N648SW

Part: FLAP — DELAMINATED (RT WING) · airframe 61,045 hrs · 47,802 cycles

RT WING OUTBOARD AFT FLAP DELAMINATED. R&R AFT FLAP PER AMM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 60,948 hrs · 47,746 cycles

RT WING NR 8 GROUND SPOILED DELAMINATED. R&R #8 SPOILER IAW AMM.

Part: BULB — INOPERATIVE (CABIN) · airframe 60,532 hrs · 47,482 cycles

LEFT AFT OVERWING EXIT LIGHT INOPERATIVE. REPLACED THE BULB IAW AMM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 60,451 hrs · 47,425 cycles

FORWARD EMERGENCY FLASHLIGHT SAFETY STRAP BROKEN. R & R SAFETY STRAP IAW MAINTENANCE.

Part: FLAP — DELAMINATED (RT WING) · airframe 60,440 hrs · 47,419 cycles

RT WING INBD AFT FLAP T/E DELAMINATED. R & R AFT FLAP IAW AMM.

Part: LIGHT — DIM (CABIN) · airframe 59,877 hrs · 47,053 cycles

RIGHT WING OVERWING EMER HATCH LIGHT DIM. R & R LAMP IAW AMM.

Part: SKIN — CRACKED (RT WING) · airframe 59,453 hrs · 46,764 cycles

RIGHT WING UPPER SKIN CRACKED AT FASTENER HOLE, AT RSS 253, AFT OF REAR SPAR. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (RT WING) · airframe 59,453 hrs · 46,764 cycles

RIGHT WING UPPER SKIN CRACKED AT FASTENER HOLE, AT RSS 249, AFT OF REAR SPAR. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (LT WING) · airframe 59,453 hrs · 46,764 cycles

LEFT WING UPPER SKIN CRACKED AT FASTENER HOLE, AT RSS 269, AFT OF REAR SPAR. REPAIRED SKIN IAW EA & ER.

Part: SKIN — CRACKED (RT WING) · airframe 59,453 hrs · 46,764 cycles

RIGHT WING UPPER SKIN CRACKED AT FASTENER HOLE, AT RSS 237.5, AFT OF REAR SPAR. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 59,453 hrs · 46,764 cycles

LEFT WING UPPER SKIN CRACKED AT FASTENER HOLE, AT RSS 251, AFT OF REAR SPAR. REPAIRED SKIN IAW EA & ER.

Part: SKIN — CRACKED (RT WING) · airframe 59,453 hrs · 46,764 cycles

RIGHT WING UPPER SKIN CRACKED AT FASTENER HOLE, AT RSS 264, AFT OF REAR SPAR. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (LT WING) · airframe 59,453 hrs · 46,764 cycles

LEFT WING UPPER SKIN CRACKED AT FASTENER HOLE AT RSS 255 AFT OF REAR SPAR. REQUIRED SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 59,453 hrs · 46,764 cycles

LEFT WING UPPER SKIN CRACKED, AT FASTENER HOLE AT RSS 239, AFT OF REAR SPAR. REPAIRED SKIN IAW EA & ER.

Part: SKIN — CRACKED (LT WING) · airframe 59,453 hrs · 46,764 cycles

LEFT WING UPPER SKIN CRACKED, AT FASTENER HOLE AT RSS 268, AFT OF REAR SPAR. REPAIRED SKIN IAW EA & ER.

Part: RIB — CRACKED (LT WING) · airframe 59,453 hrs · 46,764 cycles

LEFT WING RIB CRACKED AT WBL 135.50, AFT LOWER END. REPAIRED RIB IAW EA.

Part: ANGLE — CRACKED (LT WING) · airframe 59,453 hrs · 46,764 cycles

LEFT WING PRESS WEB LOWER ANGLE CRACKED AT RSS 277. R & R ANGLE IAW SRM.

Part: SHEAR TIE — BROKEN (RT WING) · airframe 59,453 hrs · 46,764 cycles

RIGHT WING REAR SHEAR TIE BROKEN AT RSS 201, WBL 135. R & R SHEAR TIE IAW DWG & SRM.

Part: FITTING — CORRODED (RT MLG) · airframe 59,453 hrs · 46,764 cycles

RIGHT WING MLG AFT FITTING CORRODED. R & R FITTING IAW SRM.

Part: SPAR — CRACKED (LT WING) · airframe 59,453 hrs · 46,764 cycles

LEFT WING REAR SPAR WEB CRACKED AT RSS 223. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 59,453 hrs · 46,764 cycles

RIGHT WING REAR SPAR WEB CRACKED AT RSS 223. REPAIRED WEB IAW ER & EA.

Part: SPAR — CRACKED (LT WING) · airframe 59,453 hrs · 46,764 cycles

LEFT WING UPPER REAR SPAR CHORD CRACKED AT RSS 223. REPAIRED CHORD IAW EA & ER.

Part: SPAR — CRACKED (RT WING) · airframe 59,453 hrs · 46,764 cycles

RIGHT WING UPPER REAR SPAR CHORD CRACKED AT RSS 223. REPAIRED CHORD IAW ER & EA.

Part: CABLE — MISROUTED (R2 DOOR) · airframe 57,870 hrs · 45,662 cycles

R2 DOOR EMER EVAC SLIDE CABLE MISROUTED. REROUTED CABLE IAW AMM.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 57,870 hrs · 45,662 cycles

R1 DOOR AFT FRAME TORQUE BOX CUT OUT AREA AFT LOWER CORNER FRAME CRACKED. R & R R1 DOOR IAW AMM.

Part: SPOILER — DELAMINATED (RT WING) · airframe 57,502 hrs · 45,374 cycles

RIGHT WING NR 7 SPOILER DELAMINATED. R & R SPOILER ASSEMBLY IAW MM.

