N522SW

Part: LIGHT — LOOSE (CABIN) · airframe 71,026 hrs · 67,300 cycles

RIGHT BULLNOSE EMER LIGHT LOOSE AT ROW 1. SECURED LIGHT IAW MM.

Part: FITTING — CRACKED (LT PYLON) · airframe 70,871 hrs · 67,128 cycles

LEFT PYLON STRUCTURE INTERFACE FITTING CRACKED, BETWEEN WBL 185 - 201. R & R FITTING IAW SRM & DWG.

Part: LIGHT — CRACKED (CABIN) · airframe 70,871 hrs · 67,128 cycles

AFT CABIN PHOTO LUMINESCENT FLOOR PROXIMITY LIGHTING CRACKED. R & R LIGHT IAW AMM.

Part: SUPPORT — CRACKED (LT WING) · airframe 70,871 hrs · 67,128 cycles

LEFT WING ON INBD FLAP, OTBD TRACK NR 3 FAIRING SUPPORT CRACKED. R & R SUPPORT IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

TIE CLIP CRACKED AT BS 767, STRINGER 23L. R & R TIE CLIP IAW SRM & DWG.

Part: PLATE — DELAMINATED (R1 DOOR) · airframe 70,871 hrs · 67,128 cycles

R1 DOOR EMER EVAC SLIDE, PLATE ASSEMBLY ADAPTER FLOOR MOUNT DELAMINATED. R & R PLATE ASSEMBLY IAW AMM.

Part: PLATE — DELAMINATED (R2 DOOR) · airframe 70,871 hrs · 67,128 cycles

R2 DOOR EMER EVAC SLIDE, PLATE ASSEMBLY ADAPTER FLOOR MOUNT DELAMINATED. R & R PLATE ASSEMBLY IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

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

Part: ANGLE — CRACKED (RT WING) · airframe 70,871 hrs · 67,128 cycles

RIGHT WING INBD FLAP, OTBD TRACK NR 6 FAIRING LOWER ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

INTERCOSTAL WEB CRACKED, BETWEEN BS 460 - 480, STRINGER 26R. R & R INTERCOSTAL IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

SKIN CRACKED AT BS 259.5, BETWEEN STRINGER 18L - 24L. REPAIRED SKIN IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

L1 DOOR FLOOR STRUCTURE SUPPORT ANGLE CRACKED, BETWEEN BS 312 - 344. R & R ANGLE IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

WEB CRACKED BETWEEN BS 188 - 194, STRINGER 17R. R & R WEB IAW SRM & DWG.

Part: SPAR — CRACKED (RT WING) · airframe 70,871 hrs · 67,128 cycles

RIGHT WING REAR SPAR WEB CRACKED, BETWEEN RSS 224.14 - 230. REPAIRED WEB IAW EO & EA.

Part: BRACKET — CRACKED (TE FLAP) · airframe 70,871 hrs · 67,128 cycles

RIGHT WING NR 7 MOVABLE FAIRING FLAP TRACK TRANSMISSION BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.

Part: LINK — CORRODED (LT MLG) · airframe 70,871 hrs · 67,128 cycles

LEFT MLG SWING LINK ATTACH UPPER & LOWER AFT POSITION CORRODED. REPAIRED SWING LINK IAW CMM.

Part: FITTING — CRACKED (RT WING) · airframe 70,871 hrs · 67,128 cycles

RIGHT WING REAR SPAR FITTING CRACKED AT RSS 225, FIXED TE. REPAIRED FITTING IAW EO & EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

TIE CLIP CRACKED AT BS 616, STRINGER 8L. R & R TIE CLIP IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

AFT CARGO COMPARTMENT SKIN CHANNEL CRACKED, BETWEEN BS 747 - 767, BETWEEN STRINGER 27L - 27R. R & R SKIN IAW EO & EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

WEB CRACKED BETWEEN BS 277 - 291.5, STRINGER 14R. R & R WEB IAW SRM & DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

STRINGER CRACKED AT BS 400, STRINGER 5L. REPAIRED STRINGER IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

TIE CLIP CRACKED AT BS 663.75, STRINGER 4L. R & R TIE CLIP IAW SRM & DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 70,871 hrs · 67,128 cycles

LEFT WING NR 2 SLAT SKIN LOWER SURFACE CRACKED. REPAIRED NR 2 SLAT IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

TIE CLIP CRACKED AT BS 727C, STRINGER 4L. R & R TIE CLIP IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 460, STRINGER 21L. R & R ANGLE IAW SRM & DWG.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

FORWARD CARGO COMPARTMENT WEB SILL CRACKED, BETWEEN BS 420 - 440, STRINGER 26R. R & R WEB SILL IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

FORWARD CARGO COMPARTMENT CHANNEL CRACKED AT BS 540, BETWEEN LBL 0.07 TO LBL 24. R & R CHANNEL IAW DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

TIE CLIP CRACKED AT BS 727A, STRINGER 6R. R & R TIE CLIP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

TIE CLIP CRACKED AT BS 727A, STRINGER 10L. R & R TIE CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

FRAME CRACKED AT BS 460, BETWEEN STRINGER 28L - 28R. R & R FRAME IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

TIE CLIP CRACKED AT BS 827, STRINGER 16R. R & R TIE CLIP IAW DWG & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

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

Part: SKIN — DELAMINATED (TE FLAP) · airframe 70,871 hrs · 67,128 cycles

RIGHT WING INTERNAL FORE FLAP DELAMINATED ON OTBD LOWER SURFACE. REPAIRED FORE FLAP IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

STRAP CRACKED AT BS 328, LBL 11. R & R STRAP IAW SRM & DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 70,871 hrs · 67,128 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

FRAME UPPER FLANGE CRACKED AT BS 420, STRINGER 26L. R & R FRAME IAW SRM & DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

STRINGER CRACKED AT BS 482A, STRINGER 8R. REPAIRED STRINGER IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

TIE CLIP CRACKED AT BS 520, STRINGER 16R. REPAIRED TIE CLIP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

FRAME CRACKED AT BS 400, BETWEEN STRINGER 16L - 15L. REPAIRED FRAME IAW EO & EA.

