N632SW

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,895 hrs · 50,464 cycles

AFT GALLEY ENTRANCE EMERGENCY EXIT SIGN LIGHT STRIP BULB INOPERATIVE. R & R THE SIGN ASSEMBLY IAW AMM.

Part: CONTROL MODULE — INOPERATIVE (E&E BAY) · airframe 63,887 hrs · 50,458 cycles

AIR TURNBACK, PRESSURIZATION NOT WORKING IN AUTO. WE DISCOVERED THAT THE AIRCRAFT WAS NOT PRESSURIZING AS WE CLIMBED THROUGH 10,000. R&R CABIN PRESSURE CONTROL MODULE PER MM.

Part: COVER — DETACHED (CABIN) · airframe 63,604 hrs · 50,251 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER DETACHED. REPAIRED COVER PER SIP.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 63,053 hrs · 49,891 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SHUTOFF VALVE — INOPERATIVE (HYD SYSTEM) · airframe 63,016 hrs · 49,871 cycles

TOTAL LOSS OF SYSTEM "A" HYDRAULICS. EMERGENCY DECLARED AND RETURNED TO DEPARTURE. R & R THE SHUTOFF VALVE IAW AMM.

Part: HANDLE — LOOSE (EMERGENCY EXIT) · airframe 62,371 hrs · 49,459 cycles

RIGHT EMERGENCY EXIT INTERIOR HATCH HANDLE LOOSE. R & R HANDLE IAW AMM.

Part: HANDLE — LOOSE (EMERGENCY EXIT) · airframe 62,371 hrs · 49,459 cycles

LEFT EMERGENCY EXIT INTERIOR HATCH HANDLE LOOSE. R & R HANDLE IAW AMM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 62,117 hrs · 49,299 cycles

FORWARD GALLEY EMER FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW SIP.

Part: LENS — LOOSE (CABIN) · airframe 61,418 hrs · 48,833 cycles

OVERHEAD BULLNOSE EMER EXIT LIGHT LENS LOOSE AT ROW 24. R & R LENS IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,277 hrs · 48,748 cycles

SKIN CRACKED AT BS 727, BETWEEN STRINGER 18R - 19R. REPAIRED SKIN IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,277 hrs · 48,748 cycles

FORWARD ENTRY DOOR AT FORWARD GALLEY LOWER EMERGENCY EXIT LIGHT BULB INOP. R&R BULB IAW AMM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 61,277 hrs · 48,748 cycles

AFT CARGO COMPARTMENT CHANNEL SUPPORT CRACKED, AT BS 727+3, RBL 3. R & R SUPPORT IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,277 hrs · 48,748 cycles

AFT CARGO COMPARTMENT INTERCOSTAL WEB CRACKED, BETWEEN BS 927 - 947.5, STRINGER 25R. R & R WEB IAW SRM & DWG.

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 61,277 hrs · 48,748 cycles

CENTER WING BOX SUPPORT BEAM CRACKED. R & R BEAM IAW SRM & DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 61,277 hrs · 48,748 cycles

AFT CARGO COMPARTMENT LOWER SILL CORRODED, BETWEEN BS 807 - 847, STRINGER 25R. R & R LOWER SILL IAW SRM & DWG.

Part: SKIN — CRACKED (LT MLG DOOR) · airframe 61,277 hrs · 48,748 cycles

LEFT MLG AFT EDGE INNER SKIN ON OUTER DOOR CRACKED. REPAIRED SKIN IAW SRM.

Part: HANGER ASSY — CORRODED (LT MLG) · airframe 61,277 hrs · 48,748 cycles

LEFT MLG BORE, CORRODED ON WALKING BEAM HANGER. REPAIRED BORE IAW CMM.

Part: SKIN — CRACKED (LT WING) · airframe 61,277 hrs · 48,748 cycles

LEFT WING REAR SPAR UPPER SKIN CRACKED, BETWEEN RSS 215 - 267.5. REPAIRED SKIN IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 61,277 hrs · 48,748 cycles

LT WING REAR SPAR WEB CRACKED AT RSS 186. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 61,277 hrs · 48,748 cycles

RT WING REAR SPAR UPPER SKIN CRACKED AT WSTA 186.5. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 61,277 hrs · 48,748 cycles

RT WING REAR SPAR UPPER SKIN CRACKED AT WSTA 196. REPAIRED SKIN IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 61,277 hrs · 48,748 cycles

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

Part: SKIN — DELAMINATED (LT WING) · airframe 61,277 hrs · 48,748 cycles

LEFT WING FIXED LE, UPPER SKIN DELAMINATED AT LEVEL FSS 536. REPAIRED SKIN IAW SRM.

Part: SKIN — DELAMINATED (LT WING) · airframe 61,277 hrs · 48,748 cycles

LEFT WING EXTERNAL SKIN DELAMINATED ON INBD FLAP, OTBD TRACK FAIRING. REPAIRED SKIN IAW SRM.

Part: DOUBLER — CRACKED (LT WING) · airframe 61,277 hrs · 48,748 cycles

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

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 61,277 hrs · 48,748 cycles

LT WING NR 4 SPOILER ACTUATOR SUPPORT FITTING CRACKED. R&R FITTING IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 61,277 hrs · 48,748 cycles

RIGHT WING SUPPORT ANGLE CRACKED AT EXTERNAL AREA OF INBD FLAP, OTBD TRACK FAIRING. R & R SUPPORT ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (LT WING) · airframe 61,277 hrs · 48,748 cycles

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

Part: SUPPORT FITTING — CRACKED (TE FLAP) · airframe 61,277 hrs · 48,748 cycles

LEFT WING SUPPORT CLIP CRACKED AT INTERNAL AREA OF INBD FLAP, OTBD TRACK FAIRING. R & R CLIP IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 61,277 hrs · 48,748 cycles

LEFT WING SUPPORT ANGLE CRACKED AT INTERNAL AREA OF INBD FLAP, OTBD TRACK FAIRING. R & R SUPPORT ANGLE IAW SRM & DWG.

Part: FITTING — CORRODED (RT WING) · airframe 61,277 hrs · 48,748 cycles

RIGHT WING MLG SUPPORT BEAM, SWING LINK FITTING CORRODED. REPAIRED FITTING IAW CMM.

