# Service difficulty reports: GE CF6-80C2A2 A list on [GE CF6-80C2A2](https://openairdocs.org/engine/ge-cf6-80c2a2.md). Newest first. General aviation reporting is voluntary. - [SDR CA190708004](https://openairdocs.org/sdr/CA190708004.md): O-Ring · failed · Jul 7, 2019 · Airbus A310304 · Hydraulic System, Main > (CAN) PILOT CALLED OVER PHONE PATCH TO REPORT THAT THEY GOT THE ECAM MESSAGE FOR GREEN SYSTEM HYDRAULIC LOW LEVEL. THEY HAVE PERFORMED THE ECAM AND QRH, SO THE HYDRAULIC PUMPS ARE OFF, AND THE LEVEL ON THE OVERHEAD IS JUST BELOW THE GREEN AREA, AT THE BEGINNIN - [SDR CA190403011](https://openairdocs.org/sdr/CA190403011.md): Engine · stalled · Apr 2, 2019 · Airbus A310304 · Engine (Turbine/Turboprop) > (CAN) AFTER TAKE OFF ENGINE #1 ENCOUNTERED AN ENGINE STALL AT INITIAL CLIMB PASSING 1500FT, THE CREW REPORTS THAT THEY HEARD A COUPLE OF `THUMPS`, AND THEN NOTICED THE N2 DROP. THEY PERFORMED THE QRH AND THEN THE ENGINE WAS FINE, BUT THEY ONLY ATTEMPTED TO 50% - [SDR CA180925007](https://openairdocs.org/sdr/CA180925007.md): Fitting · corroded · Sep 21, 2018 · Airbus A310304 · Passenger/Crew Doors > (CAN) STRONG WHISTLE SOUND FROM RL DOOR IN CRUISE. AFTER INVESTIGATION INSIDE OF DOOR,FITTING FOUND CORRODED. FITTING REPLACED. (TC# 20180925007) - [SDR CA180910001](https://openairdocs.org/sdr/CA180910001.md): Pump · leaking · Sep 7, 2018 · Airbus A310304 · Hydraulic Pump (Electric/Engine), Main > (CAN) CREW REPORTED DURING FLIGHT: `GREEN HYD QTY SHOW LOW QTY ON THE NEEDLE GAGE QTY ON ECAM IS STEADY` LATER REPORT: `HYD LOW QTY WARNING ON ECAM1 LANDING GEAR GRAVITY EXTENTION NOSE STERING INOP` GREEN HYDRAULIC SYSTEM ENGINE DRIVEN PUMP AND CASE DRAIN FILT - [SDR CA180423016](https://openairdocs.org/sdr/CA180423016.md): Computer · false indication · Apr 21, 2018 · Airbus A310304 · Central Warning > (CAN) DURING TAKEOOF ROLL AT 80KTS ECAM ENG INDICATION REJECTED TAKEOFF AT FULL STOP ECAM FWC AMBER CRT CAUTIONS NOT AVAIL. FWC 1 REPLACED AND CHECKED SERV, IAW AMM 31-53-34 ENG TRIM TESTED SERV IAW 73-23-00. (TC# 20180423016) - [SDR CA160223002](https://openairdocs.org/sdr/CA160223002.md): Strut · faulty · Feb 22, 2016 · Airbus A310300 · Nose/Tail Landing Gear Strut/Axle > (CAN) ESTABLISHED ON FINAL FOR LANDING THE CREW SELECTED GEAR DOWN, THEY DID NOT GET A GREEN LIGHT FOR THE NOSE GEAR FROM EITHER SYS, RED LIGHTS ONLY FOR THE NOSE GEAR INDICATING AN UNSAFE GEAR SITUATION. THE CREW COMPLETED THEIR CHECKS IAW THE QRH. AN EMERG - [SDR CA151013012](https://openairdocs.org/sdr/CA151013012.md): Valve · failed · Oct 13, 2015 · Airbus A310304 · Landing Gear Brake System > (CAN) DURING PUSHBACK OF ACFT FOR DEPARTURE, THE CREW TRIED TO SET THE PARKING BRAKE. THEY WERE UNSUCCESSFULL AND A LEAK WAS NOTED IN THE MAIN WHEEL WELL AREA. PARKING BRAKE VALVE FAILED AND WAS FOUND IN 3 PIECES. HOUSING ON THE VALVE FAILED INTERNAL PLUNGER - [SDR CA151007011](https://openairdocs.org/sdr/CA151007011.md): Attach Fitting · broken · Oct 1, 2015 · Airbus A310304 · Spoilers > (CAN) LEFT WING NR 3 SPOILER BROKEN AT ACTUATOR ATTACHMENT. SPOILER WAS FREE TO MOVE EXTEND/RETRACT DURING FLIGHT. - [SDR CA150810001](https://openairdocs.org/sdr/CA150810001.md): Pump · cracked · Aug 7, 2015 · Airbus A310304 · Hydraulic Pump (Electric/Engine), Main > (CAN) CREW