N618WN

Part: FRAME — CRACKED (AFT CARGO DOOR) · airframe 66,164 hrs · 52,255 cycles

AFT CARGO DOOR FRAME CRACKED AT BS 845. R & R DOOR IAW AMM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 66,164 hrs · 52,255 cycles

L2 DOOR SLIDE OUT OF ADJUST. ADJUSTED THE SLIDE IAW AMM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 65,794 hrs · 52,025 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW MAINTENANCE.

Part: LENS — MISSING (CABIN) · airframe 65,794 hrs · 52,025 cycles

EMERGENCY EXIT BULL NOSE LIGHT COVER LENS MISSING AT ROW 22. R & R LENS IAW SIP.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,141 hrs · 51,617 cycles

RIGHT EMERGENCY LIGHTS INOPERATIVE BETWEEN ROW 16 TO ROW 20. R & R BATTERY PACK IAW AMM.

Part: PANEL — DAMAGED (RT WING) · airframe 64,493 hrs · 51,221 cycles

AIR TURN BACK INSPECTION PANEL RT WING PEELED OFF. R & R PANEL 5348 IAW SIP.

Part: LINK — CORRODED (RT MLG) · airframe 64,451 hrs · 51,194 cycles

RIGHT MLG WALKING BEAM ATTACH LINK ASSEMBLY CORRODED, AROUND BUSHINGS ON LUGS. R & R SWING LINK IAW AMM & EA.

Part: LINK — CORRODED (LT MLG TRUNNION) · airframe 64,451 hrs · 51,194 cycles

LEFT MLG A LINK CORRODED ON LUGS FWD TRUNNION. R & R A LINK IAW EA.

Part: LINK ASSY — CORRODED (LT MLG) · airframe 64,451 hrs · 51,194 cycles

LEFT WALKING BEAM ATTACH LINK ASSEMBLY CORRODED ON LUGS. R & R LINK ASSEMBLY IAW EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 64,451 hrs · 51,194 cycles

LEFT WING INBD FORE FLAP, UPPER SKIN REPAIR DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: RIB — CRACKED (RT WING) · airframe 64,451 hrs · 51,194 cycles

RIGHT WING INNER UPPER RIB CHORD CRACKED, AT STATION 114, FWD OF MLG TRUNNION FITTING. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 64,451 hrs · 51,194 cycles

RIGHT WING REAR SPAR WEB CRACKED AT RSS 201. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 64,451 hrs · 51,194 cycles

RIGHT WING REAR UPPER SPAR CHORD CRACKED, AT RSS 224.4. REPAIRED CHORD IAW EA.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 64,451 hrs · 51,194 cycles

RT WING AFT SUPPORT FITTING CRACKED AT NR 5 HOLE. R&R FITTING PER EA.

Part: SPAR — CRACKED (LT WING) · airframe 64,451 hrs · 51,194 cycles

LEFT WING REAR SPAR WEB CRACKED, AT STATION RSS 224.14, AT UPPER FASTENER. REPAIRED WEB IAW EA.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 64,451 hrs · 51,194 cycles

LT WING AFT SUPPORT FITTING CRACKED AT NR 5 HOLE. R&R FITTING PER EA.

Part: RIB — CRACKED (LT WING) · airframe 64,451 hrs · 51,194 cycles

LEFT WING INNER UPPER RIB CHORD CRACKED, AT WBL 114, AFT SPAR AREA. REPAIRED CHORD IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 64,451 hrs · 51,194 cycles

RIGHT WING REAR SPAR WEB CRACKED, AT STATION RSS 224.14, AT FASTENER HOLE. REPAIRED WEB IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 64,450 hrs · 51,194 cycles

LEFT WING REAR UPPER SPAR CHORD CRACKED, AT RSS 224.14. REPAIRED CHORD IAW EA.

Part: MOTOR — FAULTY (TE FLAP) · airframe 64,280 hrs · 51,085 cycles

DECLARED EMER, FLAP HANDLE IN 5, FLAPS WOULD NOT GO PAST POSITION 2 ON INDICATOR. R & R FLAP HYD MOTOR IAW AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 64,058 hrs · 50,927 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,944 hrs · 50,859 cycles

LEFT AFT EMER LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 63,353 hrs · 50,473 cycles

RIGHT EEPLS LENS LOOSE AT ROW 12. REPAIRED LENS IAW EA.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 63,214 hrs · 50,366 cycles

FORWARD INBD EMER FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,214 hrs · 50,366 cycles

AFT ENTRY DOOR CENTER PANEL EMER LIGHT INOPERATIVE. REPAIRED LIGHT ASSEMBLY IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,214 hrs · 50,366 cycles

R1 DOOR JUST FORWARD OF LOWER DOOR HINGE CUT OUT CRACKED. REPAIRED CUT OUT IAW SRM.

Part: WIRE — BROKEN (CABIN) · airframe 63,214 hrs · 50,366 cycles

AFT CABIN EXIT LOCATOR SIGN WIRE BROKEN AT BS 908. REPAIRED WIRE IAW AMM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 63,214 hrs · 50,366 cycles

SEAT TRACK INBOARD & OUTBOARD FLANGE CRACKED AT BS 727B, LBL 24.8. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 63,214 hrs · 50,366 cycles

OUTBOARD SEAT TRACK FLANGE CRACKED AT BS 727B, RBL 24.8. REPAIR SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 63,214 hrs · 50,366 cycles

SEAT TRACK FLOORBEAM FLANGE CRACKED AT BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,214 hrs · 50,366 cycles

INTERCOSTAL CRACKED BETWEEN BS 747 TO 767, STRINGER 25. R & R INTERCOSTAL IAW SRM.

Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 63,214 hrs · 50,366 cycles

AFT CARGO CENTER THRESHOLD CRACKED AT THE AFT END & A FASTENER HOLE CRACKED OUT IN UPPER INBOARD EDGE. REPAIRED THRESHOLD IAW EA.