Part: LIGHT — BROKEN (CABIN) · airframe 70,871 hrs · 67,128 cycles

LEFT OVERHEAD BULLNOSE STOWAGE BIN, EMER LIGHT ASSEMBLY BROKEN AT ROW 7. R & R LIGHT ASSEMBLY IAW AMM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

TIE CLIP CRACKED AT BS 616, STRINGER 5R. R & R TIE CLIP IAW SRM & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

FRAME CRACKED AT BS 420, BETWEEN STRINGER 16L - 15L. REPAIRED FRAME IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

TIE CLIP CRACKED AT BS 482B, STRINGER 8L. R & R TIE CLIP IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

TIE CLIP CRACKED AT BS 482, STRINGER 7L. R & R TIE CLIP IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

INTERCOSTAL WEB CRACKED, BETWEEN BS 291.3 - 303.9, STRINGER 8L. R & R WEB IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

SKIN CRACKED BETWEEN BS 259.5+6 - 283, BETWEEN STRINGER 2L - 5L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

SKIN CRACKED BETWEEN BS 482+8 - 482+19, BETWEEN STRINGER 25L - 27L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

SKIN CRACKED BETWEEN BS 348 - 380, BETWEEN STRINGER 2L - 2R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

SKIN CRACKED BETWEEN BS 482B - 540, BETWEEN STRINGER 14L - 18L. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

SKIN CRACKED AT BS 787+16.5, STRINGER 24L. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

SKIN CRACKED BETWEEN BS 400 - 460, BETWEEN STRINGER 1L - 3R. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (RT WING) · airframe 70,871 hrs · 67,128 cycles

RIGHT WING REAR SPAR UPPER CHORD, AFT SKIN CRACKED AT RSS 222.5. REPAIRED SKIN IAW EO & EA.

Part: DOOR FRAME — CRACKED (R2 DOOR) · airframe 70,871 hrs · 67,128 cycles

R2 DOOR AFT EDGE INTERNAL AREA FRAME CRACKED. R & R DOOR IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

SKIN CRACKED BETWEEN BS 867 - 88, BETWEEN STRINGER 20R - 22R. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

SKIN CRACKED BETWEEN BS 807+7 - 827+13, BETWEEN STRINGER 23L - 26L. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

SKIN CRACKED AT BS 847+15.5, STRINGER 15R. REPAIRED SKIN IAW EO & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

SKIN CRACKED AT BS 867+5, STRINGER 16R. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

SKIN CRACKED AT BS 767+16, STRINGER 22L. REPAIRED SKIN IAW EO & EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

SHEAR TIE CORRODED AT BS 1006, BETWEEN STRINGER 27R TO 27L. R & R SHEAR TIE IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

SKIN CRACKED BETWEEN BS 908 - 1016, BETWEEN STRINGER 20R - 25R. R & R SKIN IAW EO & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

CENTER WING BOX LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 708, LBL 0.07. REPAIRED WEB IAW EA.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 70,871 hrs · 67,128 cycles

ENTRY DOOR FWD LOWER HINGE FRAME AT AFT GALLEY AREA CRACKED. REPAIRED FRAME IAW SRM.

Part: LENS — BROKEN (CABIN) · airframe 70,641 hrs · 66,855 cycles

FORWARD ENTRY WAY EXIT LIGHT COVER LENS BROKEN. R & R LENS IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 70,259 hrs · 66,408 cycles

AFT GALLEY EMER FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 70,152 hrs · 66,283 cycles

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

Part: ATTACH FITTING — DAMAGED (LE SLAT) · airframe 69,620 hrs · 65,656 cycles

RIGHT WING NR 6 SLAT INBD AUXILIARY TRACK ATTACH FITTING, DAMAGED AT AFT UPPER SPAR CAP. REPAIRED FITTING IAW EA & DWG.

Part: PANEL — CRACKED (FUSELAGE) · airframe 69,620 hrs · 65,656 cycles

FORWARD ENTRY DOOR CUT OUT FWD LOWER CLOSEOUT PANEL CRACKED. REPAIRED PANEL IAW SRM.

Part: BRACKET — CRACKED (RT AILERON) · airframe 69,620 hrs · 65,656 cycles

RIGHT WING AILERON COVER BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: SLAT — CRACKED (RT WING) · airframe 69,620 hrs · 65,656 cycles

RIGHT WING NR 5 SLAT COMPOSITE LE FIXED CRACKED ABOVE OTBD AUX TRACK. REPAIRED NR 5 SLAT IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 69,587 hrs · 65,617 cycles

R2 DOOR EMER EXIT SIGN LENS LOOSE. R & R LENS IAW SIP.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,345 hrs · 65,343 cycles

FUSELAGE SKIN CRACKED AT STATION 799, STRINGER 25R. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,345 hrs · 65,343 cycles

FUSELAGE SKIN CRACKED AT STATION 798 TO 800, STRINGER 25R. REPAIRED SKIN IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 69,345 hrs · 65,343 cycles

ATTACH CLIP CRACKED AT RT FUSELAGE STATION 616, WL 208. R & R CLIP IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,345 hrs · 65,343 cycles

FUSELAGE SKIN CRACKED AT STATION 931, STRINGER 21L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,345 hrs · 65,343 cycles

FUSELAGE SKIN CRACKED AT STATION 807+15, STRINGER 19L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,345 hrs · 65,343 cycles

FUSELAGE SKIN CRACKED AT STATION 850, STRINGER 16L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,345 hrs · 65,343 cycles

FUSELAGE SKIN CRACKED AT STATION 847+12, STRINGER 16L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,345 hrs · 65,343 cycles

FUSELAGE SKIN CRACKED AT STATION 787+6, STRINGER 25L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,345 hrs · 65,343 cycles

FUSELAGE SKIN CRACKED AT STATION 444, STRINGER 16R. REPAIRED SKIN IAW EA.

Part: SPOILER — UNKNOWN (RT WING) · airframe 69,327 hrs · 65,321 cycles

RIGHT WING NR 6 FLIGHT SPOILER LEAKED. R & R SPOILER IAW MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 69,221 hrs · 65,206 cycles

LEFT OTBD AFT FLAP DELAMINATED ON INBD TE. R & R AFT FLAP IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,021 hrs · 64,967 cycles

RIGHT OVERWING EXIT LOWER EMER EXIT LIGHT INOPERATIVE. REPAIRED LIGHT IAW SWPM.

Part: LENS — BROKEN (CABIN) · airframe 68,957 hrs · 64,897 cycles

R1 DOOR EXIT LIGHT LENS COVER BROKEN. SECURED LENS IAW EA.

Part: BRACKET — DIRTY (GIRT BAR) · airframe 68,804 hrs · 64,730 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR RETAINING BRACKET DIRTY. CLEANED BRACKET IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,116 hrs · 63,977 cycles

RIGHT LOWER OVERWING EMER EXIT LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW AMM.

