# Service difficulty reports: GE CF6-80C2A5

A list on [GE CF6-80C2A5](https://openairdocs.org/engine/ge-cf6-80c2a5.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 164 reports

- [SDR FDEA202404180470](https://openairdocs.org/sdr/FDEA202404180470.md): Bleed Valve · failed · Apr 18, 2024 · N683FE · Airbus A300F4605R · Compressor Bleed Valve
  > ON 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.
- [SDR FDEA202208181996](https://openairdocs.org/sdr/FDEA202208181996.md): Engine · smoke · Aug 18, 2022 · N675FE · Airbus A300F4605R · Engine (Turbine/Turboprop)
  > AT 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,
- [SDR FDEA202106171561](https://openairdocs.org/sdr/FDEA202106171561.md): Engine · failed · Jun 17, 2021 · N679FE · Airbus A300F4605R · Turbine Engine Oil System
  > AT 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 3
- [SDR FDEA202102180410](https://openairdocs.org/sdr/FDEA202102180410.md): Bleed Valve · faulted · Feb 18, 2021 · N732FD · Airbus A300B4605R · Compressor Bleed Valve
  > CLIMBING 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 KI
- [SDR FDEA2020080541766](https://openairdocs.org/sdr/FDEA2020080541766.md): Bolt · failed · Aug 4, 2020 · N667FE · Airbus A300F4605R · Turbine Engine Compressor Section
  > VBV 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.
- [SDR FDEA202007301718](https://openairdocs.org/sdr/FDEA202007301718.md): Coupling · failed · Jul 30, 2020 · N663FE · Airbus A300F4605R · Pneumatic Distribution System
  > DURING 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, RU
- [SDR FDEA2020060321106](https://openairdocs.org/sdr/FDEA2020060321106.md): Engine · failed · Jun 2, 2020 · N732FD · Airbus A300B4605R · Engine (Turbine/Turboprop)
  > AFTER 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 WITH
- [SDR FDEA2020022420371](https://openairdocs.org/sdr/FDEA2020022420371.md): Engine · leaking · Feb 22, 2020 · N657FE · Airbus A300F4605R · Engine (Turbine/Turboprop)
  > PDIS 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 DIVERTE
- [SDR FDEA201703020769](https://openairdocs.org/sdr/FDEA201703020769.md): Mec · failed · Mar 2, 2017 · N733FD · Airbus A300B4622R · Fuel Controlling System
  > DURING 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. ACCOMPLI
- [SDR FDEA201409052463](https://openairdocs.org/sdr/FDEA201409052463.md): Switch · defective · Sep 5, 2014 · N658FE · Airbus A300F4605R · Engine Thrust Reverser
  > ON 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.
- [SDR FDEA201311022669](https://openairdocs.org/sdr/FDEA201311022669.md): Turbine · damaged · Nov 2, 2013 · N733FD · Airbus A300B4605R · Turbine Section
  > ENROUTE, 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.
- [SDR FDEA201208042844](https://openairdocs.org/sdr/FDEA201208042844.md): Door · out of adjust · Aug 4, 2012 · N732FD · Airbus A300B4605R · Passenger/Crew Doors
  > ON 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 MAKI
- [SDR FDEA201203281158](https://openairdocs.org/sdr/FDEA201203281158.md): Pressure Switch · failed · Mar 28, 2012 · N733FD · Airbus A300B4605R · Engine Oil Indicating System
  > IN-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 AMM
- [SDR FDEA201106092172](https://openairdocs.org/sdr/FDEA201106092172.md): Blades · damaged · Jun 9, 2011 · N732FD · Airbus A300B4605R · Turbine Engine Compressor Section
  > ON 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, ALO
- [SDR FDEA201012044594](https://openairdocs.org/sdr/FDEA201012044594.md): Line · leaking · Dec 4, 2010 · N731FD · Airbus A300F4605R · Hydraulic System, Main
  > HYD 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 R
- [SDR FDEA201007152515](https://openairdocs.org/sdr/FDEA201007152515.md): Indicator · failed · Jul 15, 2010 · N732FD · Airbus A300B4605R · Engine EGT/TIT Indicating System
  > ENROUTE 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.
