N631SW

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 65,157 hrs · 51,287 cycles

L1 DOOR EMERGENCY EXIT PLASTIC COVER LOOSE. SECURED THE COVER IAW SIP.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 64,849 hrs · 51,064 cycles

RT WING NR 6 INBOARD FLAP FAIRING, AFT FAIRING FORWARD SECTION DELAMINATED. R&R FAIRING PER EA.

Part: FAIRING — DELAMINATED (RT WING) · airframe 64,832 hrs · 51,048 cycles

RIGHT WING INBOARD FLAP OUTBOARD NR 6 TRACK FAIRING FORWARD SECTION DELAMINATED. R & R THE FAIRING IAW EA.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 63,724 hrs · 50,297 cycles

R2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW TC.

Part: SKIN — CRACKED (LT WING) · airframe 63,212 hrs · 49,947 cycles

LEFT WING UPPER SKIN CRACKED ABOVE RSS 221, 2ND ROW FWD FROM AFT EDGE. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (LT WING) · airframe 63,212 hrs · 49,947 cycles

LEFT WING UPPER SKIN CRACKED ABOVE RSS 268 AFT ROW. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (RT WING) · airframe 63,212 hrs · 49,947 cycles

RIGHT WING UPPER SKIN CRACKED HOLE, AT RSS 270 AT 11 O'CLOCK POSITION, LOCATED ON AFT ROW REAR SPAR UPPER CHORD. REPAIRED SKIN IAW ER & EA.

Part: SPAR — CRACKED (RT WING) · airframe 63,212 hrs · 49,947 cycles

RIGHT WING REAR SPAR WEB CRACKED AT RSS 186 UPPER ROW. REPAIRED WEB IAW ER & EA.

Part: SKIN — CRACKED (RT WING) · airframe 63,212 hrs · 49,947 cycles

RIGHT WING UPPER SKIN CRACKED HOLES, BETWEEN RSS 250 - 265.5. REPAIRED SKIN IAW ER & EA.

Part: FITTING — CRACKED (RT WING) · airframe 63,212 hrs · 49,947 cycles

RIGHT WING FWD MLG FITTING CRACKED IN HOLE, FWD HOLE COMMON TO LOWER SPAR CHORD RSS 221. REPAIRED FITTING IAW ER & EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 63,212 hrs · 49,947 cycles

LEFT WING AFT FLAP DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: LINK — CORRODED (LT MLG) · airframe 63,212 hrs · 49,947 cycles

LEFT MLG SWING LINK ASSEMBLY CORRODED. REPAIRED LINK ASSEMBLY IAW EA.

Part: LINK — CORRODED (RT MLG) · airframe 63,212 hrs · 49,947 cycles

RIGHT MLG SWING LINK ASSEMBLY CORRODED. REPAIRED LINK ASSEMBLY IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 63,212 hrs · 49,947 cycles

LEFT WING REAR SPAR WEB CRACKED IN NR 5 HOLE. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 63,212 hrs · 49,947 cycles

RIGHT WING REAR SPAR UPPER CHORD CRACKED IN NR 5 HOLE. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 63,212 hrs · 49,947 cycles

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

Part: SPAR — CRACKED (RT WING) · airframe 63,212 hrs · 49,947 cycles

RIGHT WING REAR SPAR WEB CRACKED IN NR 5 HOLE. REPAIRED WEB IAW EA.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 62,621 hrs · 49,559 cycles

LEFT OVERWING DOOR EXIT LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW MM.

Part: SKIN — DAMAGED (RT WING) · airframe 62,192 hrs · 49,268 cycles

RIGHT WING NR 5 SLAT, OTBD AUXILIARY TRACK CUT OUT SKIN DAMAGED. REPAIRED CUT OUT IAW SRM.

Part: HINGE FITTING — CORRODED (LT HORIZ STAB) · airframe 62,192 hrs · 49,268 cycles

LEFT HORIZONTAL STABILIZER CTR SECTION HINGE FITTING CORRODED. R & R FITTING IAW CMM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 328, RBL 12. REPAIRED FLOORBEAM IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

TIE CLIP CRACKED AT BS 277, STRINGER 10R. R & R CLIP IAW SRM & DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

INTERCOSTAL SUPPORT STRUCTURE OUTER LOWER CHORD CRACKED, BETWEEN STRINGER 10R - 11R. R & R CHORD IAW SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

INTERCOSTAL SUPPORT CRACKED AT BS 291.5, STRINGER 10R. R & R SUPPORT IAW SRM & DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

RIGHT LONGITUDINAL FLOORBEAM STIFFENER CRACKED AT BS 663. REPAIRED STIFFENER IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

FRAME WEB CRACKED AT BS 639 AROUND FASTENER, ABOVE FLOOR LEVEL. REPAIRED WEB IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17. REPAIRED WEB IAW SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

STUB BEAM WEB DOUBLER CRACKED, AT BS 639, BBL 45.5. R & R DOUBLER IAW DWG.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

CREASE BEAM WEB CRACKED AT BS 616. R & R CREASE BEAM WEB IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB IAW FAS EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

SKIN CRACKED AT BS 178, LBL 5.7. REPAIRED SKIN IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