Part: MOUNT BRACKET — CRACKED (R2 DOOR) · airframe 67,943 hrs · 63,801 cycles

R2 DOOR EMERGENCY EVAC SLIDE MOUNT BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,686 hrs · 63,545 cycles

L1 DOOR SKIN CUT OUT LOWER AFT CORNER UNDER THRESHOLD PLATE CRACKED AT BS 348. REPAIRED SKIN IAW EA & SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,214 hrs · 63,050 cycles

FUSELAGE SKIN CRACKED BETWEEN BS 425 TO BS 428 STRINGER 26L. REPAIRED SKIN IAW SRM.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 66,965 hrs · 62,785 cycles

EMERGENCY EXIT SIGN FELL OFF. R & R LENS IAW AMM.

Part: SLAT — DELAMINATED (RT WING) · airframe 66,304 hrs · 62,051 cycles

RT WING NR 5 SLAT WEDGE DELAMINATED ON OTB END. R&R NR 5 SLAT PER AMM.

Part: TAB — DELAMINATED (RT AILERON) · airframe 66,304 hrs · 62,051 cycles

RT WING AILERON TAB DELAMINATED OTBD END. R&R TAB IAW MM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 66,150 hrs · 61,867 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR FITTING BOTH ADAPTER PLATES CORRODED. R&R FITTINGS IAW AMM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 66,150 hrs · 61,867 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FLOOR FITTING BOTH ADAPTER PLATES CORRODED. R&R FITTINGS IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

AFT CARGO COMPARTMENT STRINGER CLIP CRACKED AT STATION 927, STRINGER 24L. R&R CLIP IAW DRAWING.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

STRINGER CRACKED BETWEEN BS 749 TO BS 750, STRINGER 23L. REPAIRED STRINGER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

SKIN CRACKED AT BS 922, STRINGER 24L. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

SKIN CRACKED AT STATION 882, STRINGER 15R. REPAIRED SKIN IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

LT CREASE BEAM WEB UPPER SURFACE CORRODED AT BS 800. R&R WEB IAW SRM & DRAWING.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

RT CREASE BEAM WEB CORRODED AT BS 794 TO BS 807. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

FLOOR WEB CRACKED AT STATION 1004, RBL 40. REPAIRED WEB IAW SRM.

Part: BULKHEAD — BULGED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

FORWARD PRESSURE BULKHEAD BULGED AT STATION 178, LBL 6. REPAIRED WEB IAW SRM & DRAWING.

Part: STRINGER — CRACKED (RT WING) · airframe 66,150 hrs · 61,867 cycles

RT WING VERTICAL WEB STRINGER CRACKED AT STATION 463, STRINGER 5R. REPAIRED WEB IAW SWA EA 1-557-8383.

Part: ATTACH ANGLE — CRACKED (TE FLAP FAIRING) · airframe 66,150 hrs · 61,867 cycles

RT WING NR 8 FLAP TRACK FAIRING INBD ATTACH SKATE ANGLE CRACKED UNDER THE FIXED TE PANEL. R&R ANGLE IAW DRAWING.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

CREASE BEAM WEB CORRODED BETWEEN STATION 616-STATION 639, STRINGER 17R. REPAIRED WEB IAW SRM & DRAWING.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

SKIN CORRODED AT STATION 357, RBL 3. R&R DOUBLER IAW SRM & DRAWING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

SHEAR TIE CORRODED AT STATION 360, BETWEEN BL 0 TO LBL 7. R&R SHEAR TIE IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

FRAME CRACKED AT STATION 986, STRINGER 19R. R&R FRAME SECTION IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

ATTACH CLIPS CRACKED AT STATION 727, STRINGER 1. R&R CLIPS IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

SKIN CRACKED AT BS 328, STRINGER 17R. REPAIRED SKIN IAW SRM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

FWD CARGO DOOR CUT OUT FWD FRAME CLOSURE WEB CORRODED AT STATION 400, STRINGER 23R. REPAIRED WEB IAW SRM

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

FS FRAME TO OVERHEAD DUCT LT ATTACHED BRACKET CRACKED AT STATION 907. R&R BRACKET IAW SRM & DRAWING.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

FWD LAVATORY SERVICE PAN INTERIOR SURFACE UPPER CHANNEL CORRODED. R&R CHANNEL IAW SRM & DRAWING.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

FS FRAME TO OVERHEAD DUCT RT ATTACHED BRACKET CRACKED AT STATION 907. R&R BRACKET IAW SRM & DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

R1 DOOR AFT SIDE OF DOOR CUTOUT STIFFENER CLIP CRACKED, JUST AFT OF DOOR STOP AT FRAME. R&R CLIP IAW SRM & DRAWING.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

R1 DOOR CUTOUT STUB FRAME CRACKED AT STATION 295. R&R CUTOUT IAW DRAWING & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

STRINGER CLIP CRACKED AT STATION 482, STRINGER 16L. R&R CLIP IAW SRM & DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

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

Part: STRAP — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

RT CREASE BEAM INBD ANGLE SPLICE STRAP CRACKED AT STATION 530, RBL 53. R&R STRAP IAW DRAWING & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

STRINGER CLIP CRACKED AT STA 380, STR 8R. R&R CLIP IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

RT CREASE BEAM WEB CORRODED BETWEEN STATION 747 & STATION 767. REPAIRED WEB IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

STRINGER CLIP CRACKED AT STATION 907, STRINGER 8L. R&R CLIP IAW DRAWING & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

LT CREASE BEAM WEB UPPER SURFACE CORRODED AT BS 450. R&R WEB IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

LT CREASE BEAM WEB UPPER SURFACE CORRODED AT BS 403. R&R SHEAR WEB IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

LT CREASE BEAM WEB UPPER SURFACE CORRODED AT BS 757. R&R WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

LT CREASE BEAM WEB UPPER SURFACE CORRODED AT BS 869. REPAIRED WEB IAW SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

VERTICAL "L" BRACKET CRACKED AT STATION 986, STRINGER 3L. R&R "L" BRACKET IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

STRINGER CLIP CORRODED AT STATION 794, STRINGER 26R. R&R CLIP IAW SRM & DRAWING.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

AFT SIDE OF FRAME STRINGER CLIP CRACKED AT BS 947, STRINGER 25R. R&R STRINGER CLIP IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

LT MAIN WW FRAME STATION 727 FWD FLANGE, CRACKED AT FWD LOWER HOLE COMMON TO STRINGER 18A. R&R CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

RT MAIN WW OUTER STRAP CRACKED AT STATION 727, STRINGER 18A. REPAIRED SKIN IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

STRINGER ANGLE CORRODED AT STATION 794, STRINGER 25R. R&R ANGLE IAW SRM & DRAWING.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

VERTICAL ''Z'' ANGLE FLOOR SUPPORT WEB ATTACH ANGLE CRACKED BETWEEN STATION 927 & STATION 947, BETWEEN STRINGER 24R & STRINGER 25R. R&R ANGLE IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

RT MAIN WW FRAME STATION 727 FWD FLANGE, CRACKED AT FWD LOWER HOLE & UPPER AFT HOLE COMMON TO STRINGER 18A. R&R CHORD IAW EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

FLOOR SUPPORT INTERCOSTAL WEB CORRODED BETWEEN STATION 787 - STATION 794, STRINGER 25R. R&R INTERCOSTAL IAW SRM & DRAWING.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

AFT CARGO PIT BS 794 FORWARD DOOR FRAME UPPER CLOSE OUT WEB LOWER EDGE CRACKED. R&R WEB IAW SRM & DRAWING.

