# Service difficulty reports: GE CF6-80C2D1F

A list on [GE CF6-80C2D1F](https://openairdocs.org/engine/ge-cf6-80c2d1f.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 11 · 536 reports

- [SDR 9WGA2026071678101](https://openairdocs.org/sdr/9WGA2026071678101.md): Engine · power loss · Jul 16, 2026 · N781SN · Doug MD11F · Engine (Turbine/Turboprop)
  > AIRCRAFT TAKEOFF FROM JIB AIRPORT, DURING CLIMB OUT ENG 1 VIB 5.1 FOLLOWED BY RAPID DECELERATION OF N1 W/HIGH BUFFETING, SHUTDOWN ENG 1, AIRCRAFT RETURNED SAFELY TO JIB AIRPORT.
- [SDR IPXA2025061983508](https://openairdocs.org/sdr/IPXA2025061983508.md): Engine · flamed out · Jun 18, 2025 · N251UP · Doug MD11F · Engine (Turbine/Turboprop)
  > EMERGENCY DECLARED. DURING FLIGHT AT FL390 WE GOT A LEVEL 1 TANK 2 PUMPS OFF. FUEL SYSTEM WAS IN MANUAL MODE PER MEL 28-01-1-2. THIS WAS FOLLOWED BY A LEVEL 2 ENG 2 RPM LO. THE ENGINE 2 FLAMED OUT. WE STARTED THO DRIFT CONSULTED WITH SME IN PPE AND TECH. ALL
- [SDR 9WGA2025061054502](https://openairdocs.org/sdr/9WGA2025061054502.md): Case · corroded · May 2, 2025 · N545JN · Doug MD11F · Engine (Turbine/Turboprop)
  > DURING HEAVY CHECKENGINE #1 FAN CASE (OUTSIDE) AREA AROUND OF THE OGV'S BOLTS AND NUTS WITH CORROSION. CLEANED CORROSION, APPLIED ALODINE, & PRIMER IAW MD-11 SRM 51-21-01 ON #1 ENGINE FAN CASE BY OGV'S AREA. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR 9WGA2025061054503](https://openairdocs.org/sdr/9WGA2025061054503.md): Case · corroded · May 2, 2025 · N545JN · Doug MD11F · Engine (Turbine/Turboprop)
  > DURING HEAVY CHECK ENGINE #3 FAN CASE (OUTSIDE) AREA AROUND OF THE OGV'S BOLTS AND NUTS WITH CORROSION (RUSTY). CLEANED CORROSION (RUSTY) AT ENGINE #3 FAN CASE (OUTSIDE) AREA AROUND OGV'S BOLTS AND NUTS IAW MD-11 SRM 51-21-01. THE AIRCRAFT WAS APPROVED FOR R
- [SDR 9WGA20250428016](https://openairdocs.org/sdr/9WGA20250428016.md): Ring · corroded · Apr 14, 2025 · N546JN · Doug MD11F · Engine (Turbine/Turboprop)
  > #2 ENGINE L/E OF CONTAINMENT RING HAS CORROSION AROUND BOTTOM HALF.
- [SDR 9WGA20250428017](https://openairdocs.org/sdr/9WGA20250428017.md): Ring · corroded · Apr 14, 2025 · N546JN · Doug MD11F · Engine (Turbine/Turboprop)
  > #1 ENGINE CONTAINMENT RING FWD SIDE HAS CORROSION @ THE 8' O'CLOCK POSITION.