- [SDR FDEA200906031908](https://openairdocs.org/sdr/FDEA200906031908.md): Engine · leaking · Jun 3, 2009 · N732FD · Airbus A300F4605R · Turbine Engine Oil System
  > ON 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,
- [SDR CA090522001](https://openairdocs.org/sdr/CA090522001.md): Hose · leaking · May 16, 2009 · Airbus A310300 · Hydraulic System, Main
  > (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.
- [SDR CA090514004](https://openairdocs.org/sdr/CA090514004.md): Display · smoke · May 7, 2009 · Airbus A310300 · Central Warning
  > (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.
- [SDR FDEA200903210981](https://openairdocs.org/sdr/FDEA200903210981.md): Wire Harness · failed · Mar 21, 2009 · N655FE · Airbus A300F4605R · Engine Oil System Wiring
  > AT 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 M
- [SDR FDEA200812265299](https://openairdocs.org/sdr/FDEA200812265299.md): Unknown · unknown · Dec 26, 2008 · N686FE · Airbus A300F4605R · Engine Fuel and Control
  > LEVEL 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
- [SDR AALA200803046](https://openairdocs.org/sdr/AALA200803046.md): Fan Blade · damaged · Dec 6, 2008 · N14077 · Airbus A300B4605R · Turbine Engine Compressor Section
  > LIM 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 T
- [SDR AALA200802527A](https://openairdocs.org/sdr/AALA200802527A.md): Fan Blade · bird ingestion · Nov 17, 2008 · N80058 · Airbus A300B4605R · Turbine Engine Compressor Section
  > INFLIGHT - 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 OPE
- [SDR CA080804001](https://openairdocs.org/sdr/CA080804001.md): Flasher · burned · Jul 31, 2008 · Airbus A310304 · Exterior Lighting
  > (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. PART
- [SDR CA080728005](https://openairdocs.org/sdr/CA080728005.md): Circuit Breaker · burned · Jul 21, 2008 · Airbus A310300 · Fuel System Wiring
  > (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 CAMP
- [SDR AALA200801370](https://openairdocs.org/sdr/AALA200801370.md): Fuel Filter · dirty · May 22, 2008 · N14061 · Airbus A300B4605R · Engine Fuel Distribution
  > MCO 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 INCIDENT
- [SDR AALA200800484](https://openairdocs.org/sdr/AALA200800484.md): Pressure Switch · inoperative · Mar 3, 2008 · N70073 · Airbus A300B4605R · Engine Fuel Distribution
  > BWI 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.
- [SDR CA080213001](https://openairdocs.org/sdr/CA080213001.md): Generator · cracked · Feb 8, 2008 · Airbus A310 · AC Generator-Alternator
  > (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)
- [SDR CA071127002](https://openairdocs.org/sdr/CA071127002.md): Coffeemaker · sparks · Nov 21, 2007 · Airbus A310300 · Buffet/Galleys
  > (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)
- [SDR CA071127001](https://openairdocs.org/sdr/CA071127001.md): Pump · cracked · Nov 20, 2007 · Airbus A310304 · Hydraulic Pump (Electric/Engine), Main
  > (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. PUMP
- [SDR 07FDEA04371](https://openairdocs.org/sdr/07FDEA04371.md): Regulator Valve · failed · Sep 28, 2007 · N657FE · Airbus A300F4605R · Engine Thrust Reverser
  > DURING 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. R
- [SDR CA070731001](https://openairdocs.org/sdr/CA070731001.md): Seal · leaking · Jul 27, 2007 · Airbus A310300 · Fuel Controlling System
  > (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 SEA
- [SDR AALA20071228](https://openairdocs.org/sdr/AALA20071228.md): Bearing · leaking · Jul 2, 2007 · N19059 · Airbus A300B4605R · Turbine Engine Oil System
  > MIA - 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.