Part: WEB — CORRODED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

LAVATORY PAN WEB CORRODED BETWEEN STATION 986 TO STATION 1006, LBL 36. R&R WEB IAW SRM & DRAWING.

Part: RETAINER — CRACKED (NR 2 PYLON) · airframe 66,150 hrs · 61,867 cycles

NR 2 PYLON PLASTIC NUTPLATE RETAINER FOR PANEL 58710R CRACKED AT AFT INBD EDGE. R&R RETAINER IAW SRM & AMM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

FLOOR SUPPORT UPPER SURFACE CORRODED AT STATION 980 - 2, LBL 18. R&R SUPPORT IAW SRM & DRAWING.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

RT CREASE BEAM INNER CHORD CORRODED AT STATION 294. R&R BEAM IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

FS SKIN CRACKED AT STATION 853, STRINGER 24L. REPAIRED SKIN IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE FLOOR PANEL SUPPORT CHANNELS CORRODED AT STA 727B+6, RBL 3. REPAIRED CHANNEL IAW SRM AND EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

RT CREASE BEAM INNER CHORD CORRODED BETWEEN STATION 947 TO STATION 992. R&R CHORD IAW SRM & DRAWING.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 66,150 hrs · 61,867 cycles

LT WING INBD TE FORE FLAP UPPER SKIN DELAMINATED. REPAIRED SKIN IAW SRM & AMM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

FLOOR BEAM CORRODED AT BS 986, LBL 4 TO LBL 15. REPAIRED BEAM IAW SWA EA..

Part: CHANNEL — CRACKED (LT WING) · airframe 66,150 hrs · 61,867 cycles

LT WING UPPER T/E PANEL SUPPORT CHANNEL CRACKED. R&R CHANNEL IAW SRM & DRAWING.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

LONGITUDINAL FLOOR SUPPORT CORRODED AT BS 967 TO BS 986, RBL 18. REPAIRED SUPPORT IAW SRM.

Part: BRACKET — CRACKED (LT WING) · airframe 66,150 hrs · 61,867 cycles

LT WING TRAILING EDGE, AFT OF AILERON CABLE TURN AROUND SPRING, COVE PANEL OB ATTACH ANGLE CRACKED. R&R BRACKET IAW SRM & DRAWING.

Part: STRIP — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

L1 DOOR FWD UPPER CORNER OF DOOR CUTOUT COVER ATTACH STRIP CRACKED JUST BELOW STR 6L. REPAIRED STRIP IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,150 hrs · 61,867 cycles

FRAME CRACKED AT STATION 482, STRINGER 20L. REPAIRED FRAME IAW SRM.

Part: COVER — CRACKED (L2 DOOR) · airframe 66,150 hrs · 61,867 cycles

L2 DOOR CUTOUT WARNING SWITCH COVER CRACKED. REMOVED AND REPLACED COVER IAW AMM.

Part: FITTING — CRACKED (LT SPOILER) · airframe 66,019 hrs · 61,724 cycles

LEFT WING GROUND SPOILER FITTING ASSY LUG ON NR 4 OTBD ACTUATOR CRACKED. REPAIRED FITTING ASSY IAW EA.

Part: ACTUATOR — SHEARED (LT SPOILER) · airframe 66,019 hrs · 61,724 cycles

LEFT WING INBD GROUND SPOILER OTBD ACTUATOR ROD END SHEARED. R & R ACTUATOR IAW MM.

Part: SPOILER — BROKEN (LT WING) · airframe 66,019 hrs · 61,724 cycles

LEFT WING INBD GROUND SPOILER BROKEN AT HINGE AREA. R & R SPOILER IAW AMM CK GOOD.

Part: PUMP — FAULTY (LT WING) · airframe 65,955 hrs · 61,659 cycles

ON TAKEOFF BOTH FORE AND AFT NR 1 FUEL PUMP LOW PRESSURE LIGHTS ILLUMINATED WITH CORRESPONDING MASTER CAUTION LIGHTS. LIGHTS WENT OUT APPROX. 1 MINUTE AFTER DECK ANGLE REDUCED. NR 1 TANK AFT PUMP LIGHT ILLUMINATED IN CRUISE FLIGHT. COMPLIED WITH QRH AND OPERATED THAT PUMP WITH THE SWITCH OFF FOR THE REMAINDER OF THE FLIGHT. R & R NR 1 AFT & NR 1 FWD ELEC FUEL BOOST PUMPS IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 65,422 hrs · 61,102 cycles

EXIT SIGN LOOSE AT FWD GALLEY. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 65,021 hrs · 60,664 cycles

SKIN CRACK LOWER LT FUSELAGE STA 807 + 6 STRINGER 19L ABOVE, 11/2 LONG. VERIFIED BY HFEC PER NDT PART 6 51-00-00 PROCEDURE 23. REPAIRED IAW SRM 53-00-01-2R-31.

Part: DOOR FRAME — CRACKED (ENTRY DOOR) · airframe 64,931 hrs · 60,585 cycles

AFT ENTRY DOOR LOWER FWD CORNER FRAME CRACKED. REMOVED AND REPLACED AFT ENTRY DOOR PER AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 64,534 hrs · 60,181 cycles

RIGHT FWD PASSENGER CABIN EMERGENCY EXIT LIGHTING INOP. REMOVED & REPLACED BATTERY IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,534 hrs · 60,181 cycles

SKIN CRACKED AT BS 390, STR 16R. REPAIRED SKIN PER EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 64,533 hrs · 60,181 cycles

STRINGER CRACKED AT BS 390, STR 13R. REPAIRED STRINGER PER EA.

