# Service difficulty reports: GE CF6-6K

A list on [GE CF6-6K](https://openairdocs.org/engine/ge-cf6-6k.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 54 reports

- [SDR FDEA202105271414](https://openairdocs.org/sdr/FDEA202105271414.md): Engine · malfunctioned · May 27, 2021 · N550FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > AT FL380 ALL ENGINES WERE OPERATING NORMALLY. AS WE BEGAN OUR DESCENT AND THROTTLES CAME BACK TOWARDS IDLE ECS SURGED FOLLOWED BY A LEVEL 2 AIRSYS 2 PRES LO AND CONFIRM ENG OUT PROMPT. AIR PRESSURE OUT OF THE NUMBER 2 ENGINE WAS 9 PSI. THE NUMBER 2 THROTT
- [SDR FDEA2020042730686](https://openairdocs.org/sdr/FDEA2020042730686.md): Engine · malfunctioned · Apr 3, 2020 · N550FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > CLIMBING THRU FL340 WITH ENGINES ALL AT CLIMB POWER WE FELT A BUMP LIKE MINOR TURBULENCE. THEN ANOTHER AND ANOTHER. WE SAW ENG 2 N1 FLUCTUATING SO WE SUSPECTED A COMPRESSOR STALL. AS WE WERE RUNNING THE QRH FOR ENG COMPRESSOR STALL WE RECEIVED LEVEL 2 ENG
- [SDR FDEA2019081291831](https://openairdocs.org/sdr/FDEA2019081291831.md): Engine · failed · Aug 9, 2019 · N360FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > APPROXIMATELY 500 FEET AFTER TAKEOFF. WE RECEIVED A LEVEL 1 ENG 1 EXEEDANCE. TEMP SHOWED 1010, THROTTLE 1 WAS PULLED BACK AND TEMP DECREASED INTO A NORMAL RANGE. WAS OVERTEMP FOR APPROXIMATELY 2 SEC. ENGINE OPERATED NORMAL FOR THE REMAINDER OF FLIGHT RET
- [SDR FDEA2019122089831](https://openairdocs.org/sdr/FDEA2019122089831.md): Engine · overtemp · Aug 9, 2019 · N360FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > PDIS 360 77-20 6391 09AUG19 MEM OPEN U LOGPAGES:2977480 APPROXIMATELY 500 FEET AFTER TAKEOFF. WE RECEIVED A LEVEL 1 ENG 1 EXEEDANCE. TEMP SHOWED 1010?, THROTTLE 1 WAS PULLED BACK AND TEMP DECREASED INTO A NORMAL RANGE. WAS OVERTEMP FOR APPROX
- [SDR FDEA201803200740](https://openairdocs.org/sdr/FDEA201803200740.md): Engine · failed · Mar 20, 2018 · N372FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > ENG FAILURE NR 1 ENG CLIMBING THRU 5K. YAW, LOUD BANG RAPIDLY RISING EGT. ENG EXCEEDANCE 942 DEG. THROTTLE TRIMMED POSITIONED TO IDLE. ENG SHUT DOWN. FIRE BOTTLE DISCHARGED. REPLACED NR 1 ENGINE.
- [SDR 2013FA0000705](https://openairdocs.org/sdr/2013FA0000705.md): Engine · seized · Aug 15, 2013 · N450AX · Doug DC1010 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE HAD SUDDEN SEIZURE, NO FIRE INDICATION, PRECEDED BY LOAD BANG, PERFORMED EMERGENCY PROCEDURES.