Part: SLAT — CRACKED (RT WING) · airframe 57,451 hrs · 45,334 cycles

RIGHT WING NR 4 SLAT CRACKED ON BRACKET LOCATED ON SEAL DOOR ACTUATOR. REPLACED NR 4 SLAT IAW SRM & DWG.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 57,451 hrs · 45,334 cycles

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

Part: STRINGER CLIP — CRACKED (BS 360) · airframe 57,450 hrs · 45,333 cycles

THE STRINGER CLIP WAS FOUND CRACKED AT BS 360, STRINGER 2L. R&R THE STRINGER CLIP IAW THE SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 57,450 hrs · 45,333 cycles

TIE CLIP CRACKED AT STATION 360, STRINGER 2R. R & R CLIP IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,450 hrs · 45,333 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 57,450 hrs · 45,333 cycles

FUSELAGE WEB CRACKED AT STATION 727 BETWEEN RBL 38 & RBL 45. R & R WEB IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,450 hrs · 45,333 cycles

SPLICE STRAP CRACKED AT BS 360, STRINGER 3R. REPAIRED STRAP IAW EA.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 57,450 hrs · 45,333 cycles

STRINGER SPLICE CRACKED AT BS 908, STRINGER 4L. REPAIRED SPLICE IAW EA.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 57,450 hrs · 45,333 cycles

FORWARD CABIN PHOTO LUMINESCENT STRIP DAMAGED. R & R STRIP IAW AMM.

Part: INTERCOSTAL — CRACKED (BS 277-292) · airframe 57,450 hrs · 45,333 cycles

FOUND AN INTERCOSTAL CRACKED AT BS 277 - 292, STRINGER 11R. REPAIRED THE INTERCOSTAL IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 57,450 hrs · 45,333 cycles

LEFT WING INBD FIXED LE SKIN CRACKED AT STATION 208. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,450 hrs · 45,333 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,450 hrs · 45,333 cycles

FRAME OTBD CHORD CRACKED AT BS 727, STRINGER 18A, LT SIDE. REPAIRED CHORD IAW EA.

Part: RELEASE CABLE — DISCONNECTED (EVAC SLIDE) · airframe 56,956 hrs · 44,988 cycles

L2 DOOR EMER EVAC SLIDE RELEASE CABLE DISCONNECTED. RECONNECTED SLIDE IAW MT.

Part: LIGHT — BROKEN (CABIN) · airframe 56,356 hrs · 44,567 cycles

BULLNOSE EXIT LIGHT BROKEN AT ROW 2 ABC. R & R LIGHT IAW MM.

Part: LIGHT — BROKEN (CABIN) · airframe 56,356 hrs · 44,567 cycles

BULLNOSE EXIT LIGHT BROKEN AT ROW 6 ABC. R & R LIGHT IAW MM.

Part: PRESSURE GAUGE — DEFECTIVE (OIL SYSTEM) · airframe 56,180 hrs · 44,454 cycles

INFLIGHT SHUTDOWN, AIR TURN BACK & DECLARED EMER. NR 1 ENG OIL PRESS LOW ON TAKEOFF & CLIMB OUT, INDICATED IN YELLOW BAND. NO OIL PRESS LIGHT ILLUMINATED. R & R NR 1 ENG OIL PRESS GAUGE IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,644 hrs · 44,099 cycles

FRAME INNER CHORD CRACKED AT BS 348.2 STRINGER 17L. R & R CHORD IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 55,644 hrs · 44,099 cycles

STRAP CRACKED AT BS 348.2 STRINGER 16L. R & R STRAP IAW SRM & DWG.

Part: SIGN — LOOSE (CABIN) · airframe 55,497 hrs · 43,989 cycles

LEFT EMER OVERWING EXIT SIGN LOOSE. SECURED SIGN IAW AMM.

Part: SPOILER — DELAMINATED (LT WING) · airframe 55,497 hrs · 43,989 cycles

LEFT WING NR 1 FLIGHT SPOILER DELAMINATED. R & R NR 1 SPOILER IAW MM.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 55,441 hrs · 43,947 cycles

DIVERSION DECLARED EMERGENCY. A HYD SYS FAILED BOTH LOW PRESS LIGHT ILLUMINATED & A QTY DEPLETED. R & R A ELEC HYD PUMP IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,712 hrs · 43,410 cycles

L1 DOOR OVERHEAD EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.

Part: RELEASE CABLE — FRAYED (EVAC SLIDE) · airframe 54,712 hrs · 43,410 cycles

L2 DOOR EMER EVAC SLIDE RELEASE CABLE FRAYED. R & R CABLE IAW MM.

Part: RELEASE CABLE — FRAYED (R2 DOOR) · airframe 54,712 hrs · 43,410 cycles

R2 DOOR EMER EVAC SLIDE RELEASE CABLE FRAYED. R & R CABLE IAW AMM.

Part: BUTTSTRAP — DAMAGED (FUSELAGE) · airframe 54,712 hrs · 43,410 cycles

BUTT STRAP DAMAGED AT BS 908, BETWEEN STRINGER 3L TO STRINGER 3R. R & R BUTT STRAP IAW DWG.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 54,712 hrs · 43,410 cycles

LOWER FWD WINDOW CORNER STRINGER SPLICE CRACKED AT BS 727+10, STRINGER 13R. R & R SPLICE IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 54,712 hrs · 43,410 cycles

RIGHT BS 360+10 UPPER FWD WINDOW CORNER STRINGER 11 SPLICE ANGLE CRACKED IN HOLE 5. R & R ANGLE IAW DWG.

Part: FORGING — CRACKED (FUSELAGE) · airframe 54,712 hrs · 43,410 cycles

RIGHT BS 887+10 WINDOW FRAME FORGING CRACKED AT HOLE NR 5. R & R FORGING IAW BAC.

Part: FORGING — CRACKED (FUSELAGE) · airframe 54,712 hrs · 43,410 cycles

RIGHT BS 807+10 WINDOW FRAME FORGING CRACKED AT HOLE NR 11. R & R FORGING IAW DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,712 hrs · 43,410 cycles

LEFT BS 727+10 LOWER FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,712 hrs · 43,410 cycles

RIGHT BS 847+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,712 hrs · 43,410 cycles

LEFT BS 887+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,712 hrs · 43,410 cycles

LEFT BS 807+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW SRM.

