REMOVED AND REPLACED STRINGER PER SRM.

Part: WEB — CRACKED (NLG WW) · airframe 68,044 hrs · 60,426 cycles

DURING SCHEDULED SPV CHECK, FOUND LT NLG WHEEL WELL WEB CRACKED. REPAIRED WEB PER EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 66,950 hrs · 59,631 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 66,950 hrs · 59,631 cycles

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

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 66,899 hrs · 59,599 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,745 hrs · 59,479 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 950, STR 25L. REPAIRED SKIN PER SWA EA AND SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,823 hrs · 58,816 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747+ 6, STR 20L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,823 hrs · 58,816 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,823 hrs · 58,816 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 500B, STR 15R. REPAIRED SKIN PER SWA EA.

Part: SIGN — BROKEN (CABIN) · airframe 65,699 hrs · 58,728 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,444 hrs · 58,537 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 923, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,444 hrs · 58,537 cycles

DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 259, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,444 hrs · 58,537 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,444 hrs · 58,537 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: ACTUATOR — FAULTY (RT MLG) · airframe 64,386 hrs · 57,780 cycles

FOUND RT MLG INDICATION UNSAFE DURING NORMAL EXTENSION RECYCLED ONCE, NO CHANCE. MANUALLY EXTENDED RT MLG AND GOT SAFE INDICATION. REPLACED UPLOCK ACTUATOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,273 hrs · 57,696 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 360 + 12 STR 15L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,273 hrs · 57,696 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 727D + 10 STR 19R. REMOVED AND REPLACED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,273 hrs · 57,696 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 787 + 4 STR 17L. REMOVED AND REPLACED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,273 hrs · 57,696 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 727D + 10, STR 19R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,684 hrs · 57,255 cycles

DURING SCHEDULED MV4 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (R1 DOOR SLIDE) · airframe 63,693 hrs · 57,261 cycles

DURING SCHEDULED MV4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 63,482 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,482 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 980, STR 20L. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,482 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 986, STR 20L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,482 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 950, STR 25L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 63,482 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 987, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 63,482 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 1006, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: ACTUATOR — FROZEN (NR 4 SPOILER) · airframe 63,481 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT WING NR 4 SPOILER ACTUATOR ROD END FROZEN. REMOVED AND REPLACED ACTUATOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,481 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 494, STR 13L. REPAIRED SKIN PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,482 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 24L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 947 S25R) · airframe 63,481 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 947 S25R) · airframe 63,481 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — DELAMINATED (NR 5 SLAT) · airframe 63,482 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED AT OUTBOARD END. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (BS 380 S19L) · airframe 63,482 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 19L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727E S24L) · airframe 63,482 hrs · 57,113 cycles

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

Part: STRINGER CLIP — CRACKED (BS 747 S18L) · airframe 63,482 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 18L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 400 S16L) · airframe 63,482 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — DELAMINATED (NR 5 SLAT) · airframe 63,482 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED AT INBOARD END. REPAIRED SLAT PER SRM.

Part: STRINGER CLIP — CRACKED (BS 380 S21L) · airframe 63,482 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 767 S18L) · airframe 63,482 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 18L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 787 S23L) · airframe 63,482 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727C S22L) · airframe 63,482 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A S25L) · airframe 63,482 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 747 S22L) · airframe 63,482 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 787 S23R) · airframe 63,482 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 767 S24R) · airframe 63,482 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 24R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 787 S22R) · airframe 63,482 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 22R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500C S26R) · airframe 63,482 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727B S25L) · airframe 63,482 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,481 hrs · 57,113 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 22R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 63,481 hrs · 57,113 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 22R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: UPLOCK ACTUATOR — FAULTY (RT MLG) · airframe 63,337 hrs · 57,003 cycles

DURING LANDING GEAR EXTENSION RT MLG RED WARNING LIGHT ILLUMINATED AND NO GREEN LIGHT. CYCLED LANDING GEAR ONCE AND RT MLG GREEN LIGHT ILLUMINATED. INSPECTED WIRING, SENSOR AND TARGET PER MM. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 63,197 hrs · 56,895 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,735 hrs · 56,565 cycles

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

Part: ACM — FAULTY (A/C BAY) · airframe 62,718 hrs · 56,551 cycles

FLIGHT ATTENDANT REPORTED STRONG EXHAUST TYPE SMELL DURING CLIMB AND DESCENT. REMOVED AND REPLACED RT ACM PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,726 hrs · 56,558 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,470 hrs · 56,360 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 972, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,470 hrs · 56,360 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 972, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,470 hrs · 56,360 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 729D, STR 19R. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 62,470 hrs · 56,360 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,470 hrs · 56,360 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 914, STR 25L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,470 hrs · 56,360 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 781, STR 18L. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (NLG WW) · airframe 61,461 hrs · 55,623 cycles

DURING SCHEDULED MV1 CHECK, FOUND NLG W/W RIGHT ACCESS PANEL CUTOUT WEB CRACKED AT BS 247. REPAIRED WEB PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 61,267 hrs · 55,466 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (BS 757 S19R) · airframe 59,814 hrs · 54,289 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 19R. REPAIRED SKIN PER SRM.

