N638SW

Part: STRUCTURE — CRACKED (RT WING TE FLAP) · airframe 63,444 hrs · 50,035 cycles

R/H WING OUTBOARD FORE FLAP TRAILING EDGE CRACKED. REPAIRED FORE FLAP IAW SRM.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 63,214 hrs · 49,871 cycles

R1 WINDSHIELD SHATTERED PASSING 23K FT. RETURNED TO DEPARTURE. R & R THE R1 WINDSHIELD IAW MM.

Part: ELEMENT — FAULTY (APU) · airframe 62,484 hrs · 49,410 cycles

AIR TURNBACK, DECLARED EMERGENCY APU FIRE ALARM AND LIGHT CAME ON DURING CLIMB PERFORMED CHECKLIST FIRED BOTTLE DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. R & R APU FIRE DETECTOR ELEMENT IAW AMM.

Part: ESCAPE ROPE — OUT OF POSITION (CABIN) · airframe 62,263 hrs · 49,267 cycles

RIGHT EMERGENCY EXIT ROPE OUT OF POSITION. REPOSITIONED ROPE IAW AMM.

Part: CARRIAGE — CORRODED (LT WING TE FLAP) · airframe 62,263 hrs · 49,267 cycles

LEFT WING NR 2 FLAP CARRIAGE SPINDLE CORRODED AT THE LOWER INSPECTION AREA. R & R THE NR 2 FLAP CARRIAGE IAW MT.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 61,945 hrs · 49,050 cycles

FORWARD FLASHLIGHT SECURITY STRAP BROKEN. R & R STRAP IAW MM.

Part: ANGLE — CRACKED (LT WING) · airframe 61,748 hrs · 48,920 cycles

LEFT WING REAR SPAR RSS 280, FIRE BOX RIB LOWER ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 61,748 hrs · 48,920 cycles

AFT CARGO COMPARTMENT DOOR LOWER FWD CORNER SIDE FRAME, CRACKED OUT OF LOWER INBD FASTENER LOCATION TO STOP FITTING. R & R DOOR IAW AMM & EA.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 61,748 hrs · 48,920 cycles

AFT CARGO COMPARTMENT DOOR SIDE FRAME CRACKED, AT LOWER AFT CORNER INBD FASTENER LOCATION TO STOP FITTING. R & R DOOR IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 61,748 hrs · 48,920 cycles

L2 DOOR EMER EXIT SIGN MOUNTED ON AFT LAVATORY LENS LOCKING TAB BROKEN. R & R SIGN IAW AMM.

Part: BEAM — CRACKED (LT HORIZ STAB) · airframe 61,748 hrs · 48,920 cycles

LEFT HORIZONTAL STABILIZER LOWER TE STRUCTURE, CRACKED ON THE UPPER SURFACE, 12" OTBD OF ELEVATOR STATION 176.64. REPAIRED BEAM IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 61,748 hrs · 48,920 cycles

RIGHT WING TE SKIN FASTENER HOLE CRACKED AT APPROX RSS 251. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 61,748 hrs · 48,920 cycles

RIGHT WING TE SKIN CRACKED AT APPROX RSS 240. REPAIRED SKIN IAW EA.

Part: FITTING — CRACKED (LT WING) · airframe 61,748 hrs · 48,920 cycles

LEFT WING BATHTUB FITTING CRACKED IN BORE HOLE. R & R FITTING IAW DWG & EA.

Part: SKIN — CRACKED (LT WING) · airframe 61,748 hrs · 48,920 cycles

LEFT WING UPPER SKIN TE AT STATION RSS 256, CRACKED IN HOLE. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 61,748 hrs · 48,920 cycles

LEFT WING UPPER SKIN TE AT STATION RSS 228, CRACKED IN HOLE. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 61,748 hrs · 48,920 cycles

LEFT WING UPPER SKIN TE AT STATION RSS 252, CRACKED IN HOLE. REPAIRED SKIN IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

AFT CARGO BAY STRUCTURE BENEATH SHEAR TIE CORRODED AT BS 727E, BETWEEN STRINGER 26L - 27L. R & R FRAME IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

AFT CARGO BAY FRAME SHEAR TIE CORRODED AT BS 727E, BETWEEN STRINGER 26R - 27R. REPAIRED FRAME IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

CREASE BEAM WEB CORRODED AT BS 1000, LBL 45. R & R WEB IAW SRM.

Part: ATTACH FITTING — CRACKED (TE FLAP) · airframe 61,748 hrs · 48,920 cycles

RIGHT WING TE INBD FLAP, OTBD FLAP TRACK FAIRING, INBD ATTACH FITTING ON WING CRACKED. R & R FITTING IAW DWG.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

CREASE BEAM SPLICE CORRODED, BETWEEN BS 1006 - 1016, BETWEEN LBL 40 - 45. R & R SPLICE IAW DWG & SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

AFT CARGO VERTICAL LOWER WEB CORRODED, BETWEEN BS 767 - 787, STRINGER . R & R WEB IAW SRM.