Part: INTERCOSTAL — CRACKED (BS 278) · airframe 63,214 hrs · 50,366 cycles

INTERCOSTAL WEB CRACKED AT BS 278, STRINGER 14R. R & R IAW SRM & EA.

Part: STRINGER SPLICE — CORRODED (BS 907) · airframe 63,214 hrs · 50,366 cycles

AFT CARGO COMPARTMENT STRINGER SPLICE CORRODED AT BS 907, STRINGER 19L. R & R THE STRINGER SPLICE IAW DWG & SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 63,214 hrs · 50,366 cycles

AFT CARGO COMPARTMENT STRINGER SPLICE CORRODED AT BS 907, STRINGER 20L. R & R SPLICE IAW DWG & SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,214 hrs · 50,366 cycles

FLOOR WEB CORRODED BETWEEN BS 990 TO 1000, RBL 40. R & R WEB IAW SRM & DWG.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 63,214 hrs · 50,366 cycles

LEFT HORIZONTAL STABILIZER RIB STIFFENER CRACKED AT STAB STATION 92.7. R & R STIFFENER IAW SRM.

Part: BRACKET — CRACKED (RT WING) · airframe 63,214 hrs · 50,366 cycles

RIGHT WING NR 6 LE BRACKET CRACKED. REPAIRED BRACKET IAW DWG & SRM.

Part: STRAP — FRAYED (CABIN) · airframe 63,214 hrs · 50,366 cycles

RIGHT EMER STRAP FRAYED. R & R STRAP IAW AMM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,214 hrs · 50,366 cycles

RIGHT CREASE BEAM INNER CHORD CORRODED BETWEEN BS 976.5 TO 986.5, RBL 46. R & R BEAM IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,214 hrs · 50,366 cycles

RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 954 TO 967, RBL 54. R & R WEB IAW TC.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 63,214 hrs · 50,366 cycles

LONGITUDINAL FLOORBEAM STUB BEAM ATTACHMENT CLIP CRACKED AT BS 639, RBL 45.5. R & R CLIP IAW SRM & DWG.

Part: SKIN — CRACKED (L1 DOOR) · airframe 63,041 hrs · 50,242 cycles

L1 DOOR INNER SKIN CRACKED AT LOWER HINGE CUT OUT. REPAIRED SKIN IAW EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,973 hrs · 50,198 cycles

LEFT BULLNOSE EMER LIGHT INOPERATIVE AT ROW 22. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,973 hrs · 50,198 cycles

RIGHT BULLNOSE EMER LIGHT INOPERATIVE AT ROW 20. R & R BATTERY PACK IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,973 hrs · 50,198 cycles

RIGHT EMER EXIT BULLNOSE LIGHT INOPERATIVE AT ROW 20. REPAIRED LIGHT IAW MM.

Part: COVER — CRACKED (EMERGENCY EXIT) · airframe 62,831 hrs · 50,104 cycles

RIGHT EMER EXIT DOOR RELEASE HANDLE COVER CRACKED. R & R COVER IAW SIP.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,305 hrs · 49,744 cycles

RIGHT EMER EXIT LIGHT INOPERATIVE AT ROW 9. R & R BATTERY PACK ASSEMBLY IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 62,098 hrs · 49,608 cycles

LEFT BULLNOSE EMER LIGHTS INOPERATIVE BETWEEN ROW 1 & 2. R & R POWER SUPPLY IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 61,230 hrs · 49,030 cycles

FORWARD CABIN CEILING EMER EXIT LIGHT LENS LOOSE. SECURED LENS IAW MM.

Part: PANEL — CRACKED (LT WING) · airframe 60,692 hrs · 48,648 cycles

LEFT WING LOWER TE PANEL JUST OTBD PYLON CRACKED. REPAIRED PANEL IAW EA.

Part: PANEL — CRACKED (RT WING) · airframe 60,692 hrs · 48,648 cycles

RIGHT WING LOWER TE PANEL JUST OTBD PYLON CRACKED. REPAIRED PANEL IAW EA.

Part: WIRE — DAMAGED (CABIN) · airframe 60,692 hrs · 48,648 cycles

RIGHT EMER LIGHT INOPERATIVE AT ROW 20. REPAIRED WIRE IAW SWPM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,692 hrs · 48,648 cycles

RIGHT EMER LIGHT INOPERATIVE AT ROW 24. RELAMPED LIGHT IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 60,520 hrs · 48,513 cycles

FORWARD TWO LT BULLNOSE EMER LIGHTS INOPERATIVE. R & R POWER SUPPLY IAW AMM.

Part: LIGHT — CRACKED (CABIN) · airframe 59,467 hrs · 47,785 cycles

LEFT FWD EEPLS CRACKED. R & R EEPLS IAW AMM.

Part: COVER — MISSING (CABIN) · airframe 59,219 hrs · 47,607 cycles

R2 DOOR EMERGENCY EXIT LIGHT COVER MISSING. R & R COVER ASSEMBLY IAW SIP.

Part: WINDOW — ARCED (COCKPIT) · airframe 58,968 hrs · 47,452 cycles

R1 WINDOW ARCED. R & R WINDOW IAW AMM.

Part: BATTERY — WEAK (FLASHLIGHT) · airframe 58,358 hrs · 47,037 cycles

FWD GALLEY RT EMERGENCY FLASH LIGHT BATTERY WEAK. R & R BATTERY IAW MM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 57,914 hrs · 46,729 cycles

RT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED LENS IAW SIP.

Part: CIRCUIT CARD — FAULTY (LANDING GEAR) · airframe 57,552 hrs · 46,443 cycles

ON TAKEOFF THE NOSE GEAR RED LIGHT WOULD NOT EXTINGUISH WITH LANDING GEAR HANDLE UP, RECYCLED THE LANDING GEAR & ALL GEAR RETRACTION WAS NORMAL. R&R M983 CIRCUIT CARD IAW AMM.

