GE CF6-80C2D1F
Service difficulty reports · 536
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 = 'CF680C2D1F' 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 = 'CF680C2D1F' 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 FDEA202012183186Sensor · making metalAFTER TAKEOFF PASSING 1000', 5 IN SUCCESSION LOUD BANGS WITH HEAVY SHUTTERS. ENGINE INDICATIONS APPEARED NORMAL AND THERE WAS NO YAW ASSOCIATED WITH THE BANG/SHUTTERING. DURING NR 2 ENGINE INLET AND EXHAUST INSPECTION FOUND LEFT HAND FAN STATOR AFT INNER SEGSDR 9WGA2020121041501Warning Message · illuminatedAIR RETURN DUE TO LEVEL 3 ENGINE 2 ANTI-ICE DUCT ALERT.SDR FDEA202011282983Engine · failedPASSING THROUGH APPROX 1000 FEET DURING INITIAL CLIMB OUT AIRCRAFT BEGAN TO LURCH ACCOMPANIED BY A LOUD BANGING NOISE. THIS A/C WAS PREVIOUSLY WRITTEN UP AFTER A REJECTED T/O DUE TO THE NR 3 ENGINE COMPRESSOR STALLING. THE CREW INITIATED A SHUTDOWN OF THE NRSDR IPXA2020112162625Rivet · looseINSPECTION TYPE: 4C NR 2 ENGINE INLET NOSE COWL LIP HAS NUMEROUS LOOSE AND WORKING RIVETS. REPAIRED NR 2 ENGINE INLET NOSE COWL LIP LOOSE AND WORKING RIVETS, IAW VT-SAA EA 011-7110-01-A8735 REV IR AND UPS EO MD11-7110-78559-A. (MINOR)SDR IPXA2020112162628Fitting · gougedINSPECTION TYPE: 4C NR 3 ENGINE OUTBOARD FAN COWL FWD MOUNT FITTING IS GOUGED. REPAIRED GOUGED NR 3 ENGINE OUTBOARD FAN COWL FWD MOUNT FITTING, IAW VT-SAA EA 011-7110-01-A8699 REV IR AND UPS EO MD11-7110-78456-A. (MINOR)SDR IPXA2020101061145Angle · crackedINSPECTION TYPE: 2C NR 2 ENGINE LT T/R FWD CASCADE FRAME SUPPORT ANGLE CRACKED AT 9 O`CLOCK POSITION. REPLACED CRACKED ANGLE AT NR 2 ENGINE LT T/R FWD FRAME SUPPORT, IAW SRM 51-31-01 (MINOR).SDR 9WGA2020091644201Unknown · smokeENG OIL SMELL AND SMOKE IN COCKPIT AIR RETURN, PACK 2 DISAG.SDR 9WGA2020091105301Engine · power lossTANK 2 PUMPS OFF DURING CRUISE, FOLLOWED BY ENG 2 RPM LOW. SELECTED MAN AND RELIT ENGINE.SDR FDEA202008242009Engine · damagedPDIS 593 72-51 3549 24AUG20 MEM OPEN U LOGPAGES:3355273 PASSING FL 310 FOR 340 ON INITIAL CLIMBOUT, AIRCRAFT SUDDENLY STARTED VIBRATING CONSIDERABLY #3 ENG EVM SHOWED AMBER BOX 5.0 BUT ALL OTHER INDICATIONS NORMAL. REDUCED POWER, VIBRATION ISDR 9WGA2020072321201Compressor · vibrationNR 2 ENGINE COMPRESSOR VIBRATION HIGH 5.0 NOT CORRECTABLE, STRONG RUDDER PEDAL VIBRATION AND HAD TO REDUCE POWER.SDR IPXA2020072438141Inlet · crackedINSPECTION TYPE:2C, NR 2 ENGINE INLET COWL CRACKS BETWEEN FASTENERS REQUIRES PERMANENT REPAIR.REPAIRED CRACKED #2 ENGINE INLET COWL BETWEEN FASTENERS IAW MD-11 SRM 54-10-01 REPAIR 4. (MINOR)SDR IPXA2020042954740Sense Line · looseINSPECTION TYPE:3CREJECTED TAKEOFF DUE TO ASYMMETRICAL ENGINE ACCELERATION.FOUND PT2 AND PT5 LINES LOOSE ON THE ENGINE EEC. TIGHTENED LINES AND PERFORMED ENG. RUNS,REF AMM 71-02-03-700-800. ENG. RUNS ARE GOOD.SDR IPXA2020052055529Frame · gougedINSPECTION TYPE:2C#3 ENGINE O/B CORE COWL LOWER AFT FRAME IS GOUGED.REMOVED AND REPLACED GOUGED #3 ENGINE O/B CORE COWL LOWER AFT FRAME IAW MD-11 SRM 54-01-42. (MINOR)SDR 9WGA2020041601Pump · unknownENGINE 2 (RPM LOW) AUTO SHUTDOWN NO VIB NOTED, AFTER ENG #2 SHUTDOWN IN FLIGHT NOTED ALL PUMPS OFF ON #2 TANK.SDR IPXA2020041554221Hinge Fitting · chafedINSPECTION TYPE:3C#1 ENG. I/B FAN COWL UPPER FWD. DOOR HINGE FITTING IS CHAFED.REPAIRED CHAFED #1 I/B FAN COWL IAW VT-SAA EA 011-7110-001-A8065 REV. I/R AND UPS EO MD11-7110-75947-A. (MINOR)SDR IPXA2020041554222Hinge Fitting · chafedINSPECTION TYPE:3C#3 ENG. L/H FAN COWL HAS CHAFE DAMAGE ON THE UPPER FWD. DOOR HINGE FITTING.REPAIRED CHAFED #3 ENG. L/H FAN COWL IAW VT-SAA EA 011-7110-01-A8066 REV. I/R AND UPS EO MD11-7110-75910-A. (MINOR)SDR 9WGA20191226501Oil System · reads highOIL QUANTITY INDICATING ON MEL. OIL TEMP STARTED RISING, PRESSURE DECREASING. TEMP REACHED 161 DEGREES AND LEVEL 2 ENG OIL TEMP HI ALERT DISPLAYED. OIL PRESS AT 20. RAN CHECKLIST OBSERVED PRESS & TEMP WITH THROTTLE AT IDLE. TEMP DROPPED A FEW DEGREES AND THEN SDR 9WGA2019121610001Engine · vibration#3 ENGINE VIBRATION 5.0 IN CRUISE. ENGINE FAN BLADE INSPECTION AND LUBRICATION ACCOMPLISHED IN ACCORDANCE WITH AMM 72-31.SDR FDEA201911192991Starter · leakingON CLIMBOUT OUT OF LAX PASSING ABOUT 10,000 OIL QTY IN #2 ENGINE DROPPED TO 5. THEN STEADILY DROPPED UNTIL REACHED 0. APPROXIMATELY 15 MINUTES LATER OIL PRESSURE DECREASED. WHEN OIL PRESSURE REACHED 28 PSI AND AFTER TALKING TO MOCC, SHUTDOWN #2 ENGINE. RSDR 9WGA2019110401Skin · corrodedCENTER CARGO INTERNAL FUSELAGE SKIN HAS CORROSION AT LONGERON 50L F.S.1621-1721. CENTER CARGO INTERNAL FUSELAGE SKIN HAS CORROSION AT LONGERON 52 F.S. 1561-1601. CENTER CARGO INTERNAL FUSELAGE SKIN HAS CORROSION AT LONGERON 48R F.S.1561-1581. CENTER CARGO INTESDR 9WGA2019100493001Director · failedFLIGHT DIRECTOR 1 FAIL, NAV WON'T ENGAGE, WON'T COME OUT OF TAKEOFF THRUST GCP MODE FMS MODE NOT ENGAGING, NO PERFORMANCE DATA CLIMBSDR 9WGA201904190001Engine · failed#1 ENGINE FAILURE @ FL200 ENG 1 FADEC MAINT LEVEL 1 ALERT - INTERMITTENT ROUGH VIBRATION EVERY 10-15 SECONDS WITH NO INDICATION ON SYNOPTIC PAGESDR IPXA2019040540794Engine · fireEMERGENCY DECLARED - LEVEL 2 ENGINE OIL PRESS LOW ON ENGINE #2 2 PSI RED BOXED ON ENGINE INSTRUMENT. TOWER NOTIFIED US THAT ANOTHER UPS AIRCRAFT REPORTED A FIRE #2 ENGINE. TOWER NOTIFIED US AGAIN THAT WE NEEDED TO EVACUATE .R & R #2 ENG OIL PRESSURE TRANSMITTESDR FDEA201903200687Oil System · leakingFLT LVL 360 STARTED NOTICING THE NR 2 OIL QTY DECREASE. AFTER REFERENCING QRH, CAPTAIN DECIDED TO SHUTDOWN THE NR 2 ENGINE. NO ABNORMAL INDICATION ON OIL PRESS OR OIL TEMP. NO OTHER ISSUES AFTER SHUTDOWN. LOWEST QTY SEEN WAS 3. AFTER INSTALLATION OF NR 2 SDR FDEA2019123160658Control Unit · malfunctionedPDIS 618 30-20 7669 16MAR19 MCI OPEN U PREVIOUS WRITEUP FOR "ENG 2 A-ICE DISAG", SHOULD HAVE BEEN "ENG 2 A-ICE OFF". THE DISAG LIGHT ON THE ENG 2 ANTI-ICE SWITCH ILLUMINATED AS A RESULT OF THE "OFF" ACTION DUE TO THE AIRCRAFT DETECTING A LEAKSDR 9WGA20190225301Compressor · stalledON TAKE-OFF ROLL, ENGINE #2 COMPRESSOR STALL AT 80 KTS. ENGINE REQUIRES REPLACEMENT. ENGINE REPLACEMENT DUE TO CHRONIC ISSUE, SPECIFIC REASON UNKNOWN. WILL EVALUATE AT TEST CELL.SDR IPXA2019021543998Engine · vibrationATB - ENGINE #2 UNUSUAL VIBRATION AT TAKEOFF POWER AND CLIMB POWER, EVM COMP AT 3.6 VERY NOTICEABLE IN RUDDER PEDALS VIBRATION SUBSIDED BELOW APPROX . 95% N1. CABIN /COCKPIT VIBRATION PRESENT.FOUND 5EA FAN BLADES (1,15,24,26 & 36) BENT AT THE TIP BEYOND REPAIRSDR IPXA2019021543901Fuel Sys · fluctuatesFUEL FLOW FLUCTUATED AFTER ENG START. FROM 2300 TO 800, THEN BACK TO 2300. THE#2 ENG N1 DISAPPEARED. A PRECAUTIONARY ENG SHUTDOWN WAS ACCOMP WITH THE LOSS OF OIL PRESSURE.FLIGHT LANDED WITHOUT FURTHER COMPLICATIONS.SDR FDEA201812053431Engine · leakingPDIS 618 79-20 7309 05DEC18 SIN OPEN U LOGPAGES:1957706 # 2 LOW OIL QTY. WENT TO 1, SHUT DOWN #2 ENG RTN TO SINGAPORE . DECLARE EMERGENCY . AUTOLAND RWY 02C , CLR WIND 0.5007 KTS. INSTALLED #2 ENGINE PER W/C 71T0902-GE SDR FDEA201811163256Hmu · unknownPDIS 609 25-50 7809 WRI CLOSED, NEW WRI 72-00 7812. LOGPAGES:3040677 ON CLIMB OUT 5000 FEET, EXPERIENCED