Part: FITTING — CORRODED (LT WING) · airframe 61,277 hrs · 48,748 cycles

LEFT WING MLG SUPPORT BEAM, SWING LINK FITTING CORRODED. REPAIRED FITTING IAW CMM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,277 hrs · 48,748 cycles

LEFT WING INBD FORE FLAP INTERNAL LOWER SKIN DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,277 hrs · 48,748 cycles

INTERCOSTAL CRACKED AT STATION 312 - 328, LBL 45.5. REPAIRED INTERCOSTAL IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,277 hrs · 48,748 cycles

RIGHT WING OTBD AFT FLAP DELAMINATED ON LOWER SKIN. REPAIRED AFT FLAP IAW SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 61,277 hrs · 48,748 cycles

STRINGER SPLICE CORRODED AT BS 907, STRINGER 22R. R & R SPLICE IAW SRM & DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,277 hrs · 48,748 cycles

RIGHT WING INBD AFT FLAP, INTERNAL LOWER SKIN DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: SUPPORT BEAM — CORRODED (LT WING) · airframe 61,277 hrs · 48,748 cycles

LT WING MAIN LANDING GEAR SUPPORT BEAM CORRODED ON LOWER SURFACE. REPAIRED BEAM IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,277 hrs · 48,748 cycles

LEFT WING OTBD FORE FLAP, LOWER SKIN DELAMINATED INBD SIDE. REPAIRED FORE FLAP IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,277 hrs · 48,748 cycles

WEB INTERCOSTAL CRACKED, BETWEEN BS 787 - 807, RBL 17. R & R INTERCOSTAL IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,277 hrs · 48,748 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 22L. R & R TIE CLIP IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,277 hrs · 48,748 cycles

TIE CLIP CRACKED AT BS 380, STRINGER 21L. R & R TIE CLIP IAW SRM & DWG.

Part: BEAM — CORRODED (RT MLG) · airframe 61,277 hrs · 48,748 cycles

RIGHT MLG BEAM ARM ASSEMBLY, ACTUATOR CORRODED. REPAIRED BEAM IAW CMM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,277 hrs · 48,748 cycles

FORWARD CARGO COMPARTMENT, ANGLE CRACKED AT BS 540, BETWEEN STRINGER 28L - 28R. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,277 hrs · 48,748 cycles

FORWARD CARGO COMPARTMENT FRAME CORRODED AT BS 380, BETWEEN STRINGER 28L - 28R. REPAIRED FRAME IAW SRM.

Part: BEAM — CORRODED (LT MLG) · airframe 61,277 hrs · 48,748 cycles

LEFT MLG WALKING BEAM ARM ACTUATOR CORRODED. REPAIRED BEAM IAW CMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,277 hrs · 48,748 cycles

FRAME CRACKED AT BS 947.5, STR 25R. REPAIRED FRAME IAW EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 61,277 hrs · 48,748 cycles

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

Part: ARM — CORRODED (RT MLG) · airframe 61,277 hrs · 48,748 cycles

RT MAIN LANDING GEAR WALKING BEAM ARM ACTUATOR CORRODED. REPAIRED ARM ASSEMBLY IAW CMM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 61,277 hrs · 48,748 cycles

LEFT HORIZONTAL STABILIZER STIFFENER CTR SECTION CRACKED. R & R STIFFENER IAW SRM & DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 61,277 hrs · 48,748 cycles

AFT CARGO TEE STIFFENER CRACKED AT BS 727, STRINGER 27L. R & R TEE STIFFENER IAW SRM & DWG.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 61,277 hrs · 48,748 cycles

LEFT HORIZONTAL STABILIZER LE SKIN CRACKED AT STATION 235.43 TO 265.30. REPAIRED SKIN IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,277 hrs · 48,748 cycles

STRINGER CLIP CRACKED AT STATION 277, STRINGER 10R. R & R CLIP IAW SRM.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 61,277 hrs · 48,748 cycles

AFT CARGO COMPARTMENT DOOR CRACKED AT HOLE ON T CHORD, LOCATED 3.5" FROM FWD EDGE ON INTERNAL STRUCTURE AT FWD END OF CROSS BEAM E. REPAIRED T CHORD CROSS BEAM E IAW EA.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 61,277 hrs · 48,748 cycles

AFT CARGO COMPARTMENT DOOR, AFT END OF CROSSBEAM E, WEB CRACKED AT BS 787, 4.5" FROM AFT EDGE. REPAIRED WEB IAW EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 61,277 hrs · 48,748 cycles

AFT CARGO COMPARTMENT TEE STIFFENER CRACKED AT BS 727, STRINGER 27R. R & R TEE STIFFENER IAW SRM & DWG.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 61,277 hrs · 48,748 cycles

AFT CARGO COMPARTMENT DOOR INTERNAL STRUCTURE AT INNER CHORD CRACKED ON HOLE, LOCATED 4.5" FROM AFT EDGE ON AFT END OF CROSSBEAM E. R & R CHORD IAW SRM & DWG.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 61,277 hrs · 48,748 cycles

LT WING REAR SPAR MAIN LANDING GEAR BEAM AFT SUPPORT FITTING CRACKED AT RSS. 222.5. R&R FITTING IAW EA.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 61,277 hrs · 48,748 cycles

AFT CARGO COMPARTMENT DOOR T-CHORD CROSS BEAM E CRACKED. REPAIRED CROSS BEAM E IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 61,277 hrs · 48,748 cycles

AFT CARGO COMPARTMENT, WEB CRACKED ON LOWER SILL, LOCATED AT BS 794.3, BETWEEN STRINGER 23R - 25R. R & R WEB IAW SRM & DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 61,277 hrs · 48,748 cycles

FORWARD PRESS BULKHEAD VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB IAW EA.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 61,277 hrs · 48,748 cycles

AFT CARGO COMPARTMENT DOOR CRACKED, ON INTERNAL STRUCTURE AT HOLE ON WEB, LOCATED 5.5" FROM FWD EDGE. REPAIRED CROSS BEAM E IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 61,277 hrs · 48,748 cycles

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

Part: SPAR — CRACKED (RT WING) · airframe 61,277 hrs · 48,748 cycles

RT WING REAR SPAR WEB FASTENER HOLE CRACKED AT RSS 222.5. REPAIRED WEB IAW EA.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 61,277 hrs · 48,748 cycles

AFT CARGO DOOR FWD END OF CROSSBEAM E, T CHORD CRACKED AT BS 787, BETWEEN 1.8" TO 3.5", FROM FWD EDGE ON INTERNAL STRUCTURE. REPAIRED CROSSBEAM IAW EA.