- [SDR 9WGA2025042854616](https://openairdocs.org/sdr/9WGA2025042854616.md): Ring · corroded · Apr 14, 2025 · N546JN · Doug MD11F · Engine (Turbine/Turboprop)
  > DURING HEAVY MAINTENANCE CHECK NR 2 ENGINE L/E OF CONTAINMENT RING HAS CORROSION AROUND BOTTOM HALF. ACCOMPLISHED WITH ENGINE REMOVAL ANF REPLACEMENT IAW MD-11 T/C: MS-71-00-03-00-00-01-WG, SEQ, W/O# 15700 AND AMM 71-00-03-000-801.THE AIRCRAFT WAS APPROVED FO
- [SDR 9WGA2025042854617](https://openairdocs.org/sdr/9WGA2025042854617.md): Ring · corroded · Apr 14, 2025 · N546JN · Doug MD11F · Engine (Turbine/Turboprop)
  > DURING HEAVY MAINTENANCE CHECK NR 1 ENGINE CONTAINMENT RING FWD SIDE HAS CORROSION @ 8 O'CLOCK POSITION. ACCOMPLISHED WITH ENGINE REMOVAL AND REPLACEMENT IAW MD-11 T/C: MS-71-00-01-00-00-01-WG, SEQ,1,W/O# 15701 AND AMM 71-00-03-000-801. THE AIRCRAFT WAS APPR
- [SDR 9WGA2025042954618](https://openairdocs.org/sdr/9WGA2025042954618.md): Ring · corroded · Apr 14, 2025 · Doug MD11F · Engine (Turbine/Turboprop)
  > #3 ENGINE CONTAINMENT RING FWD SIDE HAS CORROSION @ THE 8 O'CLOCK POSITION.
- [SDR 9WGA2025042954619](https://openairdocs.org/sdr/9WGA2025042954619.md): Inlet · corroded · Apr 14, 2025 · N546JN · Doug MD11F · Turbine Engine Air Inlet Section
  > #3 INLET HAS PITTING CORROSION BETWEEN 5 & 6 O'CLOCK POS. REMOVED MILD SURFACE CORROSION AND LITE PITTING BY HAND RUBBING ON #3 INLET BETWEEN 5 & 6 O'CLOCK POSITION. FOUND WITHIN LIMITS IAW MD-11 SRM 54-12-02. NO MATERIAL LOSS AT THIS TIME. O. ARILA D0011.
- [SDR 9WGA2025042954620](https://openairdocs.org/sdr/9WGA2025042954620.md): Inlet · corroded · Apr 14, 2025 · N546JN · Doug MD11F · Turbine Engine Air Inlet Section
  > 3# INLET HAS PITTING CORROSION AT 3 O'CLOCK POS. REMOVED MILD SURFACE CORROSION AND LITE PITTING BY HAND RUBBING ON #3 INLET AT 3 O'CLOCK POSITION. FOUND WITHIN LIMITS IAW MD-11 SRM 54-12-02-1A-0, FIGURE 103, DETAIL IV AND SRM 51-21-01. NO MATERIAL LOSS AT
- [SDR 9WGA2025042954621](https://openairdocs.org/sdr/9WGA2025042954621.md): Inlet · corroded · Apr 14, 2025 · N546JN · Doug MD11F · Turbine Engine Air Inlet Section
  > #3 INLET HAS PITTING CORROSION BETWEEN 8 & 9 O'CLOCK POS. REMOVED MILD SURFACE CORROSION AND LITE PITTING BY HAND RUBBING ON #3 INLET BETWEEN 8 AND 9 O'CLOCK POSITION. FOUND WITHIN LIMITS IAW MD-11 SRM 54-12-02-1A-0, FIGURE 103 DETAIL Q AND SRM 51-21-01. NO
- [SDR 9WGA2025042854601](https://openairdocs.org/sdr/9WGA2025042854601.md): Ring · corroded · Apr 14, 2025 · N546JN · Doug MD11F · Engine (Turbine/Turboprop)
  > NR# 286 - DURING HEAVY MAINTNENANCE #2 ENGINE L/E OF CONTAINMENT RING HAS CORROSION AROUND BOTTOM HALF. ACCOMPLISHED WITH ENGINE REMOVED AND REPLACEMENT IAW MD-11 T/C: MS-71-00-03-00-00-01-WG, SEQ, W/O#15700 AND AMM 71-00-03-000-801. THE AIRCRAFT WAS APPROV
- [SDR FDEA202503300539](https://openairdocs.org/sdr/FDEA202503300539.md): Engine · failed · Mar 30, 2025 · N595FE · Doug MD11F · Engine (Turbine/Turboprop)
  > PDIS 595 79-36 8740 30MAR25 02:47 NRT OPEN ENG 3 OIL FILTER LEVEL 2 ALERT @FL350. AIRFRAME VIBRATION STARTED JUST PRIOR TO ALERT AND CONTINUED UNTIL THROTTLE AT IDLE. ENGINE PARAMETERS NORMAL. CONSULTED QRH. SHUT DOWN #3 ENGINE AS ALERT WOULD
- [SDR FDEA202407141001](https://openairdocs.org/sdr/FDEA202407141001.md): Deu · faulted · Jul 14, 2024 · N596FE · Doug MD11F · Engine Indicating System
  > ENGINE FAIL LIGHT ILLUMINATED AT ABOUT 100 KTS ON THE TAKEOFF ROLL. THE TAKEOFF WAS REJECTED. ALL ENGINES WERE OPERATING NORMALLY AFTER THE REJECT. REPLACED DEU-3. OPS CKS GOOD.
