N523SW

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 70,039 hrs · 66,658 cycles

R1 DOOR EXTERIOR EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,859 hrs · 66,450 cycles

FRAME CRACKED AT BS 520, STRINGER 16L. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,431 hrs · 65,947 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 414 TO 415, STRINGER 1L. REPAIRED SKIN IAW ER & EA.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 69,000 hrs · 65,438 cycles

R2 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 68,860 hrs · 65,275 cycles

L1 DOOR EMER EXIT SLIDE EXTERIOR LIGHT INOPERATIVE. R & R LAMP IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,718 hrs · 65,113 cycles

SKIN CRACKED AT BS 420+6, STRINGER 1L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,718 hrs · 65,113 cycles

SKIN CRACKED AT BS 440+5, STRINGER 1L. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,994 hrs · 64,252 cycles

LEFT EMER EXIT LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,994 hrs · 64,252 cycles

LEFT EMER EXIT LIGHTS INOPERATIVE BETWEEN BS 727B TO 927. R & R BATTERY PACK IAW AMM.

Part: ANGLE — CRACKED (TE FLAP) · airframe 67,994 hrs · 64,252 cycles

LEFT WING NR 3 FLAP TRACK FAIRING INTERNAL ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

FUSELAGE STRINGER CRACKED AT STATION 452, STRINGER 16R. REPAIRED STRINGER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

TIE CLIP CRACKED AT BS 986.5, STRINGER 22L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

TIE CLIP CRACKED AT BS 986.5, STRINGER 20L. R & R TIE CLIP IAW SRM & DWG.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 67,994 hrs · 64,252 cycles

AFT CARGO DOOR D BEAM AFT END CRACKED. REPAIRED D BEAM IAW EA.

Part: STRUCTURE — CRACKED (CARGO BAY) · airframe 67,994 hrs · 64,252 cycles

AFT CARGO COMPARTMENT AFT LOWER END T CHORD CRACKED AT BS 846.14. REPAIRED T CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

FRAME INNER CHORD CRACKED AT BS 348.2, STRINGER 17L. REPAIRED CHORD IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

STRINGER SPLICE CHANNEL CRACKED AT BS 908, STRINGER 6R. R & R CHANNEL IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

STRINGER CRACKED BETWEEN BS 908 TO 927 STRINGER 19R. R & R STRINGER IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

FRAME CRACKED AT BS 986, STRINGER 19L. R & R FRAME IAW EO & EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 67,994 hrs · 64,252 cycles

RIGHT WING OTBD AFT FLAP LOWER SKIN DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 67,994 hrs · 64,252 cycles

LEFT WING INBD AFT FLAP DELAMINATED ON UPPER SKIN. REPAIRED AFT FLAP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

FRAME OUTER CHORD CRACKED AT BS 452, BETWEEN STRINGER 19R TO 20R. REPAIRED FRAME IAW EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 67,994 hrs · 64,252 cycles

RIGHT WING INBD AFT FLAP DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

ELECTRONICS EQUIPMENT COMPARTMENT SUPPORT BRACKET CRACKED AT BS 294.5 STRINGER 23L. R & R BRACKET IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

SPLICE CHANNEL CRACKED AT BS360, STRINGER 4L. R & R CHANNEL IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

SPLICE ANGLE CRACKED AT BS 540 BETWEEN STRINGER 21R TO 22R. R & R ANGLE IAW EA & EO.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

INTERCOSTAL CRACKED AT BS 540, BETWEEN BL 0 TO LBL 24.75. R & R INTERCOSTAL IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

TIE CLIP CRACKED AT BS 380 STRINGER 22L. R & R TIE CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

SPLICE ANGLE CRACKED AT BS 540 BETWEEN STRINGER 21L TO 22L. R & R ANGLE IAW EA & EO.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

INTERCOSTAL CRACKED AT BS 540 BETWEEN BL 0 TO RBL 24.75. R & R INTERCOSTAL IAW SRM & DWG.

Part: LENS — BROKEN (CABIN) · airframe 67,994 hrs · 64,252 cycles

EMERGENCY EXIT LIGHT LENS ON SIDEWALL PANEL 2329Z BROKEN. R & R LENS IAW AMM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

ELECTRONICS EQUIPMENT COMPARTMENT UPPER SURFACE STRAP CRACKED AT BS 344, RBL 47. R & R STRAP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

ANGLE CRACKED AT STATION 312, STRINGER 26R TO 27R. R & R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

SUPPORT ANGLE CRACKED AT BS 360 STRINGER 10L. R & R ANGLE IAW SRM & DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

STRINGER CRACKED AT BS 328, STRINGER 20R. REPAIRED STRINGER IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

TIE CLIP CRACKED AT BS 420 STRINGER 9L. R & R TIE CLIP IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

FRAME CRACKED AT BS 360, STRINGER 20R. REPAIRED FRAME IAW EA.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

ANGLE SUPPORT CRACKED AT BS 294.5+3 BETWEEN STRINGER 26R TO 27R. R & R SUPPORT IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

FRAME WEB CRACKED AT BS 452, BETWEEN STRINGER 19R TO 20R. REPAIRED WEB IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

STRINGER CLIP CRACKED AT STATION 727A STRINGER 24R. R & R CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

FRAME OUTER CHORD CRACKED AT BS 188, STRINGER 17L. REPAIRED FRAME IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

ANGLE CLIP CRACKED AT BS 727 RBL 45.5. R & R ANGLE CLIP IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

WEB CORRODED BETWEEN BS 807 TO 827, STRINGER 17R. R & R WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

FRAME OUTER CHORD CRACKED AT BS 188, STRINGER 17R. REPAIRED FRAME IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

ANGLE CRACKED AT BS 540, BETWEEN STRINGER 22L TO 28L. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

TIE CLIP CRACKED AT BS 787 STRINGER 22R. R & R TIE CLIP IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

WEB CORRODED BETWEEN BS 847 TO 867, STRINGER 17R. R & R WEB IAW EO & EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

SUPPORT ANGLE CRACKED AT BS 787 STRINGER 18R. REPAIRED ANGLE IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

WEB CORRODED BETWEEN BS 827 TO 847, STRINGER 17R. R & R WEB IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

ANGLE CRACKED AT STATION 540, STRINGER 24R. R & R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

SUPPORT ANGLE CRACKED AT BS 727 BETWEEN STRINGER 27L TO 27R. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

AFT CARGO COMPARTMENT ANGLE CORRODED AT BS 787 BETWEEN STRINGER 24L TO 25L. R & R ANGLE IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

STRINGER CLIP CRACKED AT STATION 967, STRINGER 24L. R & R CLIP IAW SRM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

SUPPORT BRACKET CRACKED AT BS 907 BETWEEN STRINGER 1 TO 2L. R & R BRACKET IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

STRINGER CLIP CRACKED AT STATION 927 STRINGER 25R. R & R CLIP IAW SRM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

SUPPORT BRACKET CRACKED AT BS 907 BETWEEN STRINGER 1 TO 2R. R & R BRACKET IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

AFT CARGO COMPARTMENT FITTING CRACKED AT BS 727, STRINGER 27L. R & R FITTING IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

