N651SW

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 60,856 hrs · 47,354 cycles

FORWARD CABIN FLASHLIGHT SECURITY STRAP BROKEN. R&R STRAP PER SIP.

Part: SUPPRESSOR — FAULTY (RT WING FUEL) · airframe 60,597 hrs · 47,182 cycles

NR 2 FUEL TANK READING ZERO IN CRUISE, FUEL QUANTITY ON NR 2 TANK RETURNED BELOW 10K FT WITHIN 300LBS OF NR 1. DIVERTED AND DECLARED AN EMERGENCY. R & R THE NR 2 FUEL TANK ANALOG TRANSIENT SUPPRESSION DEVICE IAW AMM.

Part: ACTUATOR — LEAKING (LT SPOILER) · airframe 59,151 hrs · 46,242 cycles

LEFT WING NR 3 FLIGHT SPOILER LEAKED. R & R ACTUATOR IAW MM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 58,619 hrs · 45,909 cycles

AFT EMER FLASHLIGHT STRAP BROKEN. R & R STRAP IAW MM.

Part: HYDRAULIC LINE — FAULTY (LT MLG WW) · airframe 58,483 hrs · 45,816 cycles

DECLARED EMER, LOSS OF A SYS HYD QTY. R & R LT MLG RETRACT LINE IAW AMM.

Part: SUPPORT ANGLE — CORRODED (LT WING) · airframe 58,479 hrs · 45,812 cycles

LEFT WING NR 4 STIFFENER REAR SPAR SUPPORT ANGLE, CORRODED AT APPROX RSS 185. REPAIRED ANGLE IAW SRM & DWG.

Part: SKIN — CRACKED (RT WING) · airframe 58,479 hrs · 45,812 cycles

RIGHT WING UPPER SKIN CRACKED AT AFT FASTENER HOLES APPROX BETWEEN RSS 239 - 255. REPAIRED SKIN IAW ER & EA.

Part: SPAR — CRACKED (LT WING) · airframe 58,479 hrs · 45,812 cycles

LEFT WING REAR SPAR WEB CRACKED, AT FASTENER HOLE RSS 223. REPAIRED WEB IAW ER & EA.

Part: FITTING — DAMAGED (LT WING) · airframe 58,479 hrs · 45,812 cycles

LEFT WING MLG FWD FITTING FASTENER HOLE DAMAGED, APPROX RSS 223. REPAIRED FITTING IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 58,479 hrs · 45,812 cycles

LEFT WING UPPER SKIN CRACKED, BETWEEN RSS 239 - 288. REPAIRED SKIN IAW ER & EA.

Part: ANGLE — CRACKED (LT WING) · airframe 58,479 hrs · 45,812 cycles

LEFT WING TE SEAL BULKHEAD LOWER ANGLE CRACKED AT WBL 209. R & R ANGLE IAW SRM.

Part: SPAR — CRACKED (RT WING) · airframe 58,479 hrs · 45,812 cycles

RIGHT WING REAR SPAR UPPER CHORD CRACKED, BETWEEN RSS 223 - 220. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 58,479 hrs · 45,812 cycles

LEFT WING REAR SPAR, UPPER CHORD CRACKED AT FASTENER HOLE UPPER ROW, APPROX RSS 223. REPAIRED CHORD IAW ER & EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,246 hrs · 45,653 cycles

AFT LAVATORY EMER LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,246 hrs · 45,653 cycles

RIGHT OVERWING EXIT LIGHT BULB INOPERATIVE. RELAMPED IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,239 hrs · 45,649 cycles

FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUT OUT. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 57,146 hrs · 44,890 cycles

GALLEY 1 EXIT SIGN BULB INOPERATIVE. R & R BULB IAW AMM.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 57,146 hrs · 44,890 cycles

LEFT WING NR 1 FLAP TRACK FAIRING SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: BRACKET — CRACKED (FLAP TRACK) · airframe 57,146 hrs · 44,890 cycles

LEFT WING NR 1 FLAP TRACK BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.

Part: FLAP — DELAMINATED (TE FLAP) · airframe 57,146 hrs · 44,890 cycles

LEFT WING OUTBOARD FORE FLAP OUTBOARD END EDGE DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 57,146 hrs · 44,890 cycles

STUB BEAM UPPER CHORD CRACKED AT BS 639, WL 208. REPAIRED CHORD IAW EO & EA.

Part: COVER — BROKEN (L1 DOOR SLIDE) · airframe 57,146 hrs · 44,890 cycles

L1 DOOR EMERGENCY EVACUATION SLIDE COVER VISOR BROKEN. R & R COVER ASSEMBLY IAW AMM & MT.

Part: COVER — CRACKED (R2 DOOR SLIDE) · airframe 57,146 hrs · 44,890 cycles

R2 DOOR EMERGENCY EVACUATION SLIDE COVER VISOR CRACKED. R & R COVER ASSEMBLY IAW AMM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 57,146 hrs · 44,890 cycles

TIE CLIP CRACKED AT BS 360, STRINGER 10L. R & R TIE CLIP IAW SRM & DWG.

Part: BEAM — CRACKED (FUSELAGE) · airframe 57,146 hrs · 44,890 cycles

STUB BEAM ASSEMBLY IN LOWEST OPEN FASTENER HOLE CRACKED AT BS 616, WL 202 RT SIDE. REPAIRED BEAM ASSEMBLY IAW EA..

Part: FRAME — CRACKED (BS 500C) · airframe 57,146 hrs · 44,890 cycles

FUSELAGE FRAME CRACKED AT BS 500C, BETWEEN STRINGER 20 - 21R. REPAIRED FRAME IAW SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 57,146 hrs · 44,890 cycles

LEFT WING INBD TE STRUCTURE ANGLE CRACKED AT WBL 87.49. REPAIRED ANGLE IAW EA.

Part: ANGLE — CRACKED (RT WING) · airframe 57,146 hrs · 44,890 cycles

RIGHT WING, OTBD TE STRUCTURE ANGLE CRACKED, WBL 203. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 57,146 hrs · 44,890 cycles

LEFT WING TE SUPPORT ANGLE CRACKED AT WBL 203. R & R ANGLE IAW SRM & DWG.

Part: WEB — CRACKED (RT WING TE) · airframe 57,146 hrs · 44,890 cycles

RIGHT WING TRAILING EDGE WEB CRACKED ON STRUCTURE SUPPORT AT WBL 414.40. REPAIRED WEB IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,146 hrs · 44,890 cycles

STRAP CRACKED AT BS 344, LBL 16. REPLACED STRAP IAW SRM & DWG.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 57,146 hrs · 44,890 cycles

CENTER SECTION MAIN WHEEL WELL PRESSURE DECK CRACKED AT BS 673, RBL 38. REPAIRED DECK IAW EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 57,146 hrs · 44,890 cycles

MAIN WHEEL WELL PRESSURE DECK CRACKED AT BS 663.75, RBL 38. REPAIRED DECK IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,146 hrs · 44,890 cycles

FRAME INNER CHORD CRACKED AT BS 616, WL 202 RT SIDE. REPAIRED CHORD IAW EA.