Part: UPLOCK SENSOR — FAULTY (RT MLG) · airframe 63,597 hrs · 59,563 cycles

RED GEAR LIGHT ILLUMINATED IN FLIGHT AND REMAINED ILLUMINATED AFTER RAISING GEAR HANDLE AS DIRECTED BY QRH. FOUND RIGHT MLG UPLOCK SENSOR BAD. REMOVED AND REPLACED RIGHT MLG UPLOCK SENSOR PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,291 hrs · 59,365 cycles

R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED & REPLACED BATTERY PACK PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,103 hrs · 59,239 cycles

FUSELAGE SKIN CRACKED AT BS 772, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,103 hrs · 59,239 cycles

FUSELAGE SKIN CRACKED AT BS 761, STR 19L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,103 hrs · 59,239 cycles

SKIN CRACKED AT BS 772, STR 19L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,103 hrs · 59,239 cycles

SKIN CRACKED AT BS 761, STR 19L. REPAIRED SKIN IAW SRM.

Part: SLAT — DELAMINATED (LT WING) · airframe 63,101 hrs · 59,238 cycles

LT WING NR 2 SLAT UPPER OUTBOARD TRAILING EDGE DELAMINATED. REMOVED AND REPLACED NR 2 SLAT IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,073 hrs · 59,215 cycles

SKIN CRACKED AT BS 520, STR 16R. REPAIRED SKIN PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 61,037 hrs · 57,920 cycles

DURING SCHEDULED 20Y CHECK, FOUND KEEL BEAM CORRODED BETWEEN BS 482B+4 TO BS 490, STR 28R. REPAIRED BEAM IAW EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,037 hrs · 57,920 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CORRODED BETWEEN BS 465 TO BS 471, BETWEEN STR 28R TOS TR 28L. REPAIRED SKIN IAW EO.

Part: FLAP — DELAMINATED (RT WING) · airframe 61,037 hrs · 57,920 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,037 hrs · 57,920 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 959.5, STR 17L. REPAIRED SKIN IAW EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 61,037 hrs · 57,920 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT WING AFT O/B FLAP DELAMINATED. REPAIRED AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,037 hrs · 57,920 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED BETWEEN BS 827+4 TO BS 827+14, STR 16L. REPAIRED SKIN IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,037 hrs · 57,920 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CORRODED AT BS 927, BETWEEN STR 27R TO STR 27L. REPAIRED FRAME IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,037 hrs · 57,920 cycles

DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 827+6.5, STR 18L. REPAIRED SKIN IAW SRM.

Part: RIB — CRACKED (HORIZ STAB) · airframe 61,037 hrs · 57,920 cycles

DURING SCHEDULED 20Y CHECK, FOUND RT HORIZONTAL STABILIZER L/E RIB CRACKED AT STA 1883.94. REMOVED AND REPLACED RIB IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,037 hrs · 57,920 cycles

DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 794.3, BETWEEN STR 23R TO STR 25R. REMOVED AND REPLACED FRAME PER SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 61,037 hrs · 57,920 cycles

DURING SCHEDULED 20Y CHECK, FOUND SUPPORT ANGLE CRACKED BETWEEN BS 294.5 TO BS 303.9, STR 10L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,037 hrs · 57,920 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,325 hrs · 57,416 cycles

DURING SCHEDULED CV CHECK FOUND, SKIN CRACKED AT BS 927+4, STR 23L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,325 hrs · 57,416 cycles

DURING SCHEDULED CV CHECK FOUND, SKIN CRACKED AT BS 927+15, STR 25R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,325 hrs · 57,416 cycles

DURING SCHEDULED CV CHECK FOUND, SKIN CRACKED AT BS 887+13, STR 25R. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,325 hrs · 57,416 cycles

DURING SCHEDULED CV CHECK FOUND, SKIN CRACKED AT BS 847+4, STR 15R. REPAIRED SKIN PER EA.

Part: PRIORITY VALVE — FAULTY (LT MLG) · airframe 59,213 hrs · 56,639 cycles

ON LANDING IN SAN LOWERED LANDING GEAR AND GOT RED LIGHT ON LEFT GEAR. CYCLED GEAR 3 TIMES TO GET A GREEN LIGHT. REMOVED AND REPLACED MLG PRIORITY VALVE PER MM.

Part: ACTUATOR — FAULTY (LT MLG) · airframe 58,351 hrs · 56,030 cycles

AIR TURNBACK, AFTER T/O LEFT MAIN LANDING GEAR LIGHT REMAINED RED IN THE UP POSITION CYCLE LANDING GEAR INDICATION WERE GOOD. RAISED GEAR LEFT MAIN RED LIGHT REMAINED ON. REMOVED AND REPLACED LT MLG ACTUATOR AND UPLOCK ACTUATOR PER MM.

Part: ACTUATOR — FAULTY (LT MLG) · airframe 58,312 hrs · 56,001 cycles

AIR TURNBACK, RED LEFT GEAR LIGHT ILLUMINATED WHEN GEAR RETRACTED. RED AND GREEN LEFT GEAR LIGHT ILLUMINATED WHEN GEAR LEVEL POSITIONED TO OFF. REMOVED AND REPLACED LT MLG I/B LOCK ACTUATOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,595 hrs · 55,487 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 761, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,595 hrs · 55,487 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 760, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,595 hrs · 55,487 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 972, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,595 hrs · 55,487 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 941, STR 23R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,595 hrs · 55,487 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 971, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,595 hrs · 55,487 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 944, STR 23R. REPAIRED SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 57,109 hrs · 55,164 cycles

DURING SCHEDULED 18Y CHECK, FOUND WHEEL WELL PRESSURE DECK WEB CRACKED AT BS 664, RBL 41. REPAIRED WEB PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,109 hrs · 55,164 cycles

DURING SCHEDULED 18Y CHECK, FOUND LT EMERGENCY EXIT LIGHT INOP AT ROW 11. REMOVED AND REPLACED LIGHT PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,109 hrs · 55,164 cycles

DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CORRODED AT BS 460, BETWEEN STR 27L TO STR 28L. REPAIRED SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,109 hrs · 55,164 cycles

DURING SCHEDULED 18Y CHECK, FOUND SKIN CRACKED BETWEEN BS 784.25 TO BS 785.5, STR 23L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,109 hrs · 55,164 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 303.9, STR 16L. REPAIRED FRAME PER ER.

Part: TAB — DELAMINATED (AILERON) · airframe 57,109 hrs · 55,164 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT WING AILERON TAB I/B END DELAMINATED. REPAIRED TAB PER MM.