Part: FORGING — CRACKED (FUSELAGE) · airframe 54,712 hrs · 43,410 cycles

RIGHT BS 727B+10 WINDOW FRAME FORGING CRACKED AT HOLE 7. R & R FORGING IAW DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,712 hrs · 43,410 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,712 hrs · 43,410 cycles

LEFT BS 847+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,712 hrs · 43,410 cycles

RIGHT BS 887+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,712 hrs · 43,410 cycles

RIGHT BS 887+10 LWR FWD WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,712 hrs · 43,410 cycles

LEFT BS 787+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,712 hrs · 43,410 cycles

RIGHT BS 807+10 UPPER AFT WINDOW CORNER SKIN CUT OUT CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,712 hrs · 43,410 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,712 hrs · 43,410 cycles

LEFT BS 867+10 LOWER FWD WINDOW CORNER SKIN CUT OUT CRACKED AT HOLE 3. REPAIRED SKIN IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 54,586 hrs · 43,334 cycles

LEFT WING OTBD FOREFLAP, INBD TE DELAMINATED. R & R FORE FLAP ASSEMBLY IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,835 hrs · 42,812 cycles

SKIN CRACKED AT BS 500D+11 STRINGER 10R. REPAIRED SKIN IAW EA.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 53,801 hrs · 42,788 cycles

AIR TURN BACK, DECLARED EMERGENCY AFTER TAKEOFF. AT APPROXIMATELY 4000 FEET FWD LAVATORY SMOKE ALARM WAS ON WITH AN ACRID SMELL. RETURNED TO MIDWAY. R & R COALESCENT BAGS IAW MM.

Part: BLOWER MOTOR — FAULTY (E&E BAY) · airframe 53,752 hrs · 42,747 cycles

LOUD NOISE & VIBRATION ON CLIMB OUT & SLIGHT SMELL IN MID CABIN. WENT TO HIGH IN PACKS, CLEARED SMELL. SWITCHED TO ALT COOLING FAN, VIBRATION STOPPED. GASPAR FAN OFF ENTIRE TIME. R & R EQUIPMENT COOLING BLOWER MOTOR IAW MMM.

Part: WIRE HARNESS — FAULTY (FUEL SYSTEM) · airframe 53,173 hrs · 42,355 cycles

DECLARED EMERGENCY NR 1 FUEL QUANTITY INDICATOR CLIMBED TO 10.8 THEN DESCENDED TO "0". FMC FUEL QUANTITY ERRATIC. NR 2 FUEL QUANTITY APPEARED TO BE DECREASING AT AN ABNORMAL RATE. R & R NR 1 FUEL TANK TSO & HARNESS IAW MM.

Part: FAN — FAULTY (AC BAY) · airframe 53,058 hrs · 42,261 cycles

SLIGHT ELECTRICAL ODOR NOTED IN COCKPIT & CABIN WHEN RECIRCULATING FAN WAS ON. R & R FAN IAW MM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 52,824 hrs · 42,085 cycles

FWD AISLE EMERGENCY EXIT SIGN LENS CRACKED. R & R LENS IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 51,864 hrs · 41,347 cycles

LT AFT WING EMERGENCY LIGHT INOP. R & R LIGHT IAW MM.

Part: BATTERY PACK — DAMAGED (CABIN) · airframe 51,864 hrs · 41,346 cycles

FWD GALLEY EMERGENCY EXIT LIGHT INOP. REPAIRED BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,864 hrs · 41,346 cycles

RT EMERGENCY EXIT LIGHT INOP BETWEEN ROW 1 TO ROW 5. R & R BATTERY PACK IAW AMM.

Part: FITTING — CRACKED (LT ELEVATOR) · airframe 51,864 hrs · 41,346 cycles

LEFT ELEVATOR CLIP CRACKED AT ELEVATOR STA 63.93. R & R CLIP IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 24R TO STR 25R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: PANEL — CRACKED (CARGO DOOR) · airframe 51,864 hrs · 41,346 cycles

AFT CARGO COMPARTMENT DOOR INTERIOR HANDLE OF INTERNAL PANEL COLLAR CRACKED. REMOVED AND REPLACED PANEL IAW SRM AND DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

WEB CRACKED BETWEEN BS 500B TO BS 500C, STR 26R. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.

Part: LENS — BROKEN (CABIN) · airframe 51,864 hrs · 41,346 cycles

EMERGENCY EXIT LIGHT LENS LOCATED ON CURVED CEILING PANEL AT FWD CABIN BROKEN. REMOVED AND REPLACED LENS IAW AMM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

WEB CRACKED BETWEEN BS 500B TO 500C, STR 26L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: REVEAL — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

REVEAL STRIP CRACKED AT BS 794, BETWEEN STR 19R TO STR 25R. REMOVED AND REPLACED REVEAL STRIP IAW SRM AND DWG.

Part: PANEL — CRACKED (RT WING) · airframe 51,864 hrs · 41,346 cycles

RIGHT WING OVERWING SUPPORT ASSY PANEL CRACKED. REMOVED AND REPLACED PANEL IAW DWG.

Part: SUPPORT — CRACKED (LT WING) · airframe 51,864 hrs · 41,346 cycles

LEFT OVERWING SUPPORT ASSY CRACKED. REMOVED AND REPLACED SUPPORT ASSY IAW DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

WEB CRACKED BETWEEN BS 178 TO BS 188, WL 207.8. REMOVED AND REPLACED WEB IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

WEB CRACKED BETWEEN BS 616 AND BS 639, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

SUPPORT BRACKET CRACKED BETWEEN BS 663.75 TO BS 675, BETWEEN RBL 30 TO RBL 40. REMOVED AND REPLACED BRACKET IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

CLIP CRACKED AT BS 178, RBL 25. REMOVED AND REPLACED CLIP IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

LEFT SIDE ANGLE CRACKED AT BS 178, LBL 13.83. REMOVED AND REPLACED ANGLE IAW AND DRAWING.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

CHANNEL CRACKED BETWEEN BS 616 TO BS 639, STR 2R. REMOVED AND REPLACED CHANNEL IAW SRM AND DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

WEB CRACKED BETWEEN BS 188 TO BS 196.5, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

VERTICAL DUCT ASSY WEB CRACKED BETWEEN BS 294.5 TO BS 312, STR 27R. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

WEB CRACKED BETWEEN BS 188 TO BS 195.5, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.