Part: SUPPORT ANGLE — CRACKED (RT MLG WW) · airframe 57,146 hrs · 44,890 cycles

RIGHT MAIN WW SUPPORT ANGLE CRACKED AT BS 679. R & R ANGLE IAW SRM & DWG.

Part: SLAT — DELAMINATED (LT WING) · airframe 57,124 hrs · 44,873 cycles

LEFT WING NR 1 SLAT DELAMINATED ON INBD TE. R & R NR 1 SLAT IAW MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 57,124 hrs · 44,873 cycles

RIGHT WING NR 5 LE SLAT DELAMINATED ON INBD TE CORNER. R & R NR 5 SLAT IAW MM.

Part: TAB — LOOSE (LT ELEVATOR) · airframe 56,671 hrs · 44,542 cycles

LEFT ELEVATOR TAB HINGE NR 2 OTBD FLANGED HAT BUSHING LOOSE IN HINGE BRACKET CLEVIS. R & R LT TAB IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 55,240 hrs · 43,542 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 55,127 hrs · 43,470 cycles

FORWARD RT EMER EXIT LIGHT LENS LOOSE. SECURED LENS IAW MM.

Part: COVER — MISSING (CABIN) · airframe 54,797 hrs · 43,242 cycles

AFT GALLEY SERVICE DOOR EXIT LIGHT COVER MISSING. INSTALLED COVER IAW SIP.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

STRINGER CLIP CRACKED AT BS 440 STRINGER 14L. R & R CLIP IAW SRM & DWG.

Part: FASTENER — MISSING (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

STRINGER SPLICE UPPER FLANGE FASTENERS MISSING AT BS 908 STRINGER 9L. INSTALLED FASTENER IAW SRM & DWG.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

SPLICE ANGLE CRACKED AT BS 360 STRINGER 11L. R & R SPLICE IAW SRM & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

FORWARD LT WINDOW BELT FRAME SKIN CRACKED AT BS 480 STRINGER 14L LOWER FASTENER HOLE. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

FORWARD LT WINDOW BELT FRAME SKIN CRACKED AT BS 380 STRINGER 14L LOWER FASTENER HOLE. REPAIRED SKIN IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

LEFT BS 747+10 WINDOW FRAME CRACKED. R & R WINDOW IAW DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

RIGHT BS 727+10 LOWER FWD WINDOW CORNER STRINGER SPLICE CRACKED. R & R SPLICE IAW DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

L2 DOOR AFT UPPER CORNER CRACKED. REPAIRED CORNER IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

RIGHT BS 767+10 REMOVE WINDOW FRAME LOWER FWD CORNER CRACKED. R & R WINDOW IAW DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

LEFT BS 807+10 UPPER AFT WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

RIGHT BS 767+10 LOWER FWD WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

LEFT BS 500A+10 LOWER AFT WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

LEFT BS 767+10 UPPER AFT WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

LEFT BS 847+10 UPPER AFT WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

RIGHT BS 727+10 UPPER AFT WINDOW CORNER SKIN CRACKED. REPAIRED WINDOW SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

RIGHT BS 867+10 LOWER FWD WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

LT BS 787+10 UPPER AFT WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

LEFT BS 867+10 UPPER AFT WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

RT BS 847+10 LOWER FORWARD WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

RIGHT BS 887+10 UPPER AFT WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW TC & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

RIGHT BS 787+10 UPPER AFT WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

RT BS 847+10 UPPER AFT WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

LEFT BS 500+10 LOWER AFT WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

LT BS 727+10 LOWER FORWARD WINDOW CORNER SKIN CUTOUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

RIGHT BS 887+10 LOWER FWD WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

LEFT BS 767+10 LOWER FWD WINDOW SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

LEFT BS 480+10 LOWER AFT WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW SB & TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

LEFT BS 747+10 UPPER AFT WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,605 hrs · 43,094 cycles

RIGHT BS 827+10 UPPER AFT WINDOW CORNER SKIN CRACKED. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (LE SLAT) · airframe 54,134 hrs · 42,745 cycles

LEFT WING NR 2 SLAT CRACKED AT LOWER SURFACE AFT ROW OF FASTENERS AT ACTUATOR ATTACHMENT. REPAIRED NR 2 SLAT IAW SRM.

Part: SLAT — CRACKED (RT WING) · airframe 53,459 hrs · 42,262 cycles

RIGHT WING NR 4 LE SLAT CRACKED. R & R SLAT IAW AMM.

Part: BRACKET — LOOSE (L1 DOOR) · airframe 52,969 hrs · 41,945 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED BRACKET IAW SIP.

Part: CIRCUIT CARD — FAULTY (NLG WW) · airframe 52,544 hrs · 41,673 cycles

AIR TURN BACK IN CRUISE BOTH RED & GREEN NOSE GEAR LIGHTS ILLUMINATED WITH GEAR HANDLE IN OFF POSITION GREEN NOSE GEAR ILLUMINATED WITH GEAR HANDLE UP NO RED, THREE GREENS NO RED WITH GEAR HANDLE IN DOWN POSITION. R & R M983 CIRCUIT CARD IAW MM.

Part: SKIN — CRACKED (ELEVATOR TAB) · airframe 52,370 hrs · 41,566 cycles

RT ELEVATOR TRIM TAB CRACKED ON UPPER SURFACE AT NR 3 HINGE. R & R TAB IAW MM.

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 52,279 hrs · 41,499 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR IAW MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,785 hrs · 41,133 cycles

WEB CRACKED BETWEEN BS 380 TO BS 400, LBL 24. R&R WEB IAW SRM.

Part: TAB — DELAMINATED (RT ELEVATOR) · airframe 51,367 hrs · 40,821 cycles

RT SIDE ELEVATOR TAB LOWER CORNER O/B SIDE DELAMINATED. REPAIRED ELEVATOR TAB IAW SRM.

Part: BRACKET — CRACKED (FLAP TRACK) · airframe 51,367 hrs · 40,821 cycles

LT WING NR 3 FLAP TRACK FAIRING BRACKET CRACKED ON WBL 187 UPPER POSITION. R&R BRACKET IAW SRM & DRAWING.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

STIFFENER CRACKED BETWEEN BS 312 TO BS 328, LBL 10. R&R STIFFENER IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FWD CARGO COMPARTMENT WEB CRACKED BETWEEN STATION 500A - STATION 500B, STRINGER 26L. R&R WEB IAW SRM & DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FWD CARGO COMPARTMENT ANGLE CRACKED AT BS 500B, STRINGER 26L. R&R ANGLE IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

WEB CRACKED BETWEEN BS 332.1 - BS 344, STRINGER 17R. R&R WEB IAW SRM & DRAWING

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

CREASE BEAM CRACKED AT BS 178, STRINGER 17L. REPAIRED BEAM IAW EO.

