N675BR

Part: STRUT — LOW (NLG) · airframe 29,980 hrs · 27,896 cycles

GEAR DISAGREE WARNING MESSAGE, NOSEGEAR DID NOT RETRACT, WOW CAUTION, WOW INPUT STATUS, NOSEWHEEL STEERING INOP CAUTION MESSAGE. (FLT 4291) CLOSED SERVICED NLG SHOCK STRUT IAW TASK CARD. PERFORMED NLG SWING IAW AMM. ALL OPS CHECKS GOOD.

Part: MOUNT — CORRODED (GALLEY) · airframe 29,085 hrs · 26,896 cycles

FWD AND AFT INBD GALLEY MOUNT PLATES COMMON TO FLOOR STRUCTURE ARE CORRODED. BOTH MOUNTING PLATES WERE REMOVED AND REPLCED IAW SRM.

Part: MOUNT — CORRODED · airframe 29,085 hrs · 26,896 cycles

AFT INBD WARDROBE MOUNT PLATE COMMON TO FLOOR STRUCTURE IS CORRODED. AFT MOUNTING PLATE WAS REMOVED AND REPLACED IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 29,085 hrs · 26,896 cycles

RIGHT CARGO FLOOR SUPPORT, BS 559+84 TO 559+114 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM. OPS CHECKED GOOD.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 29,085 hrs · 26,896 cycles

LBL 9 CARGO TRACK, BS 559 + 112 HAS CORROSION. REMOVED AND REPLACED THE CARGO TRACK IAW SRM AND AMM.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 29,085 hrs · 26,896 cycles

RBL 9 CARGO TRACK, BS 559 + 112 HAS CORROSION. REMOVED AND REPLACED THE CARGO TRACK IAW SRM.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 29,085 hrs · 26,896 cycles

LBL 9 CARGO TRACK, BS 559 + 90 TO 559 + 96 HAS CORROSION. REMOVED, AND REPLACED THE CARGO TRACK IAW REO AND AMM.

Part: CARGO TRACK — CORRODED (BS 615) · airframe 29,085 hrs · 26,896 cycles

CARGO TRACK HAS CORROSION, BS 615, LBL 9. REPLACED THE CARGO TRACK IAW AMM.

Part: SKIN — DENTED (BS 654.5) · airframe 29,085 hrs · 26,896 cycles

FUSELAGE SKIN AT BS 654.5, BETWEEN STRINGERS 20L AND 21L DENTED. REPAIRED THE SKIN IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 29,085 hrs · 26,896 cycles

RIGHT INBD FLAP VANE SKIN CHAFED ON THE INBD SIDE. INSTALLED A NEW FLAP VANE, INBD CAP IAW SRM AND REO.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 29,085 hrs · 26,896 cycles

CORROSION FOUND ON THE SERVICE DOOR SILL PLATE AFTER REMOVAL. REPLACED THE DOOR SILL IAW SRM.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 25,479 hrs · 22,972 cycles

LT INBD FLAP DENTED. REMOVED AND INSTALLED NEW SERVICEABLE LT FLAP AT WS 80.50 AND 127.25 IAW AMM.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 25,479 hrs · 22,972 cycles

RT INBD FLAP DENTED. REMOVED AND INSTALLED NEW SERVICEABLE RT FLAP AT WS 80.50 AND WS 127.25 IAW AMM.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 25,479 hrs · 22,972 cycles

FLOORBEAM ANGLE AT BS 349.5 BETWEEN LBL 41.0, LBL 30.0 HAS EVIDENCE OF CORROSION. REPLACED CORRODED FLOOR SUPPORT ANGLE, PN 601R38673-43 WITH NEW PART IAW SRM.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 25,479 hrs · 22,972 cycles

SERVICE DOOR SILL LOWER ANGLE EVIDENCE OF CORROSION. REPLACED CORRODED ANGLE WITH NEW ANGLE, IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 25,479 hrs · 22,972 cycles

RIGHT INBD FLAP VANE L/E INBD CAP CHAFED. REMOVED AND INSTALLED NEW RT INBD FLAP VANE L/E INBD CAP, PN: 601R14303-54 IAW SRM.

Part: STRUCTURE — CHAFED (LT WING AILERON) · airframe 25,479 hrs · 22,972 cycles

LEFT AILERON LOWER L/E FIXED INBD SECTION HAS CHAFING. REMOVED AND INSTALLED NEW PANEL ON LT AILERON LOWER L/E INBD FIXED POSITION IAW SRM.

Part: SKIN — CHAFED (LT WING AILERON) · airframe 25,479 hrs · 22,972 cycles

CHAFING ON LT WING AILERON PANEL 599AB. R & R. LT WING AILERON PANEL.