TIE CLIP CRACKED AT BS 727A STRINGER 25L. R & R TIE CLIP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

TIE CLIP CRACKED AT BS 727B STRINGER 20L. R & R TIE CLIP IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

FORWARD CARGO COMPARTMENT SUPPORT ANGLE CRACKED AT BS 482B, STRINGER 19R. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

WEB ANGLE CRACKED AT BS 400 BETWEEN STRINGER 26L TO 25L. R & R ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

FORWARD ENTRY DOOR SKIN CUT OUT CRACKED AT BS 345, STRINGER 16L, LOWER CORNER. REPAIRED SKIN IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

TIE CLIP CRACKED AT BS 947.5 STRINGER 25R. R & R TIE CLIP IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

MAIN WW SUPPORT ANGLE CRACKED AT BS 679.65, RBL 68. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

ANGLE CRACKED AT STATION 947.5, STRINGER 25L. R & R ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 460, STRINGER 22L. R & R ANGLE IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

AFT CARGO COMPARTMENT FITTING CRACKED AT BS 727 STRINGER 27L. R & R FITTING IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

SKIN CRACKED AT BS 360 STRINGER 2L. REPAIRED SKIN IAW EA.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

L2 DOOR CUT OUT CTR SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

SKIN CRACKED AT BS 380+14, STRINGER 16R. REPAIRED SKIN IAW EO & EA.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

L1 DOOR CUT OUT FWD CORNER SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 24.5 INBD SIDE. REPAIRED SEAT TRACK IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

FRAME CRACKED AT BS 482A, BETWEEN STRINGER 21L TO 22L. REPAIRED FRAME IAW EO & EA.

Part: DOUBLER — CRACKED (SERVICE DOOR) · airframe 67,994 hrs · 64,252 cycles

FORWARD LAVATORY SERVICE DOOR LOWER LOBE FUSELAGE CRACKED. REPAIRED DOUBLER IAW EA & EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

FRAME CRACKED AT BS 482A, BETWEEN STRINGER 21R TO 22R. REPAIRED FRAME IAW EO & EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

CHORD CRACKED AT BS 727, STRINGER 18A RT SIDE, FWD LOWER HOLE. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

CHORD CRACKED AT BS 727, STRINGER 18A LT SIDE, AFT LOWER HOLE. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

CHORD CRACKED AT BS 727, STRINGER 18A RT SIDE, AFT LOWER HOLE. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

CHORD CRACKED AT BS 727, STRINGER 18A LT SIDE, FWD LOWER HOLE. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

CHORD CRACKED AT BS 727, STRINGER 18A LT SIDE, AFT UPPER HOLE. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 67,994 hrs · 64,252 cycles

CHORD CRACKED AT BS 727, STRINGER 18A LT SIDE, FWD UPPER HOLE. REPAIRED CHORD IAW EA.

Part: BATTERY — DISCHARGED (CABIN) · airframe 67,797 hrs · 64,026 cycles

R2 DOOR EMER LIGHT INOPERATIVE. R & R BATTERY ASSEMBLY IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,750 hrs · 63,976 cycles

AFT CABIN EMER LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 67,431 hrs · 63,622 cycles

RIGHT EMER EXIT LIGHT LENS LOOSE. SECURED LENS IAW SIP.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 67,414 hrs · 63,605 cycles

AIR TURN BACK FLIGHT ATTENDANTS REPORTED SMOKE SMELL THROUGHOUT CABIN. R & R GASPER FAN IAW MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 67,302 hrs · 63,493 cycles

STRINGER CRACKED AT BS 394, STRINGER 16L. REPAIRED STRINGER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,302 hrs · 63,493 cycles

EXTERNAL SKIN CRACKED BETWEEN BS 375.5 TO 378, STRINGER 15L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,302 hrs · 63,493 cycles

FUSELAGE SKIN CRACKED AT STATION 925, STRINGER 25R. REPAIRED SKIN IAW SRM & EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 67,302 hrs · 63,493 cycles

SHEAR TIE CRACKED AT BS 360, BETWEEN STRINGER 14L TO 15L. R & R SHEAR TIE IAW SRM & DWG.

Part: LENS — LOOSE (CABIN) · airframe 67,055 hrs · 63,235 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS IAW MM.

Part: LENS — UNSECURE (CABIN) · airframe 65,879 hrs · 62,001 cycles

RT OVERWING EMERGENCY EXIT LIGHT LENS OVER DOOR FELL OFF. SECURED LENS IAW EA.

Part: LENS — UNSECURE (CABIN) · airframe 65,879 hrs · 62,001 cycles

RT OVER WING EMERGENCY EXIT LIGHT LENS OVER DOOR FELL OFF. REPAIRED LENS IAW MM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 15R. R & R TIE CLIP IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

TIE CLIP CRACKED AT BS 400, STRINGER 16R. R & R TIE CLIP IAW SRM & DRAWING.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

STRINGER CRACKED AT BS 400, STRINGER 15R. REPAIRED STRINGER IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

FRAME CRACKED AT BS 380, BETWEEN STRINGER 14R TO STRINGER 15R. REPAIRED FRAME IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

STRINGER CRACKED AT BS 877+8, STRINGER 4R. REPAIRED STRINGER IAW SRM.

Part: STIFFENER — CRACKED (RT WING) · airframe 65,721 hrs · 61,845 cycles

RT WING STIFFENER CRACKED ON FAIRING TRACK 6 INBD WBL 183.40. R & R STIFFENER IAW SRM & DRAWING.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

STRINGER CRACKED BETWEEN BS 367 TO BS 375, STRINGER 15R. REPAIRED STRINGER IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

SHEAR TIE CRACKED AT BS 360, STRINGER 14R. REPAIRED SHEAR TIE IAW SRM & DRAWING.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

STRINGER SPLICE CRACKED AT BS 907, STRINGER 4R. R & R SPLICE IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

FUSELAGE SKIN CRACKED AT BS 360, BETWEEN STRINGER 3R TO STRINGER 4R. REPAIRED SKIN IAW EA.

Part: SUPPORT ANGLE — CRACKED (FLAP TRACK) · airframe 65,721 hrs · 61,845 cycles

RT WING NR 6 FLAP TRACK INBD SIDE SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

TIE CLIP CRACKED AT BS 1006, STRINGER 23L. R & R TIE CLIP IAW SRM & DRAWING.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

STRINGER SPLICE CRACKED AT BS 360, STRINGER 4R. R & R SPLICE IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

STRAP CRACKED BETWEEN BS 947.5 TO BS 967, BETWEEN STRINGER 24L TO STRINGER 26L. R & R STRAP IAW SRM & DRAWING.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

STRINGER SPLICE CRACKED AT BS 360, STRINGER 5R. R & R SPLICE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

TAIL CONE DUCT EXHAUST ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

STRINGER SPLICE CRACKED AT BS 360, STRINGER 6R. R & R SPLICE IAW SRM & DRAWING.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

SHEAR TIE CRACKED AT BS 960, BETWEEN STRINGER 21L TO STRINGER 22L. R & R SHEAR TIE IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

SHEAR TIE CRACKED AT BS 482A, BETWEEN STRINGER 28L TO STRINGER 28R. REPAIRED FRAME IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

INTERNAL STRUCTURE CRACKED AT BS 348.2, STRINGER 15L. R & R CLIP IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

FRAME WEB CRACKED AT BS 348.2, STRINGER 16L. REPAIRED FRAME IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

INTERNAL ANGLE CRACKED AT BS 348.2, STRINGER 16L. R & R ANGLE IAW SRM & DRAWING.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

FWD CARGO COMPARTMENT DOOR CUTOUT CRACKED AT BS 452.4, STRINGER 25R. REPAIRED CUTOUT IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

CLIP CRACKED AT BS 348.2, STRINGER 15L. R & R CLIP IAW SRM & DRAWING.