Part: HOOK — CRACKED (R1 DOOR) · airframe 59,198 hrs · 53,736 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK CRACKED. REMOVED AND REPLACED FWD GIRT BAR HOOK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,098 hrs · 53,736 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT BS 960, STR 18L. REPAIRED SKIN PER SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,330 hrs · 53,145 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK IAW MM.

Part: SKIN — CRACKED (BS 932 S21R) · airframe 57,852 hrs · 52,765 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, S21R. REPAIRED SKIN PER SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,852 hrs · 52,765 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,643 hrs · 52,609 cycles

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

Part: BATTERY — SHORTED (EMERGENCY LIGHTS) · airframe 57,643 hrs · 52,609 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT FWD CABIN EMERGENCY EXIT LIGHT BATTERY SHORTED. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,643 hrs · 52,609 cycles

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,574 hrs · 52,555 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND FWD CARGO DOOR CUTOUT UPPER FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN BEARSTRAP CRACKED AT AFT CARGO DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: KEELBEAM — CRACKED (BS 718) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND KEEL BEAM STRESS PANEL CRACKED AT BS 718, RBL 6. REMOVED AND REPLACED STRESS PANEL PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME WEB CRACKED AT LOWER STOP FITTING. REMOVED AND REPLACED FRAME WEB SECTION PER SRM.

Part: STRINGER — CRACKED (BS 1010 S7L) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CRACKED AT BS 1010, STR 7L. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FLOORBEAM — CRACKED (BS 727B) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 24. REPAIRED FLOORBEAM PER ER.

Part: FLOOR SUPPORT — CORRODED (BS 986) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 986 TO BS 994, LBL 40. REMOVED AND REPLACED FLOORBEAM WEB PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED EVAC SLIDE FWD GIRT BAR FITTING PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: CREASE BEAM — CORRODED (BS 440-460) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM WEB CORRODED AT RT BS 440 TO RT BS 460. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: SKIN — CRACKED (BS 379) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST CUTOUT, BS 379, LBL 3. REPAIRED SKIN PER SWA EA.

Part: FRAME — CRACKED (BS 295 S16L) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 295, STR 16L. REMOVED AND REPLACED FRAME WEB SECTION PER SRM.

Part: FRAME — CRACKED (BS 295 S8L) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 295, STR 8L. REMOVED AND REPLACED FRAME WEB SECTION PER SRM.

Part: FRAME — CRACKED (BS 663 S3L) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 3L. REPAIRED FRAME SECTION PER SRM.

Part: CREASE BEAM — CORRODED (BS 907-927) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM WEB CORRODED AT LEFT BS 907 TO LEFT BS 927. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED EVAC SLIDE AFT GIRT BAR FITTING PER SRM.

Part: FLOORBEAM — CORRODED (BS 360) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CORRODED AT BS 360 RBL 65 TO RBL 70.5. REMOVED AND REPLACED FLOORBEAM WEB PER SRM.

Part: FRAME — CRACKED (BS 440 S8R) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME SECTION PER SRM.

Part: CREASE BEAM — CORRODED (BS 400-440) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 400 TO BS 440, RBL 65 TO RBL 70.5. REMOVED AND REPLACED FLOORBEAM WEB PER SRM.

Part: STRINGER CLIP — CRACKED (BS 294) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: WEB — CHAFED (VERTICAL STAB) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND VERTICAL STAB FWD WEB COMMON TO DORSAL FIN CHAFED. REPAIRED WEB PER SRM.

Part: SHEAR TIE — CORRODED (BS 380) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 380, BL 0. REPAIRED SHEAR TIE PER SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT HORIZONTAL STAB L/E RIB WEB CRACKED AT STA 86.66, UPPER AFT END. REPAIRED RIB WEB PER ER.

Part: STRINGER CLIP — CRACKED (BS 360) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CORRODED (BS 269) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOOR SUPPORT UPPER CHORD CORRODED AT BS 269 TO BS 270, RBL 11 TO LBL 7. REMOVED AND REPLACED FLOORBEAM UPPER CHORD SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (BS 360) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FLOORBEAM — CRACKED (BS 947) · airframe 52,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CRACKED AT BS 947.5, LBL 53. REPAIRED FLOORBEAM PER ER.

Part: WEDGE — DELAMINATED (LT WING TE FLAP) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT WING INBOARD MID FLAP T/E WEDGE OUTBOARD END DELAMINATED. REPAIRED MID FLAP WEDGE PER SRM.

Part: FRAME — CORRODED (BS 992) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CORRODED AT RT BS 992, WL 209. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 987, LBL 39. REMOVED AND REPLACED FLOORBEAM UPPER CHORD PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER 15L CRACKED AT BS 360. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: BRACKET — LOOSE (CABIN) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT BRACKET LOOSE. REMOVED AND REPLACED BRACKET PER SRM.