Part: FLAP TRACK — LOOSE (TE FLAP) · airframe 61,748 hrs · 48,920 cycles

LEFT WING OTBD FLAP TRACK LOOSE, 2ND FROM OTBD END. SECURED TRACK IAW CMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

AFT CARGO DOOR CUT OUT FWD LOWER CORNER SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: WEB — CRACKED (RT WING) · airframe 61,748 hrs · 48,920 cycles

RIGHT WING WEB CRACKED AT THE 5 HOLE OF THE AFT SUPPORT FITTING. REPAIRED WEB IAW EA.

Part: WEB — CRACKED (LT WING) · airframe 61,748 hrs · 48,920 cycles

LEFT WING WEB CRACKED AT THE NR 5 HOLE, AFT SUPPORT FITTING, BETWEEN REAR SPAR WEB RSS 211 - RSS 238. REPAIRED WEB IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 8R. R & R CLIP IAW EA.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 61,748 hrs · 48,920 cycles

LEFT WING AFT MLG BEAM SUPPORT FITTING CRACKED AT NR 5 HOLE. R & R FITTING IAW EA & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

STRINGER CLIP CRACKED AT BS 440, STRINGER 8L. R & R CLIP IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

STRINGER CLIP CRACKED AT BS 400, STRINGER 8L. R & R CLIP IAW EA.

Part: STRUCTURE — CRACKED (RT WING) · airframe 61,748 hrs · 48,920 cycles

RIGHT WING UPPER CHORD CRACKED AT OF AFT SPAR FROM INBD ROOT TO RSS 285, NR 5 HOLE. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 61,748 hrs · 48,920 cycles

LEFT WING REAR SPAR UPPER CHORD CRACKED AT NR 5 HOLE. REPAIRED CHORD IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

AFT CARGO COMPARTMENT FRAME WEB CORRODED AT BS 747, BETWEEN STRINGER 27R - 25L. R & R FRAME IAW SRM & DWG.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 61,748 hrs · 48,920 cycles

RIGHT WING MLG AFT SUPPORT FITTING CRACKED AT NR 5 HOLE. R & R FITTING IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

L1 DOOR LOWER HINGE AREA CUT OUT CRACKED AT BS 304.5, WL 238.1. REPAIRED CUT OUT IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

AFT CARGO LT Z ANGLE SPLICE CORRODED AT BS 727D+4. R & R Z ANGLE IAW DWG & SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

L1 DOOR UPPER HINGE AREA CUT OUT CRACKED AT BS 304.7, WL 258.2. REPAIRED CUT OUT IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

L1 DOOR UPPER HINGE AREA CUT OUT CRACKED AT BS 304.3, WL 239.4. REPAIRED CUT OUT IAW SRM.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

AFT CARGO FAILSAFE CHORD CORRODED AT BS 747, BETWEEN STRINGER 26R - 27R. R & R FAILSAFE CHORD IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 807, BETWEEN STRINGER 27R - 27L. REPAIRED SHEAR TIE IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

L1 DOOR LOWER HINGE CUT OUT CRACKED AT BS 304.3, WL 237. REPAIRED CUT OUT IAW EA.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

AFT GALLEY & LAVATORY SHEAR WEB CORRODED AT BS 1016, BETWEEN STRINGER 26R - 27R. R & R SHEAR WEB IAW SRM & DWG.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 61,748 hrs · 48,920 cycles

R1 DOOR AFT FRAME T CHORD AT DOOR STOP CRACKED AT FWD TRIM RADIUS. REPAIRED T CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

L1 DOOR UPPER HINGE AREA CUT OUT CRACKED AT BS 304.5, WL 256.6. REPAIRED CUT OUT IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

AFT CARGO SHEAR TIE CORRODED AT BS 787, BETWEEN STRINGER 26L - 27L. R & R FRAME IAW SRM 5.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

SHEAR TIE CORRODED AT BS 787, BETWEEN STRINGER 27L - 27R. R & R FRAME IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

AFT CARGO CTR SHEAR TIE CORRODED AT BS 747, BETWEEN STRINGER 27R - 27L. REPAIRED FRAME IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

FUSELAGE SHEAR TIE CORRODED AT STATION 500C, BETWEEN STRINGER 28R & 28L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

SHEAR TIE CORRODED AT STATION 500A, BETWEEN STRINGER 28R & 28L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

AFT CARGO BAY SHEAR TIE CORRODED, AT BS 747, BETWEEN STRINGER 26R - 27R. R & R FRAME IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

AFT CARGO BAY SHEAR TIE CORRODED AT BS 787, BETWEEN STRINGER 26R - 27R. R & R FRAME IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

AFT CARGO SHEAR TIE CORRODED AT BS 747, BETWEEN STRINGER 26L - 27L. REPAIRED SHEAR TIE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

AFT CARGO BAY FRAME ATTACH ANGLE CORRODED AT BS 727E, STRINGER 27R. R & R FRAME IAW SRM & DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

AFT CARGO BAY SHEAR TIE CORRODED AT BS 727E, BETWEEN STRINGER 26L - 27L. R & R FRAME IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

FUSELAGE SHEAR TIE CORRODED AT STATION 500B, BETWEEN STRINGER 28R & 28L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

AFT CARGO BAY SHEAR TIE CORRODED AT BS 727E, BETWEEN STRINGER 26R - 27R. R & R FRAME IAW SRM.

