N637SW

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 66,185 hrs · 51,750 cycles

L2 DOOR EXTERIOR EMERGENCY LIGHT INOP. R&R LIGHT PER AMM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 65,168 hrs · 50,987 cycles

FORWARD ENTRY EXIT LIGHT COVER LOOSE. R & R THE COVER IAW AMM.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 64,952 hrs · 50,842 cycles

FWD ENTRY LOWER EXIT SIGN BROKEN. R & R THE SIGN IAW MM.

Part: SIGN — CRACKED (EMERGENCY LIGHT) · airframe 64,688 hrs · 50,664 cycles

L1 DOOR EMERGENCY EXIT SIGN CRACKED. R & R THE SIGN IAW SIP.

Part: BRACKET — CRACKED (R2 DOOR) · airframe 64,409 hrs · 50,494 cycles

R2 DOOR SLIDE CONTAINER BRACKET CRACKED. R & R THE BRACKET IAW SIP.

Part: LENS — UNSECURE (CABIN) · airframe 64,343 hrs · 50,448 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS COVER FELL OFF. SECURED COVER IAW AMM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 64,098 hrs · 50,283 cycles

L1 DOOR EMERGENCY EXIT LOWER EXIT LIGHT LENS LOOSE. R & R THE LENS IAW AMM.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 63,477 hrs · 49,860 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER LENS FELL OFF. INSTALLED THE LENS IAW SIP.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 63,434 hrs · 49,831 cycles

L1 DOOR EMERGENCY EXIT SIGN LENS LOOSE. SECURED THE LENS IAW AMM.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 63,332 hrs · 49,759 cycles

FORWARD EXIT SIGN COVER LIGHT LENS DETACHED. R & R THE LENS IAW AMM.

Part: ESCAPE ROPE — OUT OF POSITION (OVERWING DOOR) · airframe 63,271 hrs · 49,722 cycles

RIGHT DOOR EMERGENCY ESCAPE HATCH ROPE OUT OF POSITION. REPOSITIONED ROPE IAW MM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 62,886 hrs · 49,458 cycles

L1 DOOR LOWER EMERGENCY EXIT SIGN LENS COVER BROKEN. R & R THE COVER IAW MM.

Part: NUT PLATE — DAMAGED (L2 DOOR SLIDE) · airframe 62,809 hrs · 49,407 cycles

L2 DOOR SLIDE MOUNT NUT PLATES DAMAGED. R & R THE NUT PLATES IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,716 hrs · 49,340 cycles

L2 EMERGENCY LIGHT INOPERATIVE. RECHARGED BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,716 hrs · 49,340 cycles

AFT GALLEY EMERGENCY EXIT SIGN LIGHT INOPERATIVE. RECHARGED BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,716 hrs · 49,340 cycles

LEFT EMERGENCY LIGHT INOPERATIVE AT ROW 22. RECHARGED BATTERY PACK IAW AMM.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 62,716 hrs · 49,340 cycles

FRAME CHORD DAMAGED AT BS 259.5, STR 7L. REPAIRED CHORD IAW EA.

Part: SPLICE STRAP — DAMAGED (FUSELAGE) · airframe 62,716 hrs · 49,340 cycles

BUTT SPLICE STRAP DAMAGED AT BS 259.5, STR 7L. REPAIRED SPLICE STRAP IAW EA.

Part: SLAT — DELAMINATED (RT WING) · airframe 62,391 hrs · 49,136 cycles

RIGHT WING NR 4 LE SLAT DELAMINATED ON INBD EDGE. R & R NR 4 SLAT IAW AMM.

Part: SLAT — DELAMINATED (RT WING) · airframe 62,391 hrs · 49,136 cycles

RIGHT WING NR 5 LE SLAT DELAMINATED ON INBD EDGE. R & R NR 5 SLAT IAW AMM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 62,380 hrs · 49,128 cycles

FORWARD GALLEY OVERHEAD EXIT SIGN INOPERATIVE. R & R SIGN IAW AMM.

Part: COUPLING — DISCONNECTED (LT WING) · airframe 61,746 hrs · 48,720 cycles

AIR TURN BACK, DURING CLIMB & THEN DESCENT, VISIBLE FUEL STREAM EMANATING FROM WINGS, NOTICEABLE EXCESSIVE FUEL BURN. CONNECTED COUPLINGS IAW AMM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 61,727 hrs · 48,707 cycles

LEFT WING TE SUPPORT ANGLE CRACKED ON WBL 198.60. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 61,727 hrs · 48,707 cycles

RIGHT WING TE SUPPORT ANGLE CRACKED ON WBL 198.60. R & R ANGLE IAW SRM & DWG.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 61,727 hrs · 48,707 cycles

FORWARD GALLEY LAVATORY FLASHLIGHT BASE BROKEN. R & R FLASHLIGHT BASE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

SHEAR TIE CORRODED AT BS 500D, BETWEEN STRINGER 28R - 28L. R & R SHEAR TIE IAW SRM & DWG.

Part: FLAP TRACK — CRACKED (LT WING) · airframe 61,727 hrs · 48,707 cycles

LEFT WING NR 4 FLAP TRACK CRACKED. R & R NR 4 FLAP TRACK IAW AMM.

Part: ANGLE — CRACKED (WING) · airframe 61,727 hrs · 48,707 cycles

CENTER WING BOX REAR SPAR ANGLE CRACKED AT RBL 6.30 & WBL 176.4. R & R ANGLE IAW SRM & DWG.

Part: SKIN — DELAMINATED (LT SPOILER) · airframe 61,727 hrs · 48,707 cycles

LEFT WING NR 3 FLIGHT SPOILER, DELAMINATED ON UPPER SURFACE. R & R NR 3 FLIGHT SPOILER IAW AMM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,727 hrs · 48,707 cycles

LEFT WING INBD EDGE FORE FLAP DELAMINATED ON UPPER SURFACE. REPAIRED FORE FLAP IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 61,727 hrs · 48,707 cycles

RIGHT WING AFT UPPER SKIN TE, CRACKED AT RSS 255. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 61,727 hrs · 48,707 cycles

LEFT WING AFT UPPER SKIN CRACKED, BETWEEN RSS 235 - 275, IN FASTENER HOLE REAR SPAR AFT ROW. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 61,727 hrs · 48,707 cycles

RIGHT WING AFT UPPER SKIN TE CRACKED AT RSS 237. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 61,727 hrs · 48,707 cycles

RIGHT WING AFT UPPER SKIN TE, CRACKED AT RSS 253.5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 61,727 hrs · 48,707 cycles

RIGHT WING AFT UPPER SKIN TE SKIN, CRACKED AT RSS 247.5. REPAIRED SKIN IAW EA.

Part: LINK — CORRODED (RT MLG) · airframe 61,727 hrs · 48,707 cycles

RIGHT MLG SWING LINK UPPER BORE CORRODED AT FWD POSITION. REPAIRED SWING LINK IAW EA.

Part: FITTING — CRACKED (RT WING) · airframe 61,727 hrs · 48,707 cycles

RT WING REAR SPAR AFT FITTING CRACKED AT RSS 224.14. REPAIRED FITTING IAW EA.