- [SDR FDEA202407090975](https://openairdocs.org/sdr/FDEA202407090975.md): Engine · vibration · Jul 9, 2024 · N610FE · Doug MD11F · Engine Pressure Ratio (EPR)
  > NR 3 ENGINE HIGH VIBE 5.0 & ABOVE.VERBAL FROM FLIGHT CREW. REF ER 24-01792 COMPLETED #3 ENGINE INSTALLATION REF WIC 7100000-03-91. REPLACED THE ENGINE
- [SDR FDEA202405080615](https://openairdocs.org/sdr/FDEA202405080615.md): Compressor · stalled · May 8, 2024 · N583FE · Doug MD11F · Turbine Engine Compressor Section
  > ON TAKE OFF ENGINE 1 COMPRESSOR STALLED WITH N1 ROLL BACK X 3. NO OTHER INDICATIONS. DUMPED 130K AND RETURNED TO CDG. REPLACED #1 ENGINE HP FUEL PUMP PER MM 73-12-01-4-1. REMOVED AND REPLACED #1 ENG HMU IAW AMM 73-21-01-4-1. PERFORMED ENG #1 WET MOTOR TES
- [SDR FDEA202303310535](https://openairdocs.org/sdr/FDEA202303310535.md): Engine · inoperative · Mar 31, 2023 · N602FE · Doug MD11F · Engine Controls
  > ON APPROACH TO 18R IN MEM, AIRCRAFT WAS STRUCK ON THE NOSE BY LIGHTNING. SUBSEQUENTLY LOST CONTROL OF THE NUMBER 2 ENGINE. ATTEMPTED TO TROUBLESHOOT BUT NO RESPONSE FROM THE ENGINE WITH THROTTLE MOVEMENT. RAN QRH AND SHUTDOWN ENGINE. EMERGENCY DECLARED.
- [SDR 9WGA2022111280401](https://openairdocs.org/sdr/9WGA2022111280401.md): Anti-Ice Valve · inoperative · Nov 12, 2022 · N804SN · Doug MD11F · Engine Anti-Icing System
  > DISCREPANCY: LEVEL 3 ENGINE 2 A/I DUCT ALERT. CORRECTIVE ACTION: REMOVED AND REPLACED #2 ANTI-ICE VALVE PER AMM 30-22-01 AND C/W FIM 30-22-05. OPS CHECK GOOD.
- [SDR IPXA2022101487138](https://openairdocs.org/sdr/IPXA2022101487138.md): Pump · failed · Oct 13, 2022 · N251UP · Doug MD11F · Engine Fuel Pump
  > INSPECTION TYPE:N/A**SUPPLEMENTAL SDR**EMERGENCY DECLARED**#2 ENGINE FLAMED OUT IN CRUISE AT FL280. FUEL SYS DEFERRED IN MANUAL PROCEDURES. ATTEMPTED RESTART PER CHECK LIST. P/N WORK. #2 FUEL BOOST PUMP STOPPED WORKING.REMOVED AND REPLACED FUEL SYSTEM CONTROL
- [SDR FDEA202208272080](https://openairdocs.org/sdr/FDEA202208272080.md): Hose · leaking · Aug 27, 2022 · N605FE · Doug MD11F · Engine (Turbine/Turboprop)
  > ON CLIMB OUT PASSING APPROXI 2500 FT FELT A BRIEF THUMP. APPROX 10 SECS LATER, NR 2 ENG ROLLED BACK TO BELOW IDLE. GOT LVL 2 ENGINE 2 RPM LO ALERT. ENG STILL WINDMILLING AT ABOUT 20% N1. RAN QRH & ATTEMPTED A RESTART, NO SUCCESS. SHUT ENG DOWN DECLARED A
- [SDR 9WGA2022081978301](https://openairdocs.org/sdr/9WGA2022081978301.md): Oil System · leaking · Aug 19, 2022 · N783SN · Doug MD11F · Engine Oil Quantity
  > #1 ENGINE HAS NO OIL, AIR RETURN.: R & R #1 ENGINE PER AMM 71-00-01. ENGINE RUN SATISFACTORY. REPLACE #1 ENGINE ACCOMPLISHED IAW JC RNR 11071001 R0. THIS COMPLIES WITH THE INSPECTION REQUIREMENTS OF MS 71-00-01-00-00-01.
