GE CF6-80C2A2

Service difficulty reports · 26

Newest first. General aviation reporting is voluntary.

Query with SQL
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 = 'CF680C2A2'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CA190708004O-Ring · failed(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 BEGINNINJul 7, 2019 · Airbus A310304 · Hydraulic System, MainSDR CA190403011Engine · stalled(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%Apr 2, 2019 · Airbus A310304 · Engine (Turbine/Turboprop)SDR CA180925007Fitting · corroded(CAN) STRONG WHISTLE SOUND FROM RL DOOR IN CRUISE. AFTER INVESTIGATION INSIDE OF DOOR,FITTING FOUND CORRODED. FITTING REPLACED. (TC# 20180925007)Sep 21, 2018 · Airbus A310304 · Passenger/Crew DoorsSDR CA180910001Pump · leaking(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 FILTSep 7, 2018 · Airbus A310304 · Hydraulic Pump (Electric/Engine), MainSDR CA180423016Computer · false indication(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)Apr 21, 2018 · Airbus A310304 · Central WarningSDR CA160223002Strut · faulty(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 EMERGFeb 22, 2016 · Airbus A310300 · Nose/Tail Landing Gear Strut/AxleSDR CA151013012Valve · failed(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 PLUNGEROct 13, 2015 · Airbus A310304 · Landing Gear Brake SystemSDR CA151007011Attach Fitting · broken(CAN) LEFT WING NR 3 SPOILER BROKEN AT ACTUATOR ATTACHMENT. SPOILER WAS FREE TO MOVE EXTEND/RETRACT DURING FLIGHT.Oct 1, 2015 · Airbus A310304 · SpoilersSDR CA150810001Pump · cracked(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 CAug 7, 2015 · Airbus A310304 · Hydraulic Pump (Electric/Engine), MainSDR CA140919007Battery · damaged(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 REASep 16, 2014 · Airbus A310304 · Emergency LightingSDR CA140903013Coffeemaker · odor(CAN) CREW REPORTED FWD COFFEE MAKER BURNING ODOR IN FLIGHT. CIRCUIT BREAKER WAS PULLED AND ODOR DISSIPATED.Sep 3, 2014 · Airbus A310304 · Buffet/GalleysSDR CA130531004Switch · shorted(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 AMMMay 26, 2013 · Airbus A310304 · Light System WiringSDR CA120827017Control Panel · overheated(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 Aug 25, 2012 · Airbus A310304 · Automatic Direction Finder (ADF) SystemSDR CA120504003Bulkhead · corroded(CAN) FOUND BULKHEAD AT FRAME 39, CORRODED AND PERFORATED BETWEEN STRINGERS 54-55L AND BELOW WATERLINE Z-2557.Apr 25, 2012 · Airbus A310304 · Fuselage Main, BulkheadSDR CA120330005Tank · ruptured(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.Mar 27, 2012 · Airbus A310304 · Potable Water SystemSDR CA120224006Actuator · cracked(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 Feb 19, 2012 · Airbus A310304 · Drag Control ActuatorSDR CA111116008Mec · failed(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.Nov 12, 2011 · Airbus A310304 · Fuel Control/Turbine EnginesSDR CA110513007Bushing · seizedWHEN 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 WASMay 9, 2011 · Airbus A310304 · Hydraulic Pump, AuxiliarySDR CA110420006Cover · missing(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.Apr 10, 2011 · Airbus A310304 · Cargo/Baggage DoorsSDR CA110408004Wire · damaged(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 & Mar 22, 2011 · Airbus A310304 · Fuel System WiringSDR CA110203007Panel · delaminated(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 FOJan 19, 2011 · Airbus A310304 · Engine Thrust ReverserSDR CA101223006Rod End · separated(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 Dec 10, 2010 · Airbus A310304 · Drag Control ActuatorSDR CA101026002Duct · damagedDURING WALK AROUND, LEAK SOUND FROM NR 2 ENG - FOUND DUCT BESIDE PRSOV CRACKED. DUCT BLEED ELBOW CRACKED. DUCT HAS BEEN REPLACED.Oct 25, 2010 · Airbus A310304 · Pneumatic Distribution SystemSDR CA100917003Tube · chafedFUEL 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 72-00-00Sep 13, 2010 · Airbus A310304 · Engine Fuel DistributionSDR CA100630004Hook · wornDURING 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 ASSYJun 22, 2010 · Airbus A310304 · Hydraulic System, AuxiliarySDR CA091109004Generator · cracked(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.Nov 3, 2009 · Airbus A310304 · AC Generator-Alternator
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