Part: TAB — DELAMINATED (AILERON) · airframe 57,109 hrs · 55,164 cycles

DURING SCHEDULED 18Y CHECK, FOUND RT WING AILERON TAB O/B END DELAMINATED. REPAIRED TAB PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,109 hrs · 55,164 cycles

DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 482B, STR 1. REPAIRED FRAME PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 56,847 hrs · 54,984 cycles

DURING SCHEDULED OTS CHECK, FOUND RT WING O/B FORE FLAP T/E DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 56,102 hrs · 54,511 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,920 hrs · 53,754 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 794, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,920 hrs · 53,754 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 863, STR 23R. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 54,920 hrs · 53,754 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING O/B TRAILING EDGE FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,920 hrs · 53,754 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 780, STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,920 hrs · 53,754 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 795, STR 8R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,920 hrs · 53,754 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 792, STR 19L. REPAIRED SKIN PER SRM.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 54,658 hrs · 53,584 cycles

DIVERSON / DECLARED EMERGENCY. DURING CRUISE AT FL 230, CABIN ALTITUDE WARNING HORN SOUNDED, CREW DONNED 02 MASKS AND COMMENCED DESCENT, COMPLETED QRH CHECKLIST. NO OTHER PROBLEMS NOTED WITH AIRCRAFT (RAPID DEPRESSURIZATION). REMOVED AND REPLACED CABIN PRESSURE CONTROLLER, MAIN OUTFLOW VALVE, AND PRESSURE CONTROL PANEL PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,472 hrs · 53,466 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT, BETWEEN BS 292 TO BS 304, BETWEEN WL 234 TO WL 262. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,472 hrs · 53,466 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT, BETWEEN BS 292 TO BS 304, BETWEEN WL 234 TO WL 262. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,472 hrs · 53,466 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, AT BS 293, WL 236. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,472 hrs · 53,466 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, AT BS 292, WL 232. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,472 hrs · 53,466 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, AT BS 292, BETWEEN WL 232 TO WL 236. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 54,472 hrs · 53,466 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT BS 400. R&R FRAME PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,472 hrs · 53,466 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE BEARSTRAP SKIN CRACKED AT L1 DOOR LOWER HINGE, BETWEEN BS 302 TO BS 304, WL 238. REPAIRED SKIN PER AAR EA.

Part: OUTFLOW VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 54,387 hrs · 53,407 cycles

DIVERSION, CABIN PRESSURE CONTROLLER INOP. REMOVED AND REPLACED OUTFLOW VALVE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,359 hrs · 53,387 cycles

DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 954, STR 23R. REPAIRED SKIN PER SRM.

Part: WINDOW — ARCED (COCKPIT) · airframe 54,047 hrs · 53,176 cycles

ON APPROACH OBSERVED L1 WINDSHIELD SPARKING. WINDOW HEAT WORKED NORMAL. REMOVED AND REPLACED WINDOW PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 53,261 hrs · 52,500 cycles

FOUND RT FWD EMERGENCY EXIT BULL NOSE LIGHT LOOSE. SECURED LIGHT PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 53,261 hrs · 52,500 cycles

RT FWD EMERGENCY EXIT BULLNOSE LIGHT LOOSE. SECURED LIGHT PER MM.

Part: WIRE — DAMAGED (COCKPIT) · airframe 48,925 hrs · 49,031 cycles

ON DEPARTURE COWL ANTI ICE VALVE LIGHT ILLUMINATED AND ENG TO COWL C/B POPPED, ACCOMPANIED WITH ACRID SMELL. WHILE ATTEMPTING TO CLOSE VALVE ACRID SMELL RETURNED AND ENG TO WING CONTROL C/B POPPED. NO MORE RESETS WERE ATTEMPTED. FOUND WIRING DAMAGED AT DISCONNECT ATTACHED TO COWL WING ANTI ICE OVERHEAD MODULE. REPAIRED WIRING AND REMOVED AND REPLACED O/H MODULE PER MM.

Part: DRAG BRACE — VIBRATION (NLG) · airframe 51,671 hrs · 51,339 cycles

DURING CLIMB WHEN RAISING NLG EXCESSIVE VIBRATION FELT. REMOVED AND REPLACED LOWER DRAG BRACE PER MM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 51,175 hrs · 50,897 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,175 hrs · 50,897 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM WEB CORRODED BETWEEN BS 1006 AND BS 1016, LBL 38 AND LBL 39. REMOVED AND REPLACED WEB PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,175 hrs · 50,897 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST DUCT. REPAIRED SKIN PER BOEING SB AND EA.

Part: LIGHT — BROKEN (CABIN) · airframe 51,175 hrs · 50,897 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,175 hrs · 50,897 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM WEB CORRODED BETWEEN BS 1016 AND BS 1040, BL 0 AND RBL 38. REMOVED AND REPLACED WEB PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,175 hrs · 50,897 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 986, RBL 43. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,175 hrs · 50,897 cycles

DURING SCHEDULE 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,175 hrs · 50,897 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 885, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,175 hrs · 50,897 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 885, STR 25R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,175 hrs · 50,897 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 947, STR 18R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,175 hrs · 50,897 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,175 hrs · 50,897 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 277, BETWEEN STR 14R AND STR 16R. REMOVED AND REPLACED WEB PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 51,175 hrs · 50,897 cycles

DURING SCHEDULED 16Y CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 277, LBL 12, WL 208. REPAIRED STIFFENER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,175 hrs · 50,897 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT LEFT BS 616 INBOARD LOWER END. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,175 hrs · 50,897 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER 16L CRACKED AT BS 380. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,175 hrs · 50,897 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT RIGHT BS 616 INBOARD LOWER END. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,175 hrs · 50,897 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,175 hrs · 50,897 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,175 hrs · 50,897 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: LENS — CRACKED (CABIN) · airframe 51,175 hrs · 50,897 cycles

DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,175 hrs · 50,897 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 50,898 hrs · 50,681 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — CRACKED (BS 387 S14R) · airframe 49,911 hrs · 49,839 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 387, STR 14R. REPAIRED SKIN PER ER.

Part: SKIN — CRACKED (BS 482B S14L) · airframe 49,911 hrs · 49,832 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 482B, STR 14L. REPAIRED SKIN PER ER.