RIGHT BODY FRAME INNER CHORD CRACKED AT BS 616, FOURTH FASTENER FROM THE FLOORBEAM. REPAIRED CHORD IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

SHEAR TIE CORRODED AT BS 947, BETWEEN STRINGER 26R - 25R. REPAIRED SHEAR TIE IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

AFT CARGO STRINGER CORRODED, BETWEEN BS 847 - 867, STRINGER 24R. R & R STRINGER IAW SRM & DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

C2 DOOR CUT OUT UPPER SILL WEB CORRODED IN BAY, AFT OF DOOR DAMPER. R & R WEB IAW DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

SHEAR TIE CORRODED AT BS 867, BETWEEN STRINGER 27L - 27R. REPAIRED SHEAR TIE IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

SEAT TRACK CORRODED AT BS 515, RBL 24. R & R SEAT TRACK IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

AFT CARGO FRAME ANGLE CORRODED AT BS 947, BETWEEN STRINGER 26R - 25R. R & R ANGLE IAW SRM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 62,192 hrs · 49,268 cycles

R1 DOOR OVERHEAD EXIT SIGN LENS CRACKED. R & R LENS IAW AMM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

AFT CARGO FRAME, CORRODED AT BS 867, BL 0. REPAIRED FRAME IAW SRM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 62,192 hrs · 49,268 cycles

R2 DOOR OVERHEAD EXIT SIGN LENS CRACKED. R & R LENS IAW AMM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 62,192 hrs · 49,268 cycles

L1 DOOR OVERHEAD EXIT SIGN LENS CRACKED. R & R LENS IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

INTERCOSTAL WEB CRACKED AT BS 277, STRINGER 14R. R & R WEB IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

AFT CARGO FRAME CORRODED AT BS 727E, STRINGER 27L. REPAIRED FRAME IAW DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

AFT CARGO FWD & AFT SIDE OF FRAME CORRODED AT BS 727E, STRINGER 26L. REPAIRED FRAME IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

SHEAR TIE CORRODED AT BS 727C, BETWEEN STRINGER 27L - 26L. R & R SHEAR TIE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

AFT CARGO FRAME CORRODED AT BS 767, BETWEEN STRINGER 27R - 26R. REPAIRED FRAME IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

AFT CARGO SHEAR TIE CORRODED AT BS 727E, STRINGER 27L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 62,192 hrs · 49,268 cycles

FRAME SHEAR TIE CORRODED AT BS 747, STRINGER 25L. R & R SHEAR TIE IAW SRM.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 62,192 hrs · 49,268 cycles

LEFT NLG WW CHORD CRACKED, BS 251, AROUND FASTENER HEAD ON FWD ACCESS CUT OUT. REPAIRED CHORD IAW SRM & EA.

Part: FAIRING — CRACKED (LT PYLON) · airframe 62,192 hrs · 49,268 cycles

LEFT WING AFT UPPER SURFACE, FIXED PYLON FAIRING, CRACKED ON INBD AFT EDGE IN CUT OUT. REPAIRED FAIRING IAW EA.

Part: SPOILER — DELAMINATED (LT WING) · airframe 61,898 hrs · 49,062 cycles

LEFT WING NR 2 SPOILER DELAMINATED. R & R NR 2 SPOILER IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,729 hrs · 48,937 cycles

RIGHT BULLNOSE EMER LIGHT INOPERATIVE AT ROW 9. RELAMPED LIGHT IAW MM.

Part: SELECTOR VALVE — FAULTY (MLG) · airframe 60,994 hrs · 48,424 cycles

AIR TURN BACK, WHEN GEAR HANDLE POSITIONED TO OFF, SUSPECT MAIN GEAR FREE FALL. HIGH FUEL BURN FOR CONFIGURATION. R & R LG SELECTOR VLV IAW MM.

Part: ANGLE — CRACKED (LT AILERON) · airframe 60,262 hrs · 47,939 cycles

LEFT WING AILERON BALANCE BAY VERTICAL ANGLE CRACKED AT RSS 544. R & R ANGLE IAW SRM.

Part: FLAP TRACK — LOOSE (TE FLAP) · airframe 60,262 hrs · 47,939 cycles

LEFT WING MID FLAP INBD AFT FLAP TRACK LOOSE. REPAIRED FLAP TRACK IAW AMM.

Part: SPOILER — LOOSE (LT WING) · airframe 59,501 hrs · 47,442 cycles

LEFT WING INBD GND SPOILER HINGE POINT LOOSE. R & R SPOILER ASSEMBLY IAW MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 58,509 hrs · 46,719 cycles

RIGHT WW FWD CUT OUT ANGLE CRACKED UPPER CORNER. R & R ANGLE IAW DWG & SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 57,452 hrs · 45,971 cycles

R1 DOOR SLIDE OUT OF ADJUSTMENT. R & R SLIDE ASSEMBLY IAW MM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

AFT CARGO BAY FWD BULKHEAD PANEL SUPPORT CRACKED AT BS 727+4 BETWEEN BL 0 TO RBL 5. R & R SPPORT IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

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

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

STRINGER CLIP CORRODED AT BS 947.5 STRINGER 26L. R & R CLIP IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

FWD ENTRY DOOR AFT FRAME CRACKED AT BS 348 STRINGER 15L. REPAIRED FRAME IAW ER & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