- [SDR 07FDEA01660](https://openairdocs.org/sdr/07FDEA01660.md): Engine · bird ingestion · Apr 29, 2007 · N667FE · Airbus A300F4605R · Engine (Turbine/Turboprop)
  > HIGH 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 STILL
- [SDR CA070411002](https://openairdocs.org/sdr/CA070411002.md): Switch · sticking · Apr 5, 2007 · Airbus A310304 · Landing Gear Retraction/Extension System
  > (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
- [SDR CA070404004](https://openairdocs.org/sdr/CA070404004.md): Hose · punctured · Apr 4, 2007 · Airbus A310304 · Hydraulic System, Main
  > (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 DRAIN
- [SDR CA061121001](https://openairdocs.org/sdr/CA061121001.md): Engine · failed · Nov 19, 2006 · Airbus A310304 · Engine (Turbine/Turboprop)
  > (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 OU
- [SDR AALA20061067](https://openairdocs.org/sdr/AALA20061067.md): Wheel · out of balance · Nov 14, 2006 · N8067A · Airbus A300B4605R · Wheel/Ski/Float
  > INFLIGHT 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. REPLACED
- [SDR AALA20060961](https://openairdocs.org/sdr/AALA20060961.md): Engine · malfunctioned · Oct 30, 2006 · N14065 · Airbus A300B4605R · Engine (Turbine/Turboprop)
  > JFK 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.
- [SDR CA060906006](https://openairdocs.org/sdr/CA060906006.md): Warning System · multiple ind · Sep 3, 2006 · Airbus A310304 · Central Warning
  > (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. AIRCRAFT
- [SDR 06FDEA2650](https://openairdocs.org/sdr/06FDEA2650.md): Ecu · malfunctioned · Jul 21, 2006 · N665FE · Airbus A300* · Fuel Control/Turbine Engines
  > AFTER 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-
- [SDR CA060502002](https://openairdocs.org/sdr/CA060502002.md): Wire · burned · Apr 27, 2006 · Airbus A310304 · Electrical Power System Wiring
  > (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 W
- [SDR CA060502003](https://openairdocs.org/sdr/CA060502003.md): Wire · burned · Apr 22, 2006 · Airbus A310304 · Light System Wiring
  > (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 PRECAUTIONAR
- [SDR 06FDEA0812](https://openairdocs.org/sdr/06FDEA0812.md): Hydraulic Line · chafed · Feb 23, 2006 · N671FE · Airbus A300* · Hydraulic System, Main
  > PDIS 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 IN
- [SDR 06FDEA0813](https://openairdocs.org/sdr/06FDEA0813.md): Gcu · faulty · Feb 23, 2006 · N682FE · Airbus A300* · DC Regulator
  > PDIS 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 GEN
- [SDR AALA20060072](https://openairdocs.org/sdr/AALA20060072.md): Pump · failed · Jan 30, 2006 · N70054 · Airbus A300B4605R · Engine Fuel Pump
  > JFK 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. SYSTE
- [SDR AALA20050711](https://openairdocs.org/sdr/AALA20050711.md): Duct · contaminated · Oct 27, 2005 · N70079 · Airbus A300B4605R · Cabin Cooling System
  > AFTER 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 PR
- [SDR 05FDEA03488](https://openairdocs.org/sdr/05FDEA03488.md): Smoke Detector · malfunctioned · Oct 25, 2005 · N679FE · Airbus A300F4605R · Fire Detection
  > INTERMITTENT 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.
- [SDR AALA20050623](https://openairdocs.org/sdr/AALA20050623.md): Engine · bird ingestion · Sep 26, 2005 · N7076A · Airbus A300B4605R · Engine (Turbine/Turboprop)
  > MIA 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. SYSTE
- [SDR 05FDEA02326](https://openairdocs.org/sdr/05FDEA02326.md): Support Bracket · cracked · Aug 8, 2005 · N671FE · Airbus A300* · Nacelle/Pylon Miscellaneous Structure
  > NR 1 ENG HYDRAULIC CASE DRAIN LINES SUPPORT BRACKET CRACKED ACCESS THRU 473CL PNL.

Next page: https://openairdocs.org/engine/ge-cf6-80c2a5/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/engine/ge-cf6-80c2a5/reports

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