Part: BRACKET — LOOSE (CABIN) · airframe 57,279 hrs · 52,322 cycles

DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD BRACKET LOOSE. REMOVED AND REPLACED BRACKET PER SRM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,032 hrs · 52,133 cycles

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

Part: SKIN — CRACKED (BS 522 S28L) · airframe 56,965 hrs · 52,079 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 522, STR STR 28L, AUX AIR HOOK UP CUTOUT. REPAIRED SKIN PER SWA EA.

Part: GLOWSTRIP — WORN (CABIN) · airframe 56,965 hrs · 52,079 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP AT ROW 13 TO ROW 23 WORN. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: LIGHT — OUT OF ADJUST (CABIN) · airframe 56,965 hrs · 52,079 cycles

DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT OUT OF ADJUST AT ROW 10 ABC. ADJUSTED EMERGENCY EXIT LIGHT PER MM.

Part: SKIN — CRACKED (BS 500C-520) · airframe 56,760 hrs · 51,923 cycles

DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 500C TO BS 520, STR 15L TO STR 16L. REPAIRED SKIN PER SWA EA.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 56,503 hrs · 51,745 cycles

EMERGENCY BULLNOSE EXIT LIGHT LENS LOOSE AT ROW 10 ABC. REMOVED AND REPLACED LENS COVER PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 55,701 hrs · 51,116 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,448 hrs · 50,892 cycles

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

Part: FRAME — CRACKED (R1 DOORWAY) · airframe 55,034 hrs · 50,551 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE FRAME CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED FRAME PER SWA EA.

Part: GLOWSTRIP — WORN (ROW 8-12) · airframe 55,034 hrs · 50,551 cycles

DURING SCHEDULED C1 CHECK, FOUND PHOTOLUMINESCENT STRIP WORN BETWEEN ROW 8 TO ROW 12. REMOVED AND REPLACED STRIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,640 hrs · 50,229 cycles

DURING WALKAROUND INSP, FOUND FUSELAGE SKIN CRACKED AT BS 986, STR 21L. MX FERRY TO PHX FOR REPAIRS. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,551 hrs · 50,163 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,357 hrs · 50,030 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED BELOW DORSAL FIN AT BS 967, STR 2R. REPAIRED SKIN PER SRM.

Part: HINGE — BROKEN (LT WING SPOILER) · airframe 54,139 hrs · 49,850 cycles

DURING SCHEDULED RON CHECK, FOUND LT WING INBOARD T/E GROUND SPOILER BROKEN AT HINGE CASTING. REMOVED AND REPLACED SPOILER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,106 hrs · 49,823 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 18L. REPAIRED SKIN PER SWA EA & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,123 hrs · 49,040 cycles

DURING SCHEDULED C3 CHECK, FOUND 3 EA FUSELAGE SKIN CRACKS BETWEEN BS 931 TO BS 934, BETWEEN STR 23L TO STR 24L. REPAIRED SKIN PER SWA EA & SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,123 hrs · 49,040 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: STRIP — WORN (CABIN) · airframe 53,123 hrs · 49,040 cycles

DURING SCHEDULED C3 CHECK, FOUND SEVERAL EEPLS STRIPS WORN. REMOVED AND REPLACED EEPLS STRIPS PER MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 51,694 hrs · 47,909 cycles

DURING SCHEDULED RON, FOUND RT WING OUTBD FORE FLAP DELAMINATED AT UPPER SURFACE. REMOVED AND REPLACED FLAP ASSY PER MM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 51,642 hrs · 47,855 cycles

FWD RT EMERGENCY EXIT PHOTOLUMINESCENT STRIP LOOSE. SECURED EMERGENCY EXIT PHOTOLUMINESCENT STRIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,286 hrs · 47,528 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT LOWER AFT CORNER. REPAIRED SKIN PER SRM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 51,286 hrs · 47,548 cycles

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT PHOTOLUMINESCENT STRIPS AT LT ROW 16 TO LT ROW 19, AND RT FWD SECTION WORN. REMOVED AND REPLACED PHOTOLUMINESCENT STRIPS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,127 hrs · 47,421 cycles

DURING OTS, FOUND FUSELAGE SKIN AT BS 530, STRINGER 18R, CRACKED. REPAIRED SKIN PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY EXIT) · airframe 51,092 hrs · 47,390 cycles

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

Part: LINE — LEAKING (B-HYD SYSTEM) · airframe 50,998 hrs · 47,309 cycles

DECLARED EMERGENCY, HYDRAULIC B-SYSTEM LOW PRESSURE LIGHT ILLUMINATED, WITH QUANTITY GOING DOWN. REMOVED AND REPLACED HYDRAULIC B-SYSTEM PUMP PRESSURE LINE PER MM.