SHEAR TIE CORRODED AT BS 767 BETWEEN STRINGER 27L TO STRINGER 26L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

SHEAR TIE CORRODED AT BS 907 BETWEEN STRINGER 27L TO STRINGER 27R. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

SHEAR TIE CORRODED AT BS 727E, BETWEEN STRINGER 27L TO STRINGER 27R. R & R SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

STRINGER CLIP CORRODED AT BS 807 STRINGER 26L. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

STRINGER CLIP CORRODED AT BS 747 STRINGER 26L. R & R CLIP IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

SHEAR TIE CORRODED AT BS 787 BETWEEN STRINGER 26L TO STRINGER 25L. R & R SHEAR TIE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

FWD ENTRY DOOR AFT FRAME ANGLE CRACKED AT BS 348 STRINGER 15L. REPAIRED ANGLE IAW ER & EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

STRINGER CLIP CORRODED BS 787, STRINGER 26R. R & R CLIP IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

STRINGER CLIP CORRODED AT BS 767 STRINGER 26L. R & R CLIP IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

SHEAR TIE CORRODED AT BS 827 BETWEEN STRINGER 25L TO STRINGER 26L. R & R SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

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

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

LONGITUDINAL FLOOR BEAM LOWER CHORD CRACKED AT BS 662 RBL 24.8. REPAIRED CHORD IAW ER & EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

STRINGER CORRODED BETWEEN BS 500C+10 TO BS 500C-10 AT STRINGER 26R. REPAIRED STRINGER IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

LONGITUDINAL FLOOR BEAM VERTICAL WEB CRACKED AT BS 709.4 LBL 24.8. REPAIRED WEB IAW EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

RT KEEL BEAM CORRODED UNDER NUTPLATES BETWEEN BS 727 TO BS 717. REPAIRED BEAM IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

LONGITUDINAL FLOOR BEAM VERTICAL WEB CRACKED AT BS 712.5 LBL 24.8. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

LONGITUDINAL FLOOR BEAM VERTICAL WEB CRACKED AT BS 710.4 LBL 24.8. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

LONGITUDINAL FLOOR BEAM VERTICAL WEB CRACKED AT BS 708.4 LBL 24.8. REPAIRED WEB IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

SHEAR TIE CORRODED AT BS 500D BETWEEN STRINGER 28R TO STRINGER 28L. R & R SHEAR TIE IAW SRM & DRAWING.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

LT KEEL BEAM CORRODED BETWEEN BS 727 TO BS 720. REPAIRED BEAM IAW ER & EA.

Part: MECHANISM — LOOSE (TE FLAP) · airframe 57,020 hrs · 45,674 cycles

LT WING INBD EXHAUST GATE AFT DRIVE CRANK BEARING LOOSE. R & R MECHANISM IAW CMM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 57,020 hrs · 45,674 cycles

MAIN WW PRESS DECK CRACKED AT BS 664 LBL 18. REPAIRED DECK IAW ER & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 727B RBL 45.5. REPAIRED CHORD IAW ER & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED AT BS 709 LBL 24.8. REPAIRED WEB IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 57,020 hrs · 45,674 cycles

MAIN WW PRESS DECK CRACKED AT BS 664 LBL 41. REPAIRED DECK IAW ER & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED AT BS 708 LBL 24.8. REPAIRED WEB IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 57,020 hrs · 45,674 cycles

RT WING INBD FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,020 hrs · 45,674 cycles

LONGITUDINAL FLOOR BEAM UPPER CHORD CRACKED AT BS 667 LBL 24.8. REPAIRED CHORD IAW EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 57,020 hrs · 45,674 cycles

MAIN WW PRESSURE DECK CRACKED AT BS 665 RBL 39. REPAIRED DECK IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 57,020 hrs · 45,674 cycles

MAIN WW PRESS DECK CRACKED AT BS 673 LBL 42. REPAIRED DECK IAW ER & EA.

Part: SUPPORT ANGLE — CRACKED (LT AILERON) · airframe 57,020 hrs · 45,674 cycles

LT WING AILERON WIPER WEB SUPPORT ANGLE CRACKED AT RSS 546. R & R ANGLE IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,959 hrs · 45,631 cycles

CABIN EMERGENCY LIGHTS INOPERATIVE. RELAMPED LIGHTS IAW AMM.

