GE CF6-80C2B6F
Service difficulty reports · 1,456
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 = 'CF680C2B6F' 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.
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 = 'CF680C2B6F' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UIEA2015012800045Clamp · missingENGINE 1 INBD REAR OIL SUM LINE MISSING CLAMP LOCATED JUST ABOVE FIRE LOOP AFT SECTION. INSTALLED NEW CLAMP IAW AMM 20-10-11.SDR UIEA2015012800050Filter · damagedNUMBER 1 ENG MAIN FUEL FILTER HOUSING & FILTER HEAD THREADS ARE DAMAGED. R & R IAW AMM 73-11-08. LEAK CHECK ACCOMPLISHED ON TASK CARD 8007 ITEM 14.SDR UIEA2015010400001Blade · bentRIGHT ENG FAN BLADE BENT ON POST FLIGHT. INSPECTED NR 2 ENG, FOUND LE DISTORTION BLADES 21, 22 & 23 FIRST STAGE FAN. ALL DISTORTIONS WITHIN LIMITS IAW AMM 72-31-02-226-019 STEP 1 M.SDR CA141229005Power Supply · failed(CAN) AIRCRAFT LOST THE FIRST OFFICER`S FLIGHT DIRECTOR, COMMAND BARS LOST AND AUTOLAND STATUS TO NO LAND 3 THE CREW ALSO HAD A FAINT ELECTRICAL ODOR IN THE COCKPIT. ELECTED TO DIVERT AND DECLARED AN EMERGENCY. RT FCC FOUND TO HAVE A BURNED OUT POWER SUPSDR CA141229006Hose · ruptured(CAN) ARRIVED WITHOUT ISSUE AFTER THE AIRCRAFT EXPERIENCED A LOSS IN HYDRAULIC PRESSURE. RESOLUTION MAINTENANCE CREW FOUND LT HYDRAULIC FLEX LINE BETWEEN RUDDER RATIO CHANGER AND MODULE LEAKING. LINE REPLACED IAW 27-21-15 PB 201 AND AMM 20-10-10.SDR CA141212004Module · failed(CAN) CREW REPORTED LOSS OF HYDRAULIC PRESSURE IN THE CENTRE HYDRAULIC SYSTEM. ATC WAS ADVISED. STATION WAS ADVISED. MTC WAS ADVISED. A PAN PAN PAN WAS DECLARED. ATC GAVE AC117 AN EXTENDED DOWNWIND WHILE THE CREW WENT OVER THE HYDRAULICS SYSTEM PROCEDURES. MTCSDR CA141128001Module · failed(CAN) AIR RETURN DUE TO FLAP DISAGREE, PAN PAN DECLARED, OVERWEIGHT LANDING. RESOLUTION CENTER FLAP/STABILIZER POSITION MODULE M839 REPLACED AND FUNCTION CHECKED OK, REF AMM 27-58-01, PB 401. SEE L5171130 FOR RECTIFICATION OF THE SYSTEM 2 NOSE GEAR AIR/GROUNSDR UIEA2014103100532Clamp · crackedNUMBER 1 ENG LT SIDE TURBINE CASE COOLING DUCT RETAINING STRAP CLAMP CRACKED JUST AFT OF STARTER DUCT. REPLACED NR 1 ENG LT SIDE TURBINE CASE COOLING DUCT RETAINING STRAP CLAMP IAW AMM 20-11-00.SDR UIEA2014101300490Fuel Filter · faultedSTATUS MSG DISPLAY RT ENG FUEL FILTER. R & R RT ENG FUEL FILTER IAW MM 73-11-02 601. OPERATIONS CHECKED NORMAL.SDR CA140929001Idg · unserviceable(CAN) AIR RETURN FOR ENGINE GENERATOR UNSERVICEABLE. IDG REMOVED IAW J/C B767-24-11-01-004-001-04-0-A60A, NEW IDG INSTALLED IAW J/C B767-24-11-01-404-002-04-0-3D42, IDG OIL SYSTEM FLUSHED IAW AMM 12-13-03-301.SDR CA140826024Oil System · leaking(CAN) DURING THE ATLANTIC CROSSING, OIL BEGAN TO DIMINISH ON THE RIGHT ENGINE. QUANTITY FELL TO ZERO AND THE DECISION WAS MADE TO HAVE THE FLIGHT DIVERTED. A PAN WAS DECLARED. THE FLIGHT LANDED WITHOUT FURTHER EVENT AND THE ENGINE WAS SHUT DOWN IMMEDIATELY AFTSDR CA140822009Coffeemaker · odor(CAN) AFTER DEPARTURE, AN ACRID ODOR HAD RETURNED ON THE ACFT. THE CREW ELECTED TO RETURN WHERE A PAN WAS DECLARED AND AN OVERWEIGHT LANDING WILL BE CARRIED OUT. ERS WILL BE RESPONDING. MAINTENANCE CONTROL, DUTY PILOT AND CORP SAFETY ADVISED. RESOLUTION ARSDR CA140821006Coffeemaker · odor(CAN) PAN PAN DECLARED WITH ATC FOR PRIORITY HANDLING ON ARRIVAL IAW BURING ODOR FROM MID GALLEY. ESTIMATED LANDING WEIGHT, 144,500 KGS. FOUND COFFEEMAKER IN MID GALLEY AT POSITION 6416 CIRCUIT BREAKER POPPED. MAINTENANCE STAFF REMOVED THE COFFEEMAKER AND SDR UIEA2014081300397Eec · faultyENGINE NR 1 EEC SWITCHES TO ALTERNATE ON START. WILL NOT OPERATE IN NORMAL SETTING. R & R NR 1 ENG EEC IAW AMM 73-21-15.SDR CA140714009Power Supply · failed(CAN) DURING TAKEOFF ROLL AN AURAL FIRE WARNING BEGAN TO CHIME, THERE WERE NO OTHER INDICATIONS. AFTER TALKING TO MAINTENANCE THE CREW ELECTED TO RETURN TO NRT AND LAND APPROXIMATELY 25 500KG OVERWEIGHT. NO PANPAN OR MAYDAY DECLARED. RESOLUTION: PERFORMED WEUSDR CA140703006Slat System · malfunctioned(CAN) DURING APPROACH, ACFT HAD AN L/E FLAP DISAGREE LIGHT ILLUMINATE, CREW INITIATED A GO AROUND. CHECKLIST WAS COMPLETED AND FLIGHT LANDED ON SECOND ATTEMPT WITHOUT FURTHER INCIDENT. FLIGHT LEG FAULTS SHOW 301 RT L/E. OPS TEST OF FLAP/SLAT SYSTEM CARRIEDSDR CA140703008Hmu · malfunctioned(CAN) 45 MINS AFTER DEPARTURE, LEVEL CRUISE, RT ENGINE AUTO DECELERATED. ACFT YAWED THE THE RT. N2 WAS OBSERVED AT 52 PERCENT THEN THE ENGINE AUTO ACCELERATED BACK TO NORMAL PARAMETERS. REPLACED RT ENG HMU IAW T/C B767-73-21-14-004-001-00-H-FBAA AND T/C B76SDR CA140617003Antenna · failed(CAN) WEATHER RADAR FAILURE AFTER TAKEOFF, RETURNED. LANDING WEIGHT APPROXIMATELY 167.0K. EMERGENCY DECLARED WITH ATC DUE POSSIBILITY OF OVERHEATING BRAKES. EMS STANDING BY. MOC INFORMED. WEATHER RADAR ANTENNA MOUNT REPLACED. ANTENNA WAVEGUIDE SWITCHING USDR CA140613001Circuit Card · failed(CAN) ON TAXI-IN, FLIGHT CREW RECEIVED AN AURAL FIRE WARNING. CONTINUED TO THE GATE, CRF WAS CALLED TO THE ACFT FOR PRECAUTIONARY REASONS. RAMP CREW WERE KEPT CLEAR, AND CRF CLEARED ACFT WITHOUT INCIDENT. MASTER WARNING MODULE, M618 REPLACED IAW AMM 31-51-0SDR IPXA2014062083288Engine · damagedENCOUNTERED ABIRD STRIKE TO THE NR 1 ENGINE. CREW DECLARED AN EMERGENCY. RETURNED TO DEPARTURE. R & R RT ENGINE IAW WAN 2171049, TC 6002 AND TC 6001.SDR UIEA2014051300177Guide Vane · delaminatedENG 2 OUTLET GUIDE VANE, AFT OF FAN, AT 0900 POSITION, NEEDS LE TAPE. INSPECTION FINDS DELAMINATION WITHIN ALLOWED LIMITS IAW AMM 72-33-00. APPLIED REPAIR WITH APPROVED TAPE IAW AMM 72-33-00-228-046-H00.SDR UIEA2014051300178Blade · erodedENG 2 FAN BLADES LE TOWARD TIP HAVE EROSION. BLENDED SMALL NICKS AT VARIOUS FAN ROTOR BLADES ON ENG 2 IAW 72-31-02, NO FURTHER DEFECTS NOTED.SDR CA140502003Autopilot Sys · failed(CAN) SHORTLY AFTER TAKEOFF, FLIGHT CREW UNABLE TO ENGAGE AUTO-PILOT. FLIGHT HAD DEPARTED WITH 1 INOPERATIVE ON