Part: BEAM — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

INNER CHORD WEB AND STUB BEAM CRACKED AT BS 616, WL 208. R & R STUB BEAM IAW EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

WEB CORRODED BETWEEN BS 807 TO BS 827, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

SHEAR TIE CORRODED AT BS 325.38, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

INNER CHORD AND WEB CRACKED AT BS 616, STR 18L. REPAIRED INNER CHORD, OUTER CHORD AND WEB IAW EA.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

STOP PAD CRACKED AT BS 616, STR 11R. REMOVED AND REPLACED STOP PAD IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

VERTICAL DUCT ASSY CHANNEL CRACKED BETWEEN BS 294.5 TO BS 312, STR 27R. REMOVED AND REPLACED CHANNEL IAW SRM & DRAWING.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

BULKHEAD RT SIDE CHORD CRACKED AT BS 178, WL 217 LT SIDE. R & R CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

INTERCOSTAL CRACKED BETWEEN BS 639 TO BS 663.75, STR 15R. REMOVED AND REPLACED INTERCOSTAL IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

ANGLE CRACKED AT BS 328, RBL 55. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

BULKHEAD RT SIDE CHORD CRACKED AT BS 178, WL 217 RT SIDE. R & R CHORD IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

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

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

ATTACH CLIP CRACKED AT BS 348.2, STR 15L. REMOVED AND REPLACED ANGLE IAW AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

TIE CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

INNER CHORD AND WEB CRACKED AT BS 616, STR 18L. REPAIRED INNER CHORD, OUTER CHORD AND WEB IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

TIE CLIP CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

CLIP CRACKED AT BS 580, STR 11L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

CHANNEL STRINGER CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STRINGER IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

FRAME CRACKED AT BS 188, STR 17L. REPAIRED FRAME IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP IAW SRM AND DRAWING.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

THRESHOLD WEB CORRODED BETWEEN BS 947.5 TO BS 987, STR 17R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

ANGLE CRACKED BETWEEN BS 294.5 TO BS 312, STR 25L. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

SUPPORT ANGLE CRACKED AT BS 325.38, BETWEEN STR 20L TO STR 21L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

WEB CRACKED AT BS 328, BETWEEN STR 23R TO STR 24R. REMOVED AND REPLACED WEB IAW SRM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

SUPPORT CLIP CRACKED AT BS 294.5, STR 23L. REMOVED AND REPLACED CLIP IAW SRM AND DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

STRAP CRACKED BETWEEN BS 277 TO BS 294.5, STR 17R. REMOVED AND REPLACED STRAP IAW SRM AND DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

CLIP CRACKED AT BS 560, STR 11L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

WEB CORRODED BETWEEN BS 400 TO BS 420, STR 17L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

SUPPORT ANGLE CRACKED BETWEEN 380 TO BS 400, BL 0. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

CLIP CRACKED AT BS 580, STR 11R. REMOVED AND REPLACED CLIP IAW SRM AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

TIE CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG 46525.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

SUPPORT ANGLE CRACKED AT BS 328, RBL 34. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

WEB CRACKED BETWEEN BS 500A TO BS 500B, STR 26R. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.

Part: PANEL — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

SIDEWALL PANEL CRACKED AT BS 380, BETWEEN STR 25L TO STR 28L. REMOVED AND REPLACED PANEL IAW SRM AND DRAWING.

Part: DUCT — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

DUCT ASSY CRACKED BETWEEN BS 294.5 TO BS 312, BETWEEN STR 26R TO STR 26L. REPAIRED DUCT ASSY IAW EO AND EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

WEB CRACKED BETWEEN BS 351 TO BS 360, BL 0. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.

Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

THRESHOLD WEB CRACKED BETWEEN BS 294.5 TO BS 328, STR 17R. REMOVED AND REPLACED WEB IAW SRM & DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

TIE CLIP CRACKED AT BS 947.5, STR 23R. REMOVED AND REPLACED TIE CLIP IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

LONGITUDINAL FLOORBEAM WEB CRACKED ON ACCESS PANEL 2212 AT CONTROL CABIN. REPAIRED WEB IAW EA.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

STRINGER SPLICE CORRODED AT BS 787+3, STR 21R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

STRINGER SPLICE CORRODED AT BS 787+3, STR 22R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 967, LBL 27. REPAIRED BEAM IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

FRAME WEB CRACKED AT BS 420, BETWEEN STR 11L TO STR 13L. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

ANGLE CRACKED AT BS 540, LBL 1.0. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

SUPPORT ANGLE CRACKED AT STA 540, RBL 1.0. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

STIFFENER CRACKED BETWEEN BS 294.5 TO BS 303.9, STR 16L. REMOVED AND REPLACED STIFFENER IAW SRM AND DRAWING.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

STOP PAD FITTING CRACKED BETWEEN BS 616 TO BS 639, STR 11L. REMOVED AND REPLACED FITTING IAW DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

ANGLE CRACKED AT BS 947.5, BETWEEN STR 24L TO STR 25L. REMOVED AND REPLACED ANGLE IAW SRM.

Part: RUB STRIP — MISSING (NR 2 NACELLE) · airframe 51,864 hrs · 41,346 cycles

RUB STRIPS MISSING ON CUT OUT OF NACELLE STRUT ACCESS NR 5827R ENGINE NR 2. INSTALLED RUB STRIP IAW DWG.