Part: CONNECTOR — BROKEN (CABIN) · airframe 56,953 hrs · 45,630 cycles

EMERGENCY LIGHT CONNECTER ON FWD FACE OF AFT LAVATORY BROKEN. R & R CONNECTOR IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

SKIN CRACKED AT STATION 380, STRINGER 14L. REPAIRED SKIN IAW SWA EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

SHEAR TIE CRACKED AT STATION 500D, BETWEEN STRINGER 11L TO STRINGER 13L. R & R SHEAR TIE IAW SRM & DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

STRINGER CLIP CRACKED AT BS 639, STRINGER 4R. R &R CLPI IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 9R. R & R CLIP IAW SRM & DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 7R. R & R CLIPS IAW SRM & DRAWING.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

SHEAR TIE CRACKED AT BS 360, BETWEEN STRINGER 7R TO STRINGER 6R. R & R SHEAR TIE IAW DRAWING & SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

SHEAR TIE CRACKED AT BS 360, BETWEEN STRINGER 4R TO STRINGER 6R. R & R SHEAR TIE IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

SKIN CRACKED AT BS 380, STRINGER 14R. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

STRINGER CLIP CRACKED AT STATION 400 STRINGER 8L. R & R CLIP IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

RT BS 867+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

RT BS 827+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3 & 8. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

RT BS 787+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2 & 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

LT BS 887+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLES 2 & 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

RT BS 807+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 1-3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

LT BS 807+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

LT BS 887+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3,5 & 9. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

RT BS 847+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

LT BS 847+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 1. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

LT BS 867+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 1. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

RT BS 727A+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 7. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

RT BS 847+10 UP AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

LT BS 827+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3,6 & 9. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

LT BS 807+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

RT BS 867+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2,3 & 9. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

LT BS 767+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

RT BS 807+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

LT BS 787+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

RT BS 767+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 2, 3 & 7. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

RT BS 827+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLES 2 & 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

RT BS 767+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3 & 6. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

RT BS 887+10 UPPER AFT WINDOW SKIN CUTOUT CRACKED AT HOLE NR 4. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

LT BS 827+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLE NR 3. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

FUSELAGE SKIN CRACKED AT BS 847+10, UPPER AFT WINDOW CUTOUT. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,953 hrs · 45,630 cycles

RT BS 787+10 LOWER FWD WINDOW SKIN CUTOUT CRACKED AT HOLES 3,6 & 7. REPAIRED SKIN IAW SB.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 56,926 hrs · 45,610 cycles

FWD OTBD FLASH LIGHT INOPERATIVE. R & R BATTERY IAW MM.

Part: HOUSING — DEFECTIVE (CABIN) · airframe 56,761 hrs · 45,480 cycles

R2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R BATTERY PACK HOUSING IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,761 hrs · 45,480 cycles

R2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.

Part: COVER — LOOSE (CABIN) · airframe 56,732 hrs · 45,460 cycles

RT EMERGENCY EXIT LIGHT COVER ON FORWARD GALLEY LOOSE. R & R COVER IAW AMM SIP.

Part: COVER — CRACKED (CABIN) · airframe 56,582 hrs · 45,346 cycles

FWD ENTRY EMERGENCY EXIT LIGHT COVER CRACKED. R & R LIGHT ASSEMBLY IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,467 hrs · 45,258 cycles

LT EMERGENCY EXIT LIGHTS INOPERATIVE. R&R BATTERY IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,467 hrs · 45,258 cycles

LT EEPLS INOPERATIVE. R&R BATTERY IAW AMM.

Part: STRUCTURE — DAMAGED (LE SLAT) · airframe 55,980 hrs · 44,878 cycles

LT WING NR 1 INBD SLAT TRACK DAMAGED SLAT TRACK CAN. REPAIRED SLAT CAN IAW EA.

Part: COVER — BROKEN (CABIN) · airframe 55,818 hrs · 44,762 cycles

FWD GALLEY EMERGENCY EXIT LIGHT COVER BROKEN. REPAIRED COVER IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 55,341 hrs · 44,412 cycles

CABIN FLOORBEAM TIE STRAP CRACKED AT STA 328. REPAIRED STRAP PER SRM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 55,341 hrs · 44,412 cycles

RIGHT FWD CABIN OVERHEAD BULL NOSE EMERGENCY LIGHT INOP BETWEEN SEAT ROW 4 AND 5. RECONNECTED CONNECTOR PER AMM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 55,341 hrs · 44,412 cycles

CABIN FLOORBEAM TIE STRAP CRACKED AT STA 312. REPAIRED STRAP PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 55,270 hrs · 44,369 cycles

FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENSES PER M/M.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,956 hrs · 44,129 cycles

FUSELAGE SKIN CRACKED AT BS 500D+11, STR 10L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,506 hrs · 43,801 cycles

A .5 INCH SUBSURFACE CRACK ABOVE S5R 1006-5. REPAIRED PER E/A 1-353-21462 FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 53,660 hrs · 43,183 cycles

NR 2 SLAT DELAMINATED O/B END UPPER SURFACE. REMOVED AND REPLACED SLAT ASSY PER MM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 53,660 hrs · 43,183 cycles

MAIN WHEEL WELL CEILING BEADED WEB CRACKED STATION 673, LBL 32. REPAIRED WEB PER SRM.

Part: SPINDLE — CRACKED (TE FLAP) · airframe 53,406 hrs · 42,985 cycles

RIGHT WING O/B MID-FLAP NR 8 SPINDLE CRACKED. REMOVED AND REPLACED NR 8 SPINDLE PER MT.

Part: FASTENER — LOOSE (R1 DOOR) · airframe 52,749 hrs · 42,474 cycles

R1 DOOR EMERGENCY EVAC SLIDE COVER LOWER GIRT HOOKS LOOSE. REMOVED AND REPLACED FASTENERS PER SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 52,749 hrs · 42,474 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER M/M AND MT.