MEL, BUT APPARENT FAILURE OF ALL 3 OCCURRED. WORKED WITH MOC FOR POSSIBLE RE-SETS, BUT UNABLE. RETURNING TO STATION, AND IS EXPECTED TO LAND APPROXSDR UIEA2014041100144Engine · defectiveNR 2 ENG FAILED BORESCOPE IAW JOB CARD A-72-307-C1-2. R & R NR 2 ENG.SDR UIEA2014040100136Shutoff Valve · failedSTATUS MESSAGE ILLUMINATED ON RT IDG VALVE . REPLACED IDG AIR OIL HEAT EXCHANGER AIR SHUTOFF VALVE IAW AMM 24-11-07.SDR CA140327007Actuator · damaged(CAN) FLIGHT DEPARTED AND CREW HAD WHAT FELT LIKE AN ENGINE FAILURE ON THE RT SIDE, ALL ENGINE PARAMETERS NORMAL. ACFT WAS STILL YAWING AND SHOWED 9 UNITS OF RUDDER TRIM. MOC AND DISPATCH CONSULT WITH FLIGHT. DUTY PILOT CALLED AND BRIEFED BUT DUE TO POOR WEASDR UIEA2014032200125Valve · leakingLT ENG DRAIN MAST DRIPPING FUEL, FOLLOWED LINE TO TCC VLV. R & R LPTCC VLV IAW AMM 75-24-01 206. COMPLIED WITH TEST 12, EEC, ECU ACTUATORS IAW AMM 71-00-00 PP 593, NO LEAKS, LPTCCV FULL TRAVEL OBSERVED.SDR UIEA2014021700070Indication Sys · malfunctionedLEFT & RT PIMU MAINT MESSAGE. ACCOMPLISHED FIM71-01 FAULT TREE 810 CLEARED FAULT 155.15 A/B T25 SENSE DISAGREE & RT PIMU FAULT 352-15 A/B T25SENSOR DISAGREE FAULT ISOL PERFORMED, PIMU GND TEST IAW AMM 77-35-00 201NO FAULTS PRESENT OR RECORDED.SDR IPXA2014021781960Hmu · malfunctionedATB INSPECTION, NR 2 ENGINE POWER REDUCTION SHOWING 300 LBS AT CLIMB POWER, REMOVED RT THRUST LEVER, ENGINE DID NOT RESPOND, IAW AMM 73-21-14-401. REPLACED RT ENGINE HMU & PERFORMED ENGINE RUN PAGE BLOCK 71-00-00/501 CONFIG 3. FUNCTIONED NORMAL. LEAK CHECKEDSDR CA140206004Pneumatic System · malfunctioned(CAN) ECAM CABIN ALTITUDE DURING THE CLIMB. BOTH ENGINE BLEED PRESSURES REMAINED BELOW 20PSI, INSUFFICIENT TO PRESSURIZE CABIN. CREW REQUESTED DESCENT AND STARTED THE APU, SHORTLY THEREAFTER THE ENGINE BLEED SYS STARTED WORKING NORMALLY. AFTER CONSULTATION SDR NOCA2014011625Power Supply · failedL2 AND R2 THRESHOLD EMERGENCY EXIT SIGNS FAIL TO ILLUMINATE DURING TEST. TROUBLESHOT EMERGENCY LIGHT IAW FIM 33-51-00, REPLACED POWER SUPPLY N1395 IAW MM 33-51-07. OPS CKD NORMAL.SDR NOCA2014011224Battery Pack · dischargedEMERGENCY EXIT LIGHTS AT L1 AND L2 DOORS INOPERATIVE. R & R BATTERY PACK IAW MM 33-51-07. OPS CHECKED NORMAL.SDR CA140121003Ring · rotated(CAN) TROUBLESHOOTING LOG BOOK REPORT L4870735 REPEAT OF LT BRAKE GRINDING NOISE ABV 10 KTS ON LANDING AND TAXI, FOUND NR 2 BRAKE ASSY HEAT SHIELD BROKEN FROM BRAKE ASSY. APPEARS HEATSHIELD ATTACHMENTS BROKEN AND FOUND RUBBING BETWEEN BRAKE ASSY AND WHEEL ASSSDR NOCA2013122321Software · corruptedBOTH CDU'S HAVE ERRONEOUS DISPLAYS IN FLIGHT. UNABLE TO EXECUTE. PERFORMED OPS CHECK OF THE FMC IAW AMM 34-61-00, NO FAULTS NOTED. NEW FLT PLAN INPUT TO FMC WITH NO ISSUES NOTED. ACFT OK FOR SERVICE.SDR UIEA2013121500604Fuel Filter · faultedRIGHT ENG FUEL FILTER MESSAGE. R & R FUEL FILTER ELEMENT & LEAK CHECKED IAW AMM 73-11-02 OK.SDR UIEA2013121300599Valve · leakingFUEL DRIPPING FROM NR 1 ENG DRAIN