Part: SPLICE — CRACKED (LT WING) · airframe 61,277 hrs · 48,748 cycles

LEFT WING REAR SPAR UPPER CHORD SPLICE, CRACKED AT RSS 222.5. REPAIRED SPLICE IAW EA.

Part: SPLICE — CRACKED (LT WING) · airframe 61,277 hrs · 48,748 cycles

LEFT WING REAR SPAR, UPPER CHORD SPLICE, CRACKED AT RSS 225.5. REPAIRED SPLICE IAW EA.

Part: SPLICE — CRACKED (RT WING) · airframe 61,277 hrs · 48,748 cycles

RT WING REAR SPAR UPPER CHORD SPLICE CRACKED AT RSS 222.5. REPAIRED CHORD IAW EA.

Part: CROSSBEAM — CRACKED (CARGO DOOR) · airframe 61,277 hrs · 48,748 cycles

AFT CARGO COMPARTMENT DOOR AFT END OF CROSSBEAM E, T CHORD CRACKED AT BS 787, 1.8" FROM AFT EDGE. REPAIRED CROSSBEAM IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,277 hrs · 48,748 cycles

FORWARD GALLEY AREA, STUB FRAME WEB CRACKED AT BS 296.4, STRINGER 7R. REPAIRED STUB FRAME IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,277 hrs · 48,748 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 440, STRINGER 26L. R & R ANGLE IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 61,277 hrs · 48,748 cycles

TIE CLIP CRACKED AT BS 277, STRINGER 15R. R & R TIE CLIP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,277 hrs · 48,748 cycles

FORWARD GALLEY ANGLE CRACKED, BETWEEN BS 291.5 - 277, BETWEEN STRINGER 10R - 11R. R & R ANGLE IAW EA.

Part: RIB — CRACKED (LT WING) · airframe 61,277 hrs · 48,748 cycles

LEFT WING LOWER RIB CHORD CRACKED ON WBL 135.50, BETWEEN STATION 2 & 3. REPAIRED CHORD IAW EA.

Part: HOOK — CORRODED (CABIN) · airframe 61,277 hrs · 48,748 cycles

RIGHT EMER EXIT HATCH ESCAPE STRAP HOOK CORRODED. R & R HOOK IAW AMM.

Part: HOOK — CORRODED (CABIN) · airframe 61,277 hrs · 48,748 cycles

LEFT EMER EXIT HATCH ESCAPE STRAP HOOK CORRODED. R & R HOOK IAW AMM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 61,277 hrs · 48,748 cycles

RIGHT WING SUPPORT ANGLE CRACKED, BETWEEN BS 706 - 727, RBL 70.85. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,277 hrs · 48,748 cycles

FORWARD CARGO COMPARTMENT, FRAME CRACKED AT BS 500B, BETWEEN STRINGER 21L - 22L. REPAIRED FRAME IAW EA.

Part: GLOWSTRIP — CORRODED (CABIN) · airframe 61,277 hrs · 48,748 cycles

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

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 61,277 hrs · 48,748 cycles

PRESSURE DECK WEB CRACKED AT BS 665, RBL 39 AT CTR WING BOX. REPAIRED WEB IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 61,277 hrs · 48,748 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 672, LBL 39.5 AT CTR WING BOX. REPAIRED WEB IAW EA.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 61,277 hrs · 48,748 cycles

FORWARD GALLEY AREA EMER FLASHLIGHT BASE BROKEN. R & R FLASHLIGHT BASE IAW CMM.

Part: LIGHT — LOOSE (CABIN) · airframe 60,749 hrs · 48,388 cycles

MID CABIN OVERHEAD EMER EXIT LIGHT ASSEMBLY LOOSE. SECURED LIGHT ASSEMBLY IAW AMM.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 60,655 hrs · 48,320 cycles

DIVERSION, INFLIGHT SHUTDOWN & DECLARED EMER. NR 1 ENG OIL PRESS 10 PSI INFLIGHT. R & R NR 1 ENG OIL PRESS INDICATOR IAW AMM.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 60,537 hrs · 48,235 cycles

DIVERSION, AFT LAVATORY SMOKE ALARM GOING OFF IN FLIGHT. PERFORMED SATISFACTORY CONDITIONAL INSPECTION FOR FUMES IN CABIN IAW MM. AFT LAVATORY SMOKE DETECTOR CHECKED GOOD IAW MM.

Part: FUSE — INOPERATIVE (CABIN) · airframe 59,344 hrs · 47,387 cycles

RIGHT OVERWING HATCH AFT BULLNOSE EMER LIGHT INOPERATIVE. R & R FUSE IAW CMM.

Part: COVER — BROKEN (EXIT SIGN) · airframe 59,198 hrs · 47,292 cycles

L1 DOOR EMER EXIT DOOR SIGN COVER BROKEN. R & R COVER IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 59,126 hrs · 47,247 cycles

FORWARD OTBD EMER FLASHLIGHT INOPERATIVE. R & R BATTERY IAW MM.

Part: ANGLE — CRACKED (LT WING) · airframe 59,070 hrs · 47,207 cycles

LEFT WING NR 4 CANOE FAIRING INBD ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: DOOR — CRACKED (RT WING) · airframe 59,070 hrs · 47,207 cycles

RIGHT WING FIXED LE FSS 196 IN CORNER OF DOOR 6405R CRACKED. REPAIRED DOOR IAW EA.

Part: BRACKET — CRACKED (RT AILERON) · airframe 59,070 hrs · 47,207 cycles

RIGHT WING AILERON COVE BRACKET CRACKED AT LOWER CORNER. R & R BRACKET IAW SRM.

Part: ARM — CORRODED (TE FLAP) · airframe 59,070 hrs · 47,207 cycles

LEFT WING INBD FORE FLAP INBD CONNECTING ARMS CORRODED. R & R FORE FLAP IAW MM.

Part: SKIN — DELAMINATED (LT WING) · airframe 59,070 hrs · 47,207 cycles

LEFT WING NR 4 CANOE FAIRING SKIN DELAMINATED ON FWD LE SIDE. REPAIRED SKIN IAW SRM.

Part: DOOR — CRACKED (LT MLG) · airframe 59,070 hrs · 47,207 cycles

LEFT MLG MIDDLE DOOR & AFT ATTACH FITTING CRACKED. R & R DOOR IAW MM.

