GE CF6-80C2A5

Service difficulty reports · 164

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE engine_model_key = 'CF680C2A5'
  ORDER BY difficulty_date DESC"

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SDR FDEA202404180470Bleed Valve · failedON DEPARTURE PASSING 3000 FT RECEIVED ECAM ALERT BLEED HP VALVE FAULT NR 1. REFERENCED QRH BLEED VALVE FAULT. RESET OF HP BLEED VALVE UNSUCCESSFUL. RECEIVED BLEED HP VALVE STUCK OPEN. BLEED HP VALVE RESET. WITH MEL ON THE BLEED VALVE 2 RETURNED TO AFW. Apr 18, 2024 · N683FE · Airbus A300F4605R · Compressor Bleed ValveSDR FDEA202208181996Engine · smokeAT CRUISE WE NOTICED SOME SORT OF SMOKE IN THE COCKPIT. DECLARED EMERGENCY AND DIVERTED TO PIT. NO SMOKE INDICATOR LIGHTS. EMERGENCY DECLARED. NR 1 ENGINE REMOVED AND REPLACE. COALESCER SOCKS REMOVED AND REPLACED & O2 SERVICED. PERFORMED ENGINE RUNS PER JRH,Aug 18, 2022 · N675FE · Airbus A300F4605R · Engine (Turbine/Turboprop)SDR FDEA202106171561Engine · failedAT CRUISE ECAM INDICATION OF OIL FILTER CLOG FOR NR 1 ENGINE. PROCEEDED IAW ECAM AND SHUT THE MOTOR DOWN AFTER THREE MINUTES UNSUCCESSFULLY TO GET THE WARNING TO EXTINGUISH. RETURN TO KAFW FOR UNEVENTFUL SINGLE ENGINE APPROACH AND LANDING. APPROXIMATELY 3Jun 17, 2021 · N679FE · Airbus A300F4605R · Turbine Engine Oil SystemSDR FDEA202102180410Bleed Valve · faultedCLIMBING OUT OF KIND AT 9000 FT GOT BLEED VALVE 1 FAULT. COMPLIED WITH ECAM AND TRIED A RESET OF BLEED VALVE. RESET WAS UNSUCCESSFUL. FOLLOWED ECAM AND QRH PROCEDURES FOR BLEED VALVE FAULT. PACK 2 WAS MEL D INOP, AIRCRAFT WAS UNPRESSURIZED, RETURNED TO KIFeb 18, 2021 · N732FD · Airbus A300B4605R · Compressor Bleed ValveSDR FDEA2020080541766Bolt · failedVBV UNISON RING BOLTS AT POSITION 7,8,9 OCLCOCK, TORQUE STRIPE HAS BEEN COMPROMISED SHGN 04AUG20 07:13 TORQUE CHECKED GOOD ON BOLTS #7 AND# 9 BOLTS NEED TORQUE STRIPE. BOLT # 8 MOVED DURING TORQUE CHECK. #8 BOLT REQUIRES REMOVAL AND NEW BOLT INSTALLED.Aug 4, 2020 · N667FE · Airbus A300F4605R · Turbine Engine Compressor SectionSDR FDEA202007301718Coupling · failedDURING DEPARTURE, ECAM FOR HIGH NAC 250 DEG C, TROUBLSHOT NR 2 ENG IAW QRH. NO CHANGE WITH THROTTLE MOVE OR BLEED VALVE OFF. REACHED TOP OF CLIMB FL290 & TEMP DID NOT REDUCE, LOWEST 215, ONCE THROTTLE FWD 240 DEG AT 290. RETURNED TO DEPART, NR 2 MOTORED, RUJul 30, 2020 · N663FE · Airbus A300F4605R · Pneumatic Distribution SystemSDR FDEA2020060321106Engine · failedAFTER TOUCHDOWN IN KMEM NR 1 ENGINE BEGINE TO ROLL BACK & SHUT DOWN. AFTER TAXING IN