Part: ANGLE — CRACKED (TE FLAP) · airframe 57,028 hrs · 46,042 cycles

RT WING NR 6 FLAP TRACK FAIRING ANGLE CRACKED AT LEVEL WBL 204.40 O/B SIDE. R&R ANGLE IAW SRM & DRAWING.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,028 hrs · 46,042 cycles

LEFT EMERGENCY EXIT LIGHTS INOP. R & R BATTERY PACK IAW MM.

Part: SLAT — DELAMINATED (RT WING) · airframe 57,028 hrs · 46,042 cycles

RT WING NR 6 SLAT I/B EDGE DELAMINATED ON UPPER SURFACE. REPAIRED SLAT IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

STRINGER CRACKED AT BS 807+7, STRINGER 10L. REPAIRED STRINGER IAW SRM & EA.

Part: SUPPORT ANGLE — CRACKED (LT ELEVATOR) · airframe 57,028 hrs · 46,042 cycles

LT ELEVATOR SUPPORT ANGLE CRACKED AT BS 121.59. R&R ANGLE IAW SRM & DRAWING.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

FWD ENTRY DOOR FWD CORNER SCUFF PLATE STRAP CRACKED. R & R STRAP IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

ANGLE CRACKED AT BS 328, BL 0. R & R ANGLE IAW SRM AND DWG.

Part: BRACKET — CRACKED (L1 DOOR) · airframe 57,028 hrs · 46,042 cycles

L1 DOOR FWD UPPER CORNER BRACKET CRACKED. R & R BRACKET IAW SRM AND DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 57,028 hrs · 46,042 cycles

LEFT WING INBD FORE FLAP T/E SURFACE DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

KEEL BEAM CORRODED BETWEEN BS 706 TO BS 727, RBL 6.50. REPAIRED KEEL BEAM IAW EO & EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

KEEL BEAM CORRODED BETWEEN BS 706 TO BS 727, LBL 6.50. REPAIRED CHORD IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

FRAME LOWER FLANGE OF FRAME CORRODED AT BS 787, BETWEEN STRINGER 26L AND STR 27L. R & R FRAME IAW SRM AND DWG.

Part: BRACKET — CORRODED (CARGO BAY) · airframe 57,028 hrs · 46,042 cycles

AFT CARGO COMPARTMENT BRACKET CORRODED AT BS 727D, STR 27R. R & R BRACKET IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

SUPPORT Z CORRODED BETWEEN BS 727C AND BS 747+11, STR 25L. R & R SUPPORT Z IAW SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

ATTACH CLIP CRACKED AT BS 348.2, STR 15L. R & R ANGLE IAW SRM AND DWG.

Part: TIE DOWN — CRACKED (CARGO BAY) · airframe 57,028 hrs · 46,042 cycles

AFT CARGO TRACK TIE DOWN CRACKED AT BS 747, STR 26R. REPAIRED TIE DOWN IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

AFT CARGO SUPPORT ANGLE CRACKED BETWEEN BS 927 TO BS 947.5, BL 0. R&R ANGLE IAW SRM AND PER DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

WEB CRACKED BETWEEN BS 787 TO BS 807, RBL 17. R & R WEB IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

SUPPORT ANGLE CRACKED AT BS 727+4.5, BETWEEN STR 26L AND STR 27L. R & R ANGLE IAW SRM AND DWG.

Part: STRAP — CORRODED (CARGO BAY) · airframe 57,028 hrs · 46,042 cycles

CARGO TRACK STRAP CORRODED AT BS 747+17, STR 26L. R & R STRAP IAW SRM.

Part: RUB STRIP — CRACKED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

RUBSTRIP CRACKED LOCATED ON ACCESS PANEL 57720L. R & R RUBSTRIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

FWD CARGO COMPARTMENT FRAME LOWER FLANGE CORRODED AT BS 500B, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME IAW SRM.

Part: RUB STRIP — CRACKED (NR 1 NACELLE) · airframe 57,028 hrs · 46,042 cycles

RUB STRIP CRACKED AT UPPER SIDE OF STRUT TORQUE BOX, ENGINE NR 1. R & R RUB STRIP IAW SRM AND DWG.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 57,028 hrs · 46,042 cycles

LEFT WING NR 2 SLAT T/E SURFACE DELAMINATED. R & R NR 2 SLAT IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

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

Part: PLATE — CRACKED (TE FLAP) · airframe 57,028 hrs · 46,042 cycles

RIGHT WING INBD MID FLAP PLATE CRACKED. R & R PLATE IAW CMM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

FLOORBEAM CRACKED AT BS 328, BL 0. REPAIRED BEAM IAW SRM & DRAWING.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

WEB CRACKED AT BS 328, BETWEEN STR 23R TO STR 25R. R & R WEB IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 57,028 hrs · 46,042 cycles

RIGHT WING T/E ANGLE CRACKED AT WBL 185.4. R & R ANGLE IAW SRM AND DWG.

Part: FLAP — DELAMINATED (RT WING) · airframe 57,028 hrs · 46,042 cycles

RT WING I/B FORE FLAP DELAMINATED. R&R FORE FLAP IAW AMM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

BULKHEAD WEB CRACKED AT BS 1016, BETWEEN STR 5L TO STR 7L. REPAIRED WEB IAW SRM.

Part: DUCT — CRACKED (CABIN) · airframe 57,028 hrs · 46,042 cycles

DUCT ASSEMBLY CRACKED BETWEEN BS 294.5 TO BS 312, BETWEEN STRINGER 26R TO STRINGER 26L. REPAIRED DUCT ASSEMBLY IAW EO.

Part: ANGLE — CRACKED (L1 DOOR) · airframe 57,028 hrs · 46,042 cycles

L1 DOOR FWD UPPER ANGLE CRACKED. R & R ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (RT WING) · airframe 57,028 hrs · 46,042 cycles

RIGHT WING ANGLE CRACKED AT T/E CAVITY. R & R ANGLE IAW SRM AND DWG.

Part: COVER — CRACKED (L1 DOOR) · airframe 57,028 hrs · 46,042 cycles

L1 DOOR LOWER GATE COVER CRACKED. R & R COVER IAW SRM AND DWG.