Part: FLAP — DELAMINATED (RT WING) · airframe 65,721 hrs · 61,845 cycles

RT WING FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: COVER — BROKEN (CABIN) · airframe 65,721 hrs · 61,845 cycles

BROKEN COVER OF EMERGENCY LIGHT AT AFT LAVATORY. R & R COVER IAW AMM.

Part: COVER — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

AFT GALLEY DOOR CUTOUT CRACKED ON COVER LOCATED AT BS 993. R & R CUTOUT IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

FUSELAGE SKIN CRACKED AT BS 907, STRINGER 3R. REPAIRED SKIN IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

L1 DOOR UPPER CORNER STRAP CRACKED BETWEEN BS 303.5 TO BS 328, BETWEEN STRINGER 6L TO STRINGER 7L. R & R STRAP IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

FRAME CRACKED AT BS 480, BETWEEN STRINGER 15L TO STRINGER 16L. REPAIRED FRAME IAW SRM.

Part: FITTING — CRACKED (HORIZ STAB) · airframe 65,721 hrs · 61,845 cycles

CENTER SECTION HORIZONTAL STABILIZER RT UPPER CHORD FITTING CRACKED T LEVEL BS 1121. R & R FITTING IAW SRM & DRAWING.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

SHEAR TIE CRACKED AT BS 277, BETWEEN STRINGER 9L TO STRINGER 10L. R &R SHEAR TIE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (RT WING) · airframe 65,721 hrs · 61,845 cycles

RT WING TE ANGLE CRACKED AT WS 537.806. R & R ANGLE IAW SRM & DRAWING.

Part: ANGLE — CRACKED (LT WING) · airframe 65,721 hrs · 61,845 cycles

LT WING REAR SPAR ANGLE CRACKED AT WBL 71.24 + 15.5. R & R ANGLE IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

TIE CLIP CRACKED AT BS 294.5, STRINGER 12L.. R & R TIE CLIP IAW SRM & DRAWING.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

R1 DOOR UPPER CORNER CUTOUT CRACKED BETWEEN BS 294.5 TO BS 294.5+ 10, BETWEEN STRINGER 7R TO STRINGER 8R. R & R REVEAL IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

STRAP CRACKED AT BS 344, BETWEEN STRINGER 10L TO STRINGER 15L. R & R STRAP IAW SRM & DRAWING.

Part: ANGLE — CRACKED (RT WING) · airframe 65,721 hrs · 61,845 cycles

RT WING TE ANGLE CRACKED AT WBL 204.40. R & R ANGLE IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

FRAME CRACKED AT BS 277, STRINGER 16R. R & R FRAME IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 65,721 hrs · 61,845 cycles

RT WING TE SUPPORT ANGLE CRACKED AT WS 537.806. R & R ANGLE IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

FRAME CRACKED AT BS 277, BETWEEN STRINGER 15L & STRINGER 16L. REPAIRED FRAME IAW EO & EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

WEB CRACKED BETWEEN BS 294.5 TO BS 303.9, STRINGER 15L. R & R WEB IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

FWD GALLEY DOOR FITTING CRACKED AT BS 294.5, STRINGER 8R. R & R FITTING IAW SRM & DRAWING.

Part: BEAM — CORRODED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

FWD CABIN FLOOR STRUCTURE LOWER SURFACE OF CHORD BEAM CORRODED AT BS 312, BETWEEN RBL 12 & RBL 50. REPAIRED BEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

FLOOR BEAM CORRODED AT BS 312, BETWEEN RBL 11 TO LBL 20. REPAIRED BEAM IAW SRM.

Part: STIFFENER — CRACKED (TE FLAP) · airframe 65,721 hrs · 61,845 cycles

LT WING NR 3 INBD FLAP TRACK FAIRING STIFFENER CRACKED. R & R STIFFENER IAW SRM & DRAWING.

Part: LINK — CRACKED (TE FLAP) · airframe 65,721 hrs · 61,845 cycles

LT WING OTBD FORE FLAP CENTER LINK CRACKED. R & R LINK IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 65,721 hrs · 61,845 cycles

RT WING NR 6 FAIRING TRACK SUPPORT ANGLE CRACKED AT INBD WBL 183.40. R & R ANGLE IAW SRM & DRAWING.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 65,721 hrs · 61,845 cycles

MAIN WW PRESSURE DECK CRACKED AT BS 663.75+8.5, LBL 45.50-5. REPAIRED WEB IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 65,721 hrs · 61,845 cycles

MAIN WW PRESSURE DECK CRACKED AT BS 663.75+8, LBL 45.50-6. REPAIRED WEB IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 65,721 hrs · 61,845 cycles

MAIN WW PRESSURE DECK CRACKED AT BS 663.75, LBL 45.5-6". REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

FUSELAGE SKIN CRACKED AT BS 360, STRINGER 5R. REPAIRED SKIN IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 65,721 hrs · 61,845 cycles

LT WING OTBD AFT FLAP DELAMINATED. R & R AFT FLAP IAW AMM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 65,721 hrs · 61,845 cycles

MAIN WW PRESSURE DECK CRACKED AT BS 663.75, RBL 24.5-3. REPAIRED DECK IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

FUSELAGE SKIN CRACKED AT BS 360+12, STRINGER 15R. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

FUSELAGE SKIN CRACKED AT BS 908+14, STRINGER 23L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

FUSELAGE SKIN CRACKED AT BS 380+13, STRINGER 15R. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

FUSELAGE SKIN CRACKED AT BS 787+3.5, STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

SKIN CRACKED AT BS 747+ 4.5, STRINGER 25L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

SKIN CRACKED AT BS 460+17, STRINGER 16L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

FUSELAGE SKIN CRACKED AT BS 787+13, STRINGER 24L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

FUSELAGE SKIN CRACKED AT BS 747+13, STRINGER 18L. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

EXHAUST TAIL CONE ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

FUSELAGE SKIN CRACKED AT BS 787+12.5, STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

FUSELAGE SKIN CRACKED AT BS 827+1, STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

FUSELAGE SKIN CRACKED AT BS 440+6, STRINGER 16R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

SKIN CRACKED AT BS 887+ 13, STRINGER 25R. REPAIRED SKIN IAW SRM.