ONTO THE RAMP, RAMP TWR & ANOTHER AIRCRAFT LET US KNOW THERE WERE FLAMES EXTINDING OUT ABOUT 40 FEET. WE PROCEDED TO SHUT ENG DOWN & PULLED THE FIRE HANDLE & CONTINUED WITHJun 2, 2020 · N732FD · Airbus A300B4605R · Engine (Turbine/Turboprop)SDR FDEA2020022420371Engine · leakingPDIS 657 26-12 2254 22FEB20 MCI OPEN U LOGPAGES:3134646 AT CRUISE EXPERIENCED SMOKE AND FUMES IN COCKPIT AND (CABIN.) WHILE RUNNING QRH CHECKLIST, RECEIVED INTERMITTENT ECAM "MIN EQ BAY SMOKE", AND "MAIN DECK CARGO SMOKE". IMMEDIATELY DIVERTEFeb 22, 2020 · N657FE · Airbus A300F4605R · Engine (Turbine/Turboprop)SDR FDEA201703020769Mec · failedDURING CRUISE, DESCENT, AND LANDING, THE NR 2 ENGINE LAGGED TARGET POINTER BY 20% N1. BOTH WITH AUTO THROTTLES ON AND OFF. THE NR 2 ENGINE N1 STUCK AT 92.4 % IN CRUISE. FOLLOWED QRH. REMOVED AND REPLACED THE NR 2 ENGINE MEC IAW AMM 73-21-01-04. ACCOMPLIMar 2, 2017 · N733FD · Airbus A300B4622R · Fuel Controlling SystemSDR FDEA201409052463Switch · defectiveON DEPARTURE ENG NR 2 REV PRESSURIZED ECAM WARNING, PRIOR WRITE UP. DID NOT RESET REVERSER ON MEL. REPLACED THE LT AND RT CDU SWITCH ASSYS PER M/M.Sep 5, 2014 · N658FE · Airbus A300F4605R · Engine Thrust ReverserSDR FDEA201311022669Turbine · damagedENROUTE, NR 2 ENGINE STARTED A SEVERE VIBRATION, COMPLIED WITH JRH. PRECAUTIONARY SHUTDOWN. DIVERTED. REMOVED AND REPLACED NR 2 ENGINE DUE TO TURBINE DAMAGE IAW 64T0712-2. LEAK AND OPS CHECKED NORMAL. IAW JRH RUN COMPLETED.Nov 2, 2013 · N733FD · Airbus A300B4605R · Turbine SectionSDR FDEA201208042844Door · out of adjustON CLIMB OUT, AT 29,000 R1 FWD ENTRY DOOR ECAM ALERTED DOOR NOT CLOSED. JUMPSEATER REPORTED DOOR CHIME WAS SOUNDING AND DOOR LOCKS WERE INDICATING "HALF" LOCKED & HALF OPEN. DECENDED TO 10,000 SLOWLY. NO PRESSURE PROBLEMS NOTED. FOUND UPPER HOOKS NOT MAKIAug 4, 2012 · N732FD · Airbus A300B4605R · Passenger/Crew DoorsSDR FDEA201203281158Pressure Switch · failedIN-FLIGHT ENG NR 1 SHUTDOWN DUE TO ENG OIL CLOG LIGHT WOULD NOT GO OUT. REF FIM 79-00-20, FIG 109. PERFORMED INSPECTION CHECK OF MASTER CHIP DETECTOR IAW AMM CH 79-22-03-06-0. CHIP DETECTOR WITHIN PARTICLE LIMITS. R & R SCAVENGE OIL FILTER ELEMENT IAW AMMMar 28, 2012 · N733FD · Airbus A300B4605R · Engine Oil Indicating SystemSDR FDEA201106092172Blades · damagedON CLIMBOUT, HEARD VERY LOUD BANG, ACFT YAWED RT AND NR 2 ENGINE SPOOLED DOWN, NO RED ECAM. NR2 ENG FLUCUATED AT IDLE WITH HIGH EGT FOR ABOUT 30 SECS. ECAM SHOWED NR2 OVERLIMIT BUT GAUGES DID NOT SHOW ANY. ENGINE STABILIZED AT IDLE, LT IT