Part: BUSHING — GALLED (ENGINE MOUNT) · airframe 22,048 hrs · 19,512 cycles

RIGHT ENGINE FWD MOUNT LINK AND CLAMP-UP BUSHING GALLED. REMOVED RT ENGINE FWD MOUNT LINK AND CLAMP-UP BUSHING AND REPLACED WITH A SERVICEABLE LINK AND CLAMP-UP BUSHING IAW AMM.

Part: BEARING — GALLED (ENGINE MOUNT) · airframe 22,048 hrs · 19,512 cycles

RIGHT ENGINE FWD MOUNT YOKE HAS STIFF BEARINGS AND GALLED. REMOVED RT ENGINE FWD MOUNT YOKE AND REPLACED WITH A SERVICEABLE FWD MOUNT YOKE IAW AMM.

Part: BOLT — GALLED (ENGINE MOUNT) · airframe 22,048 hrs · 19,512 cycles

RT ENGINE FWD YOKE MOUNT PYLON UPPER AND LOWER BOLTS HAVE DEEP SCRATCHES AND GALLING, SERVICE REMOVED RT ENGINE FWD YOKE MOUNT PYLON UPPER AND LOWER BOLTS AND REPLACED WITH A SERVICEABLE UPPER AND LOWER BOLTS IAW AMM.

Part: HOUSING — GALLED (ENGINE MOUNT) · airframe 22,048 hrs · 19,512 cycles

RIGHT ENGINE AFT MOUNT SPHERICAL BUSHING HOUSING HAS GALLEING, SERVICE REMOVED RT ENGINE AFT MOUNT SPHERICAL BUSHING HOUSING AND REPLACED WITH A SERVICEABLE SPHERICAL BUSHING HOUSING IAW AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,003 hrs · 19,471 cycles

RIGHT NR 4 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 21,684 hrs · 19,176 cycles

CORROSION FOUND ON CARGO BAY FLOOR SUPPORT CAP FROM BS 559+112 - 621 AT LBL 27. C-CHECK, REPLACED CARGO BAY FLOOR SUPPORT IAW REO AND SRM.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 21,684 hrs · 19,176 cycles

CORROSION FOUND ON CARGO BAY FLOOR SUPPORT FROM BS 559+112 - 621 AT LBL 9. C-CHECK, REPLACED CARGO BAY FLOOR SUPPORT 9 IAW REO AND SRM.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 21,684 hrs · 19,176 cycles

INTERCOSTAL AT LBL 36.20, AFT SIDE OF PRESSURE BULKHEAD FS 621, BELOW ENGINE BOX BEAM, IS CRACKED. C-CHECK, INSTALLED INTERCOSTAL, IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 21,684 hrs · 19,176 cycles

RT INBD FLAP VANE MID-SECTION CHAFED. C-CHECK, INSTALLED NEW FLAP VANE IAW SRM.

Part: SKIN — CORRODED (RT WING) · airframe 21,684 hrs · 19,176 cycles

RIGHT LOWER WING PLANK ACCESS ORIFICE 640BB HAS LIGHT CORROSION. C-CHECK, REMOVED CORROSION IAW REO.

Part: SKIN — CORRODED (LT WING) · airframe 21,684 hrs · 19,176 cycles

LEFT LOWER WING PLANK ACCESS PANEL 510AB ORIFICE HAS LIGHT CORROSION. C-CHECK, REMOVED CORROSION FROM LT LOWER WING PLANK ACCESS PANEL ORIFICE 510AB IAW REO.

Part: SKIN — CORRODED (LT WING) · airframe 21,684 hrs · 19,176 cycles

LEFT LOWER WING PLANK ACCESS 540BB ORIFICE HAS LIGHT CORROSION. C-CHECK, REMOVED CORROSION FROM LT LOWER WING PLANK ACCESS ORIFICE IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 21,684 hrs · 19,176 cycles

LEFT INBD FLAP VANE L/E OTBD BUMPER CONTACT POINT IS CHAFED. C-CHECK, REPLACED LT FLAP VANE L/E SKIN IAW SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 21,684 hrs · 19,176 cycles

FS 280 FLOORBEAM AT LBL 9 INBD AND OTBD ANGLES ARE CRACKED. C-CHECK, REPLACED CRACKED INBD AND OTBD ANGLES IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 21,684 hrs · 19,176 cycles

LEFT INBD FLAP VANE L/E CENTER BUMPER CONTACT POINT IS CHAFED. C-CHECK, INSTALLED NEW LT INBD FLAP VANE CAP MID SECTON IAW SRM.

Part: SKIN — CHAFED (LT AILERON) · airframe 21,684 hrs · 19,176 cycles

LEFT AILERON UPPER L/E IS CHAFED FROM OTBD EDGE IN ABOUT .3333 OF L/E. C-CHECK, REPAIRED IAW REO.