Part: SKIN — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

SKIN CORRODED BETWEEN BS 500A - BS 500B, STRINGER 22R. REPAIRED SKIN IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

WEB CRACKED BETWEEN BS 188 TO BS 196.5, STRINGER 17R. R&R WEB IAW SRM & DRAWING.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FWD BULKHEAD STIFFENER CRACKED AT BS 727, BETWEEN LBL 38 - LBL 48. R&R STIFFENER IAW SRM & DRAWING.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 51,367 hrs · 40,821 cycles

LT WING SUPPORT ANGLE CRACKED AT LEVEL WBL 191.00 AFT FAIRING. R&R ANGLE IAW SRM & DRAWING.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

WEB CORRODED BETWEEN BS 992.8 TO BS 1006, STRINGER 17R. R&R WEB IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FRAME WEB CRACKED AT BS 847, BETWEEN STRINGER 11L - STRINGER 13L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FRAME WEB CRACKED AT BS 847, BETWEEN STRINGER 11L TO STRINGER 13L. REPAIRED FRAME IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

WEB CRACKED BETWEEN BS 188 - BS 196.5, STRINGER 17L. R&R WEB IAW SRM & DRAWING.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

CHANNEL CRACKED BETWEEN BS 188 & BS 203.8, RBL 6. R&R CHANNEL IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

WEB CRACKED BETWEEN BS 178 - BS 188, RBL 30. R&R WEB IAW SRM & DRAWING.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

CHANNEL CRACKED BETWEEN BS 188 AND BS 203.8, LBL 6. R&R CHANNEL IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

WEB CRACKED BETWEEN BS 178 - BS 188, LBL 30. R&R WEB IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FWD ENTRY DOOR CUTOUT STRAP CRACKED BETWEEN BS 294.5 - BS 303.9, STRINGER 16L. R&R STRAP IAW SRM & DRAWING.

Part: PLATE — CRACKED (RT HORIZ STAB) · airframe 51,367 hrs · 40,821 cycles

RIGHT HORIZONTAL STABILIZER ACCESS PANEL NR 9226 PLATE CRACKED. R&R PLATE IAW SRM.

Part: SLAT — CRACKED (LT WING) · airframe 51,367 hrs · 40,821 cycles

LT WING NR 1 SLAT LEADING EDGE CRACKED. REPAIRED NR 1 SLAT IAW SRM.

Part: SLAT — CRACKED (LT WING) · airframe 51,367 hrs · 40,821 cycles

LT WING NR 2 SLAT LEADING EDGE CRACKED. REPAIRED NR 2 SLAT IAW SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 51,367 hrs · 40,821 cycles

LT WING NR 2 SLAT INBD UPPER SURFACE DELAMINATED. REPAIRED NR 2 SLAT IAW SRM.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 51,367 hrs · 40,821 cycles

RT WING NR 5 SLAT DELAMINATED ON UPPER SURFACE AT INBD EDGE. REPAIRED NR 5 SLAT IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

STRINGER CLIP CRACKED AT BS 294.5, STR 23L. R & R CLIP IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

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

Part: SLAT — CRACKED (LT WING) · airframe 51,367 hrs · 40,821 cycles

LT WING NR 1 SLAT LEADING EDGE CRACKED. REPAIRED NR 1 SLAT IAW SRM.

Part: BOTTLE — LOW PRESSURE (EVAC SLIDE) · airframe 51,367 hrs · 40,821 cycles

L2 DOOR EMERGENCY EVAC SLIDE BOTTLE PRESSURE LOW. R&R SLIDE IAW AMM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

INTERCOSTAL CORRODED BETWEEN BS 196.3 - BS 203.8, RBL 6. R&R INTERCOSTAL IAW EA & EO.

Part: SILL — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

AFT CARGO DOOR UPPER SILL WEB CORRODED BETWEEN BS 807 & BS 827, BETWEEN STRINGER 17R & STRINGER 18R. R&R WEB IAW SRM & DRAWING.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

INTERNAL DOUBLER CRACKED BETWEEN BS 360+5" - BS 380+4, STRINGER 27L - STRINGER 28R. R&R DOUBLER IAW SRM & DRAWING.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

WEB CORRODED BETWEEN BS 727B AND BS 727C, STR 17L. R & R WEB IAW SRM AND DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FLOOR STRUCTURE CENTER WING BOX BRACKET CRACKED AT BS 693, BL 0 LT SIDE. R & R BRACKET IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

SHEAR TIE CORRODED AT BS 360 BETWEEN STR 28LT, STR 27L. R & R SHEAR TIE IAW SRM AND DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FLOOR STRUCTURE BRACKET CRACKED AT BS 693, RBL 24.5. R&R CLIP IAW SRM & DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FRAME CORRODED AT BS 360, BETWEEN STRINGER 28L - STRINGER 28R. REPAIRED FRAME IAW EO & EA.

Part: DUCT — CRACKED (CABIN) · airframe 51,367 hrs · 40,821 cycles

DUCT ASSEMBLY CRACKED BETWEEN BS 312 - BS 323.7, BETWEEN STRINGER 26L TO STRINGER 27R. REPAIRED DUCT ASSEMBLY IAW EO & EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

TIE CLIP CRACKED AT BS 380, STR 26L. R & R TIE CLIP IAW SRM AND DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

STRINGER SPLICE CRACKED AT BS 907, STR 6L. R & R SPLICE IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

CLIP CRACKED AT BS 294, STR 13L. R & R CLIP IAW SRM AND DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FWD PAX CABIN FLOOR STRUCTURE ANGLE CRACKED BETWEEN BS 380 AND BS 400, BL 0. R & R ANGLE IAW SRM AN DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 294.5 TO BS 303.9, STR 16L CUT OUT FWD ENTRY DOOR. R & R ANGLE IAW SRM & DWG.

Part: PLATE — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

L1 DOOR CUTOUT PLATE CRACKED AT BS 303.9, STRINGER 10L. R&R PLATE IAW SRM.