Part: LUG — BROKEN (LT SPOILER) · airframe 58,880 hrs · 47,082 cycles

LEFT WING INBD NR 4 GND SPOILER ATTACH LUG BROKEN. R & R NR 4 GND SPOILER IAW AMM.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 58,655 hrs · 46,932 cycles

DIVERSION, DURING CRUISE FL370 SMELLED STRONG BURNING SMELL IN COCKPIT & CABIN. NO SMOKE NOTED. R & R GASPER FAN IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,222 hrs · 46,644 cycles

LEFT BULLNOSE EMER LIGHT INOPERATIVE AT ROW 18. R & R BATTERY PACK IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 57,887 hrs · 46,429 cycles

FORWARD ENTRY EMER LIGHT LENS LOOSE. SECURED LENS IAW AMM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 57,427 hrs · 46,089 cycles

RIGHT UPPER KEEL BEAM WEB PANEL CRACKED AT BS 724. REPAIRED BEAM IAW SRM.

Part: RECTIFIER — MALFUNCTIONED (E&E BAY) · airframe 57,365 hrs · 46,043 cycles

AIR TURN BACK FLIGHT ATTENDANTS CALLED COMPLAINING OF AN ELEC ODOR. R & R NR 1 TRANSFORMER RECTIFIER IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 57,120 hrs · 45,867 cycles

RIGHT OVERWING EMER EXIT LIGHT COVER BROKEN. R & R LENS ASSEMBLY IAW SIP.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 57,050 hrs · 45,811 cycles

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

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 56,038 hrs · 45,110 cycles

DECLARED EMERGENCY. CABIN PRESS CONTROL WARN HORN SOUNDED & LOSS OF PRESS. R & R NR 1 CABIN PRESS CONTROLLER & OUTFLOW VLV IAW MM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 55,527 hrs · 44,750 cycles

CHORD CRACKED AT BS 727 STRINGER 18A RT. REPAIRED CHORD IAW SWA EA.

Part: LIGHT — BROKEN (CABIN) · airframe 55,527 hrs · 44,750 cycles

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

Part: RIB — CRACKED (RT WING) · airframe 55,527 hrs · 44,750 cycles

RT WING INSIDE THE TANK, RIB 135.5 LOWER CHORD, BETWEEN STRINGER S2 & S3, AFT LOWER CHORD RADIUS CRACKED. REPAIRED CHORD IAW SWA EA.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 55,527 hrs · 44,750 cycles

AFT CARGO DOOR SKIN CRACKED AT UPPER AFT FASTENER HOLE OF DOOR HANDLE CUTOUT. REPAIRED SKIN IAW SWA EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 55,527 hrs · 44,750 cycles

VERTICAL BEAM WEB CRACKED AT BS 178 LBL 5.7. REPAIRED WEB IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 55,527 hrs · 44,750 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 55,527 hrs · 44,750 cycles

AFT LAVATORY FWD WALL EMERGENCY EXIT LIGHT BROKEN. R & R LIGHT IAW SWPM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,527 hrs · 44,750 cycles

SHEAR TIE CORRODED AT BS 787 BETWEEN STRINGER 26R TO STRINGER 27R. REPAIRED SHEAR TIE IAW EA.

Part: WIRE — EXPOSED (CABIN) · airframe 55,527 hrs · 44,750 cycles

EMERGENCY LIGHTING WIRE EXPOSED AT BS 727D STRINGER 17R. REPAIRED WIRE IAW SWPM MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 55,527 hrs · 44,750 cycles

RT WING OTBD AFT FLAP DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 55,527 hrs · 44,750 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 55,527 hrs · 44,750 cycles

CREASE BEAM WEB CORRODED AT BS 727E STRINGER 17R. R & R WEB IAW SRM & DRAWING.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 55,527 hrs · 44,750 cycles

LT WING NR 4 FLAP TRACK FAIRING 3501L LE COMPOSITE SKIN DELAMINATED. REPAIRED FAIRING IAW SRM & DRAWING.

Part: PANEL — CRACKED (NR 2 NACELLE) · airframe 55,527 hrs · 44,750 cycles

NR 2 ENG STRUT PANEL 5864R CRACKED AT FASTENER HOLE. R & R PANEL IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 55,527 hrs · 44,750 cycles

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

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,527 hrs · 44,750 cycles

LONGITUDINAL FLOOR BEAM CRACKED AT BS 727B LBL 45.5. REPAIRED BEAM IAW SWA EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,527 hrs · 44,750 cycles

INTERCOSTAL CORNER ANGLE CRACKED AT BS 947.5 BETWEEN STRINGER 24R TO STRINGER 25R. R & R ANGLE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,527 hrs · 44,750 cycles

SHEAR TIE CORRODED AT BS 807 BETWEEN STRINGER 26L TO STRINGER 27R. REPAIRED SHEAR TIE IAW EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,527 hrs · 44,750 cycles

FRAME SHEAR TIE CORRODED AT BS 787 BETWEEN STRINGER 27L TO STRINGER 27R. REPAIRED SHEAR TIE IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,527 hrs · 44,750 cycles

LONGITUDINAL FLOOR BEAM CRACKED AT BS 727B LBL 24.8. REPAIRED BEAM IAW SWA EA.

Part: FITTING — CORRODED (FUSELAGE) · airframe 55,527 hrs · 44,750 cycles

FLOOR FITTING CORRODED AT BS 303 LBL 11. R & R FITTING IAW SRM & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,527 hrs · 44,750 cycles

FRAME CRACKED AT BS 947.5, BETWEEN STRINGER 24R TO STRINGER 25R. REPAIRED FRAME IAW SRM.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 55,527 hrs · 44,750 cycles

SHEAR WEB CRACKED BETWEEN BS 348 TO BS 351 BETWEEN STRINGER 15L TO STRINGER 17L. R & R SHEAR WEB IAW SRM & DRAWING.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,527 hrs · 44,750 cycles

CTR WING BOX LONGITUDINAL FLOOR BEAM, UPPER CHORD CRACKED AT BS 727B LBL 45.5. REPAIRED CHORD IAW SWA EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 55,527 hrs · 44,750 cycles

R1 DOOR LOWER THRESHOLD CREASE BEAM INNER SUPPORT ANGLE CORRODED AROUND FASTENER HOLE. REPAIRED ANGLE IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 55,527 hrs · 44,750 cycles

RT WING OTBD TE FLAP LOWER SKIN DELAMINATED. REPAIRED SKIN IAW SRM.