Part: COVER — BROKEN (CABIN) · airframe 52,292 hrs · 42,125 cycles

L1 DOOR EMERGENCY EXIT COVER BROKEN. REMOVED AND REPLACED COVER PER M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,944 hrs · 41,862 cycles

RT EMERGENCY EXIT LIGHT INOP AT OVERHEAD BIN AT ROW 5. REMOVED AND REPLACED BULB PER MM.

Part: RIVET — MISSING (GIRT BAR) · airframe 51,717 hrs · 41,691 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HANGER RIVET MISSING. REPAIRED GIRT BAR ASSY PER M/M.

Part: FITTING — OUT OF POSITION (CABIN) · airframe 51,588 hrs · 41,597 cycles

R1 DOOR GIRT BAR FLOOR FITTINGS OUT OF POSITION. REMOVED AND RE-INSTALLED FITTING PER AMM.

Part: FITTING — OUT OF POSITION (CABIN) · airframe 51,588 hrs · 41,597 cycles

L1 DOOR GIRT BAR FLOOR FITTINGS OUT OF POSITION. REMOVED AND RE-INSTALLED FITTINGS PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

AFT PIT DOOR CUTOUT, FWD FRAME WEB LOWER CORNER CRACKED. REMOVED AND REPLACED WEB AND SPLICE PLATE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 787, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 747+4.5, LBL 8. REMOVED AND REPLACED SUPPORT IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, RBL 45.5. REMOVED AND REPLACED CLIP IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT STUB BEAM WEB CRACKED AT BS 639. REMOVED AND REPLACED WEB IAW SRM AND EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

FLOOR SUPPORT AT BS 927 WL 207.5 BL 0. REMOVED AND REPAIRED FLOOR SUPPORT IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 767+5, LBL 3. REMOVED AND REPLACED SUPPORT IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 727D+5, LBL 3. REPAIRED SUPPORT IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 727D+5, LBL 8. REPAIRED SUPPORT IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727B, BETWEEN BL 0 TO RBL 5. REPAIRED SHEAR TIE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 727D+5, LBL 12. REPAIRED SUPPORT IAW EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO DOOR LOWER SILL ASSY FWD CHANNEL CORRODED AT BS 767. REPAIRED CHANNEL IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 907, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 807, STR 26R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME SUPPORT ANGLE CRACKED AT BS 328, STR 20L. REMOVED AND REPLACED ANGLE PER SRM.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 51,589 hrs · 41,597 cycles

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

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CREASE BEAM WEB CRACKED BETWEEN BS 847 TO BS 827, STR 17L. REMOVED AND REPLACED SHEAR WEB IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

DURING SCHEDULED 16Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17. REPAIRED WEB IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT STUB BEAM AFT I/B ATTACH FLIP CRACKED AT BS 639, LBL 45.5. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: ANGLE — PUNCTURED (FUSELAGE) · airframe 51,448 hrs · 41,748 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME ANGLE PUNCTURED AT BS 500D, LBL 6. REMOVED AND REPLACED ANGLE IAW SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

DURING SCHEDULED 16Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 180, RBL 17.0. REPAIRED WEB PER ER.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

BS 639, RBL 45.5 FLOORBEAM SUPPORT WEB FOUND AT STUB BEAM ATTACH CLIP LOWER FASTENER HOLE CRACKED. REPAIRED WEB PER SEA EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

CORROSION ON FLOOR SUPPORT STA 767+4 LBL 12. REPAIRED SUPPORT PER EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

DURING SCHEDULED 16Y CHECK, FOUND COCKPIT FLOOR CRACKED AT BS 248, RBL 23. REPAIRED FLOOR PER SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

DURING SCHEDULED 16Y CHECK, FOUND COCKPIT FLOOR CRACKED AT BS 248, RBL 17. REPAIRED FLOOR PER SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

CORROSION ON BILGE INTERCOSTAL WEB, STA 727A TO STA 727B, RBL 3. REMOVED AND REPLACED WEB PER BAC DWG AND SRM.

Part: FLAP — PUNCTURED (LT WING) · airframe 51,589 hrs · 41,597 cycles

LEFT WING I/B FORE FLAP PUNCTURED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

BS 520 FRAME CRACKED BETWEEN STR 20R AND STR 21R. REPAIRED FRAME PER SRM AND EA.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

AFT CARGO DOOR LOWER SILL ASSEMBLY FRAME CORRODED AT BS 787, RBL 2. REPAIRED FRAME PER EA.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

ATTACH CLIP CRACKED AT BS 639 RBL 45.5. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 51,589 hrs · 41,597 cycles

AFT PIT FLOOR TEE AT STA 727D+5.6 CORRODED. REMOVED AND REPLACED FLOOR TEE PER SRM AND DWG.

Part: WIRE — BROKEN (CABIN) · airframe 51,589 hrs · 41,597 cycles

G1 GALLEY EXIT SIGN SPLICES BROKEN. REPAIRED WIRE PER BS WPM.