A VERY PRONOUNCED JOLT ON THE ENTIRE AIRCRAFT. TROUBLE SHOT, FOUND NO REASON FOR PROBLEM. DECIDED TO CONTINUE CLIMB, HAD SAME INDICATION CLIMBINSDR IPXA2018110213560Vane · crackedNR 1 ENGINE OTBD THRUST REVERSER PRECOOLER VANE WAS CRACKED. REMOVED AND REPLACED THE PRECOOLER VAE IAW SRM 54-05-41.SDR IPXA2018100394641Inlet · crackedNR 2 ENGINE INLET LIP HAD A CRACK AT THE 1:00 O`CLOCK POSITION, AT A FASTENER. REPAIRED THE NR 2 ENGINE INLET LIP IAW SRM 54-10-01, REPAIR 4. MINOR.SDR IPXA2018091734054Stiffener · crackedNR 3 ENGINE OTBD THRUST REVERSER STIFFENER FITTING CRACKED, AT THE MID SPAN OF THE THRUST REVERSER. REMOVED AND REPLACED THE STIFFENER IAW SRM 54-01-41. MINOR.SDR IPXA2018070231218Compressor · stalledCONTROL TOWER SAID THEY SAW FLASHES OF LIGHT UNDER THE BELLY WHICH MIGHT HAVE BEEN COMPRESSOR STALLS ENG NR 3. REFER TO T/C 9100 DATED 11/14/2017. PERFORMED EO E-7900-62890-H APPENDIX B. ENG NR 3 P/N OFF-ON: CF6-80C2D1F, S/N OFF: 702705, S/N ON: 702814. EFF RESDR SRXR201805290033Case · corrodedNR 1 ENG FWD FAN CASE BOLT HOLES HAVE CORROSION. ACCOMPLISHED NR 1 ENG FWD FAN CASE BOLT HOLE BUSHING REPAIR PER ENGINEERING CONSULTANTS REPAIR 18-WGA-002 REV ORINGINAL.SDR 9WGA201804250001Bleed Valve · stuckON TAKE OFF, NR 3 ENGINE EXPERIENCED COMPRESSOR STALL. DUMPED FUEL AND PERFORMED AN AIR TURN BACK. TROUBLESHOT SYSTEM, BORESCOPED ENGINE WITH NO DISCREPANCIES NOTED. FOUND HIGH STAGE BLEED VALVE STUCK IN THE OPEN POSITION.SDR IPXA2018040328139Case · damagedNR 2 RT FAN COWL DENTED OUT OF LIMITS. R & R THE FAN COWL IAW MM 71-12-01-000 & 400.SDR FDEA201803120700Elbow · crackedNOTICED EXCESSIVE FUEL BURN ON THREE CONSECUTIVE WAYPOINTS, SHORTLY THEREAFTER RECIEVED A LEVEL 2 FUEL QTY USED CHECK, POSSIBLE FUEL LEAK. RAN QRH PRCEDURE AND THE NR 2 TANK OR ENGINE ISOLATED AS SOURCE OF LEAK. FURTHER TROUBLESHOOTING DETERMINED IT WAS SDR FDEA201802180430Anti-Ice Valve · failedHAD A LEVEL 1 ENGINE ANTI-ICE OFF ALERT DURING CLIMB OUT. WITH ANTI-ICE NR 2 ENGINE SELECTED. REMOVED AND REPLACED THE NR 2 ENGINE ANTI -ICE VALVE IAW AMM 30-22-01-4. ADJUSTMENT AND TESTED GOOD IAW AMM 30-22-00-5-1. ENGINE RUN PERFORMED.SDR FDEA201802180431Anti-Ice Valve · failedLEVEL 1 ENGINE ANTI-ICE OFF ALERT DURING CLIMB OUT, WITH ANTI-ICE NR 2 ENGINE SELECTED. ALSO HAD AN ANTI-ICE DISAGREE ON SELECTOR. REMOVED AND REPLACED THE NR 2 ENGINE ANTI -ICE