Part: ROLLER — CRACKED (TE FLAP) · airframe 57,028 hrs · 46,042 cycles

LT WING INTERNAL STRUCTURE OF INBD MID FLAP BEARING PLATE CRACKED. R & R ROLLER ASSY IAW SRM AND CMM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

FWD ENTRY DOOR CUT OUT CRACKED ON CLIP AT BS 360, STR 9L. R & R CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (KRUEGER FLAP) · airframe 57,028 hrs · 46,042 cycles

RT WING L/E CAVITY INTERNAL AREA KRUEGER ANGLE CRACKED AT WBL 157. R & R ANGLE IAW SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

WEB CRACKED BETWEEN BS 344 TO BS 360, BL 0. R & R WEB IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

SUPPORT ANGLE CRACKED AT BS 328, RBL 36. R & R ANGLE IAW SRM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

STRAP CRACKED AT BS 312, LBL 45.5. R & R STRAP IAW SRM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

STRAP CRACKED AT BS 312, RBL 45.5. R & R STRAP IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

PRESSURE BULKHEAD LOWER LT CORNER CRACKED AT BS 178, WL 230. R & R BULKHEAD IAW SRM AND DWG.

Part: PLATE — CRACKED (RT HORIZ STAB) · airframe 57,028 hrs · 46,042 cycles

RIGHT HORIZONTAL STABILIZER ACCESS PANEL 9226R PLATE CRACKED. REMOVED AND REPLACED PLATES IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

FWD ENTRY DOOR SUPPORT ANGLE CRACKED AT BS 348.2, STR 15L. R & R ANGLE IAW SRM AND DWG.

Part: SKIN — CRACKED (LT WING) · airframe 57,028 hrs · 46,042 cycles

LEFT WING L/E CRACKED AT STA 208. REPAIRED EDGE IAW SRM.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

OIL-CAN ON DOME WEB OF PRESSURE BULKHEAD LOCATED BS 1016 BETWEEN STR 9L TO STR 11L. REPAIRED WEB IAW EO & EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

SUPPORT ANGLE WEB CRACKED BETWEEN BS 294.5 TO BS 303.9, STR 16L. R & R WEB IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

CLIP CRACKED AT BS 360, STR 8L. R & R CLIP IAW SRM AND DWG.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 57,028 hrs · 46,042 cycles

RIGHT WING NR 5 SLAT OTBD SIDE LOWER SURFACE DELAMINATED. REPAIRED NR 5 SLAT IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 727B) · airframe 57,028 hrs · 46,042 cycles

LONGITUDINAL FLOOR SUPPORT UPPER CHORD CRACKED AT BS 727B, RBL 24.8. R & R CHORD IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

RT FRAME CHORD CRACKED AT BS 727, STRINGER 27R TO STRINGER 18R. R&R CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

LT FRAME CHORD CRACKED AT BS 727, BETWEEN STRINGER 27L TO STRINGER 18L. R&R CHORD IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 57,028 hrs · 46,042 cycles

MAIN WHEEL WELL PRESSURE DECK CRACKED AT BS 664, LBL 15. REPAIRED WEB IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

RT FRAME CHORD CRACKED AT BS 727, BETWEEN STRINGER 27R TO STRINGER 18R. R&R CHORD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,028 hrs · 46,042 cycles

LT CHORD CRACKED AT BS 727, BETWEEN STRINGER 27L TO STRINGER 18L. R&R CHORD IAW EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 57,028 hrs · 46,042 cycles

MAIN WHEEL WELL PRESSURE DECK CRACKED AT BS 663.75+9.5, LBL 40.5. REPAIRED WEB IAW EO & EA.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 56,266 hrs · 45,503 cycles

LEFT ELEVATOR TAB DELAMINATED. REMOVED AND REPLACED LEFT ELEVATOR TAB PER M/M. TAB RIG CHECK IS GOOD PER M/M. FCF TO BE C/W ON NRC E989558 TAG NO: 558596 P/N ON: 65C26384-15M S/N ON: 7713M P/N OFF: S/N OFF: 396073B

Part: WIRE — DISCONNECTED (CABIN) · airframe 56,266 hrs · 45,503 cycles

AFT ENTRY DOOR EMERGENCY LIGHT INOP ABOVE FLIGHT ATTENDANT INTERCOM. RECONNECTED WIRES, OPS CHECK GOOD PER MM.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 56,075 hrs · 45,369 cycles

LAVATORY SMOKE DETECTOR SOUNDED. REMOVED AND REPLACED DETECTOR PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

STA 500D JUST BELOW STRINGER 11 LT SHEAR TIE WAS FOUND TO HAVE EXISTING CRACK IN RADIUS. REMOVED AND REPLACED SHEAR TIE AT BS 500D, FROM STRINGER S-10L AND S-13L IAW B737-300 SRM 51-40-02 AND BAC DWG.

Part: LENS — CRACKED (CABIN) · airframe 55,765 hrs · 45,142 cycles

AFT RIGHT LAV EMERGENCY LIGHT LENS IS CRACKED. REPLACED AFT RIGHT LAV EMERGENCY LIGHT LENS WITH NEW LENS INSTALLED IAW B737-300 AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 867+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 807+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

LEFT BS 827+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 7, 8. REPAIRED LEFT BS 827+10 LOWER FORWARD WINDOW CORNER IAW EA 1-353-20815 REV-, REO G15586 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 867+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

LEFT BS 847+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 9, 12. REPAIRED LEFT BS 847+10 LOWER FORWARD WINDOW CORNER IAW EA 1-353-20814 REV-, REO G15585 REVIR FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 827+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

RIGHT BS 887+10 UPPER AFT WINDOW SKIN CUTOUT HAS HFEC NOISE INDICATION AT HOLE 6 AND HFEC CRACK INDICATION AT HOLES 2, 4. REPAIRED SKIN CUTOUT IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 787+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

LEFT BS 787+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICAITON AT HOLES 1, 3, 7, 9, 10. REPAIRED LEFT BS 787+10 LOWER FORWARD WINDOW CORNER IAW EA 1-353-20817 REV- , REO G15588 REVIR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 847+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 847+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