Part: LENS — CRACKED (CABIN) · airframe 51,144 hrs · 41,248 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 51,144 hrs · 41,248 cycles

DURING SCHEDULED CV CHECK FOUND, LT EEPLS LOOSE AT ROW 8. SECURED EEPLS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 50,436 hrs · 41,013 cycles

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

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 50,436 hrs · 41,013 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 787, STR 26L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: SLIDE — UNWANTED DEPLOY (L2 DOOR) · airframe 50,482 hrs · 40,740 cycles

L2 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MT.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,282 hrs · 40,583 cycles

DURING SCHEDULED OTS CHECK, FOUND FRAME CORRODED AT BS 380, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,282 hrs · 40,583 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 360+18, STR 28L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,279 hrs · 40,582 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 360+18, STR 28L. SKIN REPAIRED PER SRM.

Part: LENS — CRACKED (CABIN) · airframe 50,279 hrs · 40,582 cycles

DURING SCHEDULED HC2 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT LENS CRACKED AT ROW 2. REMOVED AND REPLACED LENS PER MM.

Part: LUG — BROKEN (SPOILER) · airframe 50,131 hrs · 40,459 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT WING NR 4 SPOILER I/B CASTING LUG BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,066 hrs · 40,411 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,197 hrs · 39,741 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM.

Part: ACTUATOR — BROKEN (SPOILER) · airframe 46,811 hrs · 37,915 cycles

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

Part: ATTACH FITTING — LOOSE (SPOILER) · airframe 46,811 hrs · 37,915 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 5 SPOILER I/B ATTACH BEARING LOOSE. REMOVED AND REPLACED NR 5 SPOILER PER MM.

Part: SKIN — CRACKED (NR 5 SLAT) · airframe 46,811 hrs · 37,915 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 6 SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 46,811 hrs · 37,915 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 46,811 hrs · 37,915 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 6 SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520D, LBL 10. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO DOOR CUTOUT, FWD FRAME CRACKED AT BS 794.3, BETWEEN RBL 6 TO RBL 20. REMOVED AND REPLACED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO DOOR CUTOUT, FWD FRAME CRACKED AT BS 794, STR 25R. REMOVED AND REPLACED FRAME PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN CRACKED AT BS 522, BETWEEN STR 28L TO STR 28R. REPAIRED SKIN PER AAR EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 27R. REMOVED AND REPLACED CLIP PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 46,630 hrs · 37,780 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING NR 2 SLAT UPPER T/E WEDGE I/B EDGE DELAMINATED. REMOVED AND REPLACED NR 2 SLAT PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520D, BETWEEN RBL 7 TO RBL 11. REMOVED AND REPLACED SHEAR TIE PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 46,630 hrs · 37,780 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

DURING SCHEDULED 14Y CHECK, FOUND FLOORBEAM CRACKED AT BS 727B, RBL 24.8. REPAIRED BEAM PER AAR EA.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 46,630 hrs · 37,780 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING I/B TRAILING EDGE MID FLAP TRAILING EDGE WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PER MM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO COMPT, OUTFLOW VALVE DOUBLER CORRODED BETWEEN BS 980 TO BS 983, BETWEEN STR 23R TO STR 25R. REMOVED AND REPLACED DOUBLER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

DURING SCHEDULED 14Y CHECK, FOUND FWD CARGO FRAME CRACKED AT BS 500C, BETWEEN STR 19R TO STR 22R. REPAIRED FRAME PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR CUTOUT ANGLE CRACKED AT BS 348, STR 15L. REMOVED AND REPLACED ANGLE PER SRM.

Part: SKIN — DEFORMED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN DEFORMED AT BS 511, STR 1. REPAIRED SKIN PER SRM.

Part: SKIN — DEFORMED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN DEFORMED AT BS 469, STR 3R. REPAIRED SKIN PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT LOWER RT FUSELAGE, OUTFLOW VALVE, AFT MIDDLE RETAINER ASSY ANGLE BRACKET CORRODED ON LOWER SURFACE. REMOVED AND REPLACED ANGLE PER BAC DWG AND SRM.

Part: SKIN — DEFORMED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN DEFORMED AT BS 504, STR 2R. REPAIRED SKIN PER SRM.

Part: SKIN — DEFORMED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN DEFORMED AT BS 820, STR 2R. REPAIRED SKIN PER SRM.

Part: SKIN — DEFORMED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN DEFORMED AT BS 384.25, STR 5L. REPAIRED SKIN PER SRM.

Part: SKIN — DEFORMED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN DEFORMED AT BS 508C, STR 1. REPAIRED SKIN PER SRM.

Part: SKIN — DEFORMED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

DURING SCHEDULED 14Y CHECK, FOUND SKIN DEFORMED AT BS 495, STR 2R. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

DURING SCHEDULED 14Y CHECK, FOUND AFT PIT, DOOR STUB FRAME CORRODED AT BS 992.5, BETWEEN STR 17R TO STR 20R. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,630 hrs · 37,780 cycles

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

Part: SKIN — PUNCTURED (FOREFLAP) · airframe 46,171 hrs · 37,451 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING O/B FORE FLAP UPPER SURFACED PUNCTURED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SPOILER — PUNCTURED (LT WIING) · airframe 46,171 hrs · 37,451 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING NR 1 GROUND SPOILER PUNCTURED. REMOVED AND REPLACED SPOILER PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 45,598 hrs · 37,046 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING NR 2 L/E SLAT O/B TRAILING EDGE DELAMINATED. REMOVED AND REPLACED NR 2 SLAT PER MM.