Part: ISOLATION VALVE — LEAKING (HYDRAULIC SYS) · airframe 60,423 hrs · 48,032 cycles

DIVERSION, A SYS HYD QTY DECREASED FROM 7/8 TO 3/8 IN 1ST HOUR OF FLIGHT. LOW PRESS LIGHTS DID NOT ILLUMINATE. PRESS REMAINED GOOD AT 3000 PSI AT ALL TIMES. FOUND LEAK IN TAIL SECTION. R & R NR 1 FUEL ACTUATOR MANUAL ISOLATION VLV IAW AMM.

Part: MODULE — FAULTY (FUSELAGE) · airframe 60,423 hrs · 48,032 cycles

DECLARED EMER, A HYD QTY DROPPED SIGNIFICANTLY. R & R MODULAR PACKAGE IAW MM.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 59,248 hrs · 47,187 cycles

R1 DOOR EMER EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. R & R SLIDE IAW MT.

Part: SKIN — CRACKED (L1 DOOR) · airframe 59,061 hrs · 47,052 cycles

L1 DOOR CRACKED AT LOWER HINGE INTERIOR SKIN AT VERTICAL STIFFENER. R & R DOOR IAW MM.

Part: STOP FITTING — CRACKED (L1 DOOR) · airframe 59,061 hrs · 47,052 cycles

L1 DOOR UPPER AFT STOP FITTING CRACKED. R & R DOOR IAW MM.

Part: SKIN — DELAMINATED (RT SPOILER) · airframe 59,026 hrs · 47,033 cycles

RIGHT WING INBD GND SPOILER DELAMINATED ON UPPER SKIN. R & R SPOILER ASSEMBLY IAW AMM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 59,026 hrs · 47,033 cycles

LEFT WING OTBD FORE FLAP DELAMINATED ON LOWER INBD SURFACE. REPAIRED FORE FLAP IAW SRM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 58,587 hrs · 46,748 cycles

L1 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 58,377 hrs · 46,607 cycles

RIGHT AFT EMER LIGHT BEHIND BODY FAIRING INOPERATIVE. R & R LIGHT IAW AMM.

Part: SPOILER — BROKEN (LT WING) · airframe 57,432 hrs · 45,960 cycles

LEFT WING INBD NR 4 GND SPOILER ATTACH POINT OTBD END BROKEN. R & R NR 4 SPOILER IAW AMM.

Part: LENS — OUT OF ADJUST (CABIN) · airframe 57,432 hrs · 45,960 cycles

EMERGENCY EXIT LIGHT LENS COVER OUT OF ADJUSTMENT. ADJUSTED LENS IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 57,290 hrs · 45,860 cycles

FORWARD ENTRY DOOR EMER EXIT LIGHT ASSEMBLY BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: SIGN — MISSING (CABIN) · airframe 56,913 hrs · 45,572 cycles

FORWARD EXIT SIGN MISSING. INSTALLED SIGN IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,101 hrs · 45,012 cycles

RIGHT STOW BIN BULLNOSE EMERGENCY EXIT LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 56,101 hrs · 45,012 cycles

RIGHT LOWER AUXILIARY STRAP DAMAGED AT BS 727. R & R STRAP IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 56,101 hrs · 45,012 cycles

FORWARD ENTRY DOOR UNDER CREASE BEAM WEB CORRODED. R & R WEB IAW SRM & DWG.

Part: FASTENER — MISSING (FUSELAGE) · airframe 56,101 hrs · 45,012 cycles

FRAME INNER CHORD FASTENER MISSING AT BS 348.2, STR 15L. INSTALLED FASTENER IAW EA & DWG.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 56,101 hrs · 45,012 cycles

FORWARD ENTRY DOOR CREASE BEAM CRACKED AT BS 351 AT FLOOR LEVEL. R & R BEAM IAW DWG & SRM.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 56,101 hrs · 45,012 cycles

FORWARD FACE OF 178 BULKHEAD GLIDE SLOPE ANTENNA MOUNT BRACKET CRACKED AT LOWER LT CORNER. REPAIRED MOUNT IAW EA & EA.

Part: ANGLE — CRACKED (LT WING) · airframe 56,101 hrs · 45,012 cycles

LEFT WING TE, RSS 545 AT INBD AILERON AREA, AFT SIDE OTBD CORNER ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 55,937 hrs · 44,902 cycles

R2 DOOR OUTSIDE EMERGENCY LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 55,597 hrs · 44,669 cycles

LT MAIN WW CUTOUT AT FWD UPPER CORNER FAIRING SUPPORT ANGLE CRACKED AT UPPER END. R & R ANGLE IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 55,597 hrs · 44,669 cycles

LT OVERWING EMERGENCY EXIT LIGHT LENS COVER LOOSE. R & R COVER IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,434 hrs · 44,566 cycles

LT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT IAW MM.

Part: WEDGE — CRACKED (TE FLAP) · airframe 55,429 hrs · 44,565 cycles

RT INBD MID FLAP TE WEDGE CRACKED ON BOTTOM SIDE. R & R WEDGE ASSEMBLY IAW MM.

Part: FLAP — DAMAGED (RT WING) · airframe 55,429 hrs · 44,565 cycles

RT INBD AFT FLAP DAMAGE ON TRAIL EDGE. R & R AFT FLAP IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,429 hrs · 44,565 cycles

RT EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.