RUNNING THERE, ALOJun 9, 2011 · N732FD · Airbus A300B4605R · Turbine Engine Compressor SectionSDR FDEA201012044594Line · leakingHYD YELLOW RESERVIOR LO LEVEL - ECAM QTY AND OVERHEAD GAUGE INDICATIONS SHOWED YELLOW SYS QTY. DECLARED TO RED DOT. YELLOW PUMP LO PRESS WITH SUBSEQUENT LOSS OF YELLOW SYS COMPONENTS FACT. HYD LINE FOUND LEAKING TO THE AILERON SERVO CONTROL, LINE HAS BEEN RDec 4, 2010 · N731FD · Airbus A300F4605R · Hydraulic System, MainSDR FDEA201007152515Indicator · failedENROUTE CAPT NOTICED NR2 EGT POINTER BELOW THE ZERO POSITION. DIGITAL READOUT SHOWED (4) GREEN DASHES. R & R NR2 EGT INDICATOR IAW MM 77-21-21-04-0. OPS CHECK GOOD, RAN NR2 ENGINE IAW JRH CHAP 5, ALL INDICATIONS GOOD. ACFT OK TO CONTNIUE FOR SERVICE.Jul 15, 2010 · N732FD · Airbus A300B4605R · Engine EGT/TIT Indicating SystemSDR FDEA200906031908Engine · leakingON TAKEOFF ROLL JUMP SEATERS DETECTED AN OIL ODOR AND SAW HAZY SMOKE. NOT ELECTRICAL, BUT IRRITATING. DURING CLIMB AND RETURNED TO MEM, ODOR DISSAPATED. 15 INCH OIL PUDDLE UNDER NR 2 ENGINE. COMPLETED INSTALLATION OF NR 2 ENGINE REF WORK CARD 64T0712-2, Jun 3, 2009 · N732FD · Airbus A300F4605R · Turbine Engine Oil SystemSDR CA090522001Hose · leaking(CAN) AFTER LANDING, DURING TAXI, THE GREEN HYD FLUID HAS BEEN LOST. THE ACFT HAS BEEN TOWED TO THE GATE. HOSE HAS BEEN REPLACED ON LT MLG DRAG BRACE. HYD SYS HAS BEEN BLED AND ACFT RETURNED TO SERVICE.May 16, 2009 · Airbus A310300 · Hydraulic System, MainSDR CA090514004Display · smoke(CAN) CREW DETECTED SMOKE IN FLIGHT DECK. DETERMINED IT WAS COMING FROM THE TCAS DISPLAY UNIT. ODOR DISSIPATED WHEN THE CIRCUIT BREAKER FOR TCAS MONITOR WAS PULLED. MONITOR LEFT DE-ACTIVATED UNDER MEL 34-35 WHILE PART ON ORDER.May 7, 2009 · Airbus A310300 · Central WarningSDR FDEA200903210981Wire Harness · failedAT TOP OF DESCENT NR 2 ENG OIL PRESS INDICATED 0 PSI ON ECAM AND MECHANICAL GAUGE. SHUT DOWN ENGINE. WINDMILLED FOR 33 MINUTES INDICATING 0 OIL PRESSURE OIL TEMPS MATCHED PRIOR TO SHUTDOWN. REMOVED AND REPLACED NR 2 ENG OIL PRESSURE HARNESS (224W9722) IAW MMar 21, 2009 · N655FE · Airbus A300F4605R · Engine Oil System WiringSDR FDEA200812265299Unknown · unknownLEVEL CRUISE AT FL 250, ENG 2 FUEL CLOG LIGHT CAME ON WITH ASSOCIATED ECAM ALERT. REDUCED ENG 2 POWER TO IDLE IAW ECAM. STARTED RETURN TO MEM. AFTER 7-8 MINS AT IDLE, LIGHT WENT OUT AND STAYED OUT THROUGHOUT APPROACH AND LANDING USING NORMAL POWER. REPEAT Dec 26, 2008 · N686FE · Airbus A300F4605R · Engine Fuel and ControlSDR AALA200803046Fan Blade · damagedLIM INFLIGHT, DURING TAKEOFF BIRDS INGESTED INTO NUMBER ONE ENGINE. CREW REPORTED ENGINE INDICATIONS OF FLUCTUATION. RETURNED TO LIM AND LANDED WITHOUT INCIDENT. FOUND FAN BLADE DAMAGE AND INLET COWLING DAMAGE. REPLACED ALL FAN BLADES AND ACCOMPLISHED A TDec 6, 2008 · N14077 · Airbus A300B4605R · Turbine Engine Compressor SectionSDR AALA200802527AFan Blade · bird ingestionINFLIGHT - AT ROTATION CREW REPORTED LOUD BANG AND VIBRATION FROM NUMBER TWO ENGINE DUE TO BIRDSTRIKE. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE ON 21NOV AT JFK DUE TO BLADE AND FAN CASE DAMAGE. SYSTEM GROUND CHECKED NORMAL OPENov 17, 2008 · N80058 · Airbus A300B4605R · Turbine Engine Compressor SectionSDR CA080804001Flasher · burned(CAN) UPPER SLOWER BEACON AND STROBE LIGHTS INOP. FOUND FLASHER UNIT U/S (RECEPTACLE CONNECTOR BURNED & PARTIALLY MELTED INSIDE). CONNECTING ELECTRICAL PLUG INSULATION SLIGHTLY BURNED AND PINS DAMAGED. CONNECTOR P/N E0052R14B15SNE AND TIMER UNIT REPLACED. PARTJul 31, 2008 · Airbus A310304 · Exterior LightingSDR CA080728005Circuit Breaker · burned(CAN) DURING TROUBLESHOOTING OF THE INOPERATIVE LT OUTER TANK FUEL PUMP (DEACTIVATED IAW MEL) THE CIRCUIT BREAKER 3QA WAS FOUND BURNED, BODY CRACKED AND ONE LEG MISSING. CIRCUIT BREAKER WAS REPLACED AND SYS TESTED SERVICEABLE. A DETAILED VISUAL INSPECTION CAMPJul 21, 2008 · Airbus A310300 · Fuel System WiringSDR AALA200801370Fuel Filter · dirtyMCO INFLIGHT T1075/22MAY. NR TWO ENGINE FUEL CLOG LIGHT ILLUMINATED. FOLLOWED FUEL CLOG PROCEDURE AND INDICATION EXTINGUISHED. APPLIED TAKEOFF POWER AND LIGHT ILLUMINATED AGAIN. REDUCED POWER AND LIGHT WENT OUT. RETURNED TO MCO AND LANDED WITHOUT INCIDENTMay 22, 2008 · N14061 · Airbus A300B4605R · Engine Fuel DistributionSDR AALA200800484Pressure Switch · inoperativeBWI INFLIGHT T613/03MAR JFK TO MIA - NUMBER TWO ENGINE FUEL FILTER CLOG LIGHT ILLUMINATED. LANDED BWI WITHOUT INCIDENT. REPLACED THE NUMBER TWO ENGINE FUEL FILTER AND FUEL FILTER DIFFERENTIAL PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION.Mar 3, 2008 · N70073 · Airbus A300B4605R · Engine Fuel DistributionSDR CA080213001Generator · cracked(CAN) DURING TROUBLESHOOTING FOR HIGH OIL CONSUMPTION ON THE APU, FOUND A 7 INCHES CRACK ON THE GENERATOR HOUSING. THE IDG WAS REPLACED AND THE UNIT WAS SENT TO THE VENDOR FOR INVESTIGATION. (TC NR 20080213001)Feb 8, 2008 · Airbus A310 · AC Generator-AlternatorSDR CA071127002Coffeemaker · sparks(CAN) DURING FLIGHT, THE F/A REPORTED THE FWD COFFEE MAKER/WATER BOILER