- [SDR 2022FA0000333](https://openairdocs.org/sdr/2022FA0000333.md): Disk · cracked · Jul 7, 2022 · N261UP · Doug MD11F · Turbine Engine Air Inlet Section
  > INDICATION IN BORE A ZONE CORNER, AMPLITUDE 2020MV. GE ENGINE SHOP MANUAL (ESM) EVALUATION/REJECTION LIMIT IS 1500MV.
- [SDR FDEA202207021673](https://openairdocs.org/sdr/FDEA202207021673.md): Engine · flamed out · Jul 2, 2022 · N608FE · Doug MD11F · Engine (Turbine/Turboprop)
  > ENG 2 FLAMED OUT AT FL380. EMERGENCY DECLARED DIVERTED TO TPA, LANDED SAFELY, TAXIED TO RAMP UNDER OWN POWER WITHOUT ASSISTANCE. ENGINE 2 FLAME OUT CAUSE VERIFIED TO BE TANK 2 FUEL QTY 0.00 LBS UPON ARRIVAL INTO TPA. PER MOCC, PERFORMED ENGINE 2 POST WIN
- [SDR 2022F00269](https://openairdocs.org/sdr/2022F00269.md): None · none · Jun 22, 2022 · N412SN · Doug MD11F · Powerplant System
  > #2 ENGINE SHUTDOWN DURING CRUISE, TAIL PUMPS LO, ALT PUMPS LO
- [SDR 9WGA2022062141201](https://openairdocs.org/sdr/9WGA2022062141201.md): Fuel Sys · abnormal · Jun 21, 2022 · N412SN · Doug MD11F · Aircraft Fuel System
  > TAIL PUMPS LOW, ALT PUMPS LOW, ENGINE 2 SHUTDOWN IN FLIGHT. FOUND FSC FAULTING. REPLACED AFSC, FSC AND FSC CONTROL PANEL. OPS TEST FOUND NORMAL. ACCOMPLISHED MPA RUN OF ALL 3 ENGINES TO ENSURE PUMPS ARE WORKING IAW AMM 28-22-00 AND AMM 71-00-00. ALL TEST FOU
- [SDR 9WGA2022051754301](https://openairdocs.org/sdr/9WGA2022051754301.md): Engine · out of rig · May 17, 2022 · N543JN · Doug MD11F · Engine (Turbine/Turboprop)
  > AIR RETURN DUE TO ENGINE 3 NOT DEVELOPING FULL CLIMB POWER 4% LESS N1 @ 10000 & 7% LESS AT 35000. ENGINE 3 EGT, N2 & FF CONFIRM POWER LOSS. ENGINE 3 "T" WOULD NOT ADVANCE INTO THE "V" EVEN WHEN GOING TO THE GIRT BAR. CORRECTIVE ACTION: ECU 3A & 3B CURRENT FAU
- [SDR FDEA202112203109](https://openairdocs.org/sdr/FDEA202112203109.md): Line · leaking · Dec 20, 2021 · N609FE · Doug MD11F · Turbine Engine Oil System
  > CLIMBING THROUGH 3,000' GOT INDICATE VISIBLE SMOKE WITH A BITING,ACRID SMELL.RAN CHECK LIST,DECLARED EMERGENCY,LANDED UNEVENTUALLY,NO FUEL DUMP.HOT BRAKES LIGHT MAIN MAX TEMP 618. DETAILED INSP OF #1 ENG FOUND #1 ENG L/H THRUST REVERSER OPENING ACTUAT
- [SDR MASA2021090800232](https://openairdocs.org/sdr/MASA2021090800232.md): Engine · overtemp · Sep 8, 2021 · N241LR · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > L / R ENGINE OVERTEMP ON CLIMB OUT. AIRCRAFT IS STILL CURRENTLY OOS.