Part: FUSE — BLOWN (CABIN) · airframe 55,429 hrs · 44,565 cycles

RT BULLNOSE EMERGENCY LIGHTS INOPERATIVE AT ROW 23. R & R FUSE IAW MM.

Part: FUSE — BLOWN (CABIN) · airframe 55,429 hrs · 44,565 cycles

L1 DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. R & R FUSE IAW MM.

Part: LIGHT — CRACKED (CABIN) · airframe 55,429 hrs · 44,565 cycles

AFT LAVATORY MOUNTED EMERGENCY LIGHT CRACKED. R & R LIGHT IAW MM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

INTERCOSTAL UPPER ATTACH ANGLE CRACKED AT STATION 727 BETWEEN STRINGER 4L & STRINGER 5L. R & R ANGLE IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

STRINGER CRACKED AT STATION 440 +10, STRINGER 4R. REPAIRED STRINGER IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

STRINGER SPLICE CRACKED AT STATION 907, STRINGER 11R. REPAIRED SPLICE IAW SRM & DRAWING.

Part: WINDOW — CRACKED (CABIN) · airframe 55,429 hrs · 44,565 cycles

RT BS 440+10 WINDOW CRACKED AT HOLE NR 6. R & R WINDOW IAW BAC DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

LT BS 420+10 WINDOW SKIN CUTOUT CRACKED AT HOLE NR 11. R & R SKIN IAW TC & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

LT BS 767+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1,3,4,5,6 & 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

RT BS 867+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT 3,7 & 8. REPAIRED SKIN IAW TC & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

RT BS 500+10 LOWER AFT SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

LT BS 807+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1,3,4,7 & 10. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

FUSELAGE SKIN CRACKED AT BS 460+10, LOWER AFT WINDOW CUTOUT. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

FUSELAGE SKIN CRACKED AT BS 787+10, LOWER FWD WINDOW CUTOUT. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

RT BS 400+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

LT BS 887+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2,4,5 & 6. REPAIRED SKIN IAW DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

LT BS 520+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 4,5 & 6. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

RT BS 360+10 UPPER FWD SKIN CUTOUT CRACKED AT HOLES 1,4,5 & 6. REPAIRED SKIN IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

STRINGER CRACKED AT BS 500D+10, STRINGER 10R. REPAIRED STRINGER IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

RT BS 500C+10 LOWER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

LT BS 380+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLES 4,5 & 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

LT BS 787+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 4,5,6 & 8. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

RT BS 847+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 3,5,7 & 8. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

LT BS 767+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLES 1,2,3,5,7 & 8. REPAIRED SKIN IAW SB.

Part: FRAME — WORN (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

FRAME WORN AT STATION 380, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

LT BS 420+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLES 5,6,11 & 12. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

RT BS 887+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 4 - 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

RT BS 767+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED BETWEEN 1, 2 ,3, 6, 7, 8 & 9. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

LT BS 787+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLES 4,6,7,8 & 11. REPAIRED SKIN IAW TC & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

LT BS 500A+10 UPPER FWD WINDOW SKIN CUTOUT CRACKED AT HOLES 3,5,6 & 7. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

FUSELAGE SKIN CRACKED AT BS 440+10, LOWER AFT WINDOW CUTOUT. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,429 hrs · 44,565 cycles

RT BS 500C+10 UPPER FWD SKIN CUTOUT CRACKED AT HOLE NR 2 & NR 3. REPAIRED SKIN IAW SB & TC.

Part: COVER — LOOSE (EXIT SIGN) · airframe 55,131 hrs · 44,353 cycles

RT OVER WING EMERGENCY EXIT SIGN COVER LOOSE. R & R COVER ASSEMBLY IAW MM.

Part: FLAP TRACK — CORRODED (LT WING) · airframe 55,117 hrs · 44,342 cycles

LT WING NR 2 TE FLAP TRACK CORRODED AT AFT ATTACH POINT. R & R TRACK IAW MM.

Part: FLAP TRACK — CORRODED (RT WING) · airframe 55,117 hrs · 44,342 cycles

RT WING NR 7 FLAP TRACK CORRODED AT ATTACH POINT TO WING AREA ON AFT SIDE. R &R TRACK IAW MM.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 54,731 hrs · 44,044 cycles

DIRTY SOCK SMELL DURING FLIGHT. R&R RT COALESCER BAG IAW MM.

Part: STOP — BROKEN (LE SLAT) · airframe 53,992 hrs · 43,491 cycles

RT WING NR 5 L/E SLAT INBD TRACK DOWNSTOP BROKEN. R & R DOWNSTOP IAW AMM.

Part: STOP — BROKEN (LE SLAT) · airframe 53,992 hrs · 43,491 cycles

RT WING NR 5 L/E SLAT OTBD TRACK DOWNSTOP BROKEN. R & R DOWNSTOP IAW AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 53,992 hrs · 43,491 cycles

RT WING NR 5 L/E SLAT LOWER SKIN LOWER FASTENER ROW AT OTBD END CRACKED. R & R NR 5 L/E SLAT ASSY IAW MM.

Part: SKIN — CRACKED (RT WING) · airframe 53,992 hrs · 43,491 cycles

RIGHT WING INBD FIXED L/E SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: ACTUATOR — LEAKING (SPOILERS) · airframe 53,992 hrs · 43,491 cycles

RIGHT WING T/E INBD GROUND SPOILER OTBD SPOILER ACTUATOR LEAKED. R & R ACTUATOR IAW AMM.