OVERHEATING AND NOTICED SOME SPARK COMING FROM THE UNIT. THE UNIT WAS DEACTIVATED. THE UNIT WAS REPLACED BY MAINTENANCE AND ROUTED TO THE REPAIR SHOP FOR INVESTIGATION. (TC NR 20071127002)Nov 21, 2007 · Airbus A310300 · Buffet/GalleysSDR CA071127001Pump · cracked(CAN) DURING CRUISE, THE YELLOW HYD SYS OVERHEAT ECAM MESSAGE CAME ON. LATER THE HYD RESERVOIR (LO LEVEL) WARNING CAME ON THE ECAM. NORMAL QRH PROCEDURE WAS PERFORMED. DURING INVESTIGATION, MAINT FOUND YELLOW HYD PUMP LEAKING. HYD PUMP CASING WAS CRACKED. PUMPNov 20, 2007 · Airbus A310304 · Hydraulic Pump (Electric/Engine), MainSDR 07FDEA04371Regulator Valve · failedDURING TAKEOFF ROLL BELOW APPROX 60 KNOTS ENG NR 1 REV PRESSURIZED AT APPROX 80 PERCENT N1. REJECTED TAKEOFF. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 08OCT07. REACTIVATED NR 1 REVERSER, PERFORMED OPS CHECK, NO DEFECTS NOTED. RSep 28, 2007 · N657FE · Airbus A300F4605R · Engine Thrust ReverserSDR CA070731001Seal · leaking(CAN) DURING TAXI-IN AT THE GATE, A LARGE FUEL LEAKAGE WAS OBSERVED COMING FROM THE HMU FUEL DRAIN BELOW NR 2 ENGINE. ENGINE WAS SHUTDOWN, BUT LEAKAGE CONTINUED. NR 2 ENGINE FIRE HANDLE WAS PULLED AND LEAKAGE STOPPED. FOUND LEAKAGE WAS FOM THE MEC SHAFT SEAJul 27, 2007 · Airbus A310300 · Fuel Controlling SystemSDR AALA20071228Bearing · leakingMIA - IMMEDIATELY AFTER TAKEOFF SMOKE ALARMS SOUNDED AND SMOKE REPORTED IN THE CABIN. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. ACCOMPLISHED RIGHT ENGINE CHANGE DUE TO OIL LEAK AT NUMBER ONE BEARING. SYSTEM GROUND CHECKED NORMAL OPERATION.Jul 2, 2007 · N19059 · Airbus A300B4605R · Turbine Engine Oil SystemSDR 07FDEA01660Engine · bird ingestionHIGH SPEED REJECT CLE 24L AT 135 KTS. A SEAGULL WENT IN THE NR 2 ENG FOLLOWED BY A HEAVY VIBRATION. NR 2 ENG INDICATIONS APPEARED NORMAL AFTER STOPPING THE AIRCRAFT. [SUP 05-04-07] REPLACED 5 EA. 1ST. STG. FAN BLADES PER MM 72-21-00-4-05. SPINNER STILLApr 29, 2007 · N667FE · Airbus A300F4605R · Engine (Turbine/Turboprop)SDR CA070411002Switch · sticking(CAN) DURING CLIMB THE AIRCRAFT HAD A (KRUGER) FAULT ECAM WARNING.QAH CARRIED OUT BUT WARNING REMAINED ON. AIRCRAFT RETURNED TO THE STATION. DURING TROUBLESHOOTING THE BITE TEST ON THE SFCC 1 AND 2 FAULTED THE RT RETRACT SWITCH. THE SWITCH WAS FOUND DIRTY AND Apr 5, 2007 · Airbus A310304 · Landing Gear Retraction/Extension SystemSDR CA070404004Hose · punctured(CAN) GREEN HYDRAULIC ECAM MESSAGE LOW LEVER WARNING CAME ON AFTER TAKE OFF. ON ARRIVAL, MAINTENANCE FOUND THE RT MAIN LANDING GEAR