Part: ISOLATOR — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

L1 DOOR INSULATION BRACKET CRACKED AT BS 360, STR 15L CUTOUT. R & R ISOLATOR IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

SUPPORT ANGLE CRACKED AT BS 947.5, BETWEEN STRINGER 24R TO STRINGER 25R. R&R ANGLE IAW SRM & DRAWING.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

STRINGER SPLICE CORRODED AT BS 907, STRINGER 18L. R&R SPLICE IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

AFT CARGO COMPARTMENT WEB CRACKED AT BETWEEN BS 927 TO BS 947.5, BETWEEN STR 25L TO STR 26L. R & R WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FRAME CRACKED AT BS 947.5, BETWEEN STRINGER 24R & STRINGER 25R. REPAIRED FRAME IAW EO & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

RT SIDE WING TO BODY FAIRING ANGLE CRACKED AT BS 540, STRINGER 22R. REPAIRED ANGLE IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FLOOR STRUCTURE CHANNEL CRACKED AT BS 540, BETWEEN BL 0 AND RBL 24.5. R & R CHANNEL IAW SRM AND DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

AFT CARGO COMPARTMENT WEB BRACKET CRACKED AT BS 947.5, BETWEEN STR 24L TO STR 25L. R & R BRACKET IAW SRM AND DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FLOOR STRUCTURE CHANNEL CRACKED AT BS 540, BETWEEN BL 0 AND LBL 24.5. R & R CHANEL IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

STRINGER CORRODED BETWEEN BS 907 TO BS 947.5, STRINGER 22L. R&R STRINGER IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

TIE CLIP CRACKED AT BS 663.75, STR 10L. R & R TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

TIE CLIP CRACKED AT BS 520, STR 8R. R & R TIE CLIP IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

TIE CLIP CRACKED AT BS 663.75, STR 10R. R & R TIE CLIP IAW SRM AND DWG.

Part: RUB STRIP — CRACKED (FAN COWLING) · airframe 51,367 hrs · 40,821 cycles

NR 1 ENGINE AFT EDGE OF INBD FAN COWL RUBSTRIP CRACKED. R & R RUBSTRIPS IAW SRM AND DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

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

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

STRINGER CRACKED AT BS 500, STRINGER 4L. REPAIRED STRINGER IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

SHEAR TIE CORRODED AT BS 476, STRINGER 19R. R&R ANGLE IAW SRM & DRAWING.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

STRINGER CRACKED AT BS 380, STRINGER 4R. REPAIRED STRINGER IAW SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

TIE CLIP CRACKED AT BS 440, STR 8L. R & R TIE CLIP IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FRAME CRACKED AT BS 380, BETWEEN STRINGER 11R & STRINGER 13R. REPAIRED FRAME IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

STRINGER CORRODED BETWEEN BS 927 - BS 986.5, STRINGER 21R. REPAIRED STRINGER IAW SRM & DRAWING.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

AFT CARGO COMPARTMENT STRINGER CORRODED BETWEEN BS 947.5 - BS 1016, STRINGER 22L. R&R STRINGER IAW SRM & DRAWING.

Part: BEARING — BROKEN (TE FLAP) · airframe 51,367 hrs · 40,821 cycles

LT WING NR 2 FLAP TRACK CARRIAGE A-FRAME BEARING BROKEN. R & R BEARING IAW CMM AND DWG.

Part: PLATE — BROKEN (L1 DOOR) · airframe 51,367 hrs · 40,821 cycles

L1 DOOR BROKEN PLATE OF PROXIMITY SENSOR LOCATED BETWEEN UPPER LATCH CRANK & LATCH CRANK ROLLER AT FWD FRAME. R&R PLATE IAW SRM.

Part: RUB STRIP — CRACKED (NR 2 NACELLE) · airframe 51,367 hrs · 40,821 cycles

NR 2 ENGINE NACELLE STRUT ACCESS PANEL RUBSTRIP CRACKED. R & R RUBSTRIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FWD CARGO COMPARTMENT FRAME CORRODED AT BS 500C, BETWEEN STRINGER 27L - STRINGER 28L. REPAIRED FRAME IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

SPLICE CHANNEL STRINGER CRACKED AT BS 360, STR 4L. R & R STRINGER IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FLOOR BEAM UPPER CHORD CORRODED AT BS 344, BETWEEN LBL 3 - LBL 24. REPAIRED CHORD IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FLOOR BEAM FLANGE CORRODED AT BS 986.5, BETWEEN BL 0 TO RBL 44. REPAIRED CHORD IAW EO & EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FWD CARGO COMPARTMENT STRINGER CRACKED BETWEEN BS 492.4 TO BS 500, STRINGER 22R. REPAIRED STRINGER IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

STRINGER CRACKED BETWEEN BS 492.4 - BS 500, STRINGER 23R. REPAIRED STRINGER IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

STRINGER CRACKED AT BS 400, STRINGER 4R. REPAIRED STRINGER IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

WEB CRACKED BETWEEN BS 277 TO BS 291, STR 14R. R & R WEB IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

SUPPORT ANGLE CRACKED AT BS 947.5+10, BETWEEN STR 24L TO STR 25L. R & R ANGLE IAW SRM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

STRAP CRACKED BETWEEN BS 307 TO BS 344, LBL 46. R & R STRAP IAW SRM AND DWG.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

TIE CLIP CRACKED AT BS 787, STR 20R. R & R SHEAR TIE IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

WEB CORRODED BETWEEN BS 986.5 TO BS 991, RBL 41. R&R WEB IAW SRM & DRAWING.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FLOOR BEAM CRACKED AT BS 947.5, LBL 53.5. REPAIRED BEAM IAW EO & EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

TIE CLIP CRACKED AT BS 380, STR 8L. R & R TIE CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FWD CARGO COMPARTMENT FRAME CORRODED AT BS 500C, BETWEEN STRINGER 27L - STRINGER 28L. REPAIRED FRAME IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

ANGLE CRACKED BETWEEN BS 277 TO BS 291, STR 11R. R & R ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

TIE CLIP CRACKED AT BS 787, STR 20R. R & R TIE CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

ANGLE CRACKED BETWEEN BS 277 TO BS 291, STR 10R. R & R ANGLE IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FWD CARGO COMPARTMENT STRINGER CORRODED BETWEEN BS 500A - BS 500B, STRINGER 26R. REPAIRED STRINGER IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FITTING CRACKED AT BS 332.1, STR 8R. R & R FITTING IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

STRINGER CORRODED BETWEEN BS 967 & BS 1016, STRINGER 25L. R&R STRINGER IAW SRM & DRAWING.

Part: STRUCTURE — CRACKED (RT MLG WW) · airframe 51,367 hrs · 40,821 cycles

RT MAIN WHEEL WELL CHORD CRACKED AT BS 680. R&R CHORD IAW SRM & DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

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

Part: BRACKET — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FWD BULKHEAD BRACKET CRACKED AT BS 727, STR 27R. R & R BRACKET IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FLOOR BEAM UPPER FLANGE CORRODED AT BS 986.5, BETWEEN BL 0 & LBL 44. REPAIRED CHORD IAW EO & EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

ANGLE CRACKED BETWEEN BS 277 TO BS 291, STR 12R. R & R ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FLOOR BEAM FLANGE CORRODED AT BS 967, BETWEEN RBL 4 - LBL 4. REPAIRED FLOOR BEAM IAW EO & EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

CLIP CRACKED AT BS 380, STR 26R. R & R CLIP IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

SUPPORT ANGLE CRACKED AT BS 787+1, STRINGER 18R. REPAIRED ANGLE IAW EO & EA.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FWD CARGO COMPARTMENT BRACKET CRACKED AT BS 500D, STR 19L. R & R BRACKET IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

AFT CARGO COMPARTMENT WEB BRACKET CRACKED AT BS 727A, STR 25R. R & R WEB IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FRAME LOWER FLANGE CORRODED AT BS 907, BETWEEN STRINGER 27R & STRINGER 27L. REPAIRED FLANGE IAW SRM & DRAWING.