Part: SKIN — CHAFED (TE FLAP) · airframe 55,527 hrs · 44,750 cycles

RT WING OTBD FORE FLAP OTBD LOWER SKIN CHAFFED. REPAIRED FORE FLAP IAW SRM.

Part: ANGLE — CRACKED (RT AILERON) · airframe 55,527 hrs · 44,750 cycles

RT WING TE AILERON BAY 30 INCHES OTBD OF INBD EDGE ANGLE CRACKED. R & R ANGLE IAW AAR EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,527 hrs · 44,750 cycles

CTR WING BOX LONGITUDINAL FLOOR BEAM, UPPER CHORD CRACKED AT BS 727B LBL 24.8. REPAIRED CHORD IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,527 hrs · 44,750 cycles

FRAME OTBD CHORD CRACKED AT BS 727 STRINGER 18A RT. REPAIRED CHORD IAW EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 55,370 hrs · 44,650 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 54,807 hrs · 44,234 cycles

RT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. R & R BALLAST IAW MM.

Part: LENS — WORN (EXIT SIGN) · airframe 54,273 hrs · 43,834 cycles

R1 DOOR EMERGENCY EXIT SIGN COVER WORN. R&R LENS IAW AMM.

Part: SIGN — DETACHED (CABIN) · airframe 54,198 hrs · 43,775 cycles

LT OVERWING "EMERGENCY EXIT" SIGN DETACHED. REPAIRED SIGN IAW EA.

Part: BRACKET — CRACKED (R2 DOOR) · airframe 53,887 hrs · 43,532 cycles

R2 DOOR EMERGENCY EVAC SLIDE BRACKET CRACKED. R & R BRACKET IAW AMM.

Part: STRAP — BROKEN (NR 1 PYLON) · airframe 53,887 hrs · 43,532 cycles

TEFLON NUTPLATE ATTACH STRIP BROKEN ON AFT EDGE OF WHERE NR 1 PYLON PANEL 57710L ATTACHES. REPAIRED STRAP IAW EA.

Part: DOOR — DELAMINATED (LT MLG) · airframe 53,719 hrs · 43,406 cycles

LEFT MAIN GEAR INNER DOOR AFT EDGE DELAMINATED. R & R DOOR IAW MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 53,586 hrs · 43,309 cycles

FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 53,212 hrs · 43,061 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: DOOR — DELAMINATED (LT MLG) · airframe 52,721 hrs · 42,725 cycles

LT MAIN LANDING DOOR DELAMINATED EDGE HITTING WING FAIRING WHEN GEAR RETRACTED. R & R DOOR IAW MM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 52,256 hrs · 42,390 cycles

R-1 WINDOW ARCED AND CRACKED. REMOVED AND REPLACED R1 WINDOW PER M/M.

Part: TUBE — CRACKED (LE SLAT) · airframe 52,190 hrs · 42,346 cycles

NR 4 SLAT SPRAY TUBE CRACKED. REMOVED AND REPLACED NR 4 SLAT OUTBOARD SPRAY TUBE PER AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 51,932 hrs · 42,166 cycles

FORWARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER M/M.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 51,416 hrs · 41,786 cycles

FORWARD INBD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER AMM.

Part: LENS — LOOSE (CABIN) · airframe 51,330 hrs · 41,719 cycles

FORWARD OVERHEAD EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS PER MM.

Part: MODULE — INOPERATIVE (COCKPIT) · airframe 50,515 hrs · 41,077 cycles

MULTIPLE LIGHTS ON (30-40) ON OVERHEAD PANEL ON DESCENT, NO LANDING GEAR INDICATION AT ALL WHEN LANDING GEAR LOWERED. REMOVED AND REPLACED FLT DECK DOOR MODULE IAW M/M.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 50,034 hrs · 40,724 cycles

FWD F/A FLASHLIGHT INDICATOR LIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 49,860 hrs · 40,601 cycles

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

Part: SPOILER — DELAMINATED (LT WING) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 4 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 947.5, STR 19L. REPAIRED FRAME PER SRM AND DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 747, BETWEEN STR 27R TO STR 26R. REPAIRED FRAME IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 5. REPAIRED BEAM IAW ER AND SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 28L TO STR 17L. REPAIRED SHEAR TIE PER SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL BEAM UPPER CHORD CRACKED AT BS 727A+17, RBL 45.5. REPAIRED CHORD PER ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED BETWEEN BS 328 TO BS 360, BETWEEN STR 14L TO STR 18L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 961, STR 17L. REPAIRED SKIN PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE IAW ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CRACKED AT BS 947, LBL 53. REPAIRED FLOORBEAM IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

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

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME IAW SRM EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 188, STR 17L. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 28R TO STR 28L. REPAIRED SHEAR TIE IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 947, LBL 20. REPAIRED CHORD PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 27L TO STR 26L. REPAIRED SHEAR TIE IAW EA.

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

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR WEB CORRODED AT BS 954, RBL 52. REPAIRED WEB IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 993, RBL 47. REPAIRED SHEAR TIE IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR WEB CRACKED BETWEEN BS 178 TO BS 188, WL 207. REPAIRED WEB PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 727E, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND BULKHEAD VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17. REPAIRED WEB IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 27L TO STR 28L. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 27R TO STR 28R. REPAIRED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 27L TO STR 26L. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8R. REMOVED AND REPLACED CLIP IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOOR WEB CRACKED BETWEEN BS 188 TO BS 198, STR 17L. REMOVED AND REPLACED WEB IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, BETWEEN STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, RBL 18. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 11R. REMOVED AND REPLACED CLIP IAW SRM.

Part: ATTACH FITTING — CORRODED (GIRT BAR) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTING CORRODED AT BS 344. REMOVED AND REPLACED FITTING IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 312, BL 0. REPAIRED BEAM IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK FOUND, SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE IAW SRM.