Part: SUPPORT FITTING — CRACKED (LT SPOILER) · airframe 61,727 hrs · 48,707 cycles

LEFT WING NR 4 GND SPOILER, INBD SUPPORT FITTING CRACKED. R & R FITTING IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED, BETWEEN BS 616 TO 639, RBL 45.50 AT CTR WING BOX. R & R WEB IAW SRM & DWG.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 61,727 hrs · 48,707 cycles

LEFT WING NR 2 FLAP TRACK A FRAME BORE CORRODED. REPAIRED FLAP TRACK IAW CMM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

STRINGER SPLICE CORRODED AT BS 847, STRINGER 21R. R & R SPLICE IAW SRM & DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

STRINGER SPLICE CORRODED AT BS 847, STRINGER 24R. R & R SPLICE IAW SRM & DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

STRINGER SPLICE CORRODED AT BS 908, STRINGER 22R. R & R SPLICE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

TIE CLIP CRACKED AT BS 727A, STR 25L. R&R TIE CLIP IAW SRM AND DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

AFT CARGO COMPARTMENT, STRINGER SPLICE CORRODED AT BS 847, STRINGER 23R. R & R SPLICE IAW SRM & DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,727 hrs · 48,707 cycles

RIGHT WING INBD FORE FLAP DELAMINATED AT UPPER SURFACE. REPAIRED FORE FLAP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

AFT CARGO COMPARTMENT, TIE CLIP CRACKED AT BS 727A, STRINGER 25R. R & R TIE CLIP IAW SRM & DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

AFT CARGO COMPARTMENT, ANGLE SUPPORT CRACKED AT BS 947.5, STRINGER 26L. R & R SUPPORT IAW SRM & DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,727 hrs · 48,707 cycles

RIGHT WING INBD AFT FLAP DELAMINATED ON LOWER SURFACE. REPAIRED AFT FLAP IAW SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

STRINGER SPLICE CORRODED AT BS 847, STRINGER 22R. R & R SPLICE IAW SRM & DWG.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

L1 DOOR CUT OUT REVEAL CRACKED AT BS 329, STRINGER 6L. R & R REVEAL IAW DWG & SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

AFT CARGO COMPARTMENT CLIP CRACKED AT BS 927, STR 25R. R&R CLIP IAW SRM & DWG.

Part: RIB — CRACKED (LT AILERON) · airframe 61,727 hrs · 48,707 cycles

LEFT WING AT OTBD AILERON INBD RIB CRACKED. R & R RIB IAW SRM & DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,727 hrs · 48,707 cycles

LEFT WING INBD FORE FLAP DELAMINATED AT UPPER SURFACE. REPAIRED FORE FLAP IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,727 hrs · 48,707 cycles

RT WING OUTBOARD FORE FLAP DELAMINATED AT UPPER SURFACE. REPAIRED FORE FLAP IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

FORWARD GALLEY DOORWAY INTERCOSTAL WEB CRACKED, BETWEEN BS 277 - 291.5, STRINGER 14R. REPAIRED WEB IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

FRAME CORRODED AT BS 727B, BETWEEN STRINGER 25L - 26L. REPAIRED FRAME IAW SRM.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

AFT CARGO COMPARTMENT CROSSBEAM D, T CHORD CRACKED AT FWD END. REPAIRED T CHORD IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

AFT CARGO COMPARTMENT, SUPPORT ANGLE CRACKED, AT BS 947.5, STRINGER 25L. R & R ANGLE IAW SRM & DWG.

Part: SPLICE — CRACKED (RT WING) · airframe 61,727 hrs · 48,707 cycles

RIGHT WING REAR SPAR, UPPER CHORD SPLICE ON FASTENER HOLE RSS. 222.5 CRACKED. REPAIRED SPLICE IAW EA.

Part: SPLICE — CRACKED (RT WING) · airframe 61,727 hrs · 48,707 cycles

RIGHT WING REAR SPAR WEB SPLICE CRACKED, BETWEEN RSS 211 - 238. REPAIRED SPLICE IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 61,727 hrs · 48,707 cycles

LEFT WING REAR SPAR UPPER CHORD CRACKED, BETWEEN RSS 220.5 - 285. REPAIRED CHORD IAW EA.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 61,727 hrs · 48,707 cycles

LEFT WING NR 4 FLAP TRACK, UPPER SURFACE HOLE CORRODED. REPAIRED NR 4 FLAP TRACK IAW CMM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

AFT PRESSURE BULKHEAD DOME CAP WEB CRACKED AT BS 1016, RBL 4.5. REPAIRED WEB IAW SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

AFT CARGO COMPARTMENT ANGLE SUPPORT CRACKED AT BS 727, STRINGER 25L. R & R SUPPORT IAW SRM & DWG.

Part: SKIN — DELAMINATED (LT AILERON) · airframe 61,727 hrs · 48,707 cycles

LEFT WING AILERON LE, UPPER SKIN DELAMINATED. REPAIRED AILERON IAW EA & SRM.

Part: RIB — CRACKED (RT WING) · airframe 61,727 hrs · 48,707 cycles

RIGHT WING LOWER RIB CHORD CRACKED ON WBL 135.50, BETWEEN STRINGER 2 - 3. REPAIRED LOWER RIB CHORD IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

FORWARD GALLEY DOORWAY T CHORD CRACKED AT BS 332, STRINGER 8R. REPAIRED T CHORD IAW EA.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

AFT CARGO COMPARTMENT ANGLE SUPPORT CRACKED AT BS 727B, STRINGER 25L. R & R SUPPORT IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

CLIP CRACKED AT BS 328, BETWEEN STR 20L TO STR 21L. R&R CLIP IAW SRM AND DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

AFT CARGO COMPARTMENT, FWD BULKHEAD BRACKET ASSEMBLY CRACKED AT BS 727, RBL 3.0. R & R BRACKET ASSEMBLY IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

TIE CLIP CRACKED AT BS 500A, STRINGER 22L. R & R TIE CLIP IAW SRM & DWG.

Part: RIB — CRACKED (LT WING) · airframe 61,727 hrs · 48,707 cycles

LEFT WING INSPAR RIB WEB CRACKED AT WBL 198.60, INTERNAL SURFACE REAR SPAR. REPAIRED RIB WEB IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 61,727 hrs · 48,707 cycles

RIGHT HORIZONTAL STABILIZER CRACKED ON LE RIB, LOCATED ON LE STATION 151.75. R & R RIB IAW SRM & DWG.

Part: LINK — CORRODED (RT MLG) · airframe 61,727 hrs · 48,707 cycles

RIGHT MLG SWING LINK PLATE CORRODED. REPAIRED LINK IAW CMM.

Part: LINK — CORRODED (LT MLG) · airframe 61,727 hrs · 48,707 cycles

LEFT MLG SWING LINK PLATE CORRODED. REPAIRED LINK IAW CMM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

WING TO BODY STRUCTURE AT LOWER FUSELAGE SUPPORT ANGLE, CRACKED AT BS 520, STRINGER 22R. R & R ANGLE IAW SRM.

Part: INTERCOSTAL — CRACKED (GALLEY DOOR) · airframe 61,727 hrs · 48,707 cycles

FORWARD GALLEY DOOR INTERCOSTAL WEB CRACKED, BETWEEN BS 277 - 291.5, STRINGER 14R. REPAIRED WEB IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

WING TO BODY STRUCTURE AT LOWER FUSELAGE SUPPORT ANGLE, CRACKED AT BS 520, STRINGER 22L. R & R ANGLE IAW SRM & DWG.