Part: TURBINE — FAILED (NR 1 ENGINE) · airframe 50,760 hrs · 47,115 cycles

IN FLIGHT SHUTDOWN / AIR TURNBACK, DURING CLIMB NR 1 ENGINE MADE A LOUD BANG. EGT INDICATION INCREASED TO 1060 DEGS. REMOVED AND REPLACED NR 1 ENG PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,688 hrs · 47,049 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STR 5L CRACKED AT FASTENER HOLE, BS 380. REPAIRED STRINGER PER SRM.

Part: GLOWSTRIP — DELAMINATED (CABIN) · airframe 50,617 hrs · 46,999 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DELAMINATED AT ROW 18 ABC TO ROW 20 ABC. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,073 hrs · 46,556 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 940, STRINGER 21R, CRACKED. REPAIRED SKIN PER SRM.

Part: FITTING — WORN (LT ELEVATOR) · airframe 49,418 hrs · 46,052 cycles

DURING SCHEDULED C3 CHECK, LT ELEVATOR TAB FAILED FREE PLAY INSPECTION. REMOVED AND REPLACED LT ELEVATOR TAB NR 1 HINGE FITTING PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,418 hrs · 46,052 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STRINGER 18L. REPAIRED SKIN PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 49,346 hrs · 46,000 cycles

EEPLS FLOOR TRACK LIGHT COVER LOOSE AT ROW 8 DEF. REMOVED AND REPLACED EEPLS TRACK LIGHT COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 49,334 hrs · 45,995 cycles

EEPLS FLOOR TRACK LOOSE AT ROW 8. REMOVED AND REPLACED EEPLS FLOOR STRIP PER MM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 49,287 hrs · 45,961 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 14L SPLICE CRACKED AT BS 540. REPAIRED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,287 hrs · 45,961 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CRACKED TO FRAME FROM BS 500D, BELOW STRINGER 10R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,287 hrs · 45,961 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FRAME CORRODED AT BS 787, STRINGER 25R. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,287 hrs · 45,961 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 11R CRACKED AT BS 828. REPAIRED STRINGER PER ERO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,287 hrs · 45,961 cycles

DURING SCHEDULED 1/2D CHECK, FOUND R2 DOOR CUTOUT FORWARD LOWER CORNER FUSELAGE SKIN CRACKED. REPAIRED SKIN CRACK PER SRM.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 49,287 hrs · 45,961 cycles

DURING SCHEDULED 1/2D CHECK, FOUND L1 DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED L1 DOOR EMERGENCY LIGHT PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 49,287 hrs · 45,961 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 663.75, BL 0. REPAIRED FLOORBEAM WEB PER ER.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 49,286 hrs · 45,960 cycles

DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL LEG ANGLE CRACKED AT BS 700 STRINGER 18A, LBL 63. REPAIRED PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 49,286 hrs · 45,960 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR CUTOUT FRAME WEB CRACKED AT BS 787 + 6. REPAIRED PER SRM.

Part: SKIN — CRACKED (TE FLAP) · airframe 49,286 hrs · 45,960 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT WING OUTBOARD T/E MIDFLAP L/E SKIN CRACKED AT WBL 205. REPAIRED SKIN PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 49,286 hrs · 45,960 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO COMPARTMENT BULKHEAD CENTER LOWER SUPPORT CHORD CORRODED AT BS 948. REPAIRED PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 49,286 hrs · 45,960 cycles

DURING SCHEDULED 1/2D CHECK, FOUND PRESSURE DECK CRACKED AT BS 663, LBL 30. REPAIRED PRESSURE DECK PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,286 hrs · 45,960 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN BUTT STRAP CRACKED AT BS 360, STRINGER 10L. REPAIRED BUTT STRAP PER SRM.

Part: SIGN — LOOSE (EMERGENCY EXIT) · airframe 49,286 hrs · 45,960 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT FWD EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 49,286 hrs · 45,960 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAMS CORRODED AT BS 300 TO BS 328 RT AND BS 400 TO BS 420 LT. REPAIRED CREASE BEAMS PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 49,286 hrs · 45,960 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 540, STRIGER 4L. REPAIRED STRINGER SPILCE PER SRM.

Part: BUTTSTRAP — CRACKED (FUSELAGE) · airframe 49,286 hrs · 45,960 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CRACK AT FASTENER HOLE ON BUTT SPLICE STRAP AT BS 908, BELOW STRINGER 4L. REPAIRED BUTT STRAP SPLICE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 49,286 hrs · 45,960 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 10R AT BS 500B, CRACKED. REPAIRED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,286 hrs · 45,960 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER TIE CLIP CRACKED AT BS 344, STRINGER 11R. REPAIRED STRINGER TIE CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,286 hrs · 45,960 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STRINGER 14L. REPAIRED STRINGER CLIP PER SRM.