Part: PLATE — CORRODED (GIRT BAR) · airframe 51,367 hrs · 40,821 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR PLATE & HARDWARE CORRODED. R&R PLATE & HARDWARE IAW AMM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FLOOR BEAM UPPER CHORD CORRODED AT BS 312, RBL 14. REPAIRED CHORD IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FLOOR BEAM UPPER CHORD REINFORCEMENT ANGLE CRACKED AT BS 328, RBL 58. R&R ANGLE IAW SRM & DRAWING.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 51,367 hrs · 40,821 cycles

MAIN WHEEL WELL PRESSURE DECK WEB CRACKED AT BS 664.75, LBL 39. REPAIRED WEB IAW EO & EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

STUB BEAM CRACKED AT BS 706, LBL 46. REPAIRED WEB IAW EO & EA.

Part: PLATE — CORRODED (GIRT BAR) · airframe 51,367 hrs · 40,821 cycles

LT 1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING PLATES CORRODED. R&R PLATES IAW MM.

Part: ANGLE — CRACKED (RT WING) · airframe 51,367 hrs · 40,821 cycles

RT WING T/E ANGLE CRACKED AT WBL 191. R & R ANGLE IAW SRM AND DWG.

Part: PLATE — CORRODED (GIRT BAR) · airframe 51,367 hrs · 40,821 cycles

RT 2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING PLATES CORRODED. R&R PLATES IAW MM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

L1 DOOR LOWER SILL Z ANGLE CORRODED BETWEEN BS 312 - BS 360, LBL 60.5. R&R "Z" ANGLE IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

AFT ENTRY DOOR FWD LOWER CORNER CUT OUT CRACKED AT BS 951.0+ 5.75, STRINGER 17L. REPAIRED SKIN IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FLOOR BEAM UPPER CHORD CRACKED AT BS 312, BETWEEN RBL 13 - RBL 39. REPAIRED CHORD IAW SRM.

Part: PLATE — CORRODED (GIRT BAR) · airframe 51,367 hrs · 40,821 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR PLATE & HARDWARE CORRODED. R&R PLATE & HARDWARE IAW AMM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 51,367 hrs · 40,821 cycles

LT WING SUPPORT ANGLE CRACKED FLAP AREA INTERNAL CAVITY FSS 194. R&R ANGLE IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FWD GALLEY DOOR AFT LOWER CORNER DOOR CUT OUT CRACKED AT BS 332.1, STRINGER 17R. REPAIRED SKIN IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FWD CARGO COMPARTMENT SUPPORT ANGLE CRACKED AT BS 420, STR 26L. R & R ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (RT WING) · airframe 51,367 hrs · 40,821 cycles

RT WING EXTERNAL SKIN OF FIXED LEADING CRACKED AT LEVEL WBL 208. REPAIRED SKIN IAW EA.

Part: SILL — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FWD GALLEY DOOR SILL WEB CRACKED. R&R WEB IAW SRM & DRAWING.

Part: ANGLE — CRACKED (RT WING) · airframe 51,367 hrs · 40,821 cycles

RT WING OTBD T/E ANGLE CRACKED AT WBL 204. R & R ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 51,367 hrs · 40,821 cycles

LEFT WING SUPPORT ANGLE CRACKED AT RSS 545 INTERNAL STRUCTURE T/E. R & R ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FLOOR BEAM WEB CRACKED AT BS 328, LBL 60. R&R WEB IAW SRM & DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

LOWER FLANGE OF FRAME CORRODED AT BS 747, BETWEEN STRINGER 25L - STRINGER 26L. REPAIRED FRAME IAW SRM.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 51,367 hrs · 40,821 cycles

CRACKED PHOTOLUMINSCENT STRIPS ALONG PAX CABIN. R&R EEPLS IAW AMM.

Part: PLATE — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

RIGHT OVERWING FILLER PLATE FWD SIDE HATCH CUTOUT CRACKED. R & R PLATE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FRAME LOWER FLANGE CORRODED AT BS 807, BETWEEN STRINGER 27L & STRINGER 27R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FRAME LOWER FLANGE CORRODED AT BS 747, BETWEEN STRINGER 26L - STRINGER 27L. REPAIRED FRAME IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 51,367 hrs · 40,821 cycles

LEFT WING SUPPORT STRUCTURE ANGLE CRACKED AT WBL 71.24. R & R ANGLE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

LOWER FLANGE OF FRAME CORRODED AT BS 747, BETWEEN STRINGER 25L - STRINGER 26L. REPAIRED FRAME IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

RT WING TO BODY FAIRING ANGLE CRACKED BETWEEN BS 685 + 10 TO BS 727, STRINGER 22R. R&R ANGLE IAW SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 51,367 hrs · 40,821 cycles

LEFT WING ANGLE CRACKED AT WBL 204.40. R & R ANGLE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FRAME LOWER FLANGE CORRODED AT BS 787, BETWEEN STRINGER 26R & STRINGER 27R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FRAME LOWER FLANGE CORRODED AT BS 727D, BETWEEN STRINGER 25L & STRINGER 26L. REPAIRED FLANGE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FRAME LOWER FLANGE CORRODED AT BS 727E, BETWEEN STRINGER 27L & STRINGER 27R. REPAIRED FLANGE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

AFT CARGO COMPARTMENT LOWER FRAME CORRODED AT BS 787, BETWEEN STRINGER 25L - STRINGER 26L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FRAME LOWER FLANGE CORRODED AT BS 787, BETWEEN STR 27L AND STR 27R. REPAIRED FRAME IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

LONGITUDINAL FLOOR BEAM WEB CRACKED BETWEEN BS 706 - BS 712, BBL 0.07. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

SKIN CRACKED AT BS 520+6.5, STR 28R. REPAIRED SKIN IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FLOOR BEAM WEB CRACKED BETWEEN BS 705 & BS 710, LBL 24.8. REPAIRED WEB IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FLOORBEAM WEB CRACKED BETWEEN BS 705 TO BS 710, RBL 24.8. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (LT MLG DOOR) · airframe 51,367 hrs · 40,821 cycles

LT MAIN LANDING GEAR BAY DOOR LOWER LOBE CRACKED. REPAIRED SKIN IAW SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,367 hrs · 40,821 cycles

FS SKIN CRACKED AT BS 360+18.5, STRINGER 28L. REPAIRED SKIN IAW EO & EA.

Part: LENS — BROKEN (CABIN) · airframe 51,268 hrs · 40,752 cycles

FORWARD SERVICE DOOR EMERGENCY EXIT LOWER LENS ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,929 hrs · 40,510 cycles

RIGHT EMERGENCY LIGHT INOP AT ROW 8. REMOVED AND REPLACED BATTERY ASSY IAW AMM.