Part: FLAP — CRACKED (RT WING) · airframe 65,721 hrs · 61,845 cycles

RT WING KRUGER FLAP CRACKED LE STATION 208.00. REPAIRED FLAP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

FUSELAGE SKIN CRACKED AT BS 807+13.5, STRINGER 23L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

FUSELAGE SKIN CRACKED AT BS 747+6.5, STRINGER 19L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

SKIN CRACKED AT BS 867+ 6.5, STRINGER 24R. REPAIRED SKIN IAW SRM.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 65,721 hrs · 61,845 cycles

AFT CARGO COMPARTMENT DOOR CENTER SCUFF PLATE ON CUT OUT CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 65,269 hrs · 61,328 cycles

L1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,268 hrs · 61,327 cycles

AFT LOWER FS AFT OF AFT CARGO DOOR CRACKED. REPAIRED SKIN IAW SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 65,072 hrs · 61,106 cycles

AFT EMERGENCY FLASHLIGHT BATTERY INDICATOR LIGHT INOPERATIVE. R&R BATTERY IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 64,916 hrs · 60,924 cycles

FWD ENTRY EMERGENCY EXIT LENS BROKEN. R & R LENS IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,861 hrs · 60,864 cycles

EMERGENCY EXIT LIGHTS IN AFT GALLEY INOP. R & R BATTERY PACK ASSY IAW AMM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 64,159 hrs · 60,155 cycles

AFT SERVICE DOOR EMERGENCY EXIT SLIDE IS LOOSE. TIGHTEN AFT SERVICE DOOR EMERGENCY EXIT SLIDE ATTACH BOLTS PER MM.

Part: CABLE — MISROUTED (L2 DOOR) · airframe 64,159 hrs · 60,155 cycles

AFT ENTRY DOOR SLIDE CABLE IS ROUTED INCORRECTLY. REROUTED CABLE PER TASK CARD MT325-61-06.

Part: LENS — LOOSE (CABIN) · airframe 64,159 hrs · 60,155 cycles

PASSENGER CABIN EMERGENCY LIGHT LENS AT 11ABC IS UNSECURED. RE-SECURED PER MM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 64,150 hrs · 60,149 cycles

FORWARD ENTRY DOOR, LOWER HINGE, H-STRAP IS CRACKED. REMOVED AND REPLACED H-STRAP AT FWD PASSENGER ENTRY DOOR BS 290-303 BETWEEN STR 13L & 14L IAW SRM 51-40-02-0G-0 AND DWG 65-17684. 92115U, 08FEB13

Part: SKIN — DELAMINATED (TE FLAP) · airframe 64,150 hrs · 60,149 cycles

LT WING I/B FORE FLAP UPPER SURFACE IS DELAMINATED 47" O/B FROM I/B END AND 8" FWD FROM T/E. REPAIRED LT/WING I/B FOREFLAP UPPER SURFACE DISBOND 47" FROM I/B END, 8" FROM T/E IAW SRM 51-70-10-2R-0

Part: SKIN — DELAMINATED (TE FLAP) · airframe 64,150 hrs · 60,149 cycles

RT WING I/B FORE FLAP UPPER SURFACE IS DELAMINATED 35" I/B FROM O/B END AND 8" FWD FROM T/E. REPAIRED RT/WING FORE FLAP UPPER SURFACE DISBOND, 35" FROM O/B END, 8" FROM T/E, IAW SRM 51-70-10-2R-0

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 64,150 hrs · 60,149 cycles

FAIRING ATTACH ANGLE CRACKED AT BS 727 BULKHEAD RBL 12. R & R ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,150 hrs · 60,149 cycles

A .75 INCH SUB-SURFACE CHEM-MILL CRACK AT BS 434.5 - BS 435.25 ABOVE STG-26L, ZERO INCHES OPEN TO SURFACE. NDT MARKED THE ENDS OF CRACK. REPAIRED CHEM-MILL CRACK AT BS 434.5 - BS 435.25 ABOVE STR 26L IAW SRM 53-00-01-2R-31.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,150 hrs · 60,149 cycles

A 2 INCH SUB-SURFACE CHEM-MILL CRACK FWD SIDE OF BS 908, 3 INCHES BELOW STR-3L, ZERO INCHES OPEN TO SURFACE. NDT MARKED THE END OF CRACK, THE OTHER END OF THE CRACK EXTENDS BELOW DOUBLER. REPAIRED CHEM-MILL CRACK BS 908, 3 INCHES BELOW STR 3L IAW ER 13-01432 AND EA 1-553-21705. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SLIDE — UNSECURE (L2 DOOR) · airframe 63,959 hrs · 59,943 cycles

AFT ENTRY DOOR L2 SIDE UNSECURED. REPACKED L2 DOOR SLIDE PER MX TASK 325-61-06. A/C OKAY FOR SERVICE.

Part: SWITCH — FAULTY (NLG) · airframe 63,718 hrs · 59,731 cycles

NOSE LANDING GEAR RED LIGHT REMAINS ILLUMINATED WITH GREEN LIGHT AS WELL. REMOVED AND REPLACED SWITCH PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,458 hrs · 59,448 cycles

SKIN CRACKED AT BS 927, STR 25R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,458 hrs · 59,448 cycles

SKIN CRACKED AT BS 482B+14, STR 16L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,458 hrs · 59,448 cycles

FUSELAGE SKIN CRACKED AT BS 927+7, STR 24L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,458 hrs · 59,448 cycles

SKIN CRACKED AT BS 927+5, STR 21L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,458 hrs · 59,448 cycles

FUSELAGE SKIN CRACKED AT BS 927+6, STR 21R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,458 hrs · 59,448 cycles

FUSELAGE SKIN CRACKED AT BS 927+7, STR 25R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,458 hrs · 59,448 cycles

SKIN CRACKED AT BS 787+8, STR 18L. REPAIRED SKIN IAW SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 63,375 hrs · 59,384 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 63,375 hrs · 59,384 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 62,732 hrs · 58,976 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER M/M.

Part: LENS — LOOSE (CABIN) · airframe 62,467 hrs · 58,800 cycles

LEFT BULLNOSE EMERGENCY LIGHT LENS LOOSE BETWEEN ROW 10 TO ROW 11. SECURED LENS PER MM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 62,467 hrs · 58,800 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT SIGN LENS LOOSE. REMOVED AND REPLACED SIGN PER MM.

Part: LENS — MISSING (CABIN) · airframe 62,085 hrs · 58,528 cycles

RT EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW 9. INSTALLED NEW LENS IAW M/M.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 61,980 hrs · 58,456 cycles

R1 DOOR ESCAPE SLIDE PRESS INDICATION IN RED. REMOVED AND REPLACED R1 DOOR SLIDE ASSY PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 61,798 hrs · 58,334 cycles

FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT IAW MM.

Part: LIGHT — BROKEN (CABIN) · airframe 61,048 hrs · 57,859 cycles

FWD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — DETERIORATED (CABIN) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND EEPLS DETERIORATED. REMOVED AND REPLACED EEPLS STRIPS PER DRAWING.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND CRACK ON HOLE AT KEEL OUTBD FLANGE OF KEEL BEAM BS 540, STR 28L. REPAIRED FLANGE OF KEEL BEAM PER DOC.

Part: WEB — CRACKED (COCKPIT) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND COCKPIT FLOOR WEB CUTOUT CRACKED AT BS 246+1 TO BS 251.6, RBL 23 TO RBL 16.5. REPAIRED WEB PER EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 685+6, LBL 24.5. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 859, LBL 3. REPAIRED CHANNEL IAW EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 859, LBL 12.5. REPAIRED CHANNEL IAW EA.