- [SDR 06FDEA03705](https://openairdocs.org/sdr/06FDEA03705.md): Door Frame · misrepaired · Oct 19, 2006 · N567FE · Doug DC1010F · Fuselage Main, Structure
  > MAIN CABIN R3 PASSENGER DOOR JAMB AT STA 1305 LONGERON NR 27 EXISTING REPAIR. INSPECTION OF EXISTING REPAIR CARRIED OUT IAW ED 8-5100-7-5001 P2. FOUND 2 FASTENERS NOT INSTALLED ( SEE JPF N00742). FASTENERS INSTALLED IAW SRM 53-30-00 FIG 19. PERFORMED INSPE
- [SDR 06FDEA03707](https://openairdocs.org/sdr/06FDEA03707.md): Door Frame · misrepaired · Oct 19, 2006 · N567FE · Doug DC1010 · Fuselage Main, Structure
  > INTERNAL FUSELAGE CAC AREA AT STA 1156 TO 1158 BETWEEN LONGERONS 31 TO 28 LT SIDE EXISTING REPAIR. PERFORMED INSPECTION IAW EO NR 8-5100-7-5001 P2 CRITERIA FOUND INSTALLED BOLTS INSTEAD OF HI-LOCKS IAW SRM 53-30-00 FIG 7 VOL 1. INSTALLED FASTENERS IAW SRM 53
- [SDR 06FDEA0902](https://openairdocs.org/sdr/06FDEA0902.md): Skin · cracked · Mar 2, 2006 · N563FE · Doug DC1010 · Fuselage Main, Plate/Skin
  > DISCREPANCY EXISTING DOUBLER FUSELAGE SKIN STA 383 AND 410 Z-30 FOUND EXT DOUBLER REPAIR. REMOVED OLD SKIN INSTALLED NEW SKIN P/N ABA7049-3 IAW DWG ABA7049/ABA7035 AND SRM 53-40-00 FIG 15 VOL 1. ON EXISTING HOLES AT SKIN ABA7048-3 7EA HOLES INSTALLED RIVETS
- [SDR 06FDEA0901](https://openairdocs.org/sdr/06FDEA0901.md): Skin · dented · Mar 2, 2006 · N563FE · Doug DC1010 · Fuselage Main, Plate/Skin
  > DISCREPANCY EXT FUSELAGE LOWER DEEP DENT ON EXT SKIN AT STA 1970 FROM LONG.38 LT TO LONG 39LT. REFORMED DENT AND NDI INSP. NO CRACK FOUND IAW SRM 53-20-00 FIG 13 VOL 1. FABRICATED AND INSTALLED INTERNAL DOUBLER IAW SRM 53-20-00 FIG 13 SHT 14 FABRICATED PAR
- [SDR 06FDEA0894](https://openairdocs.org/sdr/06FDEA0894.md): Skin · dented · Mar 2, 2006 · N563FE · Doug DC1010 · Fuselage Main, Plate/Skin
  > DISCREPANCY LWR FUSELAGE RT SIDE FOUND MANY DENTS ON SKIN STA 979 LONG 39 TO 42. REMOVED DENT IAW SRM 53-20-00 FIG 13 SHT 14 NOTE (C) VOL 1 PERFORMED INSP IAW SRM 53-20-00 VOL 1 NO CRACK FOUND BLENDED AND POLISH NICKS IAW SRM 53-20-00 FIG 13 SHT 2B VOL 1 ORIG
- [SDR 05FDEA04003](https://openairdocs.org/sdr/05FDEA04003.md): Skin · damaged · Nov 29, 2005 · N571FE · Doug MD1010F · Trailing Edge Flaps
  > LT IB FLAP SKIN UPPER SIDE ACCIDENTALLY DAMAGED DURING STRIPPING ACTIVITIES. REMOVED FLAP SECTION IAW SRM 51-31-01. REFORMED RIB IAW DPS 3.69. PERFORMED INSPECTION, NO CRACK FOUND. PERFORM DOUBLER REPAIR IAW SRM 57-10-00 FIG 85.
- [SDR 05FDEA04004](https://openairdocs.org/sdr/05FDEA04004.md): Skin · damaged · Nov 29, 2005 · N571FE · Doug MD1010F · Trailing Edge Flaps
  > DURING STRIPPING ACTIVITIES, RR IB FLAP SKIN UPPER SIDE ACCIDENTALLY DAMAGED CAUSING CRACK 3 INCHES LONG. REMOVED FLAP SECTION IAW SRM 51-31-01. PERFORMED INSPECTION, NO CRACK FOUND. PERFORMED DOUBLER REPAIR IAW SRM 57-10-00 FIG 85.
- [SDR 05FDEA04005](https://openairdocs.org/sdr/05FDEA04005.md): Doubler · corroded · Nov 29, 2005 · N571FE · Doug MD1010F · Wing, Plate/Skin
  > DURING PRE-PAINT INSPECTION FOUND CORROSION WITH EXFOLIATION ON BEVER/TAIL OF RT WING AT STA XORS 284. REPAIRED IAW EA 8-5710-93818.