Part: ACTUATOR — BROKEN (LT SPOILER) · airframe 53,985 hrs · 43,486 cycles

LEFT WING INBOARD NR 4 GROUND SPOILER INBOARD ACTUATOR FWD ATTACH FITTING BROKEN. REMOVED AND REPLACED ACTUATOR PER M/M.

Part: ACTUATOR — MALFUNCTIONED (LT MLG) · airframe 52,736 hrs · 42,623 cycles

LEFT MAIN GEAR DID NOT GREEN LIGHT ON EXTENSION RECYCLED LANDING. GEAR HANDLE & ALL LIGHTS NORMAL. REMOVED AND REPLACED LEFT MLG UPLOCK ACTUATOR OPS & LEAK CHECK OK PER M/M. PN: 65-44810-6, 6605 SN ON: 3431 PN: 65-44825-18.

Part: BATTERY — WEAK (CABIN) · airframe 52,349 hrs · 42,338 cycles

AFT LEFT EMERGENCY EXIT LIGHT POWER SUPPLY BATTERY WEAK. REMOVED AND REPLACED BATTERY PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 52,319 hrs · 42,317 cycles

SKIN CRACKED AT BS 758, STR 10R. REPAIRED SKIN IAW EA.

Part: HOOK — LOOSE (R1 DOOR) · airframe 51,636 hrs · 41,810 cycles

R1 DOOR EMERGENCY EVAC SLDIE AFT GIRT BAR HOOK LOOSE. SECURED HOOK ASSY PER SRM.

Part: HOOK — LOOSE (L1 DOOR) · airframe 51,636 hrs · 41,810 cycles

L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK ASSY PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,505 hrs · 41,707 cycles

AFT CABIN EEPLS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: WEB — CORRODED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

WEB CORRODED BETWEEN BS 847 TO BS 867, STR 25R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

CHANNEL CORRODED BETWEEN BS 767 TO BS 787, RBL 8.10. REPAIRED CHANNEL PER EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

SUPPORT ANGLE CRACKED AT BS 380, BETWEEN STR 27R TO STR 26R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

ANGLE CORRODED AT BS 807, STR 27L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

STRINGER CORRODED AT BS 907+8, STR 25L. REPAIRED STRINGER IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

CHANNEL CORRODED AT BS 772, RBL 3. REMOVED AND REPLACED ANGLE IAW EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

WEB CORRODED BETWEEN BS 360 TO BS 380, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

FLOORBEAM CRACKED AT BS 328, LBL 50. REPAIRED BEAM PER SRM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

SHEAR WEB CORRODED BETWEEN BS 767 TO BS 787, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

TIE CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

STUB FRAME CRACKED AT BS 959.9, STR 17L. REPAIRED FRAME IAW EO AND EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

STRINGER CORRODED AT BS 867, STR 26R. REPAIRED STRINGER IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

TIE CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

CRACK ON L2 DOOR CUTOUT FUSELAGE SKIN FITTING CRACKED AT CUT OUT FWD LOWER CORNER. REMOVED AND REPLACED FITTING IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

TIE CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

STRINGER SPLICE CORRODED BETWEEN BS 1006 TO BS 1016, STR 26R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

FRAME CORRODED AT BS 807, BETWEEN STR 27L TO STR 26L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

FRAME CRACKED AT BS 787, BETWEEN STR 27L TO STR 26L. REPAIRED FRAME IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

STRINGER CORRODED BETWEEN BS 957 TO BS 1016, STR 27L. REPAIRED STRINGER IAW SRM.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

TIE CLIP CORRODED AT BS 907, STR 26R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

SHEAR TIE CORRODED AT BS 1006, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

TIE CLIP CORRODED AT BS 807, STR 26R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

FRAME CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

FRAME CORRODED AT BS 1006, BETWEEN STR 21R TO STR 23R. REPAIRED FRAME IAW EO AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

FRAME CORRODED AT BS 787, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

TIE CLIP CRACKED AT BS 597, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

Z-ANGLE CORRODED BETWEEN BS 277 AND BS 360, RBL 59. REMOVED AND REPLACED Z-ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

TIE CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (CABIN) · airframe 50,763 hrs · 41,146 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

FRAME CRACKED AT BS 847, BETWEEN STR 12L TO STR 13L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

FRAME CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

TIE CLIP CRACKED AT BS 907, STR 8R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: LIGHT — BROKEN (CABIN) · airframe 50,763 hrs · 41,146 cycles

AFT LAVATORY WALL EMERGENCY LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW AMM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

TIE CLIP CRACKED AT BS 500B, STR 27R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

SUPPORT ANGLE CRACKED AT BS 291.5, BETWEEN STR 11R TO STR 12R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

FLOORBEAM CRACKED AT BS 947.5, LBL 54. REPAIRED BEAM IAW SRM.