Part: LIGHT — BROKEN (CABIN) · airframe 61,727 hrs · 48,707 cycles

AFT CABIN PHOTO LUMINESCENT FLOOR PROXIMITY LIGHTING STRIP BROKEN. R & R STRIP IAW AMM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

R1 DOOR CUT OUT T CHORD CRACKED AT BS 332, STRINGER 8R. REPAIRED T CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

FORWARD ENTRY DOOR SKIN CUT OUT CRACKED AT BS 342 ON EXTERNAL AFT UPPER CORNER. REPAIRED CUT OUT IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

SEAT TRACK OTBD FLANGE CRACKED AT BS 727B, RBL 24.8. REPAIRED SEAT TRACK IAW EA.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 61,727 hrs · 48,707 cycles

MAIN WW COMPARTMENT, AFT BULKHEAD ANGLE CRACKED AT LBL 16. R & R ANGLE IAW SRM & DWG.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 61,727 hrs · 48,707 cycles

RIGHT WING NR 6 FLAP TRACK FAIRING DELAMINATED AT TAIL CONE. REPAIRED FAIRING IAW SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

CENTER WING BOX SUPPORT, CREASE BEAM CHORD CRACKED, AT BS 616, RBL 63.5. REPAIRED CREASE BEAM IAW EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

VERTICAL STIFFENER REAR SPAR CRACKED AT BS 663.75, RBL 6.15 AT CTR WING BOX. R & R STIFFENER IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 61,727 hrs · 48,707 cycles

RIGHT WING NR 2 SLAT EXTERNAL SKIN CRACKED, AT INBD EDGE LOWER SURFACE. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 61,727 hrs · 48,707 cycles

RIGHT WING NR 6 EXTERNAL SKIN CRACKED, INBD EDGE LOWER SURFACE. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

ANGLE CRACKED, BETWEEN BS 500D - 520, ON INLET DUCT THE RAM AIR INTERNAL AREA, RT AT LOWER FUSELAGE. R & R ANGLE IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 61,727 hrs · 48,707 cycles

CENTER WING BOX LONGITUDINAL FLOORBEAM WEB CRACKED, BETWEEN BS 698 - 717, RBL 24.50. REPAIRED WEB IAW EA.

Part: SKIN — DELAMINATED (TAILCONE) · airframe 61,727 hrs · 48,707 cycles

RIGHT TAIL CONE EXTERNAL SKIN DELAMINATED. REPAIRED SKIN IAW SRM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 61,692 hrs · 48,680 cycles

AFT EMER FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 61,683 hrs · 48,676 cycles

L1 DOOR EXIT SIGN LENS LOOSE. INSTALLED LENS IAW MM.

Part: COVER — BROKEN (CABIN) · airframe 61,586 hrs · 48,607 cycles

L1 DOOR EMER EXIT LIGHT COVER BROKEN. R & R COVER IAW MM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 61,395 hrs · 48,482 cycles

FLOORBEAM STRAP CRACKED AT BS 312, RBL 24. R & R STRAP IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 61,395 hrs · 48,482 cycles

FORWARD ENTRY LOWER EXIT LIGHT LENS LOOSE. SECURED LENS IAW AMM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 61,395 hrs · 48,482 cycles

L1 DOOR INNER SKIN CRACKED, LOWER HINGE CUT OUT FWD VERTICAL FRAME. REPAIRED DOOR IAW EA.

Part: SKIN — DELAMINATED (RT SPOILER) · airframe 61,287 hrs · 48,412 cycles

RIGHT WING NR 8 SPOILER DELAMINATED, UPPER SURFACE. R & R SPOILER IAW MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 61,287 hrs · 48,412 cycles

LEFT WING INBD AFT FLAP DELAMINATED ON LOWER FWD AREA. R & R AFT FLAP IAW AMM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 61,265 hrs · 48,393 cycles

R2 DOOR EMER ESCAPE SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: LENS — MISSING (EXIT SIGN) · airframe 61,213 hrs · 48,358 cycles

MID CABIN OVERWING EXIT SIGN, LOWER LENS COVER MISSING. INSTALLED COVER IAW EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 61,110 hrs · 48,285 cycles

R2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW AMM.

Part: FUSE — INOPERATIVE (CABIN) · airframe 61,055 hrs · 48,246 cycles

RIGHT EMER LIGHT BATTERY PACK M1669 FUSE INOPERATIVE, BETWEEN ROW 12 - 16. R & R FUSE IAW AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 60,694 hrs · 47,986 cycles

R1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW SIP.

Part: LENS — BROKEN (CABIN) · airframe 59,953 hrs · 47,449 cycles

L1 DOOR EXIT LIGHT LENS BROKEN. R & R LENS IAW MM.

Part: STRIP — CRACKED (CABIN) · airframe 59,774 hrs · 47,320 cycles

FORWARD CABIN PAX CABIN FLOOR EGRESS PROXIMITY LIGHTING STRIP CRACKED. R & R STRIP IAW AMM.

Part: COVER — MISSING (CABIN) · airframe 59,774 hrs · 47,320 cycles

RIGHT EMER EXIT LENS COVER MISSING. INSTALLED COVER IAW AMM.

Part: LUG — BROKEN (RT SPOILER) · airframe 58,831 hrs · 46,682 cycles

RIGHT WING NR 5 GND SPOILER OTBD LUG BROKEN. R & R NR 5 GND SPOILER IAW AMM.

Part: TAB — DELAMINATED (RT ELEVATOR) · airframe 57,954 hrs · 46,092 cycles

RIGHT ELEVATOR TAB UPPER SURFACE DELAMINATED. R & R TAB IAW MM.

Part: BLOWER — FAULTY (AC BAY) · airframe 57,774 hrs · 45,959 cycles

DIVERSION SULFUR SMELL IN CABIN UPON DEPARTURE. R & R MAIN EQUIPMENT COOLING FAN BLOWER IAW MM.

Part: LIGHT — MISSING (CABIN) · airframe 57,123 hrs · 45,480 cycles

LEFT EEPLS MISSING AT ROW 14. INSTALLED EEPLS IAW MT.

Part: STRUCTURE — CRACKED (L1 DOOR) · airframe 56,434 hrs · 45,012 cycles

L1 DOOR UPPER HINGE CUT OUT CRACKED FROM LOWER EDGE. R & R CUT OUT IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 56,258 hrs · 44,891 cycles

FWD EEPLS LENS LOOSE. SECURED LENS IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,091 hrs · 44,778 cycles

RT CABIN EMERGENCY EXIT LIGHT INOPERATIVE AT SEAT ROW 7. R & R BATTERY PACK IAW AMM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

INTERCOSTAL FWD END ATTACH CLIP CRACKED BETWEEN BS 807 TO BS 827, RBL 6. R & R CLIP IAW SRM & DWG.

Part: FASTENER — MISSING (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

FORWARD ENTRY DOOR CUT OUT AFT SIDE FRAME INNER CHORD FASTENER MISSING AT BS 348.2, STRINGER 15L. INSTALLED FASTENER IAW EA & EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

FRAME ATTACH ANGLE CRACKED AT BS 1006, BETWEEN STRINGER 18R TO STRINGER 19R. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

FRAME CORRODED AT BS 1006, BETWEEN STRINGER 17R TO STRINGER 20R. R & R FRAME IAW SRM & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

STRINGER SECTION CORRODED BETWEEN BS 1006 TO BS 1016, STRINGER 26R. R & R STRINGER IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

SHEAR TIE LOWER ANGLE CORRODED AT BS 500B, BETWEEN STRINGER 27R TO STRINGER 28R. R & R ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

AFT CARGO COMPARTMENT FRAME SHEAR TIE CRACKED AT BS 747, BETWEEN STRINGER 25L TO STRINGER 26L. R & R FRAME IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

SHEAR TIE LOWER ANGLE CORRODED AT BS 500B, BETWEEN STRINGER 28L TO STRINGER 28R. R & R ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