REPORTED HYDRAULIC FLUID ON BLUE SYS LOW LEVEL ECAM WARNING AND FAULT IN CRUISE. CREW DECLARED A PAN PAN, QRH PROCEDURE CARRIED AND ACFT DIVERTED. ACFT LANDING WAS UNEVENTFUL. MAINTENANCE INVESTIGATION FOUND THE NR 1 ENGINE BLUE SYSTEM HYD PUMP C - [SDR CA140919007](https://openairdocs.org/sdr/CA140919007.md): Battery · damaged · Sep 16, 2014 · Airbus A310304 · Emergency Lighting > (CAN) DURING ROUTINE VISIT IN AVIONIC SHOP FOR REGULAR BATTERY CHECK, THE CASE OF EPSU BATTERY WAS FOUND WITH A SMALL BURN. THE ASSY WAS OPENED AND CELLS NR 4 AND 5 WERE FOUND SHORT CIRCUITED AT THE TOP WHERE THE CONNECTING TAB IS POSITIONED. FOLLOWING TWO REA - [SDR CA140903013](https://openairdocs.org/sdr/CA140903013.md): Coffeemaker · odor · Sep 3, 2014 · Airbus A310304 · Buffet/Galleys > (CAN) CREW REPORTED FWD COFFEE MAKER BURNING ODOR IN FLIGHT. CIRCUIT BREAKER WAS PULLED AND ODOR DISSIPATED. - [SDR CA130531004](https://openairdocs.org/sdr/CA130531004.md): Switch · shorted · May 26, 2013 · Airbus A310304 · Light System Wiring > (CAN) DURING TROUBLESHOOTING OF UPPER BEACON SYSTEM C/B POPPING. C/B WAS PUSHED IN AND A NOISE WAS HEARD & SPARK CAME OUT FROM PANEL 426VU. FOUND TOGGLE SWITCH AT FAULT. TOGGLE SWITCH 2LV AT PANEL 426VU REPLACED IAW AMM 20-45-21 UPPER BEACON TEST C/O IAW AMM - [SDR CA120827017](https://openairdocs.org/sdr/CA120827017.md): Control Panel · overheated · Aug 25, 2012 · Airbus A310304 · Automatic Direction Finder (ADF) System > (CAN) DURING CRUISE FLIGHT, FLIGHT CREW REPORTED SMOKE COMING OUT OF ADF NR 2 CONTROL PANEL. ADF2 CIRCUIT BREAKER WAS PULLED BUT SMOKE CONTINUED TO COME OUT OF PANEL. PANEL WAS REMOVED AND DISCONNECTED AND SMOKE STOP FROM COMING OUT OF PANEL. PANEL IS BEING - [SDR CA120504003](https://openairdocs.org/sdr/CA120504003.md): Bulkhead · corroded · Apr 25, 2012 · Airbus A310304 · Fuselage Main, Bulkhead > (CAN) FOUND BULKHEAD AT FRAME 39, CORRODED AND PERFORATED BETWEEN STRINGERS 54-55L AND BELOW WATERLINE Z-2557. - [SDR CA120330005](https://openairdocs.org/sdr/CA120330005.md): Tank · ruptured · Mar 27, 2012 · Airbus A310304 · Potable Water System > (CAN) ACFT RETURNED TO BLOCK AFTER A LOUD BANG HEARD IN CLIMB FOLLOWED BY WATER QTY AND PRESSURE INDICATE ZERO ON FAP PANEL. ON ARRIVAL, FOUND WATER TANK RUPTURED. - [SDR CA120224006](https://openairdocs.org/sdr/CA120224006.md): Actuator · cracked · Feb 19, 2012 · Airbus A310304 · Drag Control Actuator > (CAN) CLOSE TO 90KTS, ECAM MESSAGE "SPEED BRAKE WARNING", ENGINE SETTING WAS 96 PERCENT N1, REJECTED TAKEOFF CALLED, AFTER A FEW SECONDS, A SECOND ECAM MESSAGE DISPLAYED "HYD BLUE RESERVOIR LOW LEVEL". ALSO ECAM F/CTL PG DISPLAYED "SPOILER 2 EXTENDED". ACFT - [SDR CA111116008](https://openairdocs.org/sdr/CA111116008.md): Mec · failed · Nov 12, 2011 · Airbus A310304 · Fuel Control/Turbine Engines > (CAN) AFTER NORMAL ENGINE NR 2 START, NO THROTTLE RESPONSE N1 15 PERCENT, TGT 660 DEGREES, N2 60 PERCENT, FF 0.05. NR 2 ENGINE, MAIN ENGINE CONTROL (MEC) REPLACED IAW 73-21-01 AND MADE SERVICEABLE. - [SDR CA110513007](https://openairdocs.org/sdr/CA110513007.md): Bushing · seized · May 9, 2011 · Airbus A310304 · Hydraulic Pump, Auxiliary > WHEN PERFORMING TASK 292500-16-1 (OPS CHECK OF RAT UPLOCK MECHANISM) DURING A-06 CHECK, RAM AIR TURBINE (RAT) FAILED TO