- [SDR AALA202109083000](https://openairdocs.org/sdr/AALA202109083000.md): Shear Pin · corroded · Sep 7, 2021 · N149AN · Airbus A321231 · Engine Mount Section
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT ENGINE; AFT ENGINE MOUNT INNER SHEAR PIN ON INBOARD LINK UPPER POSITION. REPLACED SHEAR PIN PER AMM 71-22-11-200-804-A.
- [SDR IPXA2021090473547](https://openairdocs.org/sdr/IPXA2021090473547.md): Fastener · loose · Aug 26, 2021 · N274UP · Doug MD11F · Engine Air Intake System
  > INSPECTION TYPE:1C#2 ENGINE INLET NOSE SKIN HAS 23 LOOSE FASTENERS.REPAIRED #2 ENGINE INLET NOSE SKIN LOOSE FASTENERS IAW VT-SAA EA 011-7110-01-A9334 REV. IR AND UPS EO MD11-7110-81459-A. (MINOR)
- [SDR FDEA202108222077](https://openairdocs.org/sdr/FDEA202108222077.md): Coupling · missing · Aug 22, 2021 · N625FE · Doug MD11F · Engine Anti-Icing System
  > DURING B CHECK INSPECTION OF NR1 ENGINE, THE UPPER ANTI-ICE DUCT COUPLING WAS FOUND TO BE MISSING FROM THE UPPER ANTI-ICE DUCT ASSEMBLY. THE COUPLING WAS FOUND RESTING BETWEEN THE HIGH PRESSURE COMPRESSOR CASE AND THE RIGHT SIDE VSV ACTUATION LEVER. FU
- [SDR IPXA2021090773676](https://openairdocs.org/sdr/IPXA2021090773676.md): Sleeve · damaged · Aug 19, 2021 · N274UP · Doug MD11F · Engine Thrust Reverser
  > INSPECTION TYPE:1C#1 ENG. R/H THRUST REVERSER TRANSLATING SLEEVE ASLAND PANEL HAS AN ELONGATED HOLE.REPAIRED #1 R/H T/R IAW VT-SAA EA 011-7830-01-A9339 REV. I/R AND UPS EO MD11-7830-81516-A. (MINOR)
- [SDR 9WGA2021080655131](https://openairdocs.org/sdr/9WGA2021080655131.md): Compressor · vibration · Aug 5, 2021 · N513SN · Doug MD11 · Turbine Engine Compressor Section
  > DIVERSION DUE TO ENG 3 VIB HIGH COMP OVER 4.0 ON CLIMB ON MULTIPLE OCCASION AND HAD TO RETARD #3 MORE THAN 1 CROWN TO REDUCE THE VIBRATION.