Part: ANGLE — CRACKED (LT PYLON) · airframe 51,864 hrs · 41,346 cycles

NR 1 ENGINE STRUT TORQUE BOX ACCESS NR 5757L ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: RUB STRIP — MISSING (NR 2 NACELLE) · airframe 51,864 hrs · 41,346 cycles

RUB STRIP MISSING ON CUT OUT OF NACELLE STRUT ACCESS NR 5828R ENGINE NR 2. INSTALLED RUB STRIP IAW DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

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

Part: BEAM — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

FLOOR STRUCTURE BEAM UPPER CHORD CRACKED AT BS 947.5, LBL 54. REPAIRED CHORD IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

SUPPORT ANGLE CRACKED BETWEEN BS 277 TO BS 291.5, STR 13R. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

STRINGER CORRODED BETWEEN BS 967 TO BS 986.5, STR 21R. REMOVED AND REPLACED STRINGER IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

FRAME CRACKED AT BS 947.5, STR 19R. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

CHANNEL CRACKED AT BS 540, RBL 1.0. REMOVED AND REPLACED CHANNEL IAW SRM AND DRAWING.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

STIFFENER CRACKED BETWEEN BS 294.5 TO BS 303.9, STR 15L. REMOVED AND REPLACED STIFFENER IAW SRM AND DRAWING.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

CHANNEL CRACKED AT BS 540, LBL 1.0. REMOVED AND REPLACED CHANNEL IAW SRM AND DRAWING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

ANGLE CRACKED AT BS 947.5, BETWEEN STR 24R TO STR 25R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

SUPPORT ANGLE CRACKED AT BS 344, BETWEEN STR 4L TO STR 7L. REMOVED AND REPLACED ANGLE AND IAW SRM AND DRAWING.

Part: RUB STRIP — MISSING (NR 2 NACELLE) · airframe 51,864 hrs · 41,346 cycles

RUB STRIPS MISSING ON CUT OUT OF NACELLE STRUT ACCESS NR 5831R ENGINE NR 2. INSTALLED RUB STRIP IAW DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

WEB CRACKED BETWEEN BS 277 TO BS 291.5, STR 14R. REMOVED AND REPLACED WEB IAW SRM AND DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

STRAP CRACKED BETWEEN BS 306 TO BS 348.5, LBL 33. REMOVED AND REPLACED STRAP IAW SRM AND DRAWING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

FLOORBEAM CORRODED AT BS 986.5, RBL 45.5. REPAIRED CHORD IAW EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

STIFFENER CRACKED BETWEEN BS 312 TO BS 328, RBL 30. REMOVED AND REPLACED STIFFENER IAW SRM AND DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

STUB FRAME CRACKED AT BS 296.4, STR 7R. REPAIRED STUB FRAME IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

FLOORBEAM CORRODED AT BS 967, BETWEEN BL 0 TO RBL 40. REPAIRED BEAM IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

FLOORBEAM CORRODED AT BS 328, LBL 52. REPAIRED CHORD IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

ANGLE CRACKED AT BS 440, STR 26L. REMOVED AND REPLACED ANGLE IAW SRM AND DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

STRAP CRACKED BETWEEN BS 306 TO BS 348.5, RBL 46. REMOVED AND REPLACED STRAP IAW SRM AND DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

STRAP CRACKED BETWEEN BS 306 TO BS 348.5, BL 0. REMOVED AND REPLACED STRAP IAW SRM AND DRAWING.

Part: PLATE — CRACKED (L1 DOOR) · airframe 51,864 hrs · 41,346 cycles

FORWARD ENTRY DOOR FWD CORNER OF LOWER TRIM SWEEPER PLATE CRACKED. REMOVED AND REPLACED PLATE IAW SRM AND DRAWING.

Part: NUT PLATE — BROKEN (L1 DOOR) · airframe 51,864 hrs · 41,346 cycles

L1 DOOR EMERGENCY EVAC SLIDE SUPPORT NUT PLATE BROKEN. REMOVED AND REPLACED NUT PLATE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

ANGLE CRACKED AT BS 540, STR 22L. REPAIRED ANGLE IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

STRAP CRACKED BETWEEN BS 306 TO BS 348.5, LBL 45.5. REMOVED AND REPLACED STRAP IAW SRM AND DRAWING.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

TIE CLIP CRACKED AT BS 500D, STR 26L. REMOVED AND REPLACED TIE CLIP IAW SRM AND DRAWING.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

SUPPORT ANGLE CRACKED AT BS 500C, STR 26L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

Z-ANGLE CORRODED BETWEEN BS 294.5 TO BS 360, LBL 62. REMOVED AND REPLACED Z-ANGLE IAW SRM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

STRAP CRACKED BETWEEN BS 306 TO BS 348.5, LBL 10. REMOVED AND REPLACED STRAP IAW SRM AND DRAWING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

FLOORBEAM CORRODED AT BS 328, RBL 45. REPAIRED BEAM IAW SRM AND EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

WEB CRACKED AT BS 520+5, BETWEEN STR 22L TO STR 24L. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

ANGLE CRACKED AT BS 540, STR 22R. REPAIR ANGLE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

FRAME CORRODED AT BS 500, BETWEEN STR 28L AND STR 28R. REPAIRED FRAME IAW SRM.