RIGHT BS 847+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 4 , 9. REPAIRED RIGHT BS 847+10 UPPER AFT WINDOW CORNER IAW EA 1-353-20809 REV-, REO G15581 REV IR FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

RIGHT BS 807+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 9. REPAIRED RIGHT BS 807+10 UPPER AFT WINDOW CORNER IAW EA 1-353-20811 REV-, REO G15583 REV IR FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

LEFT BS 767+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 3, 8, 9. REPAIRED LEFT BS 767 +10 LOWER FORWARD WINDOW CORNER IAW EA 1-353-20818 REV 1 REO G15589 REV A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 867+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 887+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

LEFT BS 767+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 1, 2, 3, 7. REPAIRED LEFT BS 767+10 UPPER AFT WINDOW CORNER IAW EA 1-353-20819 REV-, REO G15590 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

RIGHT BS 727+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLE NR 7. REPAIRED RIGHT BS 727+10 LOWER FORWARD WINDOW CORNER IAW EA 1-353-20810 REV-, REO G15582 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 767+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

LEFT BS 887+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 4, 9, 12. REPAIRED LEFT BS 887+10 UPPER AFT WINDOW CORNER IAW EA 1-353-20813 REV-, REO G15584 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

LEFT BS 727+10 UPPER AFT WINDOW SKIN CUTOUT HAS HFEC CRACK INDICATION AT HOLE 4. REPAIRED SKIN CUTOUT IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

LEFT BS 807+10 LOWER FORWARD WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 9. REPAIRED LEFT BS 807+10 LOWER FORWARD WINDOW CORNER IAW EA 1-353-20816 REV-, REO G15587 REV IR FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 887+10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 867+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 847 +10 LOWER FORWARD WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

LEFT FUSELAGE SKIN CRACKED AT BS 807+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

RIGHT FUSELAGE SKIN CRACKED AT BS 767+10 UPPER AFT WINDOW CORNER CUTOUT. REPAIRED SKIN IAW SB.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,765 hrs · 45,142 cycles

LEFT BS 787+10 UPPER AFT WINDOW CORNER HAS HFEC CRACK INDICATION AT HOLES 2, 3, 4, 5, 6. REPAIRED LEFT BS 787+10 UPPER AFT WINDOW CORNER IAW EA 1-353-20820 REV-, REO G15591 REV IR FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: LIGHT — BROKEN (CABIN) · airframe 55,765 hrs · 45,142 cycles

MAIN CABIN RIGHT STOW BIN #19-20 DEF BULL NOSE PANEL EMERGENCY LIGHT ASSY BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM.

Part: HYDRAULIC LINE — CRACKED (NR 1 ENGINE) · airframe 55,434 hrs · 44,907 cycles

DIVERSION -- "A" SYSTEM ENG NR 1 LOW PRESS LIGHT. "A" SYSTEM ELEC 2 PUMP LIGHT REMAINED OUT THE ENTIRE EVENT. REMOVED AND REPLACED LACED HYDRAULIC LINE PER MM.

Part: SPINDLE — FAILED (TE FLAP) · airframe 55,092 hrs · 44,649 cycles

RIGHT WING NR 7 FLAP SPINDLE FAILED. REPLACED NR 7 SPINDLE PER MT.

Part: HINGE FITTING — BROKEN (LT SPOILER) · airframe 54,415 hrs · 44,138 cycles

LEFT WING NR 4 GROUND SPOILER CENTER O/B HINGE FITTING BROKEN. REMOVED AND REPLACED NR 4 SPOILER PER MM.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 53,629 hrs · 43,564 cycles

WING CENTER SECTION REAR SPAR VERTICAL STIFFENER CRACKED AT BS 663.75, LBL 6.15. REPAIRED STIFFENER PER EA.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 53,629 hrs · 43,564 cycles

WING CENTER SECTION REAR SPAR VERTICAL STIFFENER CRACKED AT BS 663.75, RBL 6.15. REPAIRED STIFFENER PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL CORRODED AT BS 767, BETWEEN STR 26L TO STR 25L. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,052 hrs · 42,526 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 707, LBL 24.5. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME INNER CHORD CRACKED AT BS 616, WL 208. REPAIRED CHORD IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 986.5, BETWEEN BBL 0 TO LBL 43. REPAIRED BEAM IAW EA AND E.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 656 T0 BS 686, LBL 24.5. REPAIRED BEAM IAW EA AND E.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND STUB BEAM FRAME CRACKED AT BS 616, WL 208. REPAIRED BEAM IAW EA.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND FORWARD CARGO DOOR SKIN CRACKED AT BS 460+13. REMOVED AND REPLACED DOOR IAW MM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM AND DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR FWD LOWER CORNER CUTOUT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR FWD LOWER CORNER CUTOUT. REPAIRED SKIN PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED BETWEEN BS 927 TO BS 947.5, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 25R TO STR 25R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 328, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 807, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME INNER CHORD CRACKED AT BS 616, STR 16L. REPAIRED FRAME PER EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 24R. REPAIRED FRAME IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 639, LBL 45.5. REPAIRED BEAM IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 767, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME PER SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT ANGLE CHANNEL CORRODED BETWEEN BS 770 TO BS 775, RBL 3.0. REMOVED AND REPLACED CHANNEL IAW EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT ANGLE CHANNEL CORRODED BETWEEN BS 770 TO BS 775, LBL 3.0. REMOVED AND REPLACED CHANNEL IAW EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO COMPARTMENT ANGLE CHANNEL CORRODED BETWEEN BS 770 TO BS 775, RBL 8.10. REMOVED AND REPLACED CHANNEL IAW EA.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULE 16Y CHECK, FOUND RT INNER FLOOR CHORD CORRODED BETWEEN BS 907+7 TO BS 1006. REMOVED AND REPLACED CHORD IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULE 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 22L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULE 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 294.5, STR 23L. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME CORRODED AT BS 500C, BETWEEN STR 27L TO STR 28L. REPAIRED FRAME IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULE 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 98.56, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULE 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 1006, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULE 16Y CHECK, FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT BS 807, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME PER SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULE 16Y CHECK, FOUND LT INNER FLOOR CHORD CORRODED BETWEEN BS 947.5 TO BS 1006. REMOVED AND REPLACED CHORD IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 19L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT FITTING CRACKED AT BS 332.1, STR 8R. REMOVED AND REPLACED FITTING IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CRACKED AT BS 526, BETWEEN STR 22R TO STR 24R. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 268, STR 23L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 526, STR 22L. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND WEB CRACKED BETWEEN BS 360 TO BS 380, STR 17R. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 12R. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK FOUND, STRINGER CLIP CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP PER SRM AND DWG.