SHEAR TIE LOWER ANGLE CORRODED AT BS 500B, BETWEEN STRINGER 25L TO STRINGER 26L. REPAIRED ANGLE IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

INTERCOSTAL CLIP CRACKED AT STATION 947, STRINGER 25R. R & R CLIP IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

BULKHEAD LOWER SUPPORT ANGLE CORRODED AT BS 947, BETWEEN STRINGER 25L TO STRINGER 25R. R & R ANGLE IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

LEFT CHORD CRACKED AT BS 727, STRINGER 18A. R & R CHORD IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

AFT CARGO COMPARTMENT FRAME CORRODED AT BS 787, BETWEEN STRINGER 27L TO STRINGER 27R. R & R FRAME IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

AFT CARGO COMPARTMENT FRAME SHEAR TIE CORRODED AT BS 807, BETWEEN STRINGER 26L TO STRINGER 27L. R & R FRAME IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

INTERCOSTAL CORRODED BETWEEN BS 986 TO BS 996, STRINGER 21L. R & R INTERCOSTAL IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (LT MLG WW) · airframe 56,091 hrs · 44,778 cycles

LT MLG WW PANEL SUPPORT ANGLE CRACKED AT BS 727, BETWEEN LBL 8 TO LBL 16. R & R ANGLE IAW SRM & DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

AFT CARGO COMPARTMENT FRAME CORRODED AT BS 787, BETWEEN STRINGER 26R TO STRINGER 27R. R & R FRAME IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

FRAME SHEAR TIE CORRODED AT BS 907, STRINGER 27L TO STRINGER 26L. R & R SHEAR TIE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

AFT CARGO COMPARTMENT FRAME CORRODED AT BS 787, BETWEEN STRINGER 26L TO STRINGER 27L. R & R FRAME IAW SRM & DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

STRINGER CLIP CORRODED AT BS 907, STRINGER 25R. R & R CLIP IAW SRM & DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

AFT CARGO COMPARTMENT FRAME CORRODED AT BS 787, STRINGER 27L. R & R FRAME IAW SRM & DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

STRINGER CLIP CORRODED AT BS 847, STRINGER 26R. R & R CLIP IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 807, BETWEEN STRINGER 25L TO STRINGER 26L. R & R SHEAR TIE IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

AFT CARGO COMPARTMENT FRAME CORRODED AT BS 787, STRINGER 27L. R & R FRAME IAW SRM & DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

AFT CARGO COMPARTMENT STRINGER CLIP CORRODED AT BS 747, STRINGER 27R. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

AFT CARGO BAY STRINGER CLIP CORRODED AT BS 767, STRINGER 27L. R & R CLIP IAW SRM & DWG.

Part: LIGHT — BROKEN (CABIN) · airframe 56,091 hrs · 44,778 cycles

AFT WALL OF THE FWD LAVATORY EMERGENCY EXIT LIGHT BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 56,091 hrs · 44,778 cycles

NR 5 LE SLAT WEDGE PANEL DELAMINATED. REPAIRED SLAT WEDGE IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,091 hrs · 44,778 cycles

RT WING NR 5 SLAT LOWER SURFACE SKIN CRACKED INBD OF STATION 194.01. REPAIRED SKIN IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

AFT CARGO BAY FRAME CORRODED AT BS 767, BETWEEN STRINGER 26R TO STRINGER 26L. REPAIRED FRAME IAW EA.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 56,091 hrs · 44,778 cycles

RT WING NR 6 SLAT WEDGE UPPER AFT INBD CORNER SKIN DELAMINATED. REPAIRED SKIN IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

AFT CARGO COMPARTMENT FRAME CORRODED AT BS 747, BETWEEN STRINGER 25L TO STRINGER 25R. R & R FRAME IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

AFT CARGO PIT FRAME CORRODED AT BS 787, BETWEEN STRINGER 25L TO STRINGER 26R. R & R FRAME IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

AFT CARGO COMPARTMENT FRAME CORRODED AT BS 727E, BETWEEN STRINGER 26R TO STRINGER 26L. R & R FRAME IAW DWG & SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,091 hrs · 44,778 cycles

RT WING NR 5 SLAT LOWER SURFACE SKIN CRACKED INBD OF STATION 215.4. REPAIRED SKIN IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

AFT CARGO COMPARTMENT FRAME SHEAR TIE CORRODED AT BS 727D, BETWEEN STRINGER 25L TO STRINGER 26L. REPAIRED SHEAR TIE IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 663, RBL 24.8. REPAIRED BEAM IAW EA.

Part: ANGLE — CRACKED (LT AILERON) · airframe 56,091 hrs · 44,778 cycles

LT WING TE AT AILERON 2ND BAY OTBD ANGLE CRACKED. R & R ANGLE IAW SRM & DRAWING.

Part: FLAP — DELAMINATED (RT WING) · airframe 56,091 hrs · 44,778 cycles

RT WING INBD AFT FLAP, AFT OTBD CORNER DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 56,091 hrs · 44,778 cycles

RIGHT CHORD CRACKED AT BS 727, STRINGER 18. REPAIRED CHORD IAW EA.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 56,091 hrs · 44,778 cycles

LT WING NR 3 SLAT UPPER INBD CORNER AREA SKIN DELAMINATED. REPAIRED SKIN IAW SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 55,853 hrs · 44,610 cycles

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

Part: WIRE — BROKEN (CABIN) · airframe 55,769 hrs · 44,560 cycles

AFT CENTER AISLE EMERGENCY EXIT LIGHT WIRES BROKEN AT LIGHT ASSEMBLY. R & R LIGHT ASSEMBLY IAW MM.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

STRINGER CLIP DAMAGED AT BS 986 STRINGER 6R. R & R CLIP IAW SRM & DRAWING.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

STRINGER CLIP DAMAGED AT STATION 639, STRINGER 4R. R & R STRINGER CLIP IAW SRM & BAC DRAWING.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

STRINGER SPLICE CRACKED AT BS 360 STRINGER 4L. REPAIRED SPLICE IAW EA.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

STRINGER CLIP DAMAGED AT STATION 727D, STRINGER 8R. R & R STRINGER CLIP IAW SRM & BAC DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

STRINGER CLIP CRACKED AT BS 360 STRINGER 8R. R & R CLIP IAW SRM & DRAWING.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

SPLICE CHANNEL CRACKED AT STATION 908, STRINGER 4L. R & R CHANNEL IAW DRAWING & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

STRINGER CLIP CRACKED AT STATION 380, STRINGER 8L. R & R STRINGER CLIP IAW SRM & BAC DRAWING.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

SHEAR TIE CRACKED AT BS 520 BETWEEN STRINGER 11R TO STRINGER 10R. REPAIRED SHEAR TIE IAW SRM & DRAWING.