Part: RIB — CRACKED (HORIZ STAB) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND LT HORIZONTAL STABILIZER RIB CRACKED AT STA 105.26. REMOVED AND REPLACED RIB IAW SRM AND DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT CLIP CORRODED AT BS 794.3, STR 26R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND WEB CRACKED BETWEEN BS 344 TO BS 360, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND STIFFENER CRACKED AT BS 727, RBL 8.10. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO COMPARTMENT ANGLE CLIP CORRODED AT BS 847, STR 26R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 312 TO BS 325, STR 28R. REMOVED AND REPLACED STRINGER IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,006 hrs · 57,836 cycles

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

Part: PLATE — DAMAGED (R2 DOOR) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND DAMAGED ADAPTED PLATE AND SHIM AT ESCAPE SLIDE FLOOR BRACKET AFT RT SIDE. R&R PLATE IAW MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,006 hrs · 57,836 cycles

DURING SCHDULED 20Y CHECK, FOUND ANGLE CRACKED AT BS 328, STR 21L. R&R ANGLE IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,006 hrs · 57,836 cycles

DURING SCHDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 26L. R&R CLIP IAW SRM AND DWG.

Part: PLATE — DAMAGED (L2 DOOR) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND DAMAGED ADAPTED PLATE AND SHIM AT ESCAPE SLIDE FLOOR BRACKET AFT LT SIDE. R&R PLATE IAW MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,006 hrs · 57,836 cycles

DURING SCHDULED 20Y CHECK, FOUND ANGLE CRACKED AT BS 312, STR 21L. R&R ANGLE IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 20R. R&R CLIP PER SRM AND DWG.

Part: BRACKET — DAMAGED (R2 DOOR) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE R/H FLOOR BRACKET DAMAGED. R&R BRACKET IAW MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 26R. R&R CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 27L. R&R CLIP PER SRM AND DWG.

Part: BRACKET — DAMAGED (R2 DOOR) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LT FLOOR BRACKET DAMAGED. R&R BRACKET IAW MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND DELAMINATION ON I/B EDGE OF LT SLAT. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — CRACKED (GALLEY DOOR) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND CRACK ON AFT LWR CORNER OF GALLEY DOOR, BS 332.1-3, STR 17R-3. REPAIRED SKIN PER DOC.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND CRACK ON WEB LWR CHORD BS 670+1 AND BBL 0.07 LONG FLOORBEAM. REPAIRED WEB LOC ON LWR CHORD PER DOC.

Part: SKIN — CRACKED (GALLEY DOOR) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND CRACK ON AFT LWR CORNER OF GALLEY DOOR, BS 332.0-4, STR 17R-2. REPAIRED SKIN PER DOC.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND CRACK UPPER CHORD BS 661 ABD BBL 0.07 LONG FLOORBEAM. REPAIRED FLOORBEAM PER AE.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND KEEL BEAM CORROSION STA 482B+3.5, STR 28L IN FWD CARGO COMPARTMENT. REPAIRED CORROSION PER SWA DOC.

Part: FLAP — DELAMINATED (WING) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND DELAMINATION ON I/B SIDE OF O/B AFT FLAP. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,006 hrs · 57,836 cycles

DURING SCHEDULED 20Y CHECK, FOUND EXTERNAL FUSELAGE SKIN CRACK BS 520+2, STR 28R. REPAIRED FUSELAGE CRACK PER DOC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,926 hrs · 57,791 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 947.5+12, STR 21L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,023 hrs · 57,185 cycles

DURING SCHEDULED CV CHECK FOUND, SKIN CRACKED AT BS 520+4, STR 7L. REPAIRED SKIN ER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,876 hrs · 57,080 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 59,740 hrs · 56,988 cycles

R1 DOOR EMERGENCY EXIT COVER LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,334 hrs · 56,723 cycles

DURING SCHEDULED MV2 CHECK FOUND, SKIN CRACKED AT BS 867 + 4, STR 22R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,260 hrs · 55,263 cycles

DURING SCHEDULED OTS CHECK, FOUND R2 DOOR LOWER HINGE CUTOUT CRACKED AT AFT LOWER RADIUS. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 57,260 hrs · 55,263 cycles

DURING SCHEDULED OTS CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,130 hrs · 55,160 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 405, STR 16R. REPAIRED SKIN PER SRM.

Part: COVER — BROKEN (CABIN) · airframe 56,397 hrs · 54,641 cycles

R2 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,321 hrs · 54,586 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,668 hrs · 54,154 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 716, BBL 0. REPAIRED BEAM PER ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,668 hrs · 54,154 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED BETWEEN BS 707 TO BS 708, RBL 24.8. REPAIRED BEAM PER ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,668 hrs · 54,154 cycles

DURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED BETWEEN BS 707 TO BS 708, LBL 24.6. REPAIRED BEAM PER ER.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 55,668 hrs · 54,154 cycles

DURING SCHEDULED 18Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 55,668 hrs · 54,154 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 947, STR 24L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 55,668 hrs · 54,154 cycles

DURING SCHEDULED 18Y CHECK, FOUND STRINGER CORRODED AT BS 967, STR 25L. REMOVED AND REPLACED STRINGER PER SRM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 55,668 hrs · 54,154 cycles

DURING SCHEDULED 18Y CHECK, FOUND R1 DOOR LOWER EMERGENCY EXIT SIGN WIRES LOOSE. SECURED CONNECTORS PER SWPM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 55,668 hrs · 54,154 cycles

DURING SCHEDULED 18Y CHECK, FOUND FWD CARGO DOOR CUTOUT FRAME CRACKED AT BS 400, STR 17R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,668 hrs · 54,154 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 482B LT WIRE PENETRATION HOLE. REPAIRED FRAME PER SRM.

Part: MOUNT FITTING — CRACKED (EVAC SLIDE) · airframe 55,668 hrs · 54,154 cycles

DURING SCHEDULED 18Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD MOUNT FITTING CRACKED. REMOVED AND REPLACED FITTING PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,280 hrs · 53,916 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT ENTRY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,728 hrs · 52,200 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BETWEEN BS 303 TO BS 305. REPAIRED SKIN PER AAR EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,728 hrs · 52,200 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 348, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 52,728 hrs · 52,200 cycles

DURING SCHEDULED SPV CHECK, FOUND RT SIDE EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,728 hrs · 52,200 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 348, STR 16L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 52,728 hrs · 52,200 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 16L. REMOVED AND REPLACED SPLICE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,728 hrs · 52,200 cycles

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

Part: HYDRAULIC LINE — LEAKING (RT MLG) · airframe 52,684 hrs · 52,159 cycles

AIR TURN BACK, ENGINE 'A' HYDRAULIC PUMP LOW PRESSURE LIGHT, ACCOMPANIED BY LOSS OF A SYSTEM HYDRAULIC FLUID TO LESS THAN 1/4 LEVEL. REMOVED AND REPLACED RT MLG ACTUATOR RETURN LINE HOSE ASSY PER MM.

Part: BRACKET — BROKEN (GIRT BAR) · airframe 52,271 hrs · 51,798 cycles

FOUND R2 DOOR SLIDE GIRT BAR CLIP BROKEN. REMOVED AND REPLACED BRACKET PER MM.

Part: FITTING — BROKEN (GIRT BAR) · airframe 52,272 hrs · 51,798 cycles

FOUND R2 DOOR AFT GIRT BAR CLIP BROKEN. R&R BRACKET PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 52,002 hrs · 51,590 cycles

FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 51,305 hrs · 51,086 cycles

L1 DOOR SIDEWALL EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 51,178 hrs · 50,979 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 51,178 hrs · 50,979 cycles

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

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 50,614 hrs · 50,565 cycles

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

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 50,608 hrs · 50,560 cycles

DURING SCHEDULED 16Y CHECK, FOUND FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,608 hrs · 50,560 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 21L. REPAIRED SKIN PER EA.