- [SDR IPXA2021072972246](https://openairdocs.org/sdr/IPXA2021072972246.md): Skin · cracked · Jul 21, 2021 · N273UP · Doug MD11F · Engine Thrust Reverser
  > INSPECTION TYPE:2C#1 ENGINE L/H T/R AFT FIXED INNER BARREL UPPER SKIN IS CRACKED.REPAIRED CRACKED #1 ENGINE L/H T/R AFT FIXED INNER BARREL UPPER SKIN IAW VT-SAA EA 011-7830-01-A9243 REV. IR AND UPS EO MD11-7830-81094-A. (MINOR)
- [SDR IPXA2021072772137](https://openairdocs.org/sdr/IPXA2021072772137.md): Skin · gouged · Jul 6, 2021 · N254UP · Doug MD11F · Engine Thrust Reverser
  > INSPECTION TYPE:2C#1 ENGINE I/B T/R LOWER SIDE WALL FACE SHEET IS GOUGED.REPAIRED GOUGED #1 ENGINE I/B T/R LOWER SIDE WALL FACE SHEET IAW VT-SAA EA 011-7830-01-A9229 REV. IR AND UPS EO MD11-7830-81038-A. (MINOR)
- [SDR IPXA2021062570951](https://openairdocs.org/sdr/IPXA2021062570951.md): Start Valve · faulted · Jun 24, 2021 · N260UP · Doug MD11F · Engine Start Valves/Controls
  > ATB ** LANDED WITHOUT INCIDENT ** PASSING FL220 START VALVE LIGHT ILLUMINATED. CREW WAS DIVERTED DUE TO ICING CONDITIONS. CREW WILL WORK WITH DISPATCH ON THAT. ITEM REMAINS ON DEFERRAL. M747866.RAN WIRING WDM 80-11-02. FRN-RD SHRTD TO SHIELD BTWN P1 8235 PIN "
- [SDR IPXA2021071371618](https://openairdocs.org/sdr/IPXA2021071371618.md): Fastener · loose · Jun 18, 2021 · N296UP · Doug MD11F · Nacelle/Pylon, Main Frame
  > INSPECTION TYPE:2C#2 ENGINE INLET LIP HAS LOOSE FASTENERS.REPAIRED #2 ENGINE INLET LIP LOOSE FASTENERS IAW VT-SAA EA 011-7110-01-A9204 REV. IR AND UPS EO MD11-7110-80842-A. (MINOR)
- [SDR 9WGA2021060454201](https://openairdocs.org/sdr/9WGA2021060454201.md): Oil System · low pressure · Jun 4, 2021 · N542KD · Doug MD11F · Engine Oil Pressure
  > AIR RETURN, ENGINE 3 OIL PRESSURE LOW.
- [SDR FDEA202105181286](https://openairdocs.org/sdr/FDEA202105181286.md): Engine · flamed out · May 18, 2021 · N587FE · Doug MD11F · Engine (Turbine/Turboprop)
  > NUMBER TWO ENGINE FLAMED OUT WITH THROTTLE ADVANCE FOR TAKE OFF. RAN QRH CONTACTED MOCC, RESTARTED ENGINE, NORMAL START AND CLIMB OUT. SHGN 18MAY21 08:25 MEM U STARTED AND RAN ENGINE #2 FOR 5 MINUTES IN REFERENCE PER MD11 JRH, ENGINE #2 STARTED GOOD AND
- [SDR FDEA202105181287](https://openairdocs.org/sdr/FDEA202105181287.md): Engine · flamed out · May 18, 2021 · N587FE · Doug MD11F · Engine Fuel and Control
  > ENGINE 2 FLAMEOUT AFTER ADDING POWER FOR TAKEOFF. RAN QRH CONTACTED MOCC, NORMAL RELIGHT AND TAKEOFF. SHGN 18MAY21 08:18 MEM U STARTED AND RAN ENGINE #2 FOR 5 MINUTES IN REFERENCE PER MD11 JRH, ENGINE #2 STARTED GOOD AND ALL THE PARAMETERS ARE WITHIN
- [SDR FDEA202105171260](https://openairdocs.org/sdr/FDEA202105171260.md): Engine · failed · May 17, 2021 · N573FE · Doug MD11F · Engine (Turbine/Turboprop)
  > PDIS 573 71-00 6503 17MAY21 STN OPEN U DURING DEPARTURE CLIMBING THROUGH 3000 FEET DURING POWER REDUCTION HAD 3 SEPARATE AUDIBLE BANGS WITH MODERATE RIGHT YAW- ENGINE INDICATIONS APPEARED NORMAL - UNEVENTFUL EMERGENCY RETURN LANDING ACCOMPLIS
- [SDR FDEA202104210964](https://openairdocs.org/sdr/FDEA202104210964.md): Flange · corroded · Apr 21, 2021 · N602FE · Doug MD11F · Turbine Engine Air Inlet Section
  > NR 2 ENGINE HAS SIGNS OF CORROSION ON FAN CASE FWD FLANGE FROM APPROXIMATELY 4 TO 8 O'CLOCK POS. REFERENCE NONROUTINE N00018 WORK ORDER 79912 ITEM FOUND DURING B-CHECK. CORROSION IS MORE THAN 10 INCHES IN CUMULATIVE CIRCUMFERENCE. CIRCUMFERENCE. REF N1
- [SDR 9WGA2021041841501](https://openairdocs.org/sdr/9WGA2021041841501.md): Engine · malfunctioned · Apr 18, 2021 · N415JN · Doug MD11F · Engine (Turbine/Turboprop)
  > LEVEL 2 "ENG 3 RPM LO" ON DESCENT. ATTEMPTED RESTART. SECURED ENGINE. EMERGENCY DECLARED.