Part: ANGLE — CRACKED (RT AILERON) · airframe 50,878 hrs · 40,475 cycles

RIGHT AILERON BALANCE BAY HORIZONTAL ANGLE CRACKED. REMOVED AND REPLACED ANGLE ASSEMBLY IAW SRM.

Part: SWITCH — FAULTY (E&E BAY) · airframe 50,841 hrs · 40,448 cycles

AIR TURNBACK -- ON TAKEOFF, GEAR HANDLE WOULD NOT GO PAST THE OFF POSITION. RAN APPROPRIATE CHECKLIST WHICH INDICATED FAILED GEAR HANDLE SOLENOID. PULLED TRIGGER AND GEAR CAME UP NORMALLY. REMOVED AND REPLACED S106 AIR SENSE SWITCH PER M/M.

Part: ANGLE — CRACKED (RT AILERON) · airframe 50,815 hrs · 40,429 cycles

RIGHT AILERON BALANCE BAY HORIZ ANGLE AT NR 2 HINGE CRACKED. REMOVED AND REPLACED ANGLE PER EA.

Part: ANGLE — CRACKED (RT AILERON) · airframe 50,815 hrs · 40,429 cycles

RIGHT WING AILERON BALANCE BAY VERTICAL ANGLE AT NR 2 HINGE CRACKED. REMOVED AND REPLACED ANGLE PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,815 hrs · 40,429 cycles

LEFT CABIN EMERGENCY EXIT LIGHT INOP AT ROW 21. REMOVED AND REPLACED LAMP PER MM.

Part: FAIRING — DELAMINATED (RT WING) · airframe 50,815 hrs · 40,429 cycles

RIGHT WING FAIRING DELAMINATED I/B SIDE. REPAIRED FAIRING PER SRM.

Part: ACTUATOR — FAULTY (LE SLAT) · airframe 50,338 hrs · 40,104 cycles

DIVERSION - AMBER L/E FLAPS TRANSIT LIGHT ILLUMINATED ON TAKEOFF WITH ASSOCIATED AMBER L/E FLAP NR 2 LIGHT ILLUMINATED ON AFT OVERHEAD PANEL. NO ROLL. FOUND NR 2 KRUEGER FLAP ACTUATOR NOT FULLY RETRACTING. REMOVED AND REPLACED ACTUATOR IAW AM.

Part: VALVE — FAULTY (FUEL SYSTEM) · airframe 50,060 hrs · 39,915 cycles

DIVERSION --FUEL CROSSFEED VALVE LIGHT ILLUMINATED. BRIGHT WITH CROSSFEED VALVE SELECTOR IN BOTH CLOSED OR OPEN. REMOVED AND REPLACED FUEL CROSSFEED VALVE C

Part: PLUG — FAULTY (FUEL SYSTEM) · airframe 50,060 hrs · 39,915 cycles

DIVERSION -- FUEL CROSS FEED VALVE LIGHT ILLUMINATED. REMOVED AND REPLACED PLUG IAW AMM.

Part: ACCESSORY UNIT — FAULTY (AC BAY) · airframe 49,899 hrs · 39,790 cycles

LOSS OF CABIN PRESS CONTROL. REMOVED AND REPLACED A/C ACCY UNIT PER MM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 49,845 hrs · 39,751 cycles

RIGHT EMERGENCY EXIT LIGHT INOP AT ROW 8. REMOVED AND REPLACED BULB PER AMM.

Part: CLAMP — LOOSE (AC BAY) · airframe 49,519 hrs · 39,496 cycles

DIVERSION/DECLARED EMERGENCY. CABIN ALTITUDE WARNING HORN SOUNDED AT CRUISE 37,000, CABIN ALTITUDE CLIMBED. FOUND KEEL BEAM BOOT CLAMP LOOSE AND REMOVED AND REPLACED BELLY DRAINS PER MM.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 49,465 hrs · 39,456 cycles

DIVERSION/DECLARED EMERGENCY. AT CRUISE - FL370, EQUIPMENT COOLING OFF LIGHT CAME ON, IT WAS ALREADY IN ALT, CONTINUED. ALTITUDE WARNING HORN SOUNDED ABOUT 20 MINS LATER. STARTED EMERGENCY DESCENT, SWITCHED CONTROLLER TO ALT, CABIN RISE WENT FROM 200-300 CLIMB TO 0. HORN STOPPED AT FL180. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER AND LOWER EXHAUST COOLING TEMPERATURE SENSOR PER AMM.

Part: WEB — CRACKED (FUSELAGE) · airframe 49,422 hrs · 39,425 cycles

WEB CRACKED BETWEEN BS 827 AND BS 847, STR 27R. REMOVED & REPLACED WEB IAW SRM & BAC DWG.

Part: FASTENER — LOOSE (R2 DOOR) · airframe 49,422 hrs · 39,425 cycles

R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FASTENERS IAW MM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 49,422 hrs · 39,425 cycles

STRINGER CLIP CORRODED AT BS 867, STR 27R. REMOVED AND REPLACED CLIP IAW BAC DWG AND SRM.

Part: SLAT — DAMAGED (LT WING) · airframe 49,422 hrs · 39,425 cycles

LEFT WING NR 2 SLAT I/B SLAT CAN DAMAGED BY FOD. REMOVED AND REPLACED SLAT CAN IAW BAC DWG.

Part: SLAT — DAMAGED (LT WING) · airframe 49,422 hrs · 39,425 cycles

LEFT WING NR 2 SLAT O/B CAN DAMAGED BY FOD. REMOVED AND REPLACED SLAT CAN IAW BAC DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 49,422 hrs · 39,425 cycles

AFT CARGO DOOR CUTOUT AFT FRAME CRACKED. REMOVED AND REPLACED FRAME IAW BAC DWG.

Part: WEDGE — PUNCTURED (TE FLAP) · airframe 49,227 hrs · 39,272 cycles

RIGHT WING NR 6 SLAT UPPER SURFACE TRAILING EDGE WEDGE PUNCTURED. REPAIRED WEDGE IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 49,227 hrs · 39,272 cycles

STRINGER CORRODED BETWEEN BS 352 TO BS 355, STR 28L. REMOVED AND REPLACED STRINGER IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 49,227 hrs · 39,272 cycles

STRINGER CORRODED BETWEEN BS 340 TO BS 344, STR 19R. REPAIRED STRINGER PER ER AND EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,224 hrs · 39,271 cycles

RIGHT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 8. REMOVED AND REPLACED BULB PER AMM.

Part: LENS — MISSING (EXIT SIGN) · airframe 48,153 hrs · 38,455 cycles

LT OVERWING EXIT SIGN MISSING LENS. REPLACED LENS IAW M/M.