VALVE IAW AMM 30-22-01-4. ADJUSTMENT AND TESTED GOOD IAW AMM 30-22-00-5-1.SDR IPXA2018012725936Anti-Ice Valve · inoperativeAFTER TAKE OFF, RETURNED TO DEPARTURE DUE TO A NR 2 ANTI-ICE OFF ALERT AND NR 2 ANTI-ICE SWITCH DISAGREE LIGHT ILLUMINATED THE ANTI-ICE OFF ALERT DISAPPEARED ALONG WITH THE NR 2 ENGINE ANTI-ICE SWITCH DISAGREE LIGHT. R 7 R ENG 2 ANTI-ICE VLV LAYCHING RELAYSDR FDEA201801150097Sensor · failedENROUTE WHILE DESCENDING, SELECTED ENGINE ANTI-ICE ON. RECEIVED A LEVEL 1 NR 2 ENGINE. ANTI ICE DUCT FAILED MESSAGE. RETURNED TO DEPARTURE. COMPLIED WITH FIM, INSPECTED ANTI-ICE DUCT AND FOUND NO EVIDENCE OF LEAK. CHECKED ANTI-ICE SENSOR RESISTANCE AND SDR 9WGA4152017120701Engine · power lossLOW THUD HEARD FROM LEFT SIDE #1 ENGINE. SPOOLED TO 30% N1. EGT WAS 200 DEGREES HIGHER THAN 2 & #. FUEL FLOW 640. NO CONTROL OF THROTTLE MOVEMENT. NO CURRENT FAULTS-NO LAST LEG FAULTS-NO FADEC MAINT OR FAULT IN FLIGHT. RTS TEST PERFORMED SATISFACTORY ON BOTH CSDR 9WGA5122017062101Engine · flamed outNR 1 ENGINE FLAMED OUT AT FL330 DURING DESCENT. RESTARTED AT FL170.SDR FDEA201704261269Engine · failedAT TOP OF DESCENT, RECEIVED A LEVEL 2 OIL FILTER ALERT, COMPLIED WITH QRH DIRECTS A NR 1 ENGINE SHUTDOWN. ENGINE WINDMILLING APPROX 15-20 MINS. NO OTHER ALERTS. R & R THE NR 2 ENGINE IAW WIC 71T002-GE AND 71T0902-GE.SDR FDEA201702150559Engine · leakingAFTER TO NR 1 ENG OIL QTY STEADILY DECREASED TO TO ZERO. COMPLIED WITH QRH OIL PRESSURE SUBSEQUENTLY DECREASED TO ZERO. COMPLIED WITH QRH NO ENGINE EXCEEDANCES. REMOVED AND REPLACE ENGINE.SDR IPXA2017012713350Compressor · stalledNR 3 ENGINE COMPRESSOR STALLED. RETURNED TO DEPARTURE. R & R THE NR 3 ENGINE IAW TC9100. OPS CHECKED GOOD.SDR KO0R201612160128Inlet · corrodedNR 2 ENGINE INLET DUCT PLATING IS CORRODED AT YID 279.443, ZID -44.00, XID 0.00 TO 9.5, POSITION 6 O'CLOCK.SDR FDEA201612014301Engine · failedNR 1 ENGINE FAILURE AFTER TAKEOFF. MULTIPLE COMPRESSOR STALLS AND LOSS OF POWER. RETURNED TO DEPARTURE. NO INDICATIONS OF FIRE OR EXTERNAL DAMAGE. PERFORMED STALL INSPECTION IAW AMM 72-00-05-6-1, REMOVED MASTER CHIP DETECTOR MAGNETIC PROBE NO METAL PARTICSDR IPXA2016111410618Gearbox · damagedINSPECTION TYPE: 3C, TWO AREAS OF CHAFE DAMAGE ON EXTERIOR OF NR 1 ENGINE TRANSFER GEARBOX. REPAIRED THE DAMAGE IAW EO MD11-7260-62444-A.
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