Part: SKIN — CHAFED (LT MLG DOOR) · airframe 21,684 hrs · 19,176 cycles

LEFT MLG DOOR HAS A CHAFE ON THE INTERNAL SKIN AT THE DOOR L/E. C-CHECK, REPAIRED CHAFED AREA OF LT MLG DOOR REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 21,684 hrs · 19,176 cycles

RT INBD FLAP VANE L/E OTBD BUMPER CONTACT POINT IS CHAFED. C-CHECK, INSTALLED NEW RT INBD FLAP, OTBD VANE CAP IAW SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 21,684 hrs · 19,176 cycles

FS 280 FLOORBEAM RT LOWER RADIUS CRACKED AT RBL 11. C-CHECK, REPLACED DAMAGED FLOORBEAM RADIUS SECTION IAW REO.

Part: CHANNEL — CRACKED (BS 409) · airframe 21,684 hrs · 19,176 cycles

CRACK NOTED AT BS 409+128 VERTICAL POST, LBL 18 OTBD C-CHANNEL, AFT RADIUS. C-CHECK, REPLACED CHANNEL IAW SRM AND REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 21,684 hrs · 19,176 cycles

FS 280 FLOORBEAM AT RBL 9 OTBD AND INBD ANGLES ARE CRACKED. C-CHECK, REPLACED CRACKED ANGLES AT FS 280 FLOORBEAM IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,989 hrs · 17,483 cycles

FIRST OVERHEAD EMERGENCY LIGHT IS BURNED OUT. (FLT 7394) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,989 hrs · 17,483 cycles

REAR CEILING EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 4764) RELAMPED EMERGENCY LIGHT.

Part: FIXTURE — INOPERATIVE (CABIN) · airframe 19,518 hrs · 17,020 cycles

SIDEWALL LIGHTS AT ROW 3 A/B DO NOT ILLUMINATE. (C-CHECK) REPLACED LIGHT FIXTURE AT ROW 2 AND 3 A/B IAW AMM.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 19,209 hrs · 16,718 cycles

GEAR DISAGREE WARNING AND NOSE DOOR WARNINGS, AFTER QRH, GEAR CAME DOWN NORMALLY. (FLT 4659) REPLACED NOSE GEAR SELECTOR VALVE. P/N: 750006000 S/N ON: 0465T S/N OFF: 1434

Part: FAN — MALFUNCTIONED (GALLEY) · airframe 19,193 hrs · 16,699 cycles

ON APPROACH TO LAND, SMELLED STRONG BURNING ODOR IN COCKPIT DISCOVERED CIRCUIT BREAKER GALLEY FAN TRIPPED. (FLT 4732) REPLACED GALLEY FAN IAW AMM. P/N ON: AE0607D00 P/N OFF: AE0405A03 S/N ON: L0323 S/N OFF: 260

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,978 hrs · 15,504 cycles

(C-CHECK) CRACK ON THE RIGHT SIDE FS 559.0 PRESSURE BULKHEAD. REPAIRED CRACK ON THE RIGHT SIDE FS 559.0 PRESSURE BULKHEAD.

Part: ADC — MALFUNCTIONED (NR 2) · airframe 16,257 hrs · 13,955 cycles

FIRST OFFICER'S ALTITUDE FLUCTUATES +/- 100' IN LEVEL FLIGHT; VSI FLUCTUATES +/- 1000'/MIN IN LIGHT TURBULENCE. (FLT 1361) REPLACED NR 2 AIR DATA COMPUTER. P/N ON GMT4190-020 S/N OFF 1220

Part: SKIN — DENTED (FUSELAGE) · airframe 14,371 hrs · 12,241 cycles

A 3.5 INCH LONG DENT FOUND BELOW CARGO DOOR SCUFF PLATE, FS 574.00, STRINGER 18L-19L. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-3701.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 14,373 hrs · 12,241 cycles

AT FS 621.00 (REAR PRESSURE BULKHEAD) THE AREA AROUND THE CARGO DOOR LINTEL FITTING IS CRACKED. REPAIRED IAW REO 601R-53-61-1230.

Part: OIL SYSTEM — OVERSERVICED (RT ENGINE) · airframe 13,237 hrs · 11,282 cycles

ON CLIMBOUT FROM CVG RECEIVED HIGH OIL TEMP ON RIGHT ENGINE. PERFORMED QRH, EMERGENCY DECLARED, A/C RETURNED TO CVG LANDED SAFELY. INSPECTED A/C FOUND RIGHT ENGINE OIL TANK OVER SERVICED. SERVICED OIL TANK TO CORRECT LEVEL, GROUND RUNS GOOD.

Part: ACTUATOR — FAULTY (RT T/E FLAP) · airframe 9,959 hrs · 8,586 cycles

FLIGHT 4940 - FLAPS FAILED AT 0 DEGREES ON APPROACH TO YUL. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED RIGHT I/B FLAP I/B ACTUATOR.