Part: ATTACH FITTING — CORRODED (GIRT BAR) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK FOUND, L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTING CORRODED AT BS 312. REMOVED AND REPLACED FITTING IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK FOUND, FLOORBEAM CRACKED AT BS 328, BL 0. REPAIRED BEAM IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED BS 747, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND INTERIOR STRINGER TIE CLIP CRACKED STA 578, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND INTERIOR STRINGER TIE CLIP CRACKED STA 559, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,651 hrs · 40,453 cycles

DURING SCHEDULED 16Y CHECK, FOUND CORROSION ON FRAME TEAR-STRAP AFT CARGO, BS 727E, STR 27L AND 27R. REMOVED AND REPLACED CORRODED PART PER SRM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 48,969 hrs · 39,937 cycles

AIRCRAFT VIBRATION FROM CLIMBOUT THROUGH CRUISE SLOWED TO BELOW .68 MACH TO REDUCE VIBRATION TO ACCEPTABLE LEVEL. FOUND NR 5 GROUND SPOILER DELAMINATED. REMOVED AND REPLACED NR 5 GROUND SPOILER PER MM.

Part: LENS — LOOSE (CABIN) · airframe 48,780 hrs · 39,805 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

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

DURING SCHEDULED SPV CHECK, FOUND BUTT STRAP CORRODED AT BS 908, STR 27R. REMOVED AND REPLACED BUTT STRAP PER SRM AND DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,756 hrs · 39,789 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 360 TO BS 540. REMOVED AND REPLACED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,756 hrs · 39,789 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE WINDOW SKIN CRACKED AT BS 500B+10 UPPER CORNER. REMOVED AND REPLACED SKIN IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT EEPLS LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — CRACKED (CABIN) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS IAW MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 48,756 hrs · 39,789 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 48,753 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 500A, RBL 66. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,753 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP BETWEEN ROW 10 TO ROW 17. REMOVED AND REPLACED BATTERY PACK IAW MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 787, STR 1. REPAIRED STRINGER IAW EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14L TO STR 15L. REPAIRED SHEAR TIE IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 4L. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 4L. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK FOUND, STRINGER CLIP CRACKED AT BS 847, STR 4L. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK FOUND, STRINGER CLIP CRACKED AT BS 847, STR 4R. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4R. REMOVED AND REPLACED CLIP IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK, FOUND LT LOWER AFT FUSELAGE WINDOW FRAME CRACKED AT BS 380+10. REPAIRED FRAME IAW SB AND TC.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 727, BETWEEN STR 3R TO STR 4R. REPAIRED SKIN PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED OTS CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE WINDOW FWD LT UPPER SKIN CRACKED AT BS 520+10, STR 17L. REPAIRED SKIN PER EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK, FOUND LT LOWER AFT WINDOW FRAME CRACKED AT BS 480+10. REPAIRED FRAME IAW TC.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

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

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

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

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK FOUND, SHEAR TIE CORRODED AT BS 908, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CARGO COMPARTMENT DOOR CRACKED AT LOWER CORNER. REMOVED AND REPLACED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 8R. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 9R. REMOVED AND REPLACED CLIP IAW SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND SKIN CRACKED AT BS 500B, STR 2L. REPAIRED SKIN PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK, FOUND FRAME CORRODED AT BS 809, LBL 5. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 380+1, STR 5L. REMOVED AND REPLACED STRINGER PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 48,754 hrs · 39,788 cycles

DURING SCHEDULED SPV CHECK, FOUND STA 380, S10L GOUGED. REPAIRED STR PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,748 hrs · 39,786 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 597 TO BS 613, STR 4R. REPAIRED SKIN PER SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,748 hrs · 39,786 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 578 TO BS 597, STR 4R. REPAIRED SKIN PER SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,748 hrs · 39,786 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 613 TO BS 639, STR 4R. REPAIRED SKIN PER SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,748 hrs · 39,786 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 578 TO BS 597, STR 4L. REPAIRED SKIN PER SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,748 hrs · 39,786 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 559 TO BS 578, STR 4L. REPAIRED SKIN PER SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,748 hrs · 39,786 cycles

DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED BETWEEN BS 639 TO BS 663, STR 4R. REPAIRED SKIN PER SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,748 hrs · 39,786 cycles

DIVERSION/DECLARED EMERGENCY. AT FL 360 LOST CABIN PRESSURE. UPON LANDING FOUND A HOLE APPROX 6-8 FOOT LONG 1-2 FOOT WIDE IN MID CABIN CEILING. REPAIRED SKIN PER SRM AND EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 48,722 hrs · 39,768 cycles

DURING SCHEDULED OTS CHECK, FOUND LT WING NR 2 SLAT CRACKED AT I/B AUX TRACK LOWER SURFACE. REPAIRED NR 2 SLAT PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 48,740 hrs · 39,781 cycles

DURING SCHEDULED OTS CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 48,722 hrs · 39,768 cycles

DURING SCHEDULED OTS CHECK, FOUND EEPLS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 48,722 hrs · 39,768 cycles

DURING SCHEDULED OTS CHECK, FOUND LT WING NR 1 SLAT I/B LOWER SURFACE CRACKED. REPAIRED NR 1 SLAT PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 48,722 hrs · 39,768 cycles

DURING SCHEDULED OTS CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 47,652 hrs · 38,970 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 46,852 hrs · 38,335 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: KEELBEAM — DAMAGED (FUSELAGE) · airframe 45,944 hrs · 37,641 cycles

DURING SCHEDULED 14Y CHECK FOUND, LT KEEL BEAM DAMAGED AT BS 724. REPAIRED BEAM PER EA.

Part: LIGHT — DAMAGED (CABIN) · airframe 45,944 hrs · 37,641 cycles

DURING SCHEDULED 14Y CHECK, FOUND EEPLS DAMAGED. REMOVED AND REPLACED EEPLS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,944 hrs · 37,641 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,944 hrs · 37,641 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,944 hrs · 37,641 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,944 hrs · 37,641 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,944 hrs · 37,641 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 6R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,944 hrs · 37,641 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 6L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,944 hrs · 37,641 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,944 hrs · 37,641 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,944 hrs · 37,641 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 3L. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,944 hrs · 37,641 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM AND SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,944 hrs · 37,641 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,944 hrs · 37,641 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER EA.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 45,944 hrs · 37,641 cycles

DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE BEAR STRAP SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM AND EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 45,944 hrs · 37,641 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM ANGLE CRACKED AT BS 639, RBL 45. REMOVED AND REPLACED ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,944 hrs · 37,641 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER EA.