Part: LENS — BROKEN (CABIN) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK FOUND, AFT GALLEY EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK FOUND, SUPPORT ANGLE CRACKED BETWEEN BS 277 TO BS 291, STR 13R. REMOVED AND REPLACED ANGLE PER SRM AND DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK FOUND, SUPPORT WEB CRACKED AT BS 303, BETWEEN STR 28L TO STR 27L. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK FOUND, FLOORBEAM CORRODED AT BS 967, RBL 4. REPAIRED BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,828 hrs · 42,219 cycles

DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 528 LBL 5. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,740 hrs · 42,153 cycles

DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 360+5, STR 1. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,740 hrs · 42,153 cycles

DURING SCHEDULED MV2 CHECK FOUND, CROWN SKIN CRACKED AT BS 360+6, STR 1. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,224 hrs · 41,759 cycles

DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 986+1.5, STR 7L. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,224 hrs · 41,759 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER AFT CORNER AT BS 986+1.5, STR 7L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,221 hrs · 41,758 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER AFT CORNER, BS 986+1.5, STR 7L. REPAIRED SKIN PER SRM.

Part: PROXIMITY SWITCH — FAULTY (KRUEGER FLAP) · airframe 48,957 hrs · 40,046 cycles

AIR TURNBACK - AFTER TAKEOFF, AFTER FLAP RETRACTION, NR 4 FLAP INDICATION REMAINED "FULL EXTEND" UNABLE TO VISUALLY VERIFY. REMOVED AND REPLACED NR 4 KRUEGER FLAP FULL EXTEND & FULL RETRACT PROX SWITCHES PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,349 hrs · 39,578 cycles

DURING SCHEDULED SPV, FOUND FUSELAGE SKIN CRACKED AT BS 978 TO BS 979.5, STR 5R. REPAIRED SKIN PER ER.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 46,923 hrs · 38,529 cycles

DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 666, LBL 24.5. REPAIRED BEAM PER AAR EA.

Part: FITTING — CORRODED (GIRT BAR) · airframe 46,923 hrs · 38,529 cycles

DURING SCHEDULED 14Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS PER MM.

Part: FITTING — CORRODED (GIRT BAR) · airframe 46,923 hrs · 38,529 cycles

DURING SCHEDULED 14Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,923 hrs · 38,529 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,923 hrs · 38,529 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 9R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,923 hrs · 38,529 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,923 hrs · 38,529 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,923 hrs · 38,529 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,923 hrs · 38,529 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 46,923 hrs · 38,529 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING O/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,923 hrs · 38,529 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,923 hrs · 38,529 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,923 hrs · 38,529 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,923 hrs · 38,529 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 665, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 46,923 hrs · 38,529 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,923 hrs · 38,529 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,923 hrs · 38,529 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,923 hrs · 38,529 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,923 hrs · 38,529 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,923 hrs · 38,529 cycles

DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,923 hrs · 38,529 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,923 hrs · 38,529 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,923 hrs · 38,529 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,923 hrs · 38,529 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,923 hrs · 38,529 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 8R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,923 hrs · 38,529 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 9L. REMOVED AND REPLACED CLIP PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 46,923 hrs · 38,529 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING NR 3 SLAT T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,923 hrs · 38,529 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 46,923 hrs · 38,529 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING NR 3 SLAT T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 46,923 hrs · 38,529 cycles

SUPPLEMENTAL INFORMATION - SWA CONTROL NUMBER CORRECTED. DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 46,863 hrs · 38,484 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. INSTALLED SLIDE PER MT.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 46,298 hrs · 38,067 cycles

DURING SCHEDULED SPV CHECK, FOUND LT MLG WHEEL WELL PRESSURE DECK CRACKED AT BS 664, LBL 32. REPAIRED SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 46,295 hrs · 38,066 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND LT MLG PRESSURE DECK WEB CRACKED AT BS 664, LBL 32. REPAIRED WEB PER SRM.

Part: LENS — MISSING (CABIN) · airframe 46,304 hrs · 38,070 cycles

DURING SCHEDULED 2HC1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 45,949 hrs · 37,811 cycles

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

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 44,619 hrs · 36,864 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT UPPER T/E WEDGE DELAMINATED AT I/B END. REPAIRED SLAT PER SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 44,617 hrs · 36,862 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING I/B AFT FLAP DELAMINATED AT O/B END. R&R FLAP PER MM.