Part: FORGING — CRACKED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

RT BS 480+10 UPPER FWD CORNER OF WINDOW FORGING CRACKED AT HOLE NR 7. R & R FORGING IAW DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

LT BS 867+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

RT BS 360+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

RT BS 767+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW TC & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

RT BS 460+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

LT BS 480+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

LT BS 500+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

RT BS 440+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

RT BS 360+10 LOWER AFT SKIN CUT OUT CRACKED INDICATION AT HOLE NR 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

RT BS 400+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLES 2 & 3. REPAIRED SKIN IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 55,769 hrs · 44,560 cycles

LT WING INBD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

RT BS 500A+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

RT BS 827+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 4. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

LT BS 420+10 UPPER FWD SKIN CUT OUT CRACKED INDICATION AT HOLES 5 & 6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

LT BS 400+10 UPPER FWD SKIN CUT OUT CRACKED INDICATION AT HOLES 3 & 6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

LT BS 380+10 UPPER FWD SKIN CUT OUT CRACKED INDICATION AT HOLES 3, 4 & 5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

RT BS 520+10 UPPER FWD SKIN CUTOUT CRACKED AT HOLE NR 3 - 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

LT BS 500+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3,4 & 5. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

LT BS 520+10 LOWER AFT SKIN CUT OUT CRACKED AT HOLE NR 8 & NR 7. REPAIRED SKIN IAW DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

RT BS 867+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 5, 9,10 & 12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,769 hrs · 44,560 cycles

LT BS 520+10 UPPER FWD SKIN CUTOUT CRACKED INDICATION AT HOLES 4,5 & 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 55,769 hrs · 44,560 cycles

RT WING NR 5 SLAT LOWER SURFACE SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: ACCESS PANEL — CHAFED (VERTICAL STAB) · airframe 55,769 hrs · 44,560 cycles

DORSAL FIN ACCESS PANEL 9503 CHAFFED. REPAIRED PANEL IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,584 hrs · 44,435 cycles

SKIN CRACKED AT BS 526.5, STRINGER 10R. REPAIRED SKIN IAW EA.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 55,561 hrs · 44,418 cycles

LT WING LE SLAT SKIN DELAMINATED. R & R SLAT IAW AMM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 55,583 hrs · 44,435 cycles

LT WING NR 4 SLAT LE SKIN DELAMINATED. R & R SLAT IAW MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 54,756 hrs · 43,789 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 53,972 hrs · 43,209 cycles

RIGHT EMERGENCY EXIT LIGHT LENS EDGE LOOSE AT ROW 2. SECURED LENS PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,635 hrs · 42,971 cycles

SKIN CRACKED BETWEEN BS 500D + 10" TO BS 500D +11, STR 10R. REPAIRED SKIN IAW EA.

Part: WINDOW — ARCED (COCKPIT) · airframe 53,514 hrs · 42,885 cycles

LEFT SIDE WINDOW (CAPT) ARCED AT LEADING EDGE NEAR ELECTRICAL CONNECTOR. REMOVED AND REPLACED WINDOW PER M/M.

Part: WEB — CRACKED (LT MLG WW) · airframe 52,821 hrs · 42,408 cycles

LEFT W/W CEILING BEHIND AND LEFT OF AILERON CONTROL CRACKED AT BS 663. REPAIRED WEB IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 52,821 hrs · 42,408 cycles

LEFT WW CEILING BEHIND AND LEFT OF AILERON CONTROL CRACKED AT BS 663. REPAIRED WEB PER SRM.

Part: INSERT — MISSING (BATTERY HOUSING) · airframe 52,485 hrs · 42,165 cycles

AFT RIGHT EMERGENCY LIGHT BATTERY PACK HOUSING BATTERY PACK MOUNT INSERT MISSING. INSTALLED BATTERY PACK HOUSING IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 50,412 hrs · 40,557 cycles

LT EMERGENCY EXIT BULL NOSE LIGHT INOP BETWEEN ROW 10 TO ROW 17. REMOVED AND REPLACED BATTERY PACK IAW AMM.

Part: TAB — DELAMINATED (LT AILERON) · airframe 50,412 hrs · 40,557 cycles

LT WING AILERON TAB DELAMINATED. REMOVED AND REPLACED TAB IAW AMM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

STRINGER SPLICE CORRODED AT BETWEEN BS 900 TO BS 914, STR 18L. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

FRAME CRACKED AT BS 420, STR 26R. REPAIRED FRAME IAW EA AND EO.

Part: WEB — CRACKED (E/E BAY) · airframe 50,412 hrs · 40,557 cycles

WEB CRACKED AT BS 328, BL 0. REPLACED WEB IAW SRM AND DWG

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

STUB FRAME CRACKED BS 951+10, STR 17LT. REPAIRED FRAME IAW EA AND EO.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

STRINGER CRACKED AT BS 947, STR 19L. REPAIRED STRINGER IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB IAW EO & EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17.0. REPAIRED BEAM IAW EO AND EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

SUPPORT ANGLE CRACKED AT BS 312, BL0. REPLACED ANGLE IAW SRM & DRAWING AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

FRAME CRACKED AT BS 328, BETWEEN STR 20R TO STR 21R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: PLATE — CORRODED (GIRT BAR) · airframe 50,412 hrs · 40,557 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR PLATE ASSY CORRODED. REMOVED AND REPLACED PLATE ASSY IAW AMM.

Part: PLATE — CORRODED (GIRT BAR) · airframe 50,412 hrs · 40,557 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR PLATE ASSY CORRODED. REMOVED AND REPLACED PLATE ASSY IAW AMM.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

SPLICE WEB CRACKED AT BS 616, LBL 45.5. REPAIRED WEB IAW EO AND EA.

Part: WEB — CRACKED (BS 302) · airframe 50,412 hrs · 40,557 cycles

WEB CRACKED AT BS 302, BETWEEN STR 27R TO STR 28L. REPLACED WEB IAW SRM AND DWG.

Part: WEB — CRACKED (BS 616-639) · airframe 50,412 hrs · 40,557 cycles

WEB CRACKED BETWEEN BS 616 TO BS 639, STR 17L. REPLACED WEB IAW SRM AND DWG.

Part: PLATE — CORRODED (GIRT BAR) · airframe 50,412 hrs · 40,557 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR PLATE ASSY CORRODED. REMOVED AND REPLACED PLATE ASSY IAW AMM.

Part: PLATE — CORRODED (GIRT BAR) · airframe 50,412 hrs · 40,557 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR PLATE ASSY CORRODED. REMOVED AND REPLACED PLATE ASSY IAW AMM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

CHORD CRACKED AT BS 616, STR 17L. REPAIRED CHORD IAW EA AND EO.

Part: SUPPORT ANGLE — CRACKED (BS 294.5 S23L) · airframe 50,412 hrs · 40,557 cycles

SUPPORT ANGLE OF WEB CRACKED AT BS 294.5, STR 23L. REPLACED WEB IAW SRM AND DWG.

Part: SHEAR TIE — CRACKED (BS 639) · airframe 50,412 hrs · 40,557 cycles

SHEAR TIE CRACKED AT BS 639, BETWEEN STR 6R TO STR 7R. REPLACED SHEAR TIE IAW SRM & DWG.

Part: SHEAR TIE — CRACKED (BS 639) · airframe 50,412 hrs · 40,557 cycles

SHEAR TIE CRACKED AT BS 639, BETWEEN STR 6L TO STR 7L. REPLACED SHEAR TIE IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

STRINGER CLIP CRACKED AT BS 559, STR 11L. REPLACED CLIP IAW SRM AND DWG.

Part: CHANNEL — CRACKED (CENTER WING BOX) · airframe 50,412 hrs · 40,557 cycles

CHANNEL CRACKED AT BS 540, BTW RBL 24.5 AND RBL 45.5. REPLACED CHANNEL IAW SRM AND DWG.

Part: CHANNEL — CRACKED (BS 540 S17L) · airframe 50,412 hrs · 40,557 cycles

CHANNEL CRACKED AT BS 540, STR 17L. REPLACED CHANNEL IAW SRM AND DWG.