Part: RUB STRIP — MISSING (NR 1 PYLON) · airframe 51,864 hrs · 41,346 cycles

RUB STRIP MISSING AT INTERNAL AREA OF CUT OUT OF PYLON ACCESS PANEL 5724L NR 1 ENGINE. INSTALLED RUB STRIP IAW DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

CHANNEL CRACKED BETWEEN BS 420 TO BS 440, STR 26R. REMOVED AND REPLACED CHANNEL IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

SUPPORT ANGLE CRACKED AT BS 727, RBL 3. REMOVED AND REPLACED ANGLE IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

WEB CRACKED AT BS 712, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

TIE CLIP CRACKED AT BS 727B, STR 25R. REMOVED AND REPLACED TIE CLIP IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

FRAME CORRODED AT BS 727E, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

STRINGER CORRODED BETWEEN BS 460 AND BS 480, STR 27R. REMOVED AND REPLACED STRINGER IAW SRM AND DRAWING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

FRAME CORRODED AT BS 500A, BETWEEN STR 28R TO STR 28L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

FRAME CORRODED AT BS 500B, BETWEEN STR 28R TO STR 28L. REPAIRED FRAME IAW SRM.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

SUPPORT CHANNEL CRACKED AT BS 727A, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED CHANNEL IAW SRM & DRAWING.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

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

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

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

Part: STRIP — CRACKED (SERVICE DOOR) · airframe 51,864 hrs · 41,346 cycles

ACCESS PANEL AFT EDGE STRIP CRACKED ON NR 3403R. REMOVED AND REPLACED STRIP IAW SRM AND DRAWING.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

STIFFENER CRACKED AT BS 727, STR 27L. REMOVED AND REPLACED STIFFENER IAW SRM AND DRAWING.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

SHEAR TIE CORRODED AT BS 500, BETWEEN STR 28L TO STR 28R. REMOVED AND REPLACED SHEAR TIE IAW SRM AND DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

STIFFENER CRACKED AT BS 727, STR 27R. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.

Part: ROLLER — CORRODED (LE SLAT) · airframe 51,864 hrs · 41,346 cycles

LEFT WING NR 2 SLAT TRACK CORRODED ON ROLLER. REMOVED AND REPLACED ROLLER IAW AMM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

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

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

CHANNEL CRACKED BETWEEN BS 500 TO BS 500A, STR 26R. REMOVED AND REPLACED ZEE ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (LT AILERON) · airframe 51,864 hrs · 41,346 cycles

LEFT WING AILERON ANGLE CRACKED AT LEVEL OF RSS 533 INTERIOR CAVITY. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

SKIN CRACKED AT BS 715 AND STR 27L. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 51,864 hrs · 41,346 cycles

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

Part: STRUCTURE — CRACKED (RT MLG) · airframe 51,864 hrs · 41,346 cycles

RIGHT SIDE CRACKED LOWER CHORD LOCATED AT MAIN LANDING GEAR BAY AT BS 680. REMOVED AND REPLACED CHORD IAW SRM AND DRAWING.

Part: SKIN — CRACKED (LE SLAT) · airframe 51,864 hrs · 41,346 cycles

RIGHT WING NR 6 SLAT LOWER SURFACE CRACKED. REPAIRED NR 6 SLAT IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 51,864 hrs · 41,346 cycles

MAIN WHEEL WELL PRESSURE DECK CRACKED AT BS 672.75, LBL 42. REPAIRED WEB IAW EO AND EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

STUB BEAM CRACKED AT BS 706, BETWEEN LBL 45.57 AND LBL 60.5. REPAIRED STUB BEAM IAW EO AND EA.

Part: LENS — BROKEN (CABIN) · airframe 51,864 hrs · 41,346 cycles

R1 DOOR EMERGENCY EXIT LENS BROKEN. REMOVED AND REPLACED LENS IAW AMM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 663.75, RBL 24.5. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 51,864 hrs · 41,346 cycles

LEFT WING NR 1 SLAT LOWER SURFACE CRACKED. REPAIRED SKIN IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 663.75+8, LBL 24.5. REPAIRED BEAM IAW EA.

Part: BEAM — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

STUB FRAME CRACKED AT BS 706, BETWEEN RBL45.5 TO RBL 60.5. REPAIRED BEAM IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 51,864 hrs · 41,346 cycles

MAIN WHEEL WELL PRESSURE DECK CRACKED AT BS 665.25, LBL 39. REPAIRED WEB IAW EO AND EA.

Part: DOUBLER — CRACKED (RT MLG WW) · airframe 51,864 hrs · 41,346 cycles

CRACKED FOUND ON MAIN WHEEL WELL PRESSURE DECK LOCATED AT BS 674.25, RBL 37. REMOVED AND REPLACED DOUBLER IAW SRM AND DWG.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 51,864 hrs · 41,346 cycles

MAIN WHEEL WELL PRESSURE DECK CRACKED AT BS 665.75, LBL 42.5. REPAIRED WEB IAW EO.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 51,864 hrs · 41,346 cycles

CRACKED LOCATED ON MAIN WHEEL WELL PRESSURE DECK LOCATED AT BS 665.75, RBL 39.5. REPAIRED PRESSURE DECK IAW SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

STUB BEAM CRACKED AT BS 685, BETWEEN LBL 45.57 AND LBL 60.5. REPAIRED BEAM IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

SKIN CRACKED AT BS 520 +7, BETWEEN STR 28L TO STR 28R. REPAIRED SKIN IAW EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 51,864 hrs · 41,346 cycles

CRACKED LOCATED ON MAIN WHEEL WELL PRESSURE DECK LOCATED AT BS 672.75, RBL 42. REPAIRED DECK IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 51,864 hrs · 41,346 cycles

RIGHT WING NR 5 SLAT LOWER SURFACE CRACKED. REPAIRED NR 5 SLAT IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,024 hrs · 40,747 cycles

FUSELAGE CRACKED AT BS 500D+9 ABOVE STR 10L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,024 hrs · 40,747 cycles

FUSELAGE CRACKED AT BS 500D+9 ABOVE STR 9L. REPAIRED SKIN PER EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 49,555 hrs · 39,639 cycles

SPLICE CHANNEL CRACKED AT BS 360, STR 28L. REMOVED AND REPLACED CHANNEL IAW SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 49,555 hrs · 39,639 cycles

SKIN CRACKED AT BS 360 + 19, BETWEEN STR 28L TO STR 28R. REPAIRED SKIN IAW AAR EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 47,439 hrs · 38,045 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING T/E EXTERNAL EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LENS — MISSING (CABIN) · airframe 46,985 hrs · 37,688 cycles

DURING SCHEDULED CV CHECK, FOUND OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,841 hrs · 37,572 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 500B+7, STR 4L. REPAIRED SKIN PER EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,097 hrs · 36,870 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER EA AND EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 46,259 hrs · 37,127 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CAP CORRODED AT BS 847, STR 25R. REMOVED AND REPLACED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 46,259 hrs · 37,127 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 639, RBL 45.5. REPAIRED WEB PER ER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,259 hrs · 37,129 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER ER.