Part: ACTUATOR — FAULTY (RT T/E FLAP) · airframe 9,959 hrs · 8,586 cycles

FLIGHT 4940 - FLAPS FAILED AT 0 DEGREES ON APPROACH TO YUL. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED RIGHT I/B FLAP O/B ACTUATOR.

Part: FLAP — MALFUNCTIONED (WING) · airframe 9,957 hrs · 8,585 cycles

FLIGHT 5492 - FLAPS FAIL CAUTION MESSAGE RECEIVED WHEN SELECTING FLAPS TO 8 DEGREES, FLAPS REMAINED AT 0 DEGREES. EMERGENCY DECLARED AND AIRCRAFT LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I001, FLAPS FAIL FIRST EVENT MAINTENANCE ACTION.

Part: FLEX DRIVE — FAULTY (T/E FLAP) · airframe 9,867 hrs · 8,517 cycles

FLIGHT 5391 - RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED LEFT SIDE NR 3 FLAP FLEX DRIVE. NO FURTHER DEFECTS.

Part: FLEX DRIVE — FAULTY (T/E FLAP) · airframe 9,867 hrs · 8,517 cycles

FLIGHT 5391- RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED LEFT SIDE NR 5 FLAP FLEX DRIVE. NO FURTHER DEFECTS.

Part: ACTUATOR — CONTAMINATED (T/E FLAP) · airframe 9,867 hrs · 8,517 cycles

FLIGHT 5391 - RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED LEFT SIDE NR 2 FLAP ACTUATOR, DUE TO WATER CONTAMINATION. NO FURTHER DEFECTS.

Part: FLEX DRIVE — FAULTY (T/E FLAP) · airframe 9,867 hrs · 8,517 cycles

FLIGHT 5391 - RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED RIGHT SIDE NR 2 FLAP FLEX DRIVE. NO FURTHER DEFECTS.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 9,492 hrs · 8,222 cycles

FLIGHT 5620 - EN ROUTE CVG-YUL RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C) FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES.

Part: ACTUATOR — FAULTY (TE FLAPS) · airframe 7,620 hrs · 6,735 cycles

FLIGHT 5425 - RECEIVED FLAP FAIL CAUTION MESSAGE. DIVERTED FROM LGA TO JFK. LANDED WITHOUT INCIDENT. REPLACED RIGHT OUTBOARD FLAP OUTBOARD ACTUATOR. NO FURTHER DEFECTS.

Part: SHAFT — DAMAGED (TE FLAPS)

EVENT SUMMARY STATED FLAPS FAIL AT 0 DEG ON APPROACH. REMOVED AND REPLACED LT FLAP FLEX SHAFT.

Part: WIRE — DAMAGED (EMERGENCY LIGHT)

AFT SECTION OF EMERGENCY LIGHTING INOP. REPLACED POWER SUPPLY CABLE AND LIGHTING STRIP.

Part: GCU — DEFECTIVE (NR 2 GENERATOR)

GENERATOR 2 TRIPPED ON TAXI OUT. MAINTENANCE REMOVED AND REPLACED GCU.

Part: FCU — FAILED (TE FLAPS)

EVENT SUMMARY STATED THAT AFTER TAKEOFF FLAP FAIL INDICATION RTF. REMOVED AND REPLACED FECU MM 27-51-05.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING INSPECTION THE PASSENGER DOOR EXTERIOR EMERGENCY LAMP WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING INSPECTION THE LEFT HAND FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 4,169 hrs · 3,525 cycles

DURING INSPECTION THE RIGHT HAND EMERGENCY EXTERIOR LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 4,169 hrs · 3,525 cycles

DURING INSPECTION A CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING INSPECTION THE RT EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND BURNT OUT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.

Part: DISPLAY — FAILED (COCKPIT)

DURING FLIGHT CREW REPORTED THE NR 2 MULTI FUNCTION DISPLAY FAILED. NO EMERGENCY WAS DECLARED AND FLIGHT LANDED UNEVENTFULLY. THE DISPLAY UNIT WAS IDENTIFIED AS THE CAUSE OF THE FAULT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING MAINTENANCE INSPECTION, AN INTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LINE — LEAKING (HYD SYSTEM)

DURING THE CLIMB, THE CREW REPORTED THAT THE HYDRAULIC NR 3 PRESSURE DROPPED TO ZERO WITH A GEAR DISAGREE MESSAGE AND A "HYD3A" MESSAGE. THE FLIGHT RETURNED TO ORD, LANDED WITHOUT FURTHER INCIDENT, AND WAS TOWED TO THE GATE. MAINTENANCE PERSONNEL REMOVED AND REPLACED A HYDRAULIC BRAKE LINE. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.