DEPLOY FROM EITHER THE CAPTAINS` AND FIRST OFFICERS` RELEASE HANDLE. AFTER INVESTIGATION IT WAS FOUND THAT THE UPLOCK ROLLER ON THE RAT WAS - [SDR CA110420006](https://openairdocs.org/sdr/CA110420006.md): Cover · missing · Apr 10, 2011 · Airbus A310304 · Cargo/Baggage Doors > (CAN) UPON ARRIVAL AT DESTINATION AIRPORT IT WAS DISCOVERED THAT THE FWD CARGO DOOR FWD LOCKS COVER WAS MISSING, PANEL 811AR. SUSPECT THAT IT WAS STRUCK DURING CLOSING OF THE DOOR BY LOADING EQUIPMENT AT THE DEPARTURE AIRPORT. - [SDR CA110408004](https://openairdocs.org/sdr/CA110408004.md): Wire · damaged · Mar 22, 2011 · Airbus A310304 · Fuel System Wiring > (CAN) LEFT OUTER TANK BOOST PUMP 1 & 2 INDICATE LOW PRESS & LT INNER TANK BOOST PUMP NR 2 INDICATES LOW PRESS. FOUND WIRING DAMAGED IN LT WW JUST ON TOP OF GREEN HYD HP MANIFOLD AT FEED THROUGH NR 31VP, 6 WIRES FOUND DAMAGED & SHORTED & CUT AT SPLICE 116VS & - [SDR CA110203007](https://openairdocs.org/sdr/CA110203007.md): Panel · delaminated · Jan 19, 2011 · Airbus A310304 · Engine Thrust Reverser > (CAN) MCC CONTACTED AIRPORT AUTHORITIES REGARDING PIECE OF ALUMINUM FOUND ON THE RUNWAY POSSIBLY FROM A/C OR ANOTHER A/C THAT DEPARTED SINCE THE LAST FOD INSPECTION CARRIED OUT. MCC NOTIFIED STATION AND INSPECTION WAS CARRIED OUT, BUT NO ABNORMALITIES WERE FO - [SDR CA101223006](https://openairdocs.org/sdr/CA101223006.md): Rod End · separated · Dec 10, 2010 · Airbus A310304 · Drag Control Actuator > (CAN) DURING OVERNIGHT ROUTINE MAINTENANCE AND TROUBLESHOOTING AN OPEN MEL ITEM FOR NR 2 & 3 SPOILER FAULT THAT WAS PLACED ON MEL (SYSTEM DEACTIVATED) PRIOR TO AIRCRAFT ARRIVAL, MAINTENANCE DISCOVERED THE NR 2 RT SPOILER ACTUATOR THREADED ROD END ASSEMBLY HAD - [SDR CA101026002](https://openairdocs.org/sdr/CA101026002.md): Duct · damaged · Oct 25, 2010 · Airbus A310304 · Pneumatic Distribution System > DURING WALK AROUND, LEAK SOUND FROM NR 2 ENG - FOUND DUCT BESIDE PRSOV CRACKED. DUCT BLEED ELBOW CRACKED. DUCT HAS BEEN REPLACED. - [SDR CA100917003](https://openairdocs.org/sdr/CA100917003.md): Tube · chafed · Sep 13, 2010 · Airbus A310304 · Engine Fuel Distribution > FUEL VBV ACTUATOR TUBE AND HOSE FOUND CHAFING - PN 113254-3 (IPC 72-00-00, FIG 4, ITEM 80) ON VBV FEEDBACK CABLE. THIS CHAFING CAUSED A FUEL LEAK THAT WAS FOUND DURING THE WALKAROUND. TUBE AND HOSE FUEL VBV HAS BEEN REPLACED IAW AMM 75-32-01 AND ESM 72-00-00 - [SDR CA100630004](https://openairdocs.org/sdr/CA100630004.md): Hook · worn · Jun 22, 2010 · Airbus A310304 · Hydraulic System, Auxiliary > DURING PERFORMANCE OF MPD TASK 292500-05-1, (GENERAL INSP OF CONTROL LINKAGE FOR CORROSION AND DAMAGE), RAT FAILED TO DEPLOY FROM BOTH THE CAPT`S OR F/O`S RELEASE LEVER. PROBLEM WAS IDENTIFIED TO BE WITH THE UPLOCK ACTUATOR. A NOTCH HAD WORN IN THE HOOK ASSY - [SDR CA091109004](https://openairdocs.org/sdr/CA091109004.md): Generator · cracked · Nov 3, 2009 · Airbus A310304 · AC Generator-Alternator > (CAN) ON CHECKING APU OIL QUANTITY, MX FOUND THE APU COMPARTMENT OIL SOAKED. HSG OF THE APU GENERATOR WAS FOUND CRACKED AND LEAKING. UNIT HAS BEEN REPLACED. ## 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 = 'CF680C2A2' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/engine/ge-cf6-80c2a2/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.