Part: LENS — BROKEN (CABIN) · airframe 50,763 hrs · 41,146 cycles

EMERGENCY EXIT LIGHT LENS BROKEN AT GALLEY 4. REMOVED AND REPLACED LENS IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

R1 DOOR SKIN CUTOUT CRACKED AT BS 328, STR 17R. REPAIRED SKIN IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

Z-ANGLE CORRODED BETWEEN BS 947.5 TO BS 986.5, STR 17R. REMOVED AND REPLACED Z-ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

SKIN CRACKED AT BS 959.9, STR 17L. REPAIRED SKIN IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

Z-ANGLE CORRODED BETWEEN BS 947.5 TO BS 986.5, STR 17L. REMOVED AND REPLACED Z-ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

SKIN CRACKED AT BS 961, STR 17L. REPAIRED SKIN IAW SRM.

Part: WEB — CRACKED (NLG WW) · airframe 50,763 hrs · 41,146 cycles

LT SIDE NLG WHEEL WEB CRACKED AT BS 259.5, WL 180. REPAIRED WEB IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 45.5. REPAIRED CHORD IAW EA & EO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

STUB FRAME CRACKED AT BS 296.5, STR 7R. REPAIRED FRAME IAW E/A AND E/O.

Part: FITTING — CRACKED (LT MLG) · airframe 50,763 hrs · 41,146 cycles

LT MAIN LANDING GEAR SUPPORT STRUCTURE LOWER SURFACE CRACKED ON FITTING ASSY. REMOVED AND REPLACED FITTING ASSY IAW AMM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED BETWEEN BS 706 TO BS 711, LBL 24.5. REPAIRED WEB IAW EO AND EA.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 50,763 hrs · 41,146 cycles

LONGITUDINAL FLOORBEAM ATTACHMENT CLIP CRACKED AT BS 639, LBL 45.5. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: LUG — BROKEN (NR 4 SPOILER) · airframe 50,725 hrs · 41,118 cycles

LT WING NR 4 GROUND SPOILER O/B ACTUATOR CASTING AT WBL 149.25 AFT MOUNT SUPPORT LUG BROKEN. REPAIRED LUG PER EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,725 hrs · 41,118 cycles

RT WING NR 6 SLAT LOWER LEADING EDGE CRACKED AT O/B AUX TRACK. REPAIRED SKIN PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REPAIRED SKIN IAW ER.

Part: SPOILER — DELAMINATED (RT WING) · airframe 48,469 hrs · 39,387 cycles

RT WING NR 6 FLIGHT SPOILER DELAMINATED. REMOVED AND REPLACED NR 6 SPOILER PER MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 48,252 hrs · 39,227 cycles

DURING SCHEDULED CV CHECK FOUND, R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,218 hrs · 39,203 cycles

DURING SCHEDULED RON CHECK FOUND, SKIN CRACKED AT BS 500D+12, STR 10L. REPAIRED SKIN PER EA.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 48,218 hrs · 39,203 cycles

DURING SCHEDULED RON CHECK FOUND, R2 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: FLAP — PUNCTURED (RT WING) · airframe 46,809 hrs · 38,132 cycles

DURING SCHEDULED OTS CHECK, FOUND RT WING I/B MID FLAP PUNCTURED. REMOVED AND REPLACED MID FLAP PER MM.

Part: LENS — LOOSE (CABIN) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND FWD OVERHEAD BULLNOSE EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS PER SOPM.

Part: WEB — CRACKED (FUSELAGE) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND WEB CRACKED AT BS 182, RBL 17. REPAIRED WEB PER EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND WEB CRACKED AT BS 178, LBL 17.1. REPAIRED WEB PER EA.

Part: LIGHT — BROKEN (CABIN) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND EMERGENCY EXIT LIGHT LOCATED ON AFT WALL OF FWD LAV LENS ATTACH TAB BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CORRODED AT BS 500D, STR 27R. REPAIRED STRINGER PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT OUTER CHORD CRACKED AT BS 178, WL 207. REPAIRED CHORD PER ACO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT OUTER CHORD CRACKED AT BS 178, WL 207. REPAIRED CHORD PER ACO.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED CLIP PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND FLOORBEAM CRACKED AT BS 668, LBL 24. REPAIRED BEAM PER EA.

Part: BRACKET — CRACKED (R2 DOOR) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LOWER FWD SIDE MOUNT BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 46,701 hrs · 38,053 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED SPLICE PER SRM AND BAC DWG.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING NR 2 SLAT T/E EDGE WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: WEDGE — PUNCTURED (MIDFLAP) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING I/B MID FLAP T/E WEDGE PUNCTURED AT LOWER SURFACE I/B END. REPAIRED MID FLAP PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED CLIP PER SRM AND SI.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER AAR EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,701 hrs · 38,053 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8L. REMOVED AND REPLACED CLIP PER SRM AND SI.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,701 hrs · 38,053 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727A, STR 8L. REPAIRED FRAME PER EA.

Part: LIGHT — DAMAGED (CABIN) · airframe 45,702 hrs · 37,258 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND RT EEPLS DAMAGED AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 45,702 hrs · 37,258 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND LT EEPLS DAMAGED AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 45,452 hrs · 37,056 cycles

L1 DOOR EMERGENCY EXIT SIGN COVER LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 44,112 hrs · 36,047 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING T/E FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SIGN — FADED (CABIN) · airframe 44,112 hrs · 36,047 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT LENS LETTERING FADED. REMOVED AND REPLACED SIGN PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,098 hrs · 36,033 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO COMPARTMENT FWD FRAME CRACKED AT BS 440. REMOVED AND REPLACED FRAME PER ACO.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 44,098 hrs · 36,033 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED BETWEEN BS 455 TO BS 481, STR 27R. REPAIRED STRINGER PER SRM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 42,648 hrs · 34,937 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: LENS — LOOSE (CABIN) · airframe 42,648 hrs · 34,937 cycles

DURING SCHEDULED HC1 CHECK, FOUND BULLNOSE LIGHT LENS LOOSE AT ROW 23. SECURED LENS PER MM.