Part: BUTTSTRAP — CRACKED (FUSELAGE) · airframe 49,286 hrs · 45,960 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BUTTSTRAPS CRACKED AT BS 360 STRINGER 14L, BS 908, BETWEEN STRINGERS 15L AND 16L. REPAIRED STRAPS PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 49,286 hrs · 45,960 cycles

DURING SCHEDULED 1/2D CHECK, FOUND LT CREASE BEAM CHORD CORRODED AT BS 340 TO BS 357. REPAIRED CREASE BEAM CHORD PER SRM.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 49,286 hrs · 45,960 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BELTFRAME INNER CHORD AND WEB CRACKED AT BS 344 BETWEEN STRINGERS 23L AND 24 L. REPAIRED BELTFRAME INNER CHORD PER SRM.

Part: SPLICE — CRACKED (STRINGER) · airframe 49,286 hrs · 45,960 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STRINGER 10L. REPAIRED STRINGER SPLICE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 49,286 hrs · 45,960 cycles

DURING SCHEDULED 1/2D CHECK, FOUND CREASE BEAM CORRODED AT BS 947 TO BS 1000, RBL 62.50. REPAIRED CREASE BEAM PER SRM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 49,286 hrs · 45,960 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS PER MM.

Part: STRAP — CRACKED (FUSELAGE SKIN) · airframe 49,286 hrs · 45,960 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN STRAP CRACKED AT BS 908, STR 4L. REPAIRED STRAP PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 49,286 hrs · 45,960 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER SPLICE 4R CRACKED AT BS 908. REPAIRED STRINGER SPLICE SECTION PER SRM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 49,286 hrs · 45,960 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986.5, LBL 20 TO LBL 32. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,734 hrs · 45,503 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BOTH LEFT AND RIGHT FUSELAGE FRAME ASSY'S CRACKED AT BS 188, WL 207. REPAIRED FRAMES PER SRM.

Part: LENS — MISSING (CABIN) · airframe 48,518 hrs · 45,329 cycles

DURING SCHEDULED RON, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW NR 3 ABC. INSTALLED LENS PER MM.

Part: INDICATOR — OUT OF LIMITS (FWD ENTRY DOOR) · airframe 48,306 hrs · 45,147 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — LOOSE (PAX DOOR) · airframe 48,109 hrs · 44,978 cycles

DURING SCHEDULED PM CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: WEB — CRACKED (NLG WW) · airframe 47,776 hrs · 44,686 cycles

DURING SCHEDULED C1 CHECK, FOUND NLG W/W BOTH LT/RT UPPER WEB CRACKED AT ACCESS PANEL CUTOUT TIRE STOP. REPAIRED UPPER WEB PER SWA EA.

Part: BATTERY — FAULTY (AFT CABIN) · airframe 46,892 hrs · 44,004 cycles

AFT ENTRY AND AFT SVC DOOR EMERGENCY EXIT SIDE WALL LIGHTS ILLUMINATED WITH SWITCH OFF. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER PER MM.

Part: SKIN — CRACKED (KEEL BEAM) · airframe 45,917 hrs · 43,246 cycles

DURING SCHEDULED C3 CHECK, FOUND LEFT FUSELAGE KEEL BEAM SKIN CRACKED AT BS 695. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,917 hrs · 43,246 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 2, STR 10R. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 45,917 hrs · 43,246 cycles

DURING SCHEDULED C3 CHECK, FOUND BOTH FWD AND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: TRACK — LOOSE (CABIN) · airframe 45,373 hrs · 42,795 cycles

PHOTO LUMINESCENT STRIP LOOSE AT ROW NR 8 ABC. REMOVED AND REPLACED STRIP PER MM.

Part: BATTERY — FAULTY (CABIN) · airframe 47,457 hrs · 45,663 cycles

EMERGENCY EXIT LIGHTS REMAIN ILLUMINATED WHEN SW IS IN OFF POS. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,027 hrs · 42,484 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,036 hrs · 42,494 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A+2, STR 10R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,036 hrs · 42,494 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT STR 18L, BS 753 AND BS 749. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,036 hrs · 42,494 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 13R. REPAIRED SKIN PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 44,790 hrs · 42,280 cycles

LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED EXIT LENS PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 42,507 hrs · 40,406 cycles

DURING SCHEDULED RON, FOUND EMERGENCY FLASHLIGHT INOP AFT CABIN TOP POSITION. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 42,335 hrs · 40,260 cycles

DURING SCHEDULED C3 CHECK, FOUND COCKPIT EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT PER MM.

Part: POST — CRACKED (FUSELAGE) · airframe 41,712 hrs · 39,778 cycles

DURING SCHEDULED 1/4D CHECK, FOUND CAPTAINS WINDOW POST CRACKED .2 INCHES LONG AT UPPER INBD CORNER. REPAIRED POST PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 41,712 hrs · 39,778 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT LIGHT COVER LOOSE ABOVE ROW 18 ABC. R&R LIGHT COVER PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 41,712 hrs · 39,778 cycles

DURING SCHEDULED 1/4D CHECK, FOUND ( 2 EA ) VERTICAL WEBS CRACKED AT BS 180, RBL 17.1, WL 227 AND BS 184, RBL 17.1, WL 232. R&R VERTICAL WEBS PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 41,712 hrs · 39,778 cycles

DURING SCHEDULED 1/4D CHECK, FOUND OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LOOSE AT ROW 14 ABC. SECURED EXIT LIGHT PER MM.