Part: SKIN — PUNCTURED (LT WING TE FLAP) · airframe 44,493 hrs · 36,776 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING INBD FORE FLAP PUNCTURED. REMOVED AND REPLACED FLAP PER MM.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 44,492 hrs · 36,776 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING I/B FORE FLAP PUNCTURED THROUGH LOWER SKIN AT CENTERLINE OF FORE FLAP. REPAIRED FLAP PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,579 hrs · 36,129 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,579 hrs · 36,129 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,579 hrs · 36,129 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,579 hrs · 36,129 cycles

DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,579 hrs · 36,129 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 ENTRY DOOR LOWER HINGE SKIN CRACKED AT FASTENER HOLES. REPAIRED SKIN PER AAR EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,579 hrs · 36,129 cycles

DURING SCHEDULED SPV CHECK, FOUND L1 ENTRY DOOR UPPER HINGE SKIN CRACKED AT FASTENER HOLES. REPAIRED SKIN PER AAR EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 43,075 hrs · 35,741 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 43,075 hrs · 35,741 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 43,075 hrs · 35,741 cycles

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

Part: HOOK — LOOSE (GIRT BAR) · airframe 43,075 hrs · 35,741 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: FAN — FAULTY (E&E BAY) · airframe 43,000 hrs · 35,691 cycles

FLIGHT CREW REPORTED AN ELECTRICAL ODOR IN CABIN. TURNED OFF RECIRC FAN ODOR DISSIPATED. REMOVED AND REPLACED RECIRC FAN PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 41,235 hrs · 34,396 cycles

DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 40,890 hrs · 34,138 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 40,365 hrs · 33,723 cycles

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

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 39,939 hrs · 33,364 cycles

DURING SCHEDULED C1 CHECK, FOUND LT ELEVATOR DELAMINATED AT LOWER OUTBOARD END. REMOVED AND REPLACED ELEVATOR PER MM.

Part: SKIN — CRACKED (BS 380 S28L) · airframe 39,939 hrs · 33,364 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380 BETWEEN BL 0 AND STR 28L. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 39,102 hrs · 32,690 cycles

DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 38,907 hrs · 32,532 cycles

DURING SCHEDULED A2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: WIRE — BURNED (WINDSHIELD) · airframe 37,331 hrs · 31,333 cycles

ON DESCENT, EVIDENCE OF SMOKE COMING FROM FLIGHT COMPARTMENT R5 WINDOW. NO CRACKS NOTED ON R5 WINDOW. VERIFIED SMOKE COMING FROM BURNED WIRING ON R5 WINDOW, REMOVED AND REPLACED R5 WINDOW PER MM.

Part: GCU — MALFUNCTIONED (NR 2) · airframe 37,321 hrs · 31,327 cycles

STRONG ELECTRICAL ODOR ON TAXI OUT. REMOVED AND REPLACED NR 2 GCU PER MM.

Part: COOLING FAN — FAILED (E&E BAY) · airframe 37,311 hrs · 31,319 cycles

STRONG ELECTRICAL ODOR AFTER TAKEOFF AND DURING FLIGHT. ODOR SUBSIDED, NO SMOKE, NO ABNORMALITIES NOTED. SMELL LOCATED IN AFT REAR COCKPIT. REMOVED AND REPLACED NORMAL EQUIPMENT COOLING FAN PER MM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 37,216 hrs · 31,244 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD ENTRY DOOR LOWER HINGE BOX FITTING CRACKED. REMOVED AND REPLACED HINGE BOX FITTING PER SRM.

Part: SIGN — LOOSE (EMERGENCY EXIT) · airframe 37,216 hrs · 31,244 cycles

DURING SCHEDULED C2 CHECK, FOUND RT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: SLIDE — UNSERVICEABLE (L2 DOOR) · airframe 36,779 hrs · 30,899 cycles

L2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR DIFFICULT TO READ. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: HINGE — CRACKED (PAX DOOR) · airframe 36,403 hrs · 30,608 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE BOX CRACKED. REMOVED AND REPLACED HINGE BOX PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 36,301 hrs · 30,532 cycles

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

Part: FRAME — CRACKED (FWD CARGO) · airframe 33,681 hrs · 28,511 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR CUTOUT, AFT BOTTOM DOOR STOP FITTING. REPAIRED FRAME PER BFG ER.

Part: SHEAR TIE — CORRODED (BS 767) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 767, BETWEEN RBL 4 TO RBL 9. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: FRAME — CORRODED (BS 847) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, RBL 21. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 440) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 303) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, L1 DOOR LOWER FWD STOP FITTING CUTOUT. REPAIRED FRAME PER BFG ER.

Part: FRAME — CRACKED (BS 616) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, BELOW LT CREASE BEAM WEB. REPAIRED FRAME PER BFG ER.

Part: CREASE BEAM — CORRODED (BS 988) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE CREASE BEAM WEB CORRODED AT BS 988, RBL 48. REPAIRED CREASE BEAM WEB PER SRM.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 328, LBL 27, WL 208. REPAIRED FLOORBEAM PER SRM.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D CHECK, FOUND LT AND RT VERTICAL STAB ATTACH FITTINGS CLEVIS LUG FACES CORRODED. REPAIRED LUG FACES PER BFG ER.

Part: FRAME — CRACKED (BS 907) · airframe 33,679 hrs · 28,509 cycles

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

Part: FLOORBEAM — CORRODED (BS 986) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 65 TO RBL 65, WL 208. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (BS 400) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L TO STR 9L AND STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 727D) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 787) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (CARGO DOOR) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT FWD CARGO DOOR AFT FRAME, BOTTOM DOOR STOP CUTOUT. REPAIRED FRAME PER BFG ER.

Part: FRAME — CRACKED (BS 867) · airframe 33,679 hrs · 28,509 cycles

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

Part: FRAME — CRACKED (BS 787) · airframe 33,679 hrs · 28,509 cycles

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

Part: FRAME — CRACKED (BS 747) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 33,679 hrs · 28,509 cycles

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

Part: FRAME — CRACKED (BS 907) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (BS 847) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, RBL 21. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 294.5) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294.5, L1 DOOR UPPER CUTOUT. REPAIRED FRAME PER BFG ER.

Part: SHEAR TIE — CORRODED (BS 787) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, LBL 4. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CORRODED (BS 995) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STR CORRODED AT BS 995, STR 21R. REPAIRED STR SECTION PER SRM.

Part: SPLICE — CRACKED (BS 907) · airframe 33,679 hrs · 28,509 cycles

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

Part: CREASE BEAM — CORRODED (BS 817) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE LT CREASE BEAM CORRODED AT BS 817. REPAIRED CREASE BEAM PER SRM.

Part: SHEAR TIE — CORRODED (BS 500A) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500A, STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (BS 500) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 500, STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (BS 380) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L TO STR 9L. REPAIRED FRAME PER SRM.