Part: ACTUATOR — FAULTY (RT SPOILER) · airframe 47,672 hrs · 38,123 cycles

DURING DESCENT INTO MDW, LOST "A" SYSTEM HYDRAULIC FLUID/PRESSURE. REMOVED AND REPLACED RT O/B GROUND SPOILER ACTUATOR IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,206 hrs · 37,014 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 8. RELAMPED PER MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,888 hrs · 36,772 cycles

DURING SCHEDULE 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 639, LBL 45.5. REPAIRED WEB IAW SRM AND ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,888 hrs · 36,772 cycles

DURING SCHEDULE 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 639, RBL 45.5. REPAIRED WEB IAW SRM AND ER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,888 hrs · 36,772 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP AT ROW 8. REMOVED AND REPLACED LIGHT PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 45,888 hrs · 36,772 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 28R TO STR 28L. REPAIRED SHEAR TIE PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 45,888 hrs · 36,772 cycles

DURING SCHEDULED 14Y CHECK, FOUND LOWER R1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 45,888 hrs · 36,772 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, BETWEEN STR 28R TO STR 28L. REPAIRED SHEAR TIE PER SRM.

Part: WEDGE — DELAMINATED (MIDFLAP) · airframe 45,888 hrs · 36,772 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING I/B MIDFLAP T/E WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE IAW MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 45,888 hrs · 36,772 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR BRACKET LOOSE. REMOVED AND REPLACED BRACKET PER SRM.

Part: SIGN — LOOSE (CABIN) · airframe 45,888 hrs · 36,772 cycles

DURING SCHEDULED 14Y CHECK, FOUND R2 DOOR LOWER EMERGENCY EXIT SIGN LIGHT LOOSE. REMOVED AND REPLACED SIGN PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 45,166 hrs · 36,208 cycles

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

Part: SIGN — BROKEN (CABIN) · airframe 44,769 hrs · 35,904 cycles

L1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 44,432 hrs · 35,640 cycles

DURING SCHEDULED SPV CHECK, FOUND BULKHEAD CRACKED AT BS 178, RBL 17.0. REPAIRED BULKHEAD PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 41,962 hrs · 33,740 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 66,885 hrs · 59,337 cycles

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

Part: SLAT — DELAMINATED (LT WING) · airframe 40,438 hrs · 32,617 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 2 SLAT DELAMINATED. REPAIRED SLAT PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 40,262 hrs · 32,493 cycles

R1 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM.

Part: HINGE FITTING — CRACKED (FUSELAGE) · airframe 40,212 hrs · 32,456 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR UPPER HINGE FITTING CRACKED BS 304, WL 259.6. REMOVED AND REPLACED FITTING PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,212 hrs · 32,456 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 787, BETWEEN STR 26L TO STR 26R. REPAIRED BEAM PER SRM.

Part: WEB — CRACKED (NLG WW) · airframe 40,212 hrs · 32,456 cycles

DURING SCHEDULED 12Y CHECK, FOUND NOSE WHEEL WELL CEILING WEB CRACKED AT BS 253, LBL 7.75. REPAIRED WEB PER ACO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,212 hrs · 32,456 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: WEB — CRACKED (NLG WW) · airframe 40,212 hrs · 32,456 cycles

DURING SCHEDULED 12Y CHECK, FOUND NOSE WHEEL WELL CEILING WEB CRACKED AT BS 253, LBL 7.75. REPAIRED WEB PER ACO.

Part: WEB — CRACKED (NLG WW) · airframe 40,212 hrs · 32,456 cycles

DURING SCHEDULED 12Y CHECK, FOUND NOSE WHEEL WELL CEILING WEB CRACKED AT BS 253, RBL 7.75. REPAIRED WEB PER ACO.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 40,212 hrs · 32,456 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 40,212 hrs · 32,456 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING NR1 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,212 hrs · 32,456 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CORRODED AT BS 500C, BETWEEN STR 27R TO STR 28R. REPAIRED ANGLE PER SRM.

Part: TAB — BROKEN (ELEVATOR) · airframe 40,262 hrs · 32,493 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT ELEVATOR TAB BROKEN AT CONTROL ROD MOUNTS. REMOVED AND REPLACED TAB PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 40,212 hrs · 32,456 cycles

DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 39,825 hrs · 32,159 cycles

DURING SCHEDULED CV CHECK, FOUND L2 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 39,825 hrs · 32,159 cycles

DURING SCHEDULED CV CHECK, FOUND R1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 38,973 hrs · 31,531 cycles

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

Part: FLAP — DELAMINATED (RT WING) · airframe 38,647 hrs · 31,336 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING OTBD T/E FLAP DELAMINATED AT INBD END. REMOVED AND REPLACED FLAP PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,515 hrs · 30,534 cycles

BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 13 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,515 hrs · 30,534 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 13 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 37,417 hrs · 30,461 cycles

DURING SCHEDULED HC2 CHECK, FOUND FWD SERVICE DOOR FRAME CRACKED AT LOWER FRAME AFT LOWER STOP. REMOVED AND REPLACED DOOR PER MM.

Part: MOTOR — FAULTY (HORIZ STAB) · airframe 35,710 hrs · 29,211 cycles

DURING SCHEDULED HC1 CHECK, FOUND JACKSCREW GIMBAL HITS STABILIZER JACKSCREW NOSE DOWN STOP WITH FLAPS DOWN. REMOVED AND REPLACED MAIN ELECTRIC STABILIZER MOTOR PER MM.

Part: JACKSCREW — MALFUNCTIONED (HORIZ STAB) · airframe 35,710 hrs · 29,211 cycles

DURING SCHEDULED HC1 CHECK, FOUND HORIZONTAL STABILIZER MOTOR CONTINUES TO FREE WHEEL AFTER RELEASING SWITCH IN FLIGHT DECK. REMOVED AND REPLACED STABILIZER JACKSCREWER MM.

Part: LENS — DETERIORATED (CABIN) · airframe 35,667 hrs · 29,179 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT LENS DETERIORATED. REMOVED AND REPLACED LENS PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 35,541 hrs · 29,088 cycles

FLIGHT DECK R2 WINDOW ARCING. REMOVED AND REPLACED WINDOW PER MM.

Part: FRAME — CRACKED (BS 380 S8L) · airframe 35,160 hrs · 28,791 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,946 hrs · 27,858 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,946 hrs · 27,858 cycles

DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, STR 28L. REPAIRED SHEAR TIE PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,946 hrs · 27,858 cycles

DURING SCHEDULED 10Y CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,946 hrs · 27,858 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, STR 18L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,946 hrs · 27,858 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 440 S8R) · airframe 33,946 hrs · 27,858 cycles

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

Part: FRAME — CRACKED (BS 360 S8R) · airframe 33,946 hrs · 27,858 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA.

Part: PUSHROD — WORN (LT ELEVATOR) · airframe 33,946 hrs · 27,858 cycles

DURING SCHEDULED 10Y CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL PUSHROD AND BEARING PER MM.