Part: FRAME — CRACKED (BS 360 S4-8L) · airframe 49,911 hrs · 49,832 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L AND 4L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 727A S8R) · airframe 49,911 hrs · 49,832 cycles

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

Part: SHEAR TIE — CRACKED (BS 360 S14L) · airframe 49,911 hrs · 49,832 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 482A S8R) · airframe 49,911 hrs · 49,832 cycles

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

Part: FRAME — CRACKED (BS 907 S8R) · airframe 49,911 hrs · 49,832 cycles

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

Part: STRINGER CLIP — CRACKED (BS 747 S8R) · airframe 49,911 hrs · 49,832 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 867 S4R) · airframe 49,911 hrs · 49,832 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 787 S9R) · airframe 49,911 hrs · 49,832 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 847 S10L) · airframe 49,911 hrs · 49,832 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 907 S4L) · airframe 49,911 hrs · 49,832 cycles

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

Part: STRINGER SPLICE — CRACKED (BS 908 S4L) · airframe 49,911 hrs · 49,832 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 887 S10L) · airframe 49,911 hrs · 49,832 cycles

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

Part: STRINGER CLIP — CRACKED (BS 887 S6R) · airframe 49,911 hrs · 49,832 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 616 S3R) · airframe 49,911 hrs · 49,832 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A S4L) · airframe 49,911 hrs · 49,832 cycles

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

Part: FRAME — CRACKED (BS 482A S8L) · airframe 49,944 hrs · 49,832 cycles

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

Part: STRINGER CLIP — CRACKED (BS 482B S8R) · airframe 49,911 hrs · 49,832 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 559 S8R) · airframe 49,911 hrs · 49,832 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 440 S8L) · airframe 49,911 hrs · 49,832 cycles

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

Part: STRINGER CLIP — CRACKED (BS 706 S3R) · airframe 49,911 hrs · 49,832 cycles

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

Part: STRINGER CLIP — CRACKED (BS 482A S4R) · airframe 49,911 hrs · 49,832 cycles

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

Part: STRINGER CLIP — CRACKED (BS 482A S8L) · airframe 49,944 hrs · 49,832 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482A, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 400 S8R) · airframe 49,911 hrs · 49,832 cycles

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

Part: STRINGER CLIP — CRACKED (BS 706 S1) · airframe 49,911 hrs · 49,832 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 520 S8L) · airframe 49,911 hrs · 49,832 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 482B S8L) · airframe 49,911 hrs · 49,832 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 520 S8) · airframe 49,944 hrs · 49,832 cycles

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

Part: STRINGER CLIP — CRACKED (BS 482B S7L) · airframe 49,911 hrs · 49,832 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 727A S9L) · airframe 49,944 hrs · 49,832 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 460 S4R) · airframe 49,911 hrs · 49,832 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 685 S5R) · airframe 49,911 hrs · 49,832 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 380 S8R) · airframe 49,911 hrs · 49,832 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 727B S9R) · airframe 49,911 hrs · 49,832 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 440 S8R) · airframe 49,911 hrs · 49,832 cycles

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

Part: STRINGER CLIP — CRACKED (BS 747 S4L) · airframe 49,911 hrs · 49,832 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 827 S8L) · airframe 49,911 hrs · 49,832 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727A S4R) · airframe 49,911 hrs · 49,832 cycles

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

Part: FRAME — CRACKED (BS 482 S8L/R) · airframe 49,911 hrs · 49,832 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727B S8R) · airframe 49,911 hrs · 49,832 cycles

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

Part: STRINGER CLIP — CRACKED (BS 360 S7L) · airframe 49,911 hrs · 49,832 cycles

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

Part: STRINGER CLIP — CRACKED (BS 727B S7R) · airframe 49,911 hrs · 49,832 cycles

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

Part: STRINGER CLIP — CRACKED (BS 685 S9L) · airframe 49,911 hrs · 49,832 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (BS 559 S8L) · airframe 49,911 hrs · 49,832 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 706 S2R) · airframe 49,911 hrs · 49,832 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,906 hrs · 49,831 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT FWD END. REPAIRED SKIN PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 49,906 hrs · 49,831 cycles

DURING SCHEDULED HC2 CHECK, FOUND LEFT WING OUTBOARD FOREFLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — CRACKED (BS 765 S21L) · airframe 49,625 hrs · 49,539 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 765, STR 21L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 482 S10L) · airframe 48,978 hrs · 48,875 cycles

DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 482, STR 10L. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (BS 931 S25R) · airframe 47,837 hrs · 47,807 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 931, STR 25R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 930 S24L) · airframe 47,587 hrs · 47,556 cycles

DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 24L. REPAIRED SKIN PER SWA EA.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 46,840 hrs · 46,776 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT ELEVATOR UPPER AFT INBOARD SURFACE DELAMINATED. REMOVED AND REPLACED LT ELEVATOR PER MM.

Part: ACTUATOR — FROZEN (LT WING SPOILER) · airframe 46,840 hrs · 46,776 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING NR 4 SPOILER INBOARD ACTUATOR ROD END FROZEN. REMOVED AND REPLACED NR 4 ACTUATOR PER MM.

Part: STRINGER SPLICE — CRACKED (BS 360 S15L) · airframe 46,840 hrs · 46,776 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 46,840 hrs · 46,776 cycles

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

Part: FRAME — CRACKED (BS 1016 S6R) · airframe 46,512 hrs · 46,396 cycles

DURING SCHEDULED PM CHECK, FOUND AFT PRESSURE BULKHEAD FRAME CRACKED AT BS 1016, STR 6R. REPAIRED CHORD PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,457 hrs · 46,334 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 884, STR 24R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,457 hrs · 46,334 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 841, STR 16R. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (CARGO DOORWAY) · airframe 45,755 hrs · 45,569 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FRAME CRACKED AT UPPER AFT CORNER LOWER DOOR STOP. REPAIRED FRAME PER ER.

Part: ENGINE — FAILED (LEFT) · airframe 45,358 hrs · 45,142 cycles

AIR TURNBACK / IN FLT SHUTDOWN / DECLARED EMERGENCY. NR 1 ENG FAILURE AT 10,500 FT DURING CLIMB, EGT IND 830 DEGS AND RISING. REMOVED AND REPLACED NR 1 ENG PER MT.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 44,602 hrs · 44,327 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT WING OTBD T/E AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: SKIN — CRACKED (BS 787) · airframe 44,398 hrs · 44,119 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 18L. REPAIRED SKIN PER SRM.

Part: WINDOW — LOOSE (R2 DOOR SLIDE) · airframe 44,344 hrs · 44,065 cycles

R2 DOOR EMERGENCY EVAC SLIDE CONTAINER VIEWING WINDOW LOOSE. SECURED WINDOW PER MM.