Part: COVER — LOOSE (CABIN) · airframe 45,944 hrs · 37,641 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT CEILING MOUNTED OVERHEAD EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,944 hrs · 37,641 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,944 hrs · 37,641 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,944 hrs · 37,641 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,944 hrs · 37,641 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,944 hrs · 37,641 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,944 hrs · 37,641 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REPAIRED CLIP PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,944 hrs · 37,641 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,944 hrs · 37,641 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 7L. REPAIRED CLIP PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,944 hrs · 37,641 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 44,161 hrs · 36,326 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 44,161 hrs · 36,326 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 44,069 hrs · 36,282 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS COVER LOOSE. REPAIRED LENS PER SWA EA.

Part: PRECOOLER — CRACKED (BLEED AIR SYS) · airframe 43,521 hrs · 35,892 cycles

AT FLT 360 GOT ALTITUDE WARNING HORN. NO CAUTION LIGHT NOR PRESSURIZATION PANEL LIGHTS CABIN WAS AT 10,000FT. FOUND NR 2 ENGINE PRE-COOLER CRACKED. REMOVED AND REPLACED NR 2 ENGINE PRE-COOLER PER MM.

Part: LENS — CRACKED (CABIN) · airframe 41,900 hrs · 34,750 cycles

FOUND FWD DOOR EMERGENCY EXIT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 40,882 hrs · 34,011 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 40,882 hrs · 34,011 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,901 hrs · 33,313 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, STR 26R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,901 hrs · 33,313 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 39,901 hrs · 33,313 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: COVER — MISSING (CABIN) · airframe 38,939 hrs · 32,622 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMERGENCY EXIT SIGN COVER MISSING. INSTALLED COVER PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 38,438 hrs · 32,228 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 38,281 hrs · 32,104 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,761 hrs · 31,678 cycles

DURING MV2 CHECK, FOUND FWD EEPLS INOP. RELAMPED PER MM.

Part: ACTUATOR — BYPASSING (L/E SLAT) · airframe 36,917 hrs · 31,013 cycles

DECLARED EMERGENCY. ON APPROACH L/E SLATS/FLAPS WOULD NOT EXTEND FOR LANDING. EXTENDED FLAPS PER ALTERNATE METHOD. INSPECTED AND FOUND LEFT INBOARD KRUEGER FLAP ACTUATOR BYPASSING. REMOVED AND REPLACED LEFT INBOARD ACTUATOR PER MM.

Part: LIGHT — DISLODGED (CABIN) · airframe 35,196 hrs · 29,674 cycles

R1 DOOR EMERGENCY EXIT LIGHT COVER FELL OFF. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 35,186 hrs · 29,666 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 34,344 hrs · 28,987 cycles

DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 312 TO BS 340, LBL 55. REMOVED AND REPLACED WEB SECTION PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING T/E AFT FLAP DELAMINATED. REPAIRED LT WING FLAP PER SRM, SB AND CMM.

Part: FLAP — DELAMINATED (RT WING) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING T/E AFT FLAP DELAMINATED. REPAIRED RT WING FLAP PER SRM, SB AND CMM.

Part: FRAME — CRACKED (BS 787) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, S8R. REPAIRED FRAME SECTION PER SRM.

Part: STRUCTURE — CRACKED (LT WING TE FLAP) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING T/E AFT FLAP INBOARD END CAP CRACKED. REPAIRED LT TRAILING EDGE AFT FLAP INBOARD END CAP PER BOEING SB AND SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT UPPER INBOARD FASTENER. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: FRAME — CRACKED (BS 827 S8R) · airframe 33,513 hrs · 28,325 cycles

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

Part: WEB — CORRODED (BS 303-312) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOOR WEB CORRODED AT BS 303 TO BS 312, LBL 55. REMOVED AND REPLACED FLOOR WEB PER SRM.

Part: CREASE BEAM — CORRODED (BS 346) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 346, RBL 64. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: FRAME — CRACKED (BS 907 S8L) · airframe 33,513 hrs · 28,325 cycles

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

Part: RIB — CORRODED (RT WING) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD MID FLAP OUTBOARD RIB CORRODED. REMOVED AND REPLACED MID FLAP OUTBOARD RIB PER SRM AND BOEING DRAWING.

Part: CREASE BEAM — CORRODED (BS 500-500A) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 500 TO BS 500A, WL 208. REPAIRED WEB PER MM.

Part: FRAME — CRACKED (BS 348) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 348, L1 DOOR CUTOUT, LOWER AFT INBOARD FLANGE. REPAIRED FRAME PER SRM.

Part: RIB — CORRODED (RT WING) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD T/E MIDFLAP INBOARD END RIB CORRODED. REMOVED AND REPLACED RIB PER SRM.

Part: BRACKET — LOOSE (R1 DOOR SLIDE) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE COVER LOWER AFT ATTACH BRACKET LOOSE. SECURED BRACKET PER SRM.

Part: FAILSAFE — CORRODED (RT WING) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT WING INBOARD T/E MIDFLAP INBOARD FAIL-SAFE TUBE CORRODED. REMOVED AND REPLACED TUBE PER CMM.

Part: DOOR FRAME — CORRODED (BS 992) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND R2 DOOR CUTOUT, LOWER AFT FRAME CORRODED AT BS 992, RBL 55, WL 210. REPAIRED FRAME PER SRM.

Part: RIB — CORRODED (LT WING) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD T/E MIDFLAP INBOARD END RIB CORRODED. REMOVED AND REPLACED RIB PER SRM.

Part: FRAME — CRACKED (BS 400 S8-9L) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, BETWEEN STR 8L & STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 188 S17R) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 188, STR 17R. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: WEB — CRACKED (BS 188-196) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND COCKPIT FLOOR WEB CRACKED BETWEEN BS 188 TO BS 196, STR 17R. REPAIRED FLOOR WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, RBL 10. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 500A) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, BETWEEN STR 8L & STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 400) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, BETWEEN STR 8R & STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 440) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, BETWEEN STR 8L & STR 9L. REPAIRED FRAME PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,513 hrs · 28,325 cycles

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

Part: FLOOR SUPPORT — CORRODED (BS 270) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND COCKPIT FLOOR SUPPORT CORRODED AT BS 270, BETWEEN LBL 10 TO RBL 10, WL 208. REMOVED AND REPLACED Z-CHORD PER SRM.

Part: FRAME — CRACKED (BS 360) · airframe 33,513 hrs · 28,325 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, BETWEEN STR 8R & STR 9R. REPAIRED FRAME PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 33,193 hrs · 28,071 cycles

DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LIGHT — DELAMINATED (CABIN) · airframe 31,762 hrs · 26,932 cycles

DURING SCHEDULED A1 CHECK, FOUND RT CABIN EEPLS STRIP DELAMINATED. REMOVED AND REPLACED STRIP PER MM.