Part: FAILSAFE — CORRODED (FUSELAGE) · airframe 46,259 hrs · 37,129 cycles

DURING SCHEDULED 14Y CHECK FOUND, FAIL-SAFE FRAME CORRODED AT BS 807, STR 27L. REMOVED AND REPLACED FRAME PER SRM.

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 46,259 hrs · 37,129 cycles

DURING SCHEDULED 14Y CHECK FOUND, VERTICAL SUPPORT BEAM WEB CRACKED AT BS 180, LBL 5.7. REPAIRED WEB PER SRM.

Part: HINGE — BROKEN (SPOILER) · airframe 45,591 hrs · 36,609 cycles

DURING SCHEDULED MV2 CHECK, FOUND NR 4 FLIGHT SPOILER HINGE BROKEN. REMOVED AND REPLACED SPOILER ASSY PER MM.

Part: COVER — LEAKING (NR 2 ENGINE) · airframe 44,511 hrs · 35,797 cycles

INFLIGHT SHUTDOWN/ DECLARED EMERGENCY. NR 2 ENGINE SHUTDOWN INFLIGHT DUE TO "0" OIL QUANTITY AND "0" OIL PRESSURE. FOUND AGB PAD LEAKED. REMOVED AND REPLACED AGB COVER.

Part: FITTING — BROKEN (GIRT BAR) · airframe 44,223 hrs · 35,574 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE COVER GIRT BAR AFT STORAGE CLIP BROKEN. REMOVED AND REPLACED CLIP PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 42,557 hrs · 34,288 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 42,557 hrs · 34,288 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP BETWEEN ROW 1 TO ROW 4. REMOVED AND REPLACED BATTERY PER MM.

Part: TAB — DELAMINATED (AILERON) · airframe 41,106 hrs · 33,245 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND RT WING AILERON TAB DELAMINATED. REMOVE AND REPLACED TAB PER MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,628 hrs · 32,893 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 767, BETWEEN STR 25L TO STR 25R. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,628 hrs · 32,893 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 807, BETWEEN STR 27R TO STR 26L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,628 hrs · 32,893 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 787, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,628 hrs · 32,893 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 947, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 40,628 hrs · 32,893 cycles

DURING SCHEDULED 12Y CHECK, FOUND 178 PRESSURE BULKHEAD VERTICAL BEAM WEB CRACKED BETWEEN BS 172 TO BS 176, RBL 17.0. REMOVED AND REPLACED WEB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,628 hrs · 32,893 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 2R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,628 hrs · 32,893 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 727E, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,628 hrs · 32,893 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,628 hrs · 32,893 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,628 hrs · 32,893 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,628 hrs · 32,893 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 2L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,628 hrs · 32,893 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,628 hrs · 32,893 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 4R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: RIB — CRACKED (HORIZ STAB) · airframe 40,628 hrs · 32,893 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT HORIZONTAL STAB L/E NR 6 RIB CRACKED. REPAIRED RIB PER SRM.

Part: LENS — MISSING (CABIN) · airframe 40,559 hrs · 32,837 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,198 hrs · 32,570 cycles

DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 528, STR 19R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 37,723 hrs · 30,832 cycles

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

Part: SKIN — DEBONDED (RT WING TE FLAP) · airframe 37,723 hrs · 30,832 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SURFACE DSBONDED AT OUTBOARD END. R&R FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 37,723 hrs · 30,832 cycles

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

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 51,864 hrs · 41,346 cycles

KEEL BEAM LOWER SKIN PANEL CRACKED AT FS 726.75, RBL 6.30. REPAIRED PANEL PER SRM.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 35,943 hrs · 29,545 cycles

DURING SCHEDULED HC1 CHECK, FOUND FLIGHT DECK EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BEARING — EXCESS PLAY (R2 DOOR) · airframe 34,146 hrs · 28,165 cycles

DURING SCHEDULED 10Y CHECK, FOUND R2 DOOR TORQUE TUBE BEARINGS HAVE RADIAL PLAY. REMOVED AND REPLACED TORQUE TUBE BEARINGS PER MM.

Part: TORQUE TUBE — WORN (LT ELEVATOR) · airframe 34,146 hrs · 28,165 cycles

DURING SCHEDULED 10Y CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TORQUE TUBE, HORN BEARING AND BOLTS PER MM.

Part: TORQUE TUBE — WORN (RT ELEVATOR) · airframe 34,146 hrs · 28,165 cycles

DURING SCHEDULED 10Y CHECK, RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TORQUE TUBE AND HORN BEARING PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 34,146 hrs · 28,165 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,146 hrs · 28,165 cycles

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

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 34,146 hrs · 28,165 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP INBOARD UPPER SURFACE DELAMINATED. R&R AFT FLAP PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 34,146 hrs · 28,165 cycles

DURING SCHEDULED 10Y CHECK, FOUND FWD CABIN EMERGENCY FLASHLIGHT INOP. R&R FLASHLIGHT PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,146 hrs · 28,165 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,146 hrs · 28,165 cycles

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

Part: TORQUE TUBE — CORRODED (T/E FLAP) · airframe 34,146 hrs · 28,165 cycles

DURING SCHEDULED 10Y CHECK, FOUND RIGHT WING INBOARD FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,146 hrs · 28,165 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,146 hrs · 28,165 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R AND 8L. REPAIRED FRAME PER SWA EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 34,146 hrs · 28,165 cycles

DURING SCHEDULED 10Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,146 hrs · 28,165 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,146 hrs · 28,165 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,146 hrs · 28,165 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,146 hrs · 28,165 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,146 hrs · 28,165 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,146 hrs · 28,165 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,146 hrs · 28,165 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,146 hrs · 28,165 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,146 hrs · 28,165 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,146 hrs · 28,165 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8R. REPAIRED FRAME PER SWA EA.