Part: PUSHROD — WORN (RT ELEVATOR) · airframe 33,946 hrs · 27,858 cycles

DURING SCHEDULED 10Y CHECK, RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL PUSHROD AND BEARING PER MM.

Part: FRAME — CRACKED (BS 827 S8L) · airframe 33,946 hrs · 27,858 cycles

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

Part: FRAME — CRACKED (BS 597 S8R) · airframe 33,946 hrs · 27,858 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 520 S8R) · airframe 33,946 hrs · 27,858 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 787 S8L) · airframe 33,946 hrs · 27,858 cycles

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

Part: FRAME — CRACKED (BS 500C S8R) · airframe 33,946 hrs · 27,858 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 33,946 hrs · 27,858 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT FWD CABIN EMERGENCY EXIT LIGHTS INOP. INSPECTED AND FOUND LOOSE WIRING, REPAIRED WIRING PER MM AND WDM.

Part: FRAME — CRACKED (BS 360 S8R) · airframe 33,946 hrs · 27,858 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 616 S18L) · airframe 33,946 hrs · 27,858 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, STR 18L. REPAIRED FRAME PER SB.

Part: FRAME — CRACKED (BS 520 S8R) · airframe 33,946 hrs · 27,858 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 500C S8R) · airframe 33,946 hrs · 27,858 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 827 S8L) · airframe 33,946 hrs · 27,858 cycles

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

Part: FRAME — CRACKED (BS 747 S8R) · airframe 33,946 hrs · 27,858 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 440 S8L) · airframe 33,946 hrs · 27,858 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,946 hrs · 27,858 cycles

DURING SCHEDULED RON, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,946 hrs · 27,858 cycles

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

Part: FRAME — CRACKED (BS 787 S8L) · airframe 33,946 hrs · 27,858 cycles

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

Part: FRAME — CRACKED (BS 597 S8R) · airframe 33,946 hrs · 27,858 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (BS 706 S11-11R/L) · airframe 33,946 hrs · 27,858 cycles

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

Part: FRAME — CRACKED (BS 440 S8L) · airframe 33,946 hrs · 27,858 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,946 hrs · 27,858 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 33,946 hrs · 27,858 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 32,979 hrs · 27,094 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EVACUATION SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSY PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 32,979 hrs · 27,094 cycles

DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS ASSY PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 32,979 hrs · 27,094 cycles

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

Part: ACTUATOR — BROKEN (NR 5 SPOILER) · airframe 31,917 hrs · 26,301 cycles

DURING SCHEDULED C3 CHECK, FOUND RT WING NR 5 GROUND SPOILER INBOARD ACTUATOR ROD END BROKEN. REMOVED AND REPLACED INBOARD ACTUATOR PER MM.

Part: FRAME — CRACKED (BS 492 S24R) · airframe 31,601 hrs · 26,060 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, STR 24R. REMOVED AND REPLACED FRAME SECTION PER ACO AND BOEING DRAWING.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 31,045 hrs · 25,624 cycles

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

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 30,624 hrs · 25,309 cycles

AFT SERVICE DOOR LOWER EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LINE — LEAKING (B-HYD SYSTEM) · airframe 29,625 hrs · 24,543 cycles

DECLARED EMERGENCY, LOST B-SYSTEM HYDRAULIC PRESSURE. B-SYSTEM HYDRAULIC QUANTITY DROPPED TO 1/4 FULL. REMOVED AND REPLACED B-SYSTEM HYDRAULIC ELECTRIC DRIVEN PUMP LINE PER MM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 28,511 hrs · 23,687 cycles

DURING SCHEDULED RON CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 28,168 hrs · 23,408 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 28,168 hrs · 23,408 cycles

DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EVACUATION SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 24,505 hrs · 20,529 cycles

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

Part: STRUCTURE — DELAMINATED (LT WING TE FLAP) · airframe 19,733 hrs · 16,752 cycles

DURING SCHEDULED C2 CHECK, FOUND LT OTBD AFT T/E FLAP DELAMINATED AT INBD LOWER CORNER. R&R LT OTBD AFT T/E FLAP PER MM.

Part: TRUNNION PIN — CORRODED (LT AND RT MLG) · airframe 19,040 hrs · 16,200 cycles

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

Part: LENS — MISSING (CABIN) · airframe 50,223 hrs · 37,684 cycles

DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT SIGN LENS MISSING AT ROW 23. REMOVED AND REPLACED EMERGENCY EXIT SIGN AT ROW 23 PER M/M.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 50,223 hrs · 37,684 cycles

DURING SCHEDULED C1 CHECK, FOUND THE R1 DOOR ESCAPE SLIDE OUT OF ADJUSTMENT. ADJUSTED THE R1 DOOR ESCAPE SLIDE PER M/M.

Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 17,806 hrs · 15,223 cycles

DURING SCHEDULED BC4 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REPOSITIONED SLIDE PER MM.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 16,899 hrs · 14,461 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 859, LBL 13 AND LBL 8. REPAIRED FLOORBEAM PER SWA RA.

Part: ELEVATOR — DEBONDED (RT ELEVATOR) · airframe 16,899 hrs · 14,461 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT ELEVATOR DEBONDED ON LOWER SKIN AT 2ND MOST INBD HINGE POINT. REPAIRED ELEVATOR PER SRM.

Part: COVER — MISSING (CABIN) · airframe 15,373 hrs · 13,187 cycles

EEPLS COVER MISSING AT MID CABIN. INSTALLED COVER PER MM.

Part: CAP — MISSING (CABIN) · airframe 14,991 hrs · 12,907 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS END CAP MISSING AT FWD CABIN. INSTALLED END CAP PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 13,848 hrs · 11,942 cycles

EEPLS LOOSE AT OVERWING EXIT. SECURED EEPLS PER MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 13,591 hrs · 11,719 cycles

EEPLS INOP AT ROW 14. RECONNECTED EEPLS WIRES PER MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 13,551 hrs · 11,684 cycles

DURING SCHEDULED PM CHECK, FOUND EEPLS INOP AT MID CABIN. RECONNECTED WIRES PER MM.

Part: COVER — LOOSE (CABIN FLOOR) · airframe 13,440 hrs · 11,594 cycles

EEPLS COVER LOOSE AT ROW 14. SECURED COVER PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 12,421 hrs · 10,750 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,160 hrs · 10,531 cycles

DURING SCHEDULED C2 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT BULLNOSE, ROW 20 DEF. RELAMPED LIGHT ASSY PER MM.

Part: SOCKET — UNPLUGED (CABIN)

DURING SCHEDULED A1 CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 14-18 INOPERATIVES. FOUND SOCKET ASSY UNPLUGED AT ROW 14, RESECURED PLUG PER BOEING MM.

Part: ENGINE — OIL LEAK (NR 2)

DURING WALKAROUND CHECK, FOUND NR 2 ENGINE DRIPPING OIL FROM DRAIN HOLE AT 9 O'CLOCK POSITION. REPLACED ENGINE ASSEMBLY PER BOEING M/M.