Part: LENS — MISSING (L1 DOOR) · airframe 31,204 hrs · 26,493 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY EXIT) · airframe 30,391 hrs · 25,840 cycles

DURING SCHEDULED C2 CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 30,032 hrs · 25,540 cycles

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

Part: ROD END — WORN (ELEVATOR TAB) · airframe 28,406 hrs · 24,303 cycles

DURING SCHEDULED C4 CHECK, LT AND RT ELEVATOR TABS FAILED FREEPLAY CHECK. REMOVED AND REPLACED BOTH NR 1 ELEVATOR TABS ROD END HARDWARE PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 28,406 hrs · 24,303 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,460 hrs · 22,696 cycles

DURING SCHEDULED SPECIAL VISIT AT SAT AERSPACE, FOUND EMERGENCY LIGHTS BATTERY PACKS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 26,424 hrs · 22,667 cycles

FORWARD INBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: FITTING — CORRODED (RT MLG) · airframe 25,771 hrs · 22,165 cycles

DURING SC RT MLG WALKING BEAM OUTBOARD FWD HANGER FITTING ON REAR SPAR CORRODED IN THE BORE. REPAIRED FITTING PER SRM.

Part: FITTING — CORRODED (LT MLG) · airframe 25,771 hrs · 22,165 cycles

WALKING BEAM OUTBOARD FWD HANGER FITTING ON REAR SPAR HAS CORROSION IN THE BORE. REPAIRED FITTING PER EA.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 25,661 hrs · 22,080 cycles

DURING SCHEDULED C1 CHECK, FOUND RT WING O/B FLAP I/B END DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 25,415 hrs · 21,879 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT LOWER STOP FITTING. REMOVED AND REPLACED DOOR PER MM.

Part: INDICATOR — OUT OF POSITION (SERVICE DOOR) · airframe 24,892 hrs · 21,439 cycles

FWD SERVICE DOOR EMERGENCY EVAC SLIDE PRESS INDICATOR OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 24,642 hrs · 21,231 cycles

DURING SCHEDULED C4 CHECK, FOUND CENTER KEEL BEAM CRACKED (3 EA) AT LOWER SKIN PANEL BETWEEN W/W'S. REPAIRED KEEL BEAM PER SRM.

Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE) · airframe 23,723 hrs · 20,492 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 21,879 hrs · 18,960 cycles

DURING SCHEDULED C1 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: ACTUATOR — CRACKED (NLG) · airframe 21,801 hrs · 18,903 cycles

NOSE GEAR HYDRAULIC LEAK, DUE TO CRACKED NLG DOWN LOCK HYD ACTUATOR. REMOVED AND REPLACED NOSE GEAR DOWN LOCK ACTUATOR.

Part: BUSHING — WORN (RH ELEVATOR) · airframe 20,624 hrs · 17,971 cycles

DURING SCHEDULED A1 CHECK, SWA SI 11111-55, FOUND RT ELEVATOR TAB LOCKOUT FWD MOUNT BUSHINGS WORN. REMOVED AND REPLACED TAB LOCKOUT MOUNT BUSHINGS.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 19,170 hrs · 16,801 cycles

DURING SCHEDULED BC2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: BULKHEAD — PUNCTURED (NLG W/W) · airframe 18,818 hrs · 16,515 cycles

DURING SCHEDULED RON, FOUND A .9 BY 1.6 HOLE PUNCTURED AT NLG W/W AFT BULKHEAD. MX FERRY TO DAL AND REPAIRED BULKHEAD PER SWA RA.

Part: BEARING — OUT OF POSITION (NLG TRUNNION) · airframe 18,214 hrs · 16,017 cycles

DURING SCHEDULED C1 CHECK, FOUND LEFT MAIN NOSE GEAR TRUNNION BEARING SHIMS MIGRATED .625 INCH TO .75 INCH FROM MOUNT FLANGE. REMOVED AND REPLACED TRUNNION BEARING AND SHIMS PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 18,063 hrs · 15,893 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE PER MM.

Part: COVER — LOOSE (CABIN) · airframe 16,542 hrs · 14,590 cycles

EEPLS TRACK COVER LOOSE AT OVERWING EXIT. SECURED TRACK COVER PER MM.

Part: WIRE — EXPOSED (CABIN FLOOR) · airframe 15,877 hrs · 14,057 cycles

EEPLS WIRING EXPOSED AT ROWS 14 & 15. SECURED FLOOR TRACK COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,694 hrs · 13,899 cycles

EEPLS INOP AND LOOSE AT ROW 16 AND MID CABIN. R&R LIGHT ASSY AND SECURED LOOSE ONE PER MM.

Part: COVER — MISSING (CABIN) · airframe 15,457 hrs · 13,726 cycles

EEPLS TRACK COVER MISSING. REPLACED TRACK COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 15,469 hrs · 13,735 cycles

EEPLS TRACK COVER LOOSE AT ROW 15. SECURED TRACK COVER PER MM.

Part: COVER — LOOSE (CABIN FLOOR) · airframe 15,330 hrs · 13,617 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK COVER LOOSE AT ROW 14. SECURED COVER PER MM.

Part: INDICATOR — ERRATIC (COCKPIT) · airframe 13,982 hrs · 12,483 cycles

ABORTED TAKE-OFF. NR 2 ENGINE EGT INDICATOR LIGHT ILLUMINATED, MOVED THROTTLE TO IDLE POSITION AND EGT INDICAOR ERRATIC. INSPECTED NR 2 ENGINE INLET AND TAILPIPE SECTIONS. OPERATED ENGINE, NO DEFECT FOUND. COULD NOT DUPLICATE.

Part: LIGHT — BROKEN (CABIN)

DURING SCHEDULED C1 CHECK, FOUND EEPLS LIGHT LOOSE AND BROKEN AT MID CABIN. REMOVED AND REPLACED LIGHT ASSY AND SECURED TRACK PER MM.

Part: SKIN — CRACKED (GALLEY DOORWAY)

DURING SCHEDULED SERVICE CHECK, FOUND FWD GALLEY DOOR UPPER HINGE FRAME CUTOUT CASTING CRACKED. REMOVED AND REPLACED PER BOEING SRM.