- [SDR FDEA202104110885](https://openairdocs.org/sdr/FDEA202104110885.md): Hmu · malfunctioned · Apr 11, 2021 · N589FE · Doug MD11F · Fuel Controlling System
  > PASSING - 1000 FT MSL, EXPERIENCED 4-5 LOUD BANGS WITH ACFT VIBRATION. F/O NOTICED A FLUCUATION ON THE #3 ENG N1 GAGE. TOWER REPORTED BLACK SMOKE FROM #3 ENG. AFTER THRUST REDUCTION, NO FURTHER ABNORMAL INDICATIONS REMOVED AND REPLACED CIT SENSOR, HMU, A
- [SDR IPXA2021052869913](https://openairdocs.org/sdr/IPXA2021052869913.md): Rib · gouged · Apr 11, 2021 · N265UP · Doug MD11F · Engine Thrust Reverser
  > INSPECTION TYPE:3C#1 ENGINE I/B T/R RIB AT NAC STA 210.130 HAS 2 GOUGES.REPAIRED GOUGED #1 ENGINE I/B T/R ZEE RIB AT NAC STA 210.130 IAW VT-SAA EA 011-7832-01-A9067 REV. IR AND UPS EO MD11-7830-80474-A. (MINOR).
- [SDR FDEA202103260774](https://openairdocs.org/sdr/FDEA202103260774.md): Fuel Control · failed · Mar 26, 2021 · N582FE · Doug MD11F · Fuel Control/Turbine Engines
  > RIGHT AFTER TAKEOFF,HEARD ABOUT 5 COMPRESSOR STALLS FROM THE NO 3 ENGINE ALSO NOTICED FLASHES OUT OF THE RIGHT WINDOW. N1 EGT SHOWED FLUCUATIONS UNTIL POWER WAS REDUCED TO CLIMB POWER TAKEOFF WAS MAX THRUST ENGINE OPERATED NORMAL REMAINDER OF FLIGHT DID NOT
- [SDR IPXA2021022065873](https://openairdocs.org/sdr/IPXA2021022065873.md): Fadec · malfunctioned · Feb 20, 2021 · N286UP · Doug MD11F · Fuel Controlling System
  > INSPECTION TYPE: N/A ATB A/C OOS. NO EMERGENCY DECLARED. LANDED SUCCESSFUL LEVEL ONE FADEC MAIN.
- [SDR 9WGA20210112](https://openairdocs.org/sdr/9WGA20210112.md): Warning Message · illuminated · Jan 12, 2021 · N415JN · Doug MD11F · Engine Anti-Icing System
  > LEVEL 3 ENGINE 2 A-ICE DUCT IN FLIGHT AT 7000 MSL AND 8500 MSL. SHUT DOWN NR 2 ENGINE, PER QRH.
- [SDR IPXA2020123063953](https://openairdocs.org/sdr/IPXA2020123063953.md): Engine · flamed out · Dec 28, 2020 · N261UP · Doug MD11F · Engine (Turbine/Turboprop)
  > INSPECTION TYPE: N/A DURING TAXI, NR 2 ENGINE FLAMED OUT, ALL ENGINE PARAMETER ROLLED BACK. NO FCC FAULTS ON ECU 2A ON 2B FAULTS, PER FON MTS NORMAL START, PER MD11 AMM 71-00-00. OPERATIONS TEST GOOD AT THIS TIME.

Next page: https://openairdocs.org/engine/ge-cf6-80c2d1f/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 = 'CF680C2D1F'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/ge-cf6-80c2d1f/reports

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