Part: TAB — CRACKED (ELEVATOR) · airframe 40,785 hrs · 33,591 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT ELEVATOR TAB CRACKED AT UPPER LEADING EDGE I/B SIDE OF I/B HINGE CUTOUT. REMOVED AND REPLACED TAB PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,816 hrs · 33,618 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26R TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,785 hrs · 33,591 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT MAIN WHEEL WELL LOWER CHORD SKIN CRACKED AT BS 679. REMOVED AND REPLACED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,816 hrs · 33,618 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 27R TO STR 27L, WL 148. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 40,816 hrs · 33,618 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE BELLY SKIN CORRODED BETWEEN BS 445 TO BS 455, WL 148, BETWEEN RBL 5 TO LBL 5. REPAIRED SKIN PER PAE ER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,816 hrs · 33,618 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 727E, RBL 17, WL 150. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,816 hrs · 33,618 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 10R. REPAIRED SKIN PER SWA EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 40,785 hrs · 33,591 cycles

DURING SCHEDULED 12Y CHECK, FOUND HORIZONTAL WEB CRACKED AT BS 178, LBL 18. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 40,785 hrs · 33,591 cycles

DURING SCHEDULED 12Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 180, LBL 17. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 40,785 hrs · 33,591 cycles

DURING SCHEDULED 12Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 184, LBL 17. REPAIRED WEB PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 40,785 hrs · 33,591 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING NR 2 SLAT T/E WEDGE O/B END DELAMINATED. REPAIRED WEDGE PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 40,303 hrs · 33,250 cycles

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

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 40,058 hrs · 33,070 cycles

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

Part: SIGN — LOOSE (EMERGENCY LIGHT) · airframe 40,030 hrs · 33,047 cycles

LEFT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: LENS — LOOSE (CABIN) · airframe 39,920 hrs · 32,974 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 39,920 hrs · 32,974 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 38,750 hrs · 32,108 cycles

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

Part: SKIN — CRACKED (BS 510 S10R) · airframe 36,301 hrs · 30,198 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 10R. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 510 S10R) · airframe 36,301 hrs · 30,198 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 10R. REPAIRED SKIN PER SWA EA.

Part: TAB — CRACKED (LT ELEVATOR) · airframe 34,298 hrs · 28,663 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT ELEVATOR TAB CRACKED AT INBOARD CONTROL ROD ATTACH POINT. REMOVED AND REPLACED ELEVATOR TAB PER MM.

Part: TAB — CRACKED (RT ELEVATOR) · airframe 34,298 hrs · 28,663 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT ELEVATOR TAB CRACKED AT INBOARD CONTROL ROD ATTACH POINT. REMOVED AND REPLACED ELEVATOR TAB PER MM.

Part: SKIN — CRACKED (R2 DOOR) · airframe 34,298 hrs · 28,663 cycles

DURING SCHEDULED 10Y CHECK, FOUND R2 DOOR SKIN CRACKED AT LOWER FWD CORNER. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (BS 827 S8L-8R) · airframe 34,298 hrs · 28,663 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L AND STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 867 S8R) · airframe 34,298 hrs · 28,663 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 907 S8R) · airframe 34,298 hrs · 28,663 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 663 S10L) · airframe 34,298 hrs · 28,663 cycles

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

Part: FRAME — CRACKED (BS 440 S8R) · airframe 34,298 hrs · 28,663 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 663 S10R) · airframe 34,298 hrs · 28,663 cycles

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

Part: FRAME — CRACKED (BS 787 S8L) · airframe 34,298 hrs · 28,663 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 908 S8L) · airframe 34,298 hrs · 28,663 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 908, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 480 S8L) · airframe 34,298 hrs · 28,663 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 867 S8L) · airframe 34,298 hrs · 28,663 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 440 S8L) · airframe 34,298 hrs · 28,663 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 706 S11L) · airframe 34,298 hrs · 28,663 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 (BS 663 S10L) · airframe 34,298 hrs · 28,663 cycles

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

Part: FRAME — CRACKED (BS 380 S8L) · airframe 34,298 hrs · 28,663 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 787 S8R) · airframe 34,298 hrs · 28,663 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 480 S8R) · airframe 34,298 hrs · 28,663 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 400 S8L-8R) · airframe 34,298 hrs · 28,663 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L AND STR 8R. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,298 hrs · 28,663 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT LT BS 616, WL 208. REPAIRED FRAME SECTION PER SWA EA.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 34,298 hrs · 28,663 cycles

DURING SCHEDULED 10Y CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 665, RBL 39. REPAIRED PRESSURE WEB IAW SWA EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 34,298 hrs · 28,663 cycles

DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CRACKED AT BS 328, LBL 28. REPAIRED FLOORBEAM PER SRM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 33,089 hrs · 27,717 cycles