Part: COVER — BROKEN (CABIN) · airframe 44,988 hrs · 36,574 cycles

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

Part: SKIN — CRACKED (RT WING) · airframe 43,998 hrs · 35,862 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING I/B LEADING EDGE HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 43,998 hrs · 35,862 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 1 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 43,528 hrs · 35,530 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FWD CARGO DOORWAY AFT SIDE FRAME CRACKED. REMOVED AND REPLACED FRAME PER ACO.

Part: COVER — BROKEN (CABIN) · airframe 43,546 hrs · 35,543 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,516 hrs · 34,827 cycles

DURING SCHEDULED MV4 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 22. RELAMPED LIGHT PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 42,378 hrs · 34,737 cycles

AFT I/B FLASHLIGHT BATTERY INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 42,313 hrs · 34,699 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 42,313 hrs · 34,699 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: ACTUATOR — FAULTY (NLG) · airframe 41,789 hrs · 34,313 cycles

RAISED GEAR HANDLE TO UP POSITION, NLG WARNING LIGHT ILLUMINATED. LANDING GEAR HANDLE PLACED TO OFF POSITION NLG FELL OUT. REMOVED AND REPLACED NLG RETRACT ACTUATOR PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 41,344 hrs · 33,962 cycles

AFT CABIN EMERGENCY FLASHLIGHT INOP. R&R FLASHLIGHT PER MM.

Part: FRAME — CORRODED (BS 727E S27R) · airframe 40,925 hrs · 33,653 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 727E, STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (BS 727C S27R) · airframe 40,925 hrs · 33,653 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 727C, STR 27R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 500C S8L) · airframe 40,925 hrs · 33,653 cycles

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

Part: FRAME — CRACKED (BS 827 S8L) · airframe 40,925 hrs · 33,653 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 520 S8L) · airframe 40,925 hrs · 33,653 cycles

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

Part: FRAME — CRACKED (BS 500A S8L) · airframe 40,925 hrs · 33,653 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,925 hrs · 33,653 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,925 hrs · 33,653 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,925 hrs · 33,653 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,925 hrs · 33,653 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,925 hrs · 33,653 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,925 hrs · 33,653 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,925 hrs · 33,653 cycles

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

Part: MOUNT — BROKEN (NR 4 SPOILER) · airframe 40,917 hrs · 33,645 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 4 SPOILER OUTBOARD MOUNT LUG BROKEN. REMOVED AND REPLACED SPOILER ACTUATOR PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,489 hrs · 33,338 cycles

DURING SCHEDULED MV1 CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,489 hrs · 33,338 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 480, BL 0. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,489 hrs · 33,338 cycles

DURING SCHEDULED MV1 CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,489 hrs · 33,338 cycles

DURING SCHEDULED MV1 CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 28L. REPAIRED SHEAR TIE PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,137 hrs · 33,075 cycles

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

Part: FITTING — BROKEN (GIRT BAR) · airframe 39,354 hrs · 32,489 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING BROKEN. REMOVED AND REPLACED FITTING PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 37,944 hrs · 31,371 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: FAN — FAULTY (E&E BAY) · airframe 36,383 hrs · 30,193 cycles

CREW REPORTED A SMELL ON CLIMB-OUT, GASPER FAN AND RECIRC FAN TURNED OFF, SMELL DISSIPATED. REMOVED AND REPLACED RECIRC FAN PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,348 hrs · 29,404 cycles

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

Part: SKIN — DEBONDED (RT WING TE FLAP) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD MID FLAP T/E WEDGE DISBONDED. REPAIRED MID FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,165 hrs · 28,532 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R AND STR 8L. REPAIRED FRAME SECTION PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM WEB CORRODED AT RT BS 943 TO RT BS 986. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,165 hrs · 28,532 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME AT FWD CARGO DOOR CUTOUT FWD WEB CRACKED, LOWER CORNER NR 5 DOOR STOP. REPAIRED FRAME WEB PER ER.

Part: CHANNEL — CORRODED (EMERGENCY EXIT) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT OVERWING EMERGENCY EXIT DOOR LOWER CHANNEL CORRODED. REMOVED AND REPLACED LOWER CHANNEL PER SRM.

Part: CHANNEL — CORRODED (EMERGENCY EXIT) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT OVERWING EMERGENCY EXIT DOOR LOWER CHANNEL CORRODED. REMOVED AND REPLACED LOWER CHANNEL PER SRM.

Part: TORQUE TUBE — CORRODED (RT MIDFLAP) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD MID FLAP TORQUE TUBES CORRODED. REMOVED AND REPLACED MID FLAP TORQUE TUBES PER SRM AND CMM.

Part: SKIN — CRACKED (L/E SLAT) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING NR 3 SLAT UPPER SURFACE SKIN CRACKED AT LEADING EDGE. REPAIRED SLAT SKIN PER CMM AND SRM.

Part: SKIN — DEBONDED (LT MIDFLAP) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD MID FLAP AFT LOWER INBOARD SURFACE DISBONDED. REPAIRED MID FLAP PER SRM.