Part: STIFFENER — CRACKED (MLG W/W) · airframe 41,712 hrs · 39,778 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL STIFFENER CRACKED AT MLG W/W, BS 663 & LBL 6.15. REPAIRED STIFFENER PER SWA RA.

Part: WEB — CRACKED (FUSELAGE) · airframe 41,712 hrs · 39,778 cycles

DURING SCHEDULED 1/4D CHECK, FOUND ( 2 EA ) WEB CRACKS AT BS 178, LBL 5.1, WL 201 & WL 199. REPAIRED WEB PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 41,397 hrs · 39,512 cycles

DURING SCHEDULED C2 CHECK, FOUND OVERHEAD BULL NOSE EMERGENCY LIGHT LENS LOOSE AT ROWS 16 DEF & 18 DEF. SECURED BULL NOSE LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,397 hrs · 39,512 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 950, STR 24L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 41,397 hrs · 39,512 cycles

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

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 40,793 hrs · 39,001 cycles

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

Part: WEDGE — DELAMINATED (L/E SLAT) · airframe 40,489 hrs · 38,744 cycles

DURING SCHEDULED C1 CHECK, FOUND NR 2 L/E SLAT T/E WEDGE DELAMINATED 4 X 18 ON UPPER SURFACE. R&R SLAT ASSY PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 40,489 hrs · 38,744 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM.

Part: SEAL — OUT OF POSITION (CARGO DOOR) · airframe 40,442 hrs · 38,705 cycles

AIR TURNBACK, CABIN DIFFICULT TO PRESSURIZE. REPOSITIONED AFT CARGO DOOR PRESSURE SEAL PER MM. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,279 hrs · 38,577 cycles

DURING SCHEDULED A2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS INOP AT ROWS 12 DEF & 18 ABC. RELAMPED LIGHTS PER MM.

Part: SWITCH — INOPERATIVE (APU) · airframe 39,851 hrs · 38,235 cycles

AIR TURNBACK, APU WENT TO OVERSPEED CONDITION DURING CLIMBOUT. REMOVED AND REPLACED 280 MODULE (P/N 65-52801) AND ELECTRONIC 3 SPEED SWITCH. OPS CHECK GOOD PER MM.

Part: SIGN — MISSING (CABIN) · airframe 39,529 hrs · 37,968 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,463 hrs · 37,906 cycles

DURING SCHEDULED SERVICE CHECK, FOUND 4 EXTERNAL FUSELAGE SKIN CRACK AT BS 530, STR 9R. REPAIRED SKIN PER SRM.

Part: HINGE FITTING — CRACKED (DOOR FRAME) · airframe 37,753 hrs · 36,469 cycles

DURING SCHEDULED RON, FOUND FWD SERVICE DOOR UPPER HINGE FITTING CRACKED. REMOVED AND REPLACED HINGE FITTING PER SRM.

Part: ACM — ODOR (A/C BAY) · airframe 37,716 hrs · 36,434 cycles

SHORTLY AFTER TAKEOFF, SMOKE AND ACRID SMELL DEVELOPED IN THE CABIN, RT A/C PACK WAS TURNED OFF AND SMELL/SMOKE WENT AWAY. REMOVED AND REPLACED RIGHT A/C AIR CYCLE MACHINE PER MM.

Part: LENS — MISSING (CABIN)

EMERGENCY LIGHT LENS MISSING AT BULLNOSE IN FWD LOUNGE. REPLACED LENS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: SLIDE — LOOSE (CABIN)

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

Part: LENS — MISSING (ROW 5)

DURING SCHEDULED C4 CHECK, FOUND BULLNOSE EMERGENCY LIGHT LENS MISSING AT ROW 5DEF. REPLACED LENS ASSY PER MM.

Part: SKIN — CRACKED (HORIZ STAB)

DURING SCHEDULED D-CHECK, FOUND HORIZONTAL STAB LOWER SURFACE SKIN CRACKED FWD OF REAR SPAR, (CRACK APPROX 2 LONG). REPAIRED STAB PER SWA ER NR 99-0169, AND SRM.

Part: WEB — CORRODED (BS 798)

DURING SCHEDULED D-CHECK, FOUND 2 CRACKED FRAMES, FS 827 AND FS 867 BETWEEN STRINGERS 8L-8R.

Part: SHEAR TIE — CRACKED (BS 597)

DURING SCHEDULED D-CHECK, FOUND CRACKED SHEAR TIE AT BS 597 BETWEEN STR 13-14 LEFT. REPAIRED SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (BS 986)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 6, 21, 29, 36, 40.5, 44 AT WL 208. REPAIRED PER SWA ER NR 99-0158.

Part: FRAME — CRACKED (BS 827 ,867, 787)

DURING SCHEDULED D-CHECK, FOUND 3 FRAMES CRACKED BETWEEN STRINGERS 8R-9R AT BS 827, BS 867 AND BS 787. REPAIRED FRAMES PER SWA ER NR 99-0168.