Part: CABLE — FRAYED (EVAC SLIDE) · airframe 34,146 hrs · 28,165 cycles

DURING SCHEDULED 10Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 32,615 hrs · 26,947 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 1 ABC. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: SIGN — BROKEN (EMERGENCY EXIT) · airframe 31,163 hrs · 25,811 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD RT EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM.

Part: SIGN — BROKEN (EMERGENCY EXIT) · airframe 31,163 hrs · 25,811 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD LAV EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 30,844 hrs · 25,563 cycles

DURING SCHEDULED C2 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RIGHT FLAP PER MM.

Part: SKIN — DELAMINATED (LT FOREFLAP) · airframe 30,844 hrs · 25,563 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: COVER — BROKEN (EXIT SIGN) · airframe 29,966 hrs · 24,873 cycles

DURING SCHEDULED C1 CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT SIGN LENS COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,421 hrs · 24,466 cycles

DURING SCHEDULED SERVICE CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — DELAMINATED (NR 2 SLAT) · airframe 28,965 hrs · 24,110 cycles

DURING SCHEDULED C4 CHECK, FOUND NR 2 L/E SLAT DELAMINATED. REMOVED AND REPLACED SLAT PER MM.

Part: SKIN — DELAMINATED (LT WING FOREFLAP) · airframe 28,965 hrs · 24,110 cycles

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

Part: WIRE — DAMAGED (FUEL SHUTOFF VLV) · airframe 27,964 hrs · 23,299 cycles

DIVERSION, EVIDENCE OF ELECTRICAL ODOR IN COCKPIT. FOUND WIRES DAMAGED IN OVERHEAD P-5 PANEL, NR 1 ENGINE FUEL SHUT-OFF VALVE & MLG POSITION SENSOR CIRCUIT BREAKERS POPPED. REPAIRED WIRES PER SWPM. REMOVED AND REPLACED P52 FUEL MODULE & T492 LEFT MLG POSITION SENSOR PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 27,049 hrs · 22,596 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 & R1 DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 27,049 hrs · 22,596 cycles

DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.

Part: LENS — LOOSE (R1 DOOR) · airframe 26,449 hrs · 22,110 cycles

R1 DOOR LOWER EMERGENCY EXIT SIGN LENS LOOSE. SECURED EXIT SIGN LENS PER MM.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 26,298 hrs · 21,987 cycles

R1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED R1 DOOR EVAC SLIDE PER MM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 25,689 hrs · 21,510 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 664, LBL 31.5, CRACKED. REPAIRED PRESSURE WEB PER SRM.

Part: TAB — DELAMINATED (RT AILERON) · airframe 25,689 hrs · 21,510 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING AILERON TAB DELAMINATED. REMOVED AND REPLACED RT WING AILERON TAB PER MM.

Part: CABLE — MISROUTED (R2 DOOR) · airframe 25,689 hrs · 21,510 cycles

DURING SCHEDULED 1/4D CHECK, FOUND R2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: STRUCTURE — CRACKED (RT WING FLAP) · airframe 25,689 hrs · 21,510 cycles

DURING SCHEDULED 1/4D CHECK, FOUND RT WING OUTBOARD T/E MID FLAP, CRACKED. REPAIRED RT WING MID FLAP PER SRM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 25,283 hrs · 21,207 cycles

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

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 24,575 hrs · 20,630 cycles

L1 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED L1 DOOR EVAC SLIDE PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 23,894 hrs · 20,048 cycles

R1 DOOR EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM.

Part: SLIDE — OUT OF LIMITS (L2 DOOR) · airframe 22,434 hrs · 18,872 cycles

L2 DOOR SLIDE PRESSURE GAUGE IN THE RED. REMOVED AND REPLACED L2 DOOR SLIDE PER MM.

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT) · airframe 21,183 hrs · 17,860 cycles

DIVERSION, LANDING GEAR WOULD NOT RETRACT. FOUND, LANDING GEAR LEVER LATCH CIRCUIT BREAKER TRIPPED, RESET CIRCUIT BREAKER AND CYCLED GEAR PER MM. OPS CHECKED GOOD PER MM.

Part: SLIDE — OUT OF ADJUST (SERVICE DOOR) · airframe 20,678 hrs · 17,441 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 19,357 hrs · 16,378 cycles

L1 DOOR ESCAPE SLIDE PARTIALLY FELL OUT OF CONTAINER. REINSTALLED THE L1 ESCAPE SLIDE PER MM.

Part: PIN — CORRODED (LT MLG TRUNNION) · airframe 18,884 hrs · 15,984 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT MLG STRUT AND TRUNNION PIN CORRODED. REMOVED AND REPLACED LT MLG STRUT AND TRUNNION PIN PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 18,399 hrs · 15,585 cycles

FWD INBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 17,912 hrs · 15,188 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 17,247 hrs · 14,645 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 986.5, STR 24L. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FRAME — CRACKED (FWD SVC DOOR) · airframe 17,247 hrs · 14,645 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR AFT FRAME CRACKED AT STOP CUTOUT, 4TH FROM TOP. REPAIRED FRAME PER SRM.

Part: LENS — LOOSE (CABIN) · airframe 17,247 hrs · 14,645 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD LAV EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 16,017 hrs · 13,677 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — DISLODGED (SERVICE DOOR) · airframe 11,322 hrs · 9,806 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.

Part: LENS — LOOSE (EVAC SLIDE)

AFT SERVICE DOOR EVACUATION SLIDE PRESSURE INDICATOR LENS LOOSE. SECURED LENS ASSY PER MM.