Part: LENS — MISSING (CABIN) · airframe 50,607 hrs · 50,560 cycles

DURING SCHEDULED 16Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 20 DEF. INSTALLED LENS PER MM.

Part: FITTING — CORRODED (L1 DOOR GIRT BAR) · airframe 50,608 hrs · 52,560 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.

Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 50,608 hrs · 50,560 cycles

DURING SCHEDULED 16Y CHECK, FOUND NLG W/W CEILING PANEL CUTOUT WEB CRACKED AT LBL 7.5. REPAIRED WEB PER ACO.

Part: PRESSURE PANEL — CRACKED (NLG W/W) · airframe 50,608 hrs · 50,560 cycles

DURING SCHEDULED 16Y CHECK, FOUND NLG W/W CEILING PANEL CUTOUT WEB CRACKED AT RBL 7.5. REPAIRED WEB PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,607 hrs · 50,560 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SLAT — CRACKED (LT WING) · airframe 50,607 hrs · 50,560 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,385 hrs · 50,376 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 50,385 hrs · 50,376 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,385 hrs · 50,376 cycles

DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 16 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,385 hrs · 50,376 cycles

DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 22 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 50,385 hrs · 50,376 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,605 hrs · 49,693 cycles

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

Part: STRINGER CLIP — CRACKED (BS 380 S9L) · airframe 49,601 hrs · 49,692 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 440 S8L) · airframe 49,601 hrs · 49,692 cycles

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

Part: STRINGER CLIP — CRACKED (BS 807 S9R) · airframe 49,601 hrs · 49,692 cycles

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

Part: STRINGER CLIP — CRACKED (BS 887 S9R) · airframe 49,601 hrs · 49,692 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 827 S9R) · airframe 49,601 hrs · 49,692 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 847 S9R) · airframe 49,601 hrs · 49,692 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 482B S10L) · airframe 49,601 hrs · 49,692 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482B, STR 10L. REPAIRED FRAME PER SRM AND BOEING DRAWING.

Part: SKIN — CHAFED (BS 826-1006) · airframe 49,601 hrs · 49,692 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE UPPER SKIN CHAFING BETWEEN BS 826 AND BS 1006, BELOW DORSAL FIN. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CRACKED (BS 520 S9R) · airframe 49,601 hrs · 49,692 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 9R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (BS 360 S15L) · airframe 49,601 hrs · 49,692 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 482A S5R) · airframe 49,601 hrs · 49,692 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482A, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 420 S16R) · airframe 49,601 hrs · 49,692 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 727B S8R) · airframe 49,601 hrs · 49,692 cycles

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

Part: CREASE BEAM — CORRODED (BS 639 S17R) · airframe 49,601 hrs · 49,692 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 639, STR 17R. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,601 hrs · 49,692 cycles

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

Part: STRINGER CLIP — CRACKED (BS 482 S4R) · airframe 49,601 hrs · 49,692 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 360 S8L) · airframe 49,601 hrs · 49,692 cycles

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

Part: FRAME — CRACKED (BS 747 S8R) · airframe 49,601 hrs · 49,692 cycles

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

Part: FRAME — CRACKED (BS 400 S9L) · airframe 49,601 hrs · 49,692 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 9L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 482 S8R) · airframe 49,601 hrs · 49,692 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 482B S5R) · airframe 49,601 hrs · 49,692 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 520 S10R) · airframe 49,601 hrs · 49,692 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 400 S8R) · airframe 49,601 hrs · 49,692 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727 S4R) · airframe 49,601 hrs · 49,692 cycles

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

Part: STRINGER CLIP — CRACKED (BS 520 S10R) · airframe 49,601 hrs · 49,692 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 440 S8R) · airframe 49,601 hrs · 49,692 cycles

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

Part: FRAME — CRACKED (BS 827 S8R) · airframe 49,601 hrs · 49,692 cycles

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

Part: FRAME — CRACKED (BS 787 S8R) · airframe 49,601 hrs · 49,692 cycles

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

Part: STRINGER CLIP — CRACKED (BS 400 S8R) · airframe 49,601 hrs · 49,692 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 482A S8L) · airframe 49,601 hrs · 49,692 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 747 S8L) · airframe 49,601 hrs · 49,692 cycles

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

Part: FRAME — CRACKED (BS 787 S16L) · airframe 49,601 hrs · 49,692 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 787, STR 16L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 482 S8L/R) · airframe 49,601 hrs · 49,692 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 787 S8L) · airframe 49,601 hrs · 49,692 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 685 S3L) · airframe 49,601 hrs · 49,692 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,601 hrs · 49,690 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,601 hrs · 49,690 cycles

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

Part: STRINGER CLIP — CRACKED (BS 706 S2R) · airframe 49,601 hrs · 49,642 cycles

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

Part: STRINGER CLIP — CRACKED (BS 706 S3R) · airframe 49,601 hrs · 49,642 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 482A S10L) · airframe 49,489 hrs · 49,583 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 482A, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (BS 497B S10L) · airframe 49,489 hrs · 49,583 cycles

DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 497B, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SHEAR TIE — CRACKED (BS 482A S10L) · airframe 49,489 hrs · 49,583 cycles

DURING SCHEDULED MV3 CHECK, FOUND SHEAR TIE CRACKED AT BS 482A, STR 10L. REPAIRED SHEAR TIE PER SRM.

Part: SIGN — LOOSE (EMERGENCY EXIT) · airframe 49,489 hrs · 49,583 cycles

FWD CABIN EMERGENCY EXIT SIGN ASSY LOOSE. SECURED SIGN ASSY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 49,339 hrs · 49,419 cycles

L1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COALESCER BAG — CONTAMINATED (A/C BAY) · airframe 49,310 hrs · 49,388 cycles

AIRTURN BACK, ENCOUNTERED HYDRAULIC FLUID SMELL ON TAKEOFF. REMOVED AND REPLACED WATER SEPARATOR BAGS PER MM.

Part: CHECK VALVE — FAULTY (HYDRAULIC SYS) · airframe 49,309 hrs · 49,388 cycles

DURING FLIGHT WITH RT PACK RUNNING, BAD HYDRAULIC FLUID SMELL IN CABIN. REMOVED AND REPLACED HYDRAULIC CHECK VALVES ON RESERVOIR PRESSURIZATION MODULE PER MM.

Part: STRINGER — CRACKED (BS 747 S18L) · airframe 48,906 hrs · 48,969 cycles

DURING SCHEDULED MV2 CHECK, FOUND STRINGER 18L CRACKED AT BS 747. REPAIRED STRINGER PER SRM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 48,767 hrs · 48,824 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 5 DEF. SECURED STRIP PER MM.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 48,565 hrs · 48,644 cycles

EEPLS PHOTOLUMINESCENT STRIP MISSING AT ROW 3 DEF. INSTALLED STRIP PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 48,429 hrs · 48,521 cycles

DURING SCHEDULED MV4 CHECK, FOUND R1 DOOR FWD STUB FRAME CRACKED AT BS 294.5, STR 12R. REPAIRED FRAME PER SWA EA.