MAST, FUEL DIRECT TUBE AFTER STATIC AIRCRAFT ENG RUN UP AT A RATE OF 7 DROPS PER MINUTE. DEFERRED TO MDDR 44901, FOUND FUEL TO BE COMING FROM THE TCC PORT OF THE LPT ACC VLV. LEAK RATE IS ACCEPTABLE FOR DISPATCH IAW AMM 71-7SDR CA131212007Indication Sys · failed(CAN) QTY OIL INDICATOR FOR NR 1 ENGINE WENT TO ZERO AND THE OIL PRESSURE STARTED DECREASING. THE CREW SHUTDOWN NR 1 ENGINE AND RETURNED TO POINT OF DEPARTURE.SDR CA131105008Unknown · odor(CAN) AT APPROXIMATELY 0150Z, IN CRUISE, AT FL340 THE CREW EXPERIENCED A FUME LIKE ODOR "STINKY SOCKS " NOT AN ELECTRICAL BURNING ODOR. THE CREW DAWNED THE COCKPIT O2 MASKS FOR 5 MINS TILL THE FUMES DISSIPATED. A PHONE PATCH BETWEEN DISPATCH, ACFT AND MOC WASDR CA131017001Oven · failed(CAN) SMOKE ODOR IN MID GALLEY. BREAKERS PULLEY, ODOR DISSIPATED. NO FOOD OR PLASTIC IN OVENS, APPEARS TO BE IN WIRING. SMOKE ODOR FROM OVEN CONTROLLER, TOP OF OVEN VENT AND BACK OF THE OVEN. OVEN FAN MOTOR CHECKED , THERE IS BLACK MARKER IN IT. GALLEY WISDR NOCA20131008013Stiffener · crackedRIGHT WING L/E RIB LOWER TEE STIFFENER WS512 IS CRACKED. REMOVED AND REPLACED RT WING LOWER RIB CORD AT W/S 512 IAW SRM 51-40-02.SDR NOCA2013100314Web · crackedINTERNAL L/E WEB AT L/E WS 516 CRACKED INBD OF REPAIR ON UPPER FLANGE. REPLACED INTERNAL L/E WEB AT W/S 516 IAW SRM 51-70-13 AND 51-40-02 PARA 4 AND PARA 7.SDR NOCA20131008011Stiffener · crackedRIGHT WING L/E RIB LOWER TEE STIFFENER WS 530 IS CRACKED. REMOVED, FABRICATED AND INSTALLED LOWER TEE STIFFENER AT RIGHT WING WS 530 IAW SRM 51-40-02 AND DWG 114T2707.SDR NOCA20131008012Mount · crackedNR 2 PYLON IS CRACKED ON INBD MOUNTING FLANGE FOR THE AFT STRUT FAIRING PANEL 447DB. CRACK MEASURES 6" LONG. R & R NEWLY FABRICATED NR 2 PYLON MOUNTING FLANGE IAW SRM
51-40-02, DWG 313T3380 USING 2024T3, .063.SDR CNMA20131004001Frame · corrodedCORROSION ON LOWER FAN CASE FRAME FROM 5 TO 7 O`CLOCK POSITION BLENDED AND FOUND TO BE OUT OF LIMITS. R & R FAN CASE.SDR NOCA201310010010Angle · crackedNOSE WHEEL WELL RT VERTICAL ANGLE CRACKED. REPAIRED IAW SRM 51-70-12.SDR NOCA201310150009Rib · crackedLEFT WING OF SLAT STATION RIB LOWER SUPPORT ANGLE HAS A TWO INCH CRACK. REMOVED AND REPLACED RIB IAW SRM 51-40-02.SDR NOCA201310010008Rib · crackedLEFT WING LEADING EDGE RIB AT OSS 531 CRACKED. R & R RIB IAW SRM 51-40-02.SDR NOCA201310010007Skin · crackedLEFT WING L/E PANEL SPLICE CRACKED. FABRICATED NEW SPLICE PLATE AND INSTALLED, ALODINE, AND PRIMED IAW DWG 114T2800, SRM 51-40-02 AND 51-20-01.SDR NOCA201310010006Rib · crackedLEFT WING L/E RIB 549.75 HAS .2500 CRACK FWD. R & R RIB IAW SRM 51-40-02.SDR DALA13042881601Oil System · failedRT ENGINE OIL QTY DECREASED TO ZERO, OIL PRESSURE DECREASED TO RED INDICATION. IAW QRH AND MCC, PERFORMED A PRECAUTIONARY SHUTDOWN AND DIVERTED. FOUND TAILPIPE, NR 2 ENG, FULL OF OIL. OPENED FAN COWLS THRUST REVERSER AND CORE COWLS. CHECKED CHIP DETECTORS,
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