DOWN LOCK ACTUATOR FLEX LINE HOSE LEAKING. FOUND HOLE IN FLEX LINE. FLEX LINE WAS REPLACED WITH BOTH HYDRAULIC PUMPS, CASE DRAINApr 4, 2007 · Airbus A310304 · Hydraulic System, MainSDR CA061121001Engine · failed(CAN) AFTER TAKE OFF AND DURING LEVEL AT 40,000 FT CREW GOT ECAM MESSAGE MIN EQUIPMENT SMOKE WITH OVERHEAD WITH OVERHEAD LIGHT ON AND ODOR IN THE CABIN AND COCKPIT. CREW DECIDED TO RETURN BACK TO THE AIRPORT. QRH PROCEDURES WERE FOLLOWED. BOROSCOPE CARRIED OUNov 19, 2006 · Airbus A310304 · Engine (Turbine/Turboprop)SDR AALA20061067Wheel · out of balanceINFLIGHT T1700/14NOV AT LIFT OFF AIRCRAFT BEGAN TO VIBRATE. LANDING GEAR WAS LT DOWN. 2 TO 4 MINUTES LATER VIBRATION GRADUALLY STOPPED. GEAR WAS LT DOWN FOR DURATION OF FLIGHT. LANDED WITHOUT INCIDENT. FOUND NR 1 MAIN WHEEL ASSEMBLY OUIT OF BALANCE. REPLACEDNov 14, 2006 · N8067A · Airbus A300B4605R · Wheel/Ski/FloatSDR AALA20060961Engine · malfunctionedJFK INFLIGHT T837/30 OCT - AFTER TAKEOFF THE AFT LAVATORY FIRE SMOKE ALARM WENT OFF. FLIGHT ATTENDANT REPORTED SOMETHING BURNING IN AFT LAVATORY. ALSO REPORTED A GRINDING MOTOR SOUND WHEN THE SMOKE DISSIPATED. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. Oct 30, 2006 · N14065 · Airbus A300B4605R · Engine (Turbine/Turboprop)SDR CA060906006Warning System · multiple ind(CAN) AT 50 KNOTS, FLIGHT CREW REJECTED TAKE OFF DUE TO NAV ADC, GPS DISAGREE WARNING. DURING TAXI TO THE GATE, FAULT CLEARED IT`S SELF. FMS WAS RESET IAW MM, GPS, IRS AND FM POSITIONAL FOUND MATCHING. AUTO FLIGHT SYSTEMS TESTED AND FOUND SERVICEABLE. AIRCRAFTSep 3, 2006 · Airbus A310304 · Central WarningSDR 06FDEA2650Ecu · malfunctionedAFTER TAKEOFF APPROXIMATELY AT 500' AGL, GOT A MASTER CAUTION ECAM MESSAGE FOR FADEC 2 FAULT. COMPLIED WITH CHECKLIST. RETURNED TO KMEM BECAUSE OF KBTR SHORT RW AND CAUTION ABOUT OVERBOOST WITH REVERSE THRUST. REMOVED AND REPLACED NR 2 ENGINE ECU REF A300-Jul 21, 2006 · N665FE · Airbus A300* · Fuel Control/Turbine EnginesSDR CA060502002Wire · burned(CAN) DURING ROUTINE INSPECTION, FOUND THE ELECTRICAL OUTLET WIRE FIN 8ME CHAFED ON FRAME 17 BETWEEN STR 28 AND 29 RT SIDE. THE GROMMET PROTECTION HAD FALLEN OFF FROM THE FRAME AND WIRE WAS HANGING ON THE FRAME WITH THE RESULT OF ARCING AND FRAME DAMAGE. THE WApr 27, 2006 · Airbus A310304 · Electrical Power System WiringSDR CA060502003Wire · burned(CAN) DURING AIRCRAFT TOWING, THE NAV 2 POSITION LIGHT CB POPPED. UNABLE TO RESET. DURING INVESTIGATION, FOUND THE 4 WIRES FROM THE LIGHT UNIT ASSY (7LA) BURNED ABOUT 8 INCHES