Part: SIGN — BROKEN (EMERGENCY EXIT) · airframe 48,367 hrs · 48,468 cycles

FOUND FWD CABIN EMERGENCY EXIT SIGN COVER BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: SKIN — DELAMINATED (NR 2 SLAT) · airframe 47,975 hrs · 48,097 cycles

DURING SCHEDULED MV1 CHECK, FOUND NR 2 L/E SLAT DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED NR 2 L/E SLAT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 47,739 hrs · 47,857 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,701 hrs · 47,816 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 21L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,629 hrs · 47,744 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 390, BL 0. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,856 hrs · 46,914 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT DOOR HANDLE CUTOUT. REPAIRED DOOR PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,711 hrs · 46,759 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 46,216 hrs · 46,212 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR FRAME CUTOUT, FWD FRAME WEB CRACKED LOWER FWD CORNER. REPAIRED FRAME SECTION PER SWA EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 46,216 hrs · 46,212 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR FRAME CUTOUT, AFT FRAME CRACKED AT NR 5 STOP. REPAIRED FRAME SECTION PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,109 hrs · 46,090 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 23L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 45,623 hrs · 45,553 cycles

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

Part: SKIN — CRACKED (L2 DOOR) · airframe 45,103 hrs · 44,962 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA AND SRM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,980 hrs · 43,783 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT AFT LOWER EXTERNAL EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: WIRE — SHORTED (EMERGENCY LIGHT) · airframe 43,980 hrs · 43,783 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD GALLEY EMERGENCY EXIT LIGHTS INOP. REPAIRED WIRE NR W1150-011-20 PER WDM.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT) · airframe 43,980 hrs · 43,783 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BLOWN FUSES IN LT FWD CABIN EMERGENCY LIGHTS BATTERY PACK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,722 hrs · 43,535 cycles

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

Part: BATTERY — INOPERATIVE (FWD GALLEY) · airframe 43,528 hrs · 43,343 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 43,484 hrs · 43,290 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT T/E WEDGE DELAMINATED. REPAIRED SLAT PER SWA EA.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,674 hrs · 42,408 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY & FUSES PER MM.

Part: BATTERY — INOPERATIVE (R1 DOOR) · airframe 42,195 hrs · 41,900 cycles

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

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 42,153 hrs · 41,855 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REPAIRED WIRE PER WDM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 41,854 hrs · 41,570 cycles

DURING SCHEDULED C2 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BUSHING PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,758 hrs · 41,467 cycles

DURING SCHEDULED A2 CHECK, FOUND FWD SERVICE DOOR EMERGENCY ESCAPE SLIDE LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,501 hrs · 41,204 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,355 hrs · 40,043 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT SERVICE DOOR CUTOUT FWD LOWER CORNER, CRACKED. REPAIRED DOOR CUTOUT PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,345 hrs · 40,033 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR CUTOUT LOWER FWD CORNER, CRACKED. REPAIRED AFT ENTRY DOOR CUTOUT PER EA.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 40,345 hrs · 40,033 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 664, LBL 31.5, CRACKED. REPAIRED PRESSURE WEB PER SRM.

Part: DOOR FRAME — CRACKED (R1) · airframe 40,345 hrs · 40,033 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SERVICE DOOR FRAME, LOWER AFT CORNER CRACKED. REPAIRED FRAME SECTION PER SRM.

Part: STRUCTURE — CRACKED (AFT CARGO DOOR) · airframe 40,345 hrs · 40,033 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO DOOR LOWER T-CHORD, CRACKED. REMOVED AND REPLACED T-CHORD PER SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 40,345 hrs · 40,033 cycles

DURING SCHEDULED 1/4D CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,302 hrs · 38,994 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT TOP AFT CORNER. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,151 hrs · 30,969 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 24L. REPAIRED SKIN PER SRM.

Part: BLOWER — FAULTY (E/E COMP) · airframe 36,785 hrs · 36,632 cycles

EN ROUTE, ELECTRIC TYPE BURNING SMELL IN COCKPIT AND CABIN. REMOVED AND REPLACED SECONDARY EQUIPTMENT COOLING BLOWER PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 35,424 hrs · 35,360 cycles

DURING SCHEDULED RON, FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REMOVED AND REPLACED SLIDE PER MM.

Part: MECHANISM — OUT OF ADJUST (COCKPIT) · airframe 32,482 hrs · 32,603 cycles

DURING SCHEDULED D-CHECK, FOUND R2 COCKPIT WINDOW EMERGENCY RELEASE MECHANISM INOP. ADJUSTED R2 COCKPIT WINDOW RELEASE HANDLE MECHANISM PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 32,482 hrs · 32,603 cycles

DURING SCHEDULED D-CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 15 DEF. REPAIRED WIRING PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,482 hrs · 32,603 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT STR 8R, BS'S 380, 400 AND 867. REPAIRED FRAMES PER BFG ER..

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 32,482 hrs · 32,603 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 13R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,482 hrs · 32,603 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT STR 8L, BS'S 400, 727, 867, 887 AND 907. REPAIRED FRAMES PER BFG ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,482 hrs · 32,603 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,482 hrs · 32,603 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (2) AT STR 8R, BS 520 AND 639. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 32,482 hrs · 32,603 cycles

DURING SCHEDULED D CHECK, FOUND SHEAR TIE CRACKED AT BS 967, BETWEEN STR'S 6L AND 7L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,482 hrs · 32,603 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,482 hrs · 32,603 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (3) AT STR 8L, BS 482A, 482B AND 520. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,482 hrs · 32,603 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, WL 207 LT. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,482 hrs · 32,603 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT BS 616, STR 1R AND 2R. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 32,482 hrs · 32,603 cycles

DURING SCHEDULED D CHECK, FOUND WEB CRACKED AT BS 294.5, STR 16L. REMOVED AND REPLACED WEB PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 32,482 hrs · 32,603 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICES CRACKED (2 EA) AT BS 907, STR 4L AND 4R. REMOVED AND REPLACED STR SPLICES PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,482 hrs · 32,603 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 6L. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,482 hrs · 32,603 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED (2 EA) AT BS 685, STR 1L AND 2L. REMOVED AND REPLACED STR CLIPS PER SRM.

Part: GIRT BAR — OUT OF ADJ (ENTRY DOOR) · airframe 30,602 hrs · 30,747 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED EMERGENCY EVAC SLIDE ASSY PER MM.

Part: COVER — DAMAGED (CABIN FLOOR) · airframe 29,453 hrs · 29,604 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK COVER DAMAGED AT ROW 12. REPLACED TRACK COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN FLOOR) · airframe 29,272 hrs · 29,431 cycles

EEPLS WIRING EXPOSED AND SEVERAL BULBS INOP IN AFT CABIN. SECURED LOOSE WIRE PIN AT SOCKET PER MM. OPS CHECK GOOD.

Part: BATTERY — INOPERATIVE (AFT CABIN) · airframe 29,260 hrs · 29,420 cycles

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

Part: COVER — MISSING (CABIN) · airframe 29,170 hrs · 29,317 cycles

EEPLS TRACK COVER CRACKED IN FRONT SECTION OF CABIN AND MISSING IN REAR SECTION OF CABIN. INSTALLED TRACK COVERS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,577 hrs · 27,659 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD LT SIDE CHORD CRACKED, WL 207. REPAIRED CHORD SECTION PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 27,577 hrs · 27,659 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD CRACKED IN 4 PLACES, LBL 6 TO RBL 6. REPAIRED BULKHEAD PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 27,569 hrs · 27,649 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BS 178 BULKHEAD AND CHORD CRACKED AT LBL 5. REPAIRED BULKHEAD AND CHORD PER SRM.