Part: RIB — CORRODED (LT MIDFLAP) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD MID FLAP, INBOARD RIB CORRODED. REMOVED AND REPLACED INBOARD RIB PER SRM AND CMM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME AT AFT CARGO DOOR CUTOUT AFT WEB CRACKED, LOWER CORNER NR 5 DOOR STOP. REPAIRED FRAME WEB PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 34,165 hrs · 28,532 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND CORROSION ON STR 21R AT BS 263. REMOVED AND REPLACED STR SECTION PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,165 hrs · 28,532 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CRACKED AT BS 947, LBL 35 TO LBL 54. REPAIRED FLOORBEAM PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 34,165 hrs · 28,532 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 616, RBL 64, WL 200. REPAIRED FRAME CHORD SECTION PER ER.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 14R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: PIN — CORRODED (RT PYLON) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING PYLON INBOARD MID SPAR FUSE PIN CORRODED. REMOVED AND REPLACED MID SPAR FUSE PIN PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 14R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 34,165 hrs · 28,532 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 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,165 hrs · 28,532 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: HOOK — LOOSE (L1 DOOR) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. REPAIRED GIRT BAR HOOK PER SRM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. REPAIRED GIRT BAR HOOK PER SRM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT STOP PIN CUTOUT BELOW GUIDE ROLLER. REPAIRED DOOR FRAME PER SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING CORRODED AT BS 312, LBL 58. REMOVED AND REPLACED EVAC SLIDE GIRT BAR FITTING PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND STR 23R CRACKED AT BS 496. REPAIRED STRINGER SECTION PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, RBL 7. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — DEBONDED (RT FORE FLAP) · airframe 34,165 hrs · 28,532 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING T/E INBOARD FORE FLAP DISBONDED. REPAIRED FORE FLAP PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 33,219 hrs · 27,818 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR LOWER FUSELAGE HINGE BOX FITTING CRACKED. REMOVED AND REPLACED HINGE BOX FITTING PER SRM.

Part: SKIN — DELAMINATED (RT WING FOREFLAP) · airframe 33,219 hrs · 27,818 cycles

DURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 32,244 hrs · 27,000 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING INBD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 32,244 hrs · 27,000 cycles

DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 31,330 hrs · 26,238 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 28,029 hrs · 23,615 cycles

FWD SERVICE DOOR LOWER EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 27,789 hrs · 23,426 cycles

DURING SCHEDULED RON, FOUND EMERGENCY EXIT BULLNOSE LIGHT AT ROW 17 ABC, DIM. REMOVED AND REPLACED BULLNOSE LIGHT ASSEMBLY PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 27,062 hrs · 22,848 cycles

AT FL 350 COCKPIT R2 OUTER PANE CRACKED WHILE ARCING. REMOVED AND REPLACED COCKPIT R2 WINDOW AND WINDOW HEAT CONTROLLER PER MM.

Part: STRIP — LOOSE (CABIN) · airframe 26,766 hrs · 22,621 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 DEF. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: PIN — CORRODED (LT & RT MLG) · airframe 23,907 hrs · 20,358 cycles

DURING SCHEDULED C3 CHECK, FOUND BOTH LT & RT MLG TRUNNION PINS CORRODED. REMOVED AND REPLACED BOTH LT & RT MLG TRUNNION PINS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 23,027 hrs · 19,681 cycles

DURING SCHEDULED C2 CHECK, FOUND BS 670 KEEL BEAM OUTER SKIN CRACKED 1.1 INCHES ON THE LT AND RT SIDE. REPAIRED SKIN PER SRM AND SWA T1.

Part: LIGHT — BROKEN (CABIN) · airframe 17,332 hrs · 15,066 cycles

DURING SCHEDULED 1/2D CHECK, FOUND EMERGENCY EXIT LIGHT BROKEN AND COVER MISSING AT FWD LAV OUTER WALL. REMOVED AND REPLACED EMERGENCY LIGHT ASSY PER MM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 16,983 hrs · 14,781 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM.

Part: INDICATOR — ERRATIC (ALTIMETER) · airframe 14,371 hrs · 12,618 cycles

DIVERSION, F/O''S ALTIMETER IND ERRATIC AND FLAGS IN VIEW. REMOVED AND REPLACED F/O''S ALTIMETER IND PER MM.

Part: LIGHT — LOOSE (ROW 13)

EEPLS TRACK LOOSE AT ROW 13. SECURED FLOOR TRACK PER MM.

Part: HOLDER — LOOSE (PAX DOORWAY)

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE GIRT BAR HOLDER LOOSE. REMOVED AND REPLACED GIRT BAR HOLDER FASTENER PER MM.

Part: SLIDE — LOW PRESS (CABIN)

DURING WALKAROUND CHECK, FOUND AFT SERVICE DOOR EMERGENCY SLIDE PRESSURE LOW. REMOVED AND REPLACED PER BOEING MM.

Part: GUSSET — DAMAGED (HORIZ STAB)

DURING SCHEDULED C-CHECK, FOUND REAR SPAR OF HORIZ STAB CENTER SECTION GUSSET PLATE DAMAGE ON TOP SIDE. REPAIRED PER BOEING SRM.