Part: SKIN — CRACKED (BS 944) · airframe 43,981 hrs · 43,678 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 944) · airframe 43,975 hrs · 43,671 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 24L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,495 hrs · 43,149 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 774, STR 25L. REPAIRED SKIN PER SRM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 42,300 hrs · 41,923 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR LOWER FRAME CRACKED AT AFT DOOR STOP FITTING. REMOVED AND REPLACED R1 DOOR PER MM.

Part: FRAME — CRACKED (R2 DOOR) · airframe 42,290 hrs · 41,913 cycles

DURING SCHEDULED C3 CHECK, FOUND R2 DOOR LOWER FRAME CRACKED AT AFT DOOR STOP FITTING. REMOVED AND REPLACED R2 DOOR PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,290 hrs · 41,913 cycles

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

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 41,683 hrs · 41,288 cycles

DURING SCHEDULED RON CHECK, FOUND FLOOR SUPPORT STIFFENER CORRODED AT BS 270, LBL 4, WL 207.5. REPAIRED STIFFENER PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 40,114 hrs · 39,730 cycles

DURING SCHEDULED A2 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,689 hrs · 39,324 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT LOWER FWD CORNER. REPAIRED SKIN PER EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 39,689 hrs · 39,324 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 663, BL 0, CRACKED. REPAIRED FLOORBEAM SECTION PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,689 hrs · 39,324 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM AT BS 770, RBL3, CORRODED. REPAIRED BEAM PER EA.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 39,689 hrs · 39,324 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR EVAC SLIDE GIRT BAR FWD FITTING RIVET, LOOSE. REMOVED AND REPLACED R1 DOOR EVAC SLIDE GIRT BAR FWD FITTING RIVET PER MM.

Part: MODULE — DIRTY (COCKPIT) · airframe 37,621 hrs · 37,360 cycles

AIR TURNBACK, AIRCRAFT WOULD NOT PRESSURIZE. FOUND, P5-10 AIR COND MODULE SOILED. REMOVED AND REPLACED AIR COND MODULE PER MM.

Part: BLEED VALVE — FAULTY (NR 2 ENGINE) · airframe 36,707 hrs · 36,499 cycles

AIR TURNBACK, NR 2 ENGINE WOULD NOT MAKE CLIMB POWER. REMOVED AND REPLACED BLEED VALVE PER MM.

Part: LINE — LEAKING (RT MLG) · airframe 35,019 hrs · 34,914 cycles

DECLARED EMERGENCY, DURING LANDING,HYD A-SYS QTY INDICATION WENT TO ZERO AND HYD LOW PRESS LIGHTS ILLUMINATED. FOUND RT MLG ACTUATOR DOWN LINE LEAKING. REMOVED AND REPLACED BOTH ACTUATOR LINES PER MM.

Part: LINE — LOOSE (NR 2 ENGINE) · airframe 31,846 hrs · 31,883 cycles

ENGINE SHUT DOWN, DECLARED EMERGENCY. DURING FLIGHT SHUT DOWN NR 2 ENGINE 0 OIL QUANTITY, LOW OIL PRESS. FOUND NR 5 BEARING SUMP EXTERNAL OIL LINE LOOSE. TIGHTENED AND SAFETIED, SERVICED AND RAN ENG. NO LEAKS NOTED AND OPS CK GOOD PER MM.

Part: WARNING LIGHT — ERRATIC (COCKPIT) · airframe 31,813 hrs · 31,868 cycles

DURING FLIGHT FIRE WARNING LIGHT CAME ON FOR 2 SECONDS AT FLIGHT LEVEL 310 AND WENT OUT, NO OTHER INDICATIONS NOTED. INSPECTED CARGO COMP & ENGINE FOR DEFECTS, NONE NOTED. FIRE TEST OF CARGO COMP & ENGINES NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,818 hrs · 31,851 cycles

DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: WIRE — BROKEN (CABIN) · airframe 31,818 hrs · 31,851 cycles

DURING SCHEDULED D-CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT INOP. REPAIRED BROKEN WIRE PER MM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 31,818 hrs · 31,851 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 31,818 hrs · 31,851 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,818 hrs · 31,851 cycles

DURING SCHEDULED D CHECK AT DALFORT, FOUND Z FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,708 hrs · 30,734 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 5, WL 213. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,705 hrs · 30,730 cycles

DURING SCHEDULED SPECIAL VISIT CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 6, WL 213. REPAIRED WEB PER SRM.

Part: COVER — MISSING (CABIN FLOOR) · airframe 29,481 hrs · 29,543 cycles

EEPLS TRACK COVER MISSING AT FWD SECTION. REPLACED TRACK COVER PER MM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 29,409 hrs · 29,471 cycles

DURING SCHEDULED LINE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS LOW. R&R EVAC SLIDE ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 28,808 hrs · 28,896 cycles

EEPLS LOOSE AT EMERGENCY EXIT ROW. SECURED EEPLS TRACK PER MM.

Part: COVER — CRACKED (CABIN) · airframe 28,318 hrs · 28,398 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROW 1. REMOVED AND REPLACED TRACK COVER PER MM.

Part: SKIN — DELAMINATED (AILERON TAB) · airframe 27,535 hrs · 27,587 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING AILERON TAB LOWER SKIN DELAMINATED. REMOVED AND REPLACED TAB ASSY PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SPECIAL VISIT FOUND, FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/4D CHECK, FOUND THROUGH UT INSPECTION, A 1 INCH LONG CRACK AT BS 178 BULKHEAD RH SIDE, WL 200. REPAIRED PER SRM.

Part: LIGHT — MISSING (ROW 7)

EMERGENCY ESCAPE FLOOR TACK LIGHT BULB AND LENS MISSING AT ROW 7. REPLACED LIGHT BULB AND LENS PER MM.

Part: FRAME — CRACKED (FWD ENTRY DOOR)

DURING SCHEDULED 1/2 D-CHECK, FOUND FWD ENTRY DOOR FRAME CRACKED 8 INCHES ABOVE HANDLE OUT FRAME. REPAIRED PER SWA RA 1-552-0264.

Part: ACM — FAILED (CABIN)

HOT AIR AND SMOKE ENTERED CABIN AND COCKPIT AREAS DURING TAXI OUT. RETURNED TO GATE. REMOVED AND REPLACED NR 1 AIR CYCLE MACHINE DUE TO SEVERE OIL LEAK, ALONG WITH DISCHARGE SENSOR AND BAG PER BOEING M/M. ALSO, REMOVED AND REPLACED NR 2 AIR CYCLE MACHINE AND BAG AS PRECAUTIONARY PER BOEING M/M.

Part: EEL BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND A CABIN EMERGENCY LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M.