LONG. WIRING WAS REPLACED AND LIGHT ASSEMBLY AND RELAY WERE REPLACED AS PRECAUTIONARApr 22, 2006 · Airbus A310304 · Light System WiringSDR 06FDEA0812Hydraulic Line · chafedPDIS 671 29-11 0007374 22FEB06 OAK OPEN R LOGPAGES: 01086620 ECAM ALERT AT FL320 GREEN HYD SYS QNT LOW ALERT. MANUAL GEAR EXTENSION ACCOMPLISHED. FLUID DRIPPING FROM NR1 ENG RESEARCHING. FOUND 2 HYDR LINES LEAKING THAT HAD BEEN CHAFED THROUGH AT A CLAMP INFeb 23, 2006 · N671FE · Airbus A300* · Hydraulic System, MainSDR 06FDEA0813Gcu · faultyPDIS 682 24-30 0004948 22FEB06 MEM CLOSE R LOGPAGES: 01107636 GEN NR1 FAULT AFTER TAKEOFF WOULD NOT RESET. APU WAS INOP (ON MEL) FACT 23FEB06 07:18 MEM R VERIFIED NR 1 ENGINE IDG OIL SERVICED PROPERLY. PERFORMED BITE TEST OF THE GPCU. FAULTED LT GENFeb 23, 2006 · N682FE · Airbus A300* · DC RegulatorSDR AALA20060072Pump · failedJFK INFLIGHT T1473/30JAN, RIGHT HAND FUEL FILTER LIGHT ILLUMINATED DURING CLIMB. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. RIGHT HAND ENGINE FUEL FILTER PULLED AND INSPECTED. FOUND METAL PARTICLES IN FILTER. REPLACED RIGHT HAND ENGINE FUEL PUMP. SYSTEJan 30, 2006 · N70054 · Airbus A300B4605R · Engine Fuel PumpSDR AALA20050711Duct · contaminatedAFTER LANDING GEAR EXTENSION THERE WAS A SLIGHT ODOR OF PLASTIC AND SMOKE DETECTORS 2R AND 4R WERE ALARMING. LANDED WITHOUT INCIDENT. REPLACED GREEN, BLUE, AND YELLOW HYD PRES CHECK VALVES AT RESERVOIRS, APU PRESSURIZATION LINE ISOLATION CHECK VALVE, ENGINE PROct 27, 2005 · N70079 · Airbus A300B4605R · Cabin Cooling SystemSDR 05FDEA03488Smoke Detector · malfunctionedINTERMITTENT AVIONICS SMOKE WARNING. DID NOT SMELL ANY SMOKE. REMOVED AND REPLACED AVIONICS SMOKE DETECTOR 11WA IAW A 300 MM 26-15-12-4. OPS CHECKS GOOD. SERVICEABLE PART CANNED FROM ACFT 653 MFG CG7GO-11. SN ON AB1058 SN OFF 1021. SERVICEABLE TAG B55383. Oct 25, 2005 · N679FE · Airbus A300F4605R · Fire DetectionSDR AALA20050623Engine · bird ingestionMIA INFLIGHT T903/26SEPT - NR 2 ENGINE INGESTED A BIRD DURING CLIMB. EXPERIENCED SOME VIBRATION WITHIN LIMITS. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. PERFORMED BIRD STRIKE INSPECTION AND BOROSCOPE. REPLACED THREE FAN BLADES AND RIGHT TRANSCOWL. SYSTESep 26, 2005 · N7076A · Airbus A300B4605R · Engine (Turbine/Turboprop)SDR 05FDEA02326Support Bracket · crackedNR 1 ENG HYDRAULIC CASE DRAIN LINES SUPPORT BRACKET CRACKED ACCESS THRU 473CL PNL.Aug 8, 2005 · N671FE · Airbus A300* · Nacelle/Pylon Miscellaneous Structure
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