Part: FRAME — CORRODED (BS 993) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 993, RBL 46, WL 208. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 360) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CORRODED (BS 787) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, LBL 18 TO RBL 18. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (BS 578) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (BS 1121) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CLIPS CRACKED AT BS 1121, STR 2L & STR 2R. REMOVED AND REPLACED CLIPS PER SRM.

Part: SHEAR TIE — CORRODED (BS 787) · airframe 33,679 hrs · 28,509 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 787, LBL 9. REPAIRED SHEAR TIE PER SRM.

Part: LIGHT — MISSING (FWD GALLEY) · airframe 33,521 hrs · 28,389 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD GALLEY SIDEWALL EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 33,521 hrs · 28,389 cycles

DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SKIN — DELAMINATED (RT WING FLAP) · airframe 29,805 hrs · 25,419 cycles

DURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD AFT FLAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 29,797 hrs · 25,413 cycles

DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 868 TO BS 886, STRINGER 1L, CRACKED. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 28,934 hrs · 24,707 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 25,631 hrs · 21,971 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT OTBD T/E AFT FLAP DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED LEFT OTBD T/E AFT FLAP PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,631 hrs · 21,971 cycles

DURING SCHEDULED 1/4D CHECK, FOUND LT SIDE CHORD CRACKED AT BS 178, WL 207 AND LBL 26. REMOVED AND REPLACED LT SIDE CHORD PER SWA ACO AND SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,631 hrs · 21,971 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 767, RBL 8 TO LBL 12. REPAIRED FLOORBEAM PER SWA RA.

Part: WINDOW — CRACKED (COCKPIT) · airframe 25,550 hrs · 21,908 cycles

DURING FLIGHT CAPTAINS L4 WINDOW SHATTERED. REMOVED AND REPLACED CAPTAINS L4 WINDOW PER MM.

Part: LENS — MISSING (ENTRY DOOR) · airframe 19,499 hrs · 16,964 cycles

FWD ENTRY DOOR EMERGENCY EXIT LIGHT MISSING LENS. INSTALLED EMERGENCY EXIT LIGHT LENS PER MM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 19,162 hrs · 16,696 cycles

DURING SCHEDULED A2 CHECK, FOUND SKIN CRACKED ON AFT CARGO DOOR AT LWR FWD CORNER. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF TOLERANCE (ENTRY DOOR) · airframe 18,339 hrs · 16,010 cycles

DURING SCHEDULED A1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE ASSY PER MM.

Part: ENGINE — FAILED (NR 2) · airframe 17,989 hrs · 15,744 cycles

INFLIGHT ENGINE SHUTDOWN, NR 2 ENGINE FAILED. BOTH ENGINES WERE STABLE HOLDING 250 KTS AT 14,000 FT. NO PRIOR WARNING INDICATIONS BEFORE FAILURE. REMOVED AND REPLACED NR 2 ENGINE ASSY PER SAM 385. PERFORMED TRIM RUN PER SAM 625 AND SAM 390, NO DEFECTS NOTED.

Part: PRESSURE SWITCH — MALFUNCTIONED (NR 2 ENGINE) · airframe 58,818 hrs · 63,496 cycles

AIR TURNBACK NR 2 ENG OIL FILTER BYPASS ILLUMINATED STEADILY. LIGHT FLICKERED WITH THROTTLE AT IDLE. OIL PRESS INDICATED NORMAL IN FLIGHT - NO DECREASE NOTED. R&R DIFFERENTIAL PRESS SWITCH PER MM, OPS CHECK GOOD.

Part: CONNECTOR — DAMAGED (OUTFLOW VAVLE) · airframe 17,502 hrs · 15,345 cycles

DECLARED EMERGENCY AT FL 370, CABIN PRESSURIZATION FAILED. COULD NOT REGAIN CABIN PRESS IN ALT MODE. REMOVED AND REPLACED OUTFLOW VALVE CONNECTORS PER MM.

Part: GUSSET — CRACKED (SERVICE DOOR) · airframe 17,312 hrs · 15,177 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR AFT LOWER GUSSET CRACKED AT OUTBOARD FASTENER. REMOVED AND REPLACED GUSSET PER T1-152-007 AND DWG 69-68854.

Part: STRINGER CLIP — CRACKED (CABIN) · airframe 17,312 hrs · 15,177 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STR CLIP CRACKED A BS 663, STR 10R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: FLOORBEAM — CORRODED (GALLEY) · airframe 17,312 hrs · 15,177 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 25 TO RBL 56. REPAIRED FLOORBEAM PER RA 1-353-2382.

Part: FLOORBEAM — CORRODED (GALLEY) · airframe 17,312 hrs · 15,177 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM AFT FLANGE CORRODED AT BS 986, RBL 24 TO RBL 48. REPAIRED FLOORBEAM PER SRM.

Part: FRAME — CRACKED (SERVICE DOOR) · airframe 17,312 hrs · 15,177 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR FWD LOWER STUB FRAME CRACKED. REPAIRED STUB FRAME PER SRM.

Part: FLOORBEAM — CORRODED (GALLEY) · airframe 17,312 hrs · 15,177 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM FWD FLANGE CORRODED AT BS 986, LBL 35. REPAIRED FLOORBEAM PER SRM.

Part: SLIDE — LOOSE (PAX DOOR)

FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. INSTALLED SLIDE ASSY PER MM.

Part: SLIDE — LOW PRESSURE (PASSENGER DOOR)

DURING SCHEDULED A2 CHECK, FOUND FWD ENTRY DOOR ESCAPE SLIDE PRESSURE BELOW LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: LIGHT — INOP (CABIN)

AFT UPPER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASH LIGHT PER MM.

Part: FAN — FAILED (AC BAY)

AT 35,000 FT, F/A NOTED A BURNT SMELL IN THE CABIN, UNABLE TO LOCATED SOURCE. DIVERTED TO TUS DUE TO SMOKE IN THE CABIN. INSPECTED AND FOUND GASPER FAN BURNT. REPLACED PER BOEING M/M.