Part: FRAME — CRACKED (BS 907, 787 ,747)

DURING SCHEDULED D-CHECK, FOUND 3 FRAMES CRACKED BETWEEN STRINGERS 8L-9L AT BS 907, BS 787 AND BS 747. REPAIRED FRAMES PER SWA ER NR 99-0168.

Part: WEB — CORRODED (BS 500)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB AT BS 500-500A RBL 65, WL 208. REPLACED WEB SECTION PER SRM.

Part: WEB — CORRODED (BS 798)

DURING SCHEDULED D-CHECK, FOUND CORRODED CREASE WEB, BS 798, RBL 67, WL 208. REPLACED WEB PER SRM.

Part: BULKHEAD WEB — CRACKED (BS178)

DURING SCHEDULED D-CHECK, FOUND 2 CRACKS AT BS 178 BULKHEAD WEB, RBL 4.7 AND RBL 6.7, WL 211. REPAIRED BULKHEAD PER SRM.

Part: FRAME — CRACKED (BS 380-400)

DURING SCHEDULED D-CHECK, FOUND 2 FRAMES CRACKED BETWEEN STRINGERS 8L-9L, FS 380 AND 400. REPAIRED PER SRM 53-00-07-2 AND 51-40-02-0.

Part: FRAME — CRACKED (BS 440 & 500)

DURING SCHEDULED D-CHECK, FOUND 2 FRAMES CRACKED BETWEEN STRINGERS 8L-9L AT BS 440, BS 500A. REPAIRED FRAMES PER SWA ER NR 99-0168.

Part: BLKHD STIFFENER — CRACKED (BS 663)

DURING SCHEDULED D-CHECK, FOUND CRACK ON VERTICAL STIFFENER BS 663 BULKHEAD, WL 178, RBL 6. REPLACED PART PER SRM.

Part: BEAM — CRACKED (VERT STAB)

DURING SCHEDULED D-CHECK, FOUND LEFT VERTICAL STAB TRAILING EDGE BEAM CRACKED 15 FROM BOTTOM OF STAB. REPLACED BEAM SECTION FROM STA 13.33 TO 141.52 PER SRM.

Part: SHEAR TIE — CRACKED (BS 360)

DURING SCHEDULED D-CHECK, FOUND CRACKED SHEAR TIE BS 360, STR 14R. REPAIRED PART PER SRM 53-00-07, REPAIR 1, FIGURE 207.

Part: BLANKET — TORN (OVERWING DOORS)

DURING SCHEDULED D-CHECK, FOUND LEFT AND RIGHT OVERWING EXIT HATCHES INSULATION BLANKETS TORN AND CAUGHT ON FWD AND AFT SIDE LATCH ROLLERS. REPAIRED BLANKETS PER MM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND 4 CRACKS AT STA 178 BULKHEAD, WL 188 AND 207, RBL 1 TO LBL 1, AND RBL 28.5 TO LBL 28.5. REPAIRED PER SRM 51-20-07, 51-40-05 AND 53-10-08.

Part: STRINGER — CRACKED (BS 500)

DURING SCHEDULED D-CHECK, FOUND STRINGER 16R CRACKED AT BS 500C. REPAIRED STRINGER PER SRM.

Part: SHEAR TIE — CRACKED (BS 360)

DURING SCHEDULED D-CHECK, FOUND CRACKED SHEAR TIE BETWEEN STRINGER 14 AND 15 BS 360 LT SIDE. REPLACED SHEAR TIE PER SRM.

Part: CLIP — CRACKED (BS 277)

DURING SCHEDULED D-CHECK, CRACKED STRINGER CLIP AT BS 277, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER — CRACKED (BS 360)

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CHANNEL STR 14L, BS 360. REMOVED AND REPLACED STRINGER CHANNEL PER SRM.

Part: SHEAR TIE — CRACKED (BS 360)

DURING SCHEDULED D-CHECK, FOUND CRACKED SHEAR TIE BETWEEN STRINGER 13 AND 14, BS 360 LT. REMOVED SHEAR TIE, FABRICATED NEW SHEAR TIE, ALODINED AND PRIMED, INSTALLED NEW SHEAR TIE PER SRM.

Part: FLOORBEAM — CORRODED (BS 344)

DURING SCHEDULED D-CHECK, FOUND BS 344 FLOORBEAM HAS SURFACE CORROSION ON TOP SIDE AND BOTTOM SIDE OF UPPER CHORD BL 0, RBL 1.5, LBL 7, WL 208. BLENDED CORROSION REMOVED SECTION THAT WAS OUT OF LIMITS, FABRICATED REPAIR PARTS, ALODINED AND PRIMED AND INSTALLED. ALL WORK DONE PER SRM.

Part: FITTING — CORRODED (LT MLG)

DURING SCHEDULED D-CHECK, FOUND LT MLG AFT STABILIZER BEAM FITTING CORRODED. REMOVED AND REPLACED PER BOEING M/M.