Part: SHEAR TIE — CRACKED (BS 616) · airframe 50,412 hrs · 40,557 cycles

SHEAT TIE CRACKED AT BS 616, BETWEEN STR 6R TO STR 7R. REPLACED SHEAR TIE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

TIE CLIP CRACKED AT BS 597, STR 9R. REPLACED CLIP IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

WEB CRACKED BETWEEN BS 787 TO BS 807, RBL 18. REPLACED WEB IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

SHEAR TIE CORRODED AT BS 360, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

TIE CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP IAW EA AND EO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

STRINGER TIE CLIP CRACKED AT BS 663.75, S-10L. REPLACED CLIP IAW SRM AND DWG

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

ANGLE CLIP CRACKED AT BS 706, STR 11R. REPLACED CLIP IAW SRM AND DWG

Part: STRINGER — CORRODED (BS 1115-1128) · airframe 50,412 hrs · 40,557 cycles

STRINGER CORRODED BETWEEN BS 1115 TO BS 1128 RT TORQUE BOX AT UPPER AREA. REPLACED STRINGER IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

ANGLE CLIP CRACKED AT BS 706 AND STR 11L. REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

STRINGER CLIP CRACKED AT BS 360, STR 5L. REPLACED CLIP IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (BS 945 S12R) · airframe 50,412 hrs · 40,557 cycles

SUPPORT ANGLE CRACKED AT BS 945, STR 12R. REPLACED ANGLE IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

STRINGER OF THE RIGHT TORQUE BOX CORRODED AT APU LOWER AREA BETWEEN BS 1115 TO BS 1128. REPLACED STRINGER PER SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

FUSELAGE SKIN CRACKED AT R1 DOOR AFT LOWER CORNER CUTOUT AT BS 328, STR 17R. REPAIRED SKIN IAW SRM AND EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

FLOORBEAM CORRODED AT BS 344, LBL 54. REPAIRED BEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

FLOORBEAM CORRODED AT BS 344, LBL 45. REPAIRED BEAM IAW SRM.

Part: ANGLE — CRACKED (BS 294.5 S16L) · airframe 50,412 hrs · 40,557 cycles

SUPPORT ANGLE CRACKED AT BS 294.5, STR 16L. REPLACED ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

SUPPORT ANGLE CRACKED AT STA 291.5 AND BETWEEN STR 10R TO STR 11R. REPLACED ANGLE PER SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

SUPPORT ANGLE CRACKED AT STA 291.5 AND BETWEEN STR 12R TO STR 13R. REPLACED ANGLE PER SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

STUB FRAME CRACKED AT STA 294.5, STR 7R. REPLACED STUB FRAME IAW SRM AND DWG.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

SUPPORT FITTING CRACK AT BS 332.1, STR 8R. REPLACED FITTING IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

STUB FRAME CRACKED AT BS 294.5,STR 17R. REPLACED STUB FRAME IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

FLOORBEAM CORRODED AT BS 328, BETWEEN LBL 30 TO RBL 65. REPAIRED BEAM IAW SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

LT SIDE STUB BEAM CRACKED AT BS 616. REMOVED AND REPLACED BEAM IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

FUSELAGE SKIN CRACKED ON FWD LOWER CORNER OF L2 DOOR CUTOUT AT BS 951.10, STR 17L. REPAIRED SKIN IAW EA.

Part: FRAME — CORRODED (BS 500D) · airframe 50,412 hrs · 40,557 cycles

FRAME CORRODED AT BS 500D, BETWEEN STR 27R TO STR 28R. REPLACED FRAME IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

FLOORBEAM CORRODED AT BS 986.5, BETWEEN STR 17L TO STR 17R. REPAIRED BEAM IAW EA AND EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

LT SIDE LOWER END OF THE FRAME CRACKED ON THE LOWEST TWO FASTENERS OF THE INNER CHORD LOCATED AT BS 616. REPLACED CHORD IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

FLOORBEAM WEB CRACKED BETWEEN BS 700 TO BS 710, LBL 24.5. REPAIRED WEB IAW EA AND EO.

Part: LENS — BROKEN (CABIN) · airframe 50,412 hrs · 40,557 cycles

BROKEN LENS ASSY IN EMERGENCY EXIT GALLEY NR 4. REMOVED AND REPLACED LENS ASSY IAW AMM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

SHEAR TIE CORRODED AT BS 500, BETWEEN STR 27R TO STR 28R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: LENS — BROKEN (CABIN) · airframe 50,412 hrs · 40,557 cycles

EMERGENCY EXIT LIGHT LENS ASSY BROKEN AT GALLEY 1. REPLACED LENS ASSY PER AMM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

STIFFENER CRACKED AT BS 727, LBL 3. REMOVED AND REPLACED STIFFENER PER SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

FRAME CRACKED AT BS 727E, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,412 hrs · 40,557 cycles

FRAME INNER CHORD CRACKED AT BS 616 RT SIDE. REPAIRED CHORD IAW EA.

Part: STRUCTURE — CRACKED (CENTER WING BOX) · airframe 50,412 hrs · 40,557 cycles

LT CENTER SECTION INNER CHORD CRACKED AT BS 616, STR 17R. REPAIRED CHORD IAW EA AND EO.

Part: STRUCTURE — CRACKED (CENTER WING BOX) · airframe 50,412 hrs · 40,557 cycles

LT CENTER SECTION INNER CHORD CRACKED AT BS 616, STR 17L. REPAIRED CHORD IAW EA AND EO.

Part: LENS — BROKEN (CABIN) · airframe 50,412 hrs · 40,557 cycles

BROKEN LENS EMERGENCY EXIT ON BULLNOSE AT OVERHEAD STOWAGE BIN NR 6. REPLACED LENS IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 50,412 hrs · 40,557 cycles

EMERGENCY SIGN LIGHT ASSY BROKEN ON SIDEWALL PANEL 2319X. REMOVED AND REPLACED LIGHT ASSY IAW AMM 33-51-81.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,412 hrs · 40,557 cycles

EMERGENCY EXIT LIGHT BULB ON SIDEWALL INOP. REMOVED AND REPLACED BULB IAW AMM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 50,412 hrs · 40,557 cycles

AFT CARGO DOOR CRACKED ON LOWER FORWARD FRAME. REMOVED AND REPLACED DOOR IAW AMM & SRM.

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 50,412 hrs · 40,557 cycles

R2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE FRAYED. REMOVED AND REPLACED CABLE IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REPAIRED SPLICE PER ER.

Part: COVER — CRACKED (CABIN) · airframe 49,757 hrs · 40,057 cycles

DURING SCHEDULED HC2 CHECK FOUND, LT EEPLS COVER CRACKED. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 49,717 hrs · 40,025 cycles

L2 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 49,242 hrs · 39,642 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,903 hrs · 38,631 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM AND BAC DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,903 hrs · 38,631 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT AT BS 292.50, WL 260.50. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,903 hrs · 38,631 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT, BS 292.50, WL 259.50. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 47,736 hrs · 38,505 cycles

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

Part: SKIN — DELAMINATED (TE FLAP) · airframe 45,692 hrs · 36,948 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING O/B AFT FLAP INNER SKIN I/B CORNER DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,692 hrs · 36,948 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 672, LBL 24.8. REPAIRED BEAM PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 45,692 hrs · 36,948 cycles

DURING SCHEDULED 14Y CHECK, FOUND PRESSURE DECK WEB STAB BEAM CRACKED AT BS 707, LBL 47. REPAIRED BEAM PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,692 hrs · 36,948 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 7L. REMOVED AND REPLACED CLIP PER ER.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 45,692 hrs · 36,948 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING O/B AFT FLAP LOWER SURFACE DELAMINATED AT INBOARD EDGE. REPAIRED AFT FLAP PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,692 hrs · 36,948 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 45,692 hrs · 36,948 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING O/B AFT FLAP INNER SKIN INBOARD CORNER DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 45,692 hrs · 36,948 cycles

DURING SCHEDULED 14Y CHECK, FOUND PRESSURE BULKHEAD VERTICAL BEAM WEB CRACKED BETWEEN BS 178 TO BS 181, LBL 17. REPAIRED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,692 hrs · 36,948 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 45,692 hrs · 36,948 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 45,692 hrs · 36,948 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL BEAM WEB CRACKED AT BS 711, BL 0. REPAIRED WEB PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,692 hrs · 36,948 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 7L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,692 hrs · 36,948 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,692 hrs · 36,948 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,692 hrs · 36,948 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 7R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,692 hrs · 36,948 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3L. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,692 hrs · 36,948 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5R. REMOVED AND REPLACED CLIP PER SI.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,692 hrs · 36,948 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4L. REMOVED AND REPLACED CLIP PER SI.