Part: RELAY — INOPERATIVE (E/E BAY) · airframe 27,054 hrs · 27,133 cycles

DIVERSION, ACFT PRESSURIZATION INOP, LT NAV SYS INOP. DESCENDED AND AVOIDED DROPPING O2 MASKS. DIVERTED TO AUS. REMOVED AND REPLACED RELAY R275. SYSTEMS OP CK GOOD PER MM.

Part: COVER — CRACKED (ROW 2 - 15) · airframe 27,036 hrs · 27,109 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK COVERS CRACKED AT ROWS 2 AND 15. REMOVED AND REPLACED FLOOR TRACK COVERS PER MM.

Part: TARGET — OUT OF ADJUST (CARGO DOOR)

AIR TURNBACK, DURING CLIMB, FWD CARGO DOOR LIGHT ILLUMINATED. ADJUSTED FWD CARGO DOOR TARGET PER MM. OPS CK GOOD.

Part: LIGHT — LOOSE (ROW 17 - 18)

EEPLS LOOSE BETWEEN ROWS 17-18. RESECURED LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (CABIN)

EEPLS LOOSE AT MID CABIN. REPOSITIONED WIRES AND REINSTALLED LIGHT ASSY PER MM.

Part: COVER — MISSING (ROW 10)

EEPLS COVER MISSING AT ROW 10. REPLACED COVER PER MM.

Part: LIGHT — INOP (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND 7 EA EEPLS LIGHTS INOP NEAR OVERWING EXIT. RECONNECTED WIRING AND OPS CHECK GOOD PER MM.

Part: LENS — MISSING (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS LENS MISSING. REPLACED LENS PER MM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED ON RBL 5.7, WL 213-214. REPAIRED BULKHEAD PER SRM.

Part: FRAME — CRACKED (CARGO DOOR)

DURING SCHEDULED C2 CHECK, FOUND FWD CARGO DOOR, FWD LOWER FRAME CRACKED. REMOVED AND REPLACED FWD CARGO DOOR ASSY.

Part: SOLENOID — MALFUNCTIONED (LANDING GEAR)

LANDING GEAR WOULD NOT RETRACT NORMALLY AFTER TAKEOFF FROM SMF. LANDING GEAR OVERRIDE TRIGGER WAS UTILIZED. AFTER DETERMINING THERE WAS NOT AN AIR/GROUND SENSOR PROBLEM, GEAR RETRACTED NORMALLY. REMOVED AND REPLACED LANDING GEAR SAFETY SOLENOID PER MM.

Part: BUNGEE CORD — OUT OF POSITION (CARGO DOOR)

ABORTED TAKEOFF BELOW 80 KNOTS BECAUSE OF FWD CARGO LIGHT ON COCKPIT. FOUND BUNGEE CORD TOUCHING CARGO DOOR PROX SWITCH. REPOSITIONED CORD PER MM.

Part: LIGHT — INOPERATIVE (EMER EXIT DOOR)

EGRESS FLOOR LIGHTS AT OVERWING EXIT INOP. REMOVED AND REPLACED LIGHT FIXTURE PER MM.

Part: WIRE — LOOSE (LT EMER EXIT)

WIRE LOOSE FROM EMERGENCY EXIT LIGHT AT LT OVERWING EXIT. RESECURED WIRE AND OPS CHECKED GOOD PER MM.

Part: WIRE — LOOSE (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY FLOOR LIGHTING WIRING EXPOSED AT EMERGENCY EXIT ROW ON CAPTAINS SIDE. CONNECTED LOOSE WIRES PER BOEING MM.

Part: LIGHTS — LOOSE (CABIN)

DURING WALKAROUBD CHECK, FOUND TRACKS LIGHTS LOOSE AND WIRES EXPOSED. SECURED ALL PER BOEING M/M.

Part: CHARGER — INOPERATIVE (CABIN)

DURING RON CHECK, FOUND RT AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK CHARGER PER BOEING M/M.

Part: LIGHT — INOPERATIVE (CABIN)

DURING WALKAROUND CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REPLACED ONE LIGHT AND REPAIRED WIRES PER BOEING M/M.

Part: TIRE — FAILED (NR 2 MLG)

SECTION OF TREAD SEPARATED FROM NR 2 MAIN GEAR TIRE DURING TAKEOFF. INSPECTED, NO DAMAGE NOTED. REPLACED NR 2 MAIN GEAR WHEEL/TIRE ASSEMBLY PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING WALKAROUND INSPECTION, FOUND CABIN FLOOR TRACK LIGHTING INOP. REMOVED AND REPLACED BATTERY PACK AND HOUSING PER BOEING M/M.

Part: BATTERY — DISCHARGED (CABIN)

DURING WALKAROUND INSPECTION, FOUND EMERGENCY AND LIGHTING AT OVERWING EXIT AND A SECTION OF FLOOR TRACK LIGHTING INOP. REMOVED AND REPLACED BATTERY PACK AND CHARGER UNIT PER BOEING M/M.

Part: BULKHEAD ANGLE — CRACKED (BS 727)

DURING SCHEDULED D-CHECK, FOUND BULKHEAD SUPPORT ANGLE CRACKED AT BS 727, WL 162. REPLACED PER BOEING SRM.

Part: SKIN — GOUGED (BS 386)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 386, 4 ABOVE S17L. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 1016)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, LBL 33 TO 37, WL 208. REPAIRED PER BOEING SRM.

Part: MOPSILL — CRACKED (BS 295)

DURING SCHEDULED D-CHECK, FOUND GALLEY MOPSILL CHORD CRACKED AT BS 295, WL 208R. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 1014)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM SUPPORT CORRODED AT BS 1014, LBL 39, WL 208. REPAIRED PER BOEING SRM.

Part: WEB — CORRODED (BS 1016-1019)

DURING SCHEDULED D CHECK, FOUND SHEAR WEB CORRODED AT BS 1016, TO 1019, LBL 33 TO 37, WL 208. REPAIRED PER BOEING SRM.

Part: ANGLE — CORRODED (BS 270)

DURING SCHEDULED D CHECK, FOUND Z ANGLE CORRODED AT BS 270, WL 208, LBL 11 TO RBL 11. REPAIRED PER BOEING SRM.

Part: SUPPORT — CORRODED (BS 312-344)

DURING SCHEDULED D CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 328 TO 344, LBL 11, WL 208, ALSO AT BS 312-328, LBL 11, WL 208. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 987/947)

DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORROSION AT BS 987, RBL 45 TO LBL 22, WL 208, AND AT BS 947, LBL 16, TO RBL 7. REPAIRED PER BOEING SRM.

Part: DOOR — CRACKED (FWD CARGO)

DURING SCHEDULED B-CHECK, FOUND FWD CARGO DOOR CRACKED ON FWD LOWER CORNER ADJACENT TO UPLOCK HOOK. REPAIRED PER SWA TYPICAL REPAIR T1-A25-005.