Part: SHEAR TIE — CRACKED (BS 360)

DURING SCHEDULED D-CHECK, FOUND CRACKED SHEAR TIE BETWEEN STRINGER 14 AND 15 BS 360 LT SIDE. REPLACED SHEAR TIE PER SRM.

Part: SPAR — CRACKED (RT WING)

DURING SCHEDULED D-CHECK, FOUND DURING NDI INSPECTION, CRACK IN RIGHT WING REAR SPAR UPPER CHORD AT LOWER ROW OR VERTICAL FLANGE, FIRST HOLE I/B OF MLG BEAM FITTING CUTOUT. REMOVED CRACK FROM RIGHT WING UPPER SPAR CHORD ON LOWER ROW FIRST INBOARD HOLE OF MAIN LANDING GEAR BEAM FITTING BY OVERSIZING HOLE. INSTALLED FASTENERS PER TRAMCO EWO 99-0175.

Part: WEB — CORRODED (BS 986.5)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON WEB AT BS 986.5 - 993, RBL 45, WL 208. REMOVED CORROSION, MAX MATERIAL. REMOVED 4 BY 3 BY.013 OUT OF LIMITS PER SRM. REMOVED WEB BS 986.5-993, WL 208, RBL 45. DRILLED UP, ALODINED, PRIMED AND INSTALLED NEW WEB PER SRM.

Part: FLOORBEAM — CRACKED (BS 947)

DURING SCHEDULED D-CHECK, FOUND BS 947 FLOORBEAM IS CRACKED AT LT BL 54, WL 208. CUT OUT CRACK, FABRICATED REPAIR PARTS, LOCATED AND DRILLED REPAIR PARTS. ALODINED, PRIMED, SEALED AND INSTALLED REPAIR SECTION, STRAPS AND ANGLES PER SRM.

Part: WEB — CORRODED (BS 295-328)

DURING SCHEDULED D-CHECK, WEB BS 295-328, RBL 62, WL 208 HAS CORROSION. REMOVED CORROSION ON WEB AT BS 295-328, RBL 62, WL 208. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-1 FIG 101. REMOVED DAMAGED WEB AND FABRICATED, DRILLED UP, ALODINED, PRIMED AND INSTALLED REPLACEMENT WEB PER SRM.

Part: FLOORBEAM — CORRODED (BS 947.5)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 947.5 AT LBL 54. REPAIRED PER BOEING SRM.

Part: SHEAR TIE — CRACKED (BS 360)

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STRINGERS 13 AND 14L. REPAIRED PER BOEING SRM.

Part: WEB — CORRODED (BS 986.5)

DURING SCHEDULED D-CHECK, FOUND WEB CORROSION AT BS 986.5 AND AT 295-328. REPAIRED PER BOEING SRM.

Part: CLIP — CRACKED (BS 227)

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 227, STRINGER 15R. REPLACED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 986.5)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 986.5 CORRODED AT BL 5, 14.5, 31.5 AND 36. REPAIRED PER BOEING SRM.

Part: SLIDE — LOW PRESS (L1 & L2 DOOR)

DURING SCHEDULED CHECK, FOUND L1 AND 2 SLIDE PRESSURES LOW. REMOVED AND REPLACED BOTH SLIDES PER BOEING M/M.

Part: BULB — FAILED (ROW 7ABC)

DURING SCHEDULED SC CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 7ABC INOP. RELAMPED PER BOEING M/M.

Part: BEAM — CORRODED (COCKPIT)

DURING SCHEDULED C3 CHECK, FOUND CORROSION UNDER NLG VIEW DOOR SUPPORT BEAM. REPAIRED PER BOEING TR NR T1-A53-024.

Part: SKIN — GOUGED (BS 300)

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN GOUGED IN CROWN AREA AT BS 300 BETWEEN S4L AND 5L. REPAIRED PER BOEING SRM.

Part: SKIN — GOUGED (FUSELAGE)

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN GOUGED, APPROX 4 INCHES FWD OF FWD ENTRY DOOR OPENING. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (LT HORZ STAB)

DURING SCHEDULED C4 CHECK, FOUND LEFT HORZI STAB L/E DENTED BEYOND LIMITS. REPAIRED PER BOEING SRM.

Part: CSD — LOW OIL (NR 1)

EN ROUTE, NR 1 CSD BECAME INOPERATIVE. ALSO, NOTED FLUID OVER TOP OF LEFT WING. AIRCRAFT DIVERTED TO ELP AND MADE AN UNEVENTFUL LANDING. SERVICED CSD, FUEL LEAK INSPECTED WITHIN M/M LIMITS.

Part: SKIN — GOUGED (BS 992)

DURING SCHEDULED BC4 CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 992, AT S15R. REPAIRED PER SWA RA 1-353-1577.

Part: SKIN — GOUGED (BS 410)

DURING SCHEDULED BC4 CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 410, AT S14R. REPAIRED PER SWA RA 1-353-1577.