Part: TAB — DEBONDED (AILERON) · airframe 45,282 hrs · 36,624 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING AILERON TAB T/E DISBONDED. REMOVED AND REPLACED TAB ASSY PER MM.

Part: COVER — LOOSE (CABIN) · airframe 42,435 hrs · 34,508 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,268 hrs · 34,394 cycles

DURING SCHEDULED SPV CHECK, FOUND EGRESS LIGHT INOP BETWEEN ROW 15 TO ROW 16. REMOVED AND REPLACED BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,268 hrs · 34,394 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 42,022 hrs · 34,223 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY LIGHT PER MM.

Part: COVER — OUT OF POSITION (CABIN) · airframe 41,284 hrs · 33,680 cycles

LT MID CABIN EMERGENCY EXIT LIGHT COVER FELL OFF. SECURED COVER PER MM.

Part: SHEAR TIE — CORRODED (BS 807) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, STR 26L TO 27R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 727D S26L) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 294 S15R) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 294, STR 15R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 520 S8L) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 747 S8R) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 727B S8R) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 947, STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER 25R CORRODED AT BS 727D. REPAIRED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CRACKED AFT SERVICE DOOR LOWER FWD CORNER. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L AND STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500C S8L) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 500C S9L) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: TAB — DELAMINATED (LT AILERON) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING AILERON TAB T/E DELAMINATED. R&R TAB PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. R&R STRINGER CLIP PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD PRESSURE BULKHEAD VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,233 hrs · 32,912 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 40,229 hrs · 32,911 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP OUTBOARD LOWER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 40,131 hrs · 32,842 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 40,132 hrs · 32,842 cycles

L1 DOOR EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: CONNECTOR — CORRODED (CROSSFEED VALVE) · airframe 39,760 hrs · 32,568 cycles

INFLIGHT SHUTDOWN/DECLARED EMERGENCY/DIVERSION. NR 1 ENGINE FAILED AT FL 350, EGT FLUCTUATED. RESTARTED ENGINE AT FL 200. INSPECTED ENGINE FOUND CORRODED CONNECTOR ON CROSSFEED VALVE. REMOVED AND REPLACED VALVE PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 39,732 hrs · 32,549 cycles

R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: ACTUATOR — LOOSE (NR 4 SPOILER) · airframe 36,814 hrs · 30,357 cycles

DURING SCHEDULED HC2 CHECK, FOUND LEFT WING NR 4 SPOILER INBOARD ACTUATOR CASTING LOOSE. REMOVED AND REPLACED ACTUATOR PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 36,841 hrs · 30,357 cycles

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

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 35,139 hrs · 29,100 cycles

DURING SCHEDULED HC1 CHECK, FOUND KEEL BEAM SKIN PANEL CRACKED AT BS 699, STR 27L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,139 hrs · 29,100 cycles

DURING SCHEDULED HC1 CHECK, FOUND KEEL BEAM SKIN CRACKED AT BS 716, STR 27R. REPAIRED SKIN PER SRM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 33,930 hrs · 28,141 cycles

L2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED EVAC SLIDE PER MM.

Part: FLOORBEAM — CORRODED (BS 1016) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM WEB CORRODED AT BS 1016, RBL 5 TO RBL 16. REMOVED AND REPLACED FLOORBEAM WEB SECTION PER SRM.

Part: KEELBEAM — CORRODED (BS 528) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND KEEL BEAM CORRODED AT BS 528, LBL 7, WL 148. REPAIRED KEEL BEAM PER SRM.

Part: TORQUE TUBE — WORN (LT ELEVATOR) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, LT ELEVATOR BUSS LINKAGE FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR OUTPUT TORQUE TUBE PER MM.

Part: RIB — CRACKED (LT WING) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING LOWER RIB CHORD CRACKED AT WBL 135.5, STR 2. REPAIRED CHORD PER ER.

Part: STRINGER CLIP — CORRODED (BS 925) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 925, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CORRODED (BS 993) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 993, RBL 47, WL 212. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 727D) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME SECTION PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 580, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER SPLICE — CRACKED (BS 907 S4R) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: FRAME — CRACKED (BS 907) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 9L. REPAIRED FRAME SECTION PER SRM.

Part: SKIN — CRACKED (BS 378) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST CUTOUT, BS 378, BL 0. REPAIRED SKIN PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 560, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FITTING — LOOSE (L2 DOOR) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED GIRT BAR FITTING PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 1006, RBL 46, WL 209. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: TORQUE TUBE — CORRODED (T/E FLAP) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 9L. REPAIRED FRAME SECTION PER SRM.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT AND RT HORIZONTAL STAB FITTING LUG FACES CORRODED. REPAIRED STAB FITTING PER SRM.

Part: TORQUE TUBE — CORRODED (T/E FLAP) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACCED TORQUE TUBE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 9L. REPAIRED FRAME SECTION PER SRM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND FWD CARGO DOOR CUTOUT, AFT FRAME CORRODED AT BS 492, RBL 26 TO RBL 37. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: TORQUE TUBE — CORRODED (FORE FLAP) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD FOREFLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 9R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 9R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 9R AND STR 9L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 9R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 9R AND STR 9L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 9R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 9L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 9R. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 9L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SKIN — DEBONDED (FORE FLAP) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD FORE FLAP UPPER OUTBOARD SURFACE DISBONDED. REPAIRED FORE FLAP UPPER SURFACE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,393 hrs · 27,708 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 9L. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 32,752 hrs · 27,193 cycles

EMERGENCY EXIT LIGHT LENS LOOSE AT R1 DOOR. SECURED LIGHT LENS PER MM.

Part: COVER — DISLODGED (CABIN) · airframe 31,664 hrs · 26,345 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER FELL OFF. INSTALLED COVER PER MM.

Part: HOOK — LOOSE (L1 DOOR GIRT BAR) · airframe 31,380 hrs · 26,098 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINING HOOK LOOSE. SECURED HOOK PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 31,308 hrs · 26,037 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS STRIP LOOSE AT ROW 8 DEF. SECURED STRIP IAW MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 31,308 hrs · 26,037 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 31,308 hrs · 26,037 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 31,308 hrs · 26,037 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW MM.

Part: GLOWSTRIP — WORN (ROW 8 DEF) · airframe 30,336 hrs · 25,272 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS STRIP WORN AT ROW 8 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 30,207 hrs · 25,165 cycles

LEFT ELEVATOR TAB DELAMINATED. REMOVED AND REPLACED LT ELEVATOR TAB PER MM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 29,800 hrs · 24,837 cycles

AIR TURNBACK/DECLARED EMERGENCY. CLIMBING THROUGH 20,000FT NOTICED LARGE CRACK DEVELOPING ON R1 COCKPIT WINDSHIELD. REMOVED AND REPLACED R1 WINDOW & HEAT CONTROLLER PER MM.