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

Part: STRIP — LOOSE (EMERGENCY LIGHT) · airframe 30,886 hrs · 27,553 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 7 ABC. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 32,739 hrs · 27,436 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR SLIDE PER MM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 32,739 hrs · 27,436 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED R1 DOOR GIRT BAR HOOKS PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 30,736 hrs · 25,839 cycles

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

Part: LENS — MISSING (EMERGENCY LIGHT)

L1 DOOR EMERGENCY EXIT SIGN LENS COVER MISSING. INSTALLED LENS PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 29,123 hrs · 24,530 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. SLIDE DID NOT DEPLOY. REINSTALLED SLIDE PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 28,795 hrs · 24,265 cycles

EEPLS FLOOR STRIP LOOSE AT ROW 9L. RESECURED EEPLS FLOOR STRIP PER MM.

Part: COVER — MISSING (CABIN) · airframe 28,752 hrs · 24,238 cycles

FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT COVER, MISSING. REMOVED AND REPLACED COVER PER MM.

Part: STRIP — LOOSE (CABIN) · airframe 28,752 hrs · 24,238 cycles

EEPLS LIGHT STRIP AT ROW 9 ABC, LOOSE. SECURED EEPLS STRIP PER MM.

Part: LIGHT — LOOSE (ROWS 6 & 7) · airframe 28,134 hrs · 23,741 cycles

EEPLS STRIP AT ROWS 6 AND 7 DEF, LOOSE. REPAIRED EEPLS STRIP PER MM.

Part: STRUCTURE — DELAMINATED (T/E FLAP) · airframe 28,073 hrs · 23,693 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING INBOARD T/E AFT FLAP PER MM.

Part: STRUCTURE — DELAMINATED (T/E FLAP) · airframe 28,073 hrs · 23,693 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,318 hrs · 22,274 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR LOWER HINGE BOX FITTING, CRACKED. REPAIRED HINGE BOX FITTING PER EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,318 hrs · 22,274 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE BOX FITTING, CRACKED. REPAIRED HINGE BOX FITTING PER EA.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 24,608 hrs · 20,936 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM.

Part: THROTTLE — FOD (NR 2 ENGINE) · airframe 24,020 hrs · 20,476 cycles

DECLARED EMERGENCY, AIR TURNBACK, IN FLIGHT SHUTDOWN, NR 2 ENGINE THROTTLE LEVER COULD NOT BE REDUCED BELOW 89.5 PERCENT. FOUND FOREIGN OBJECT DEBRIS INSIDE THROTTLE QUADRANT BOX. REMOVED DEBRIS, OPS CHECKED GOOD PER MM.

Part: HOOK — LOOSE (ENTRY DOOR) · airframe 18,280 hrs · 15,800 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 17,865 hrs · 15,438 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,396 hrs · 37,036 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: WIRE — EXPOSED (CABIN) · airframe 17,152 hrs · 14,854 cycles

EEPLS WIRING EXPOSED AT ROW 12. SECURED EEPLS WIRING PER MM.

Part: LENS — LOOSE (CABIN) · airframe 16,596 hrs · 14,403 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD OVERHEAD EXIT SIGN LENS LOOSE. SECURED LENS PER MM.

Part: BEARING — WORN (LT ELEVATOR) · airframe 15,639 hrs · 13,598 cycles

DURING SCHEDULED C2 CHECK, LT ELEVATOR FAILED HINGE PLAY INSPECTION. REMOVED AND REPLACED ELEVATOR PUSH ROD BEARING PER MM.

Part: COVER — LOOSE (CABIN) · airframe 15,639 hrs · 13,598 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER LOOSE AT ROW 11. SECURED TRACK COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 15,285 hrs · 13,303 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS TRACK COVERS MISSING AT ROWS 16 & 18. INSTALLED TRACK COVERS PER MM.

Part: WIRE — EXPOSED (CABIN FLOOR) · airframe 14,878 hrs · 12,984 cycles

EEPLS WIRES EXPOSED AT OVERWING EXIT. SECURED WIRING PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 14,603 hrs · 12,759 cycles

EEPLS WIRING EXPOSED AT OVERWING EXIT. INSTALLED TRACK COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 14,219 hrs · 12,453 cycles

EEPLS COVER MISSING. INSTALLED COVER PER MM.

Part: INDICATOR — DISLODGED (ESCAPE SLIDE)

DURING SCHEDULED BC2 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: CONTROLLER — MALFUNCTIONED (CABIN)

AIR TURNBACK PRESSURIZATION FAIL IN AUTO. AC MADE AN UNEVENTFUL LANDING. PERFORMED BITE TEST ON BOTH LT AND RT PRESS CONTROLLERS PER BOEING MM, SYSTEM OPS NORMAL. NO FAULTS NO LEAKS FOUND.

Part: HINGE — BENT (LAV SERVICE DOOR)

AIRCRAFT RETURNED TO DAL DUE TO FWD LAVATORY SERVICE DOOR OPEN AND STRIKING AGAINST SIDE OF FUSELAGE IN FLIGHT. INSPECTED AREA, REMOVED AND REPLACED DOOR HINGE. CHECKED DOOR OPERATION AND CONTINUED PER BOEING M/M.