Part: LENS — MISSING (L1 DOOR) · airframe 29,394 hrs · 24,494 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: COVER — OUT OF POSITION (CABIN) · airframe 28,811 hrs · 24,054 cycles

EMERGENCY EXIT LIGHT COVER NEAR F/A JUMPSEAT FELL OFF. SECURED LIGHT COVER PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 28,569 hrs · 23,867 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 27,075 hrs · 22,716 cycles

L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 26,966 hrs · 22,624 cycles

EMERGENCY EXIT LIGHT LENS LOOSE NEXT FWD F/A'S SEAT. REMOVED AND REPLACED LENS ASSY PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 26,789 hrs · 22,483 cycles

DURING SCHEDULED C2 CHECK, FOUND LEFT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED INBOARD AFT T/E FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 26,789 hrs · 22,483 cycles

DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 26,634 hrs · 22,360 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 25,062 hrs · 21,111 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 24,911 hrs · 20,985 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 24,911 hrs · 20,985 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CRACKED AT BS 500A, RBL 15. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 24,911 hrs · 20,985 cycles

DURING SCHEDULED 1/4D CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BL 0. REPAIRED SHEAR TIE PER SRM.

Part: SLIDE — DISLODGED (FWD ENTRY DOOR) · airframe 22,837 hrs · 19,335 cycles

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

Part: LIGHT — DEFECTIVE (CABIN) · airframe 22,270 hrs · 18,868 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT ON BULKHEAD ILLEGIBLE. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (ENTRY DOOR) · airframe 22,270 hrs · 18,868 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 20,868 hrs · 17,799 cycles

FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED EXIT LIGHT PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 20,451 hrs · 17,455 cycles

DURING SCHEDULED C3 CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT LOOSE AT ROW NR 12 DEF. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 20,451 hrs · 17,455 cycles

DURING SCHEDULED C3 CHECK, FOUND RT OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT OTBD T/E AFT FLAP PER MM.

Part: PIN — SHEARED (RT MLG) · airframe 20,277 hrs · 17,309 cycles

DURING APPROACH CREW HEARD LOUD BANG AND AIRCRAFT SHUTTER WHEN GEAR WAS LOWERED. FOUND RT MLG ACTUATOR TRUNNION PIN SHEARED. MX FERRY TO HOU, REMOVED AND REPLACED RT MLG PER MM.

Part: SWITCH — DEFECTIVE (COCKPIT) · airframe 19,522 hrs · 16,668 cycles

DURING FLIGHT, THE FIRE WARNING BELL CAME ON. REMOVED AND REPLACED BELL CUTOUT SWITCH PER MM.

Part: BUSHING — WORN (LT/RT ELEV) · airframe 19,392 hrs · 16,557 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55,BOTH LT AND RT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BUSHINGS ON BOTH LT AND RT TABS PER MM.

Part: LENS — BROKEN (ENTRY DOOR) · airframe 19,334 hrs · 16,509 cycles

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

Part: SIGN — DAMAGED (ENTRY DOOR) · airframe 17,652 hrs · 15,160 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT SIGN DAMAGED. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 16,568 hrs · 14,263 cycles

DURING SCHEDULED 1/2D CHECK, FOUND WEB CRACKED AT BS 178+2, RBL 17.1 & WL 230. R&R WEB PER BFG ER.

Part: COVER — MISSING (CABIN) · airframe 16,000 hrs · 13,759 cycles

EEPLS COVER MISSING AND WIRES EXPOSED AT ROW 16. REPLACED EEPLS COVER AND SECURED WIRES PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 15,537 hrs · 13,381 cycles

FWD ENTRY DOOR EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED LIGHT ASSY PER MM.

Part: COVER — BROKEN (CABIN FLOOR) · airframe 14,968 hrs · 12,937 cycles

EEPLS TRACK COVER BROKEN AT ROW 11. INSTALLED TRACK COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 13,929 hrs · 12,120 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK COVER CRACKED. REPAIRED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,371 hrs · 11,647 cycles

EEPLS LIGHT INOP AT ROW 20. REPAIRED LIGHTS PER MM.

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 12,991 hrs · 11,324 cycles

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

Part: COVER — MISSING (ROW 9) · airframe 12,484 hrs · 10,904 cycles

EEPLS TRACK COVER MISSING AT ROW 9. INSTALLED TRACK COVER PER MM.

Part: COVER — MISSING (CABIN)

FWD ENTRY DOOR EMERGENCY EXIT LIGHT COVER MISSING. REPLACED COVER PER MM.

Part: LIGHT — LOOSE (CABIN)

EEPLS LOOSE IN MID CABIN. REPAIRED LIGHTS PER MM.

Part: LENS — MISSING (CABIN)

FWD EEPLS MISSING LENS AND LOOSE COVER. REMOVED AND REPLACED LENS AND REINSTALLED COVER PER MM.

Part: LIGHT — INOP (ROW 8)

EEPLS LIGHT INOP AT ROW 8. RECONNECTED EEPLS WIRING PER MM.

Part: LENS — MISSING (ROW 8)

EEPLS LIGHT LENS MISSING NEXT TO ROW 8. INSTALLED LENS PER MM.

Part: COVER — OUT OF POSITION (CABIN)

EMERGENCY FLOOR TRACK LIGHTING COVER CAME OFF AT MID CABIN. REPLACED COVER PER MM.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED C1 CHECK, FOUND FLOOR PROXIMITY LIGHTS INOP AT SEAT ROW 12ABC. RELAMPED AND OP CHECKED PER M/M.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EGRESS LIGHT C ROW 7 INOPERATIVE AND MISSING LENS. REMOVED AND REPLACED PER BOEING MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT AFT OF L2 DOOR INOPERATIVE. REMOVED AND REPLACED PER BOEING MM.

Part: LIGHT — LOOSE (CABIN)

DURING WALKAROUND CHECK, FOUND EGRESS LIGHTS MID CABIN CAME LOOSE. REPAIRED PER BOEING MM.

Part: PUMP — LEAKING (B-HYD SYS)

AFTER TAKEOFF, HYDRAULIC SYSTEM B-PUMP PRESSURE LIGHT ILLUM DURING FLT. REMOVED AND REPLACED B-SYS HYD PUMP AND FILTERS PER BOEING MM.

Part: FRAME — DAMAGED (FUSELAGE)

DURING SPECIAL VISIT REPAIR DUE TO GROUND EQUIPMENT DAMAGE, FOUND FUSELAGE FRAMES DAMAGED AT BS 380, RBL 13 TO SPLICE RBL 30, AT BS 360, RBL 13 TO SPLICE RBL 30, AT BS 351, RBL 15, AT BS 344, RBL 15 TO RBL 23, AND AT BS 388, RBL 36. REPLACED DAMAGED FRAME SECTIONS PER BOEING SRM.

Part: BULKHEAD ANGLE — DAMAGED (BS 388)

DURING SPECIAL VISIT REPAIR DUE TO GROUND EQUIPMENT DAMAGE, FOUND FLOOR TO BULKHEAD SUPPORT ANGLE CRACKED AT BS 388, RBL 18. REPLACED ANGLE PER BOEING SRM.

Part: SKIN — DAMAGED (BS 344-385)

DURING SPECIAL VISIT REPAIR DUE TO GROUND EQUIPMENT DAMAGE, FOUND FUSELAGE SKIN DAMAGE AT BS 344-360, S25R, AND AT BS 360-385, S26-27R. REPLACED SKIN SECTION PER BOEING SRM.