- [SDR 05FDEA04006](https://openairdocs.org/sdr/05FDEA04006.md): Doubler · corroded · Nov 29, 2005 · N571FE · Doug MD1010F · Wing, Plate/Skin
  > DURING PRE-PAINT INSPECTION FOUND CORROSION WITH EXFOLIATION ON BEVER/TAIL OF LT WING AT STA XORS 284. REPAIRED IAW EA 8-5710-93818.
- [SDR 05FDEA03465](https://openairdocs.org/sdr/05FDEA03465.md): Skin · dented · Oct 21, 2005 · N556FE · Doug DC1010 · Fuselage Main, Plate/Skin
  > LWR FUS RT SIDE ON SKIN: BTW LONG 37 AND LONG 38 FOUND AT STA 1009 NR 1EA DENT (LENGTH 1,063 INCH X DEPTH 0,082 INCH) AND AT STA 1006 FOUND 1EA DENT (DEPTH 0,161 INCH X LENGTH 2 INCH) BTW LONG38 AND LONG 39 AT STA Y=1007 FOUND NR1 DENT (LENGTH 1.57 INCH X DE
- [SDR 05FDEA03475](https://openairdocs.org/sdr/05FDEA03475.md): Rib · corroded · Oct 21, 2005 · N556FE · Doug DC1010 · Horizontal Stabilizer, Spar/Rib
  > LT HORIZ STAB LEADING EDGE OB FOUND CORROSION BETWEEN SKIN AND RIB. REMOVED CORROSION AND REPAIRED WITH NR 2EA DOUBLER IAW SRM 55-13-01 FIG 1 VOL3.
- [SDR 05FDEA02603](https://openairdocs.org/sdr/05FDEA02603.md): Frame · worn · Aug 24, 2005 · N556FE · Doug DC1010 · Fuselage Main, Frame
  > AIR COND COMPT LT SIDE FOUND WORN FRAME AT STA 588 X=64. TRIMMED WORN AREA AND REPAIR IAW SRM.
- [SDR 05FDEA02604](https://openairdocs.org/sdr/05FDEA02604.md): Skin · dented · Aug 24, 2005 · N556FE · Doug DC1010 · Ailerons
  > LT WING LOWER SURFACE ON IB AILERON: FOUND NR 1 DENT ( LENGTH 0.87 INCH; DEPTH 0.094 INCH) AND FOUND NR 1 DENT (LENGTH 0.63 INCH; DEPTH 0.027 INCH) AT STA XW 343 CUT DAMAGED PORTION OF LOWER SKIN AND REPAIRED IAW SRM.
- [SDR 05FDEA02605](https://openairdocs.org/sdr/05FDEA02605.md): Rib · cracked · Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/Bulkhead
  > RT WING L/E AT XORS 526 FOUND RIB CRACKED. ACCOMPLISHED WING OB EDGE FORMER REPAIR IAW SRM.
- [SDR 05FDEA02606](https://openairdocs.org/sdr/05FDEA02606.md): Skin · cracked · Aug 24, 2005 · N556FE · Doug DC1010 · Leading Edge Devices
  > RT WING FIXED L/E AT SLAT TRACK NR 7 FOUND NR 1 CRACK 1 INCH LONG ON SKIN AT XORS 372. CUT DAMAGED AREA AND REPAIRED WITH DOUBLER IAW SRM.
- [SDR 05FDEA02607](https://openairdocs.org/sdr/05FDEA02607.md): Structure · damaged · Aug 24, 2005 · N556FE · Doug DC1010 · Fuselage Main, Structure
  > MAIN CABIN INTERNAL FUSELAGE FOUND NR 2 HOLES DIAM. 0.25 INCH TOO CLOSE AT STA 1561, LONGERON 8 LT SIDE. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM.
- [SDR 05FDEA02608](https://openairdocs.org/sdr/05FDEA02608.md): Fastener · wrong part · Aug 24, 2005 · N556FE · Doug DC1010 · Fasteners
  > AIR COND COMPT LT SIDE FOUND EXISTING REPAIR WITH WRONG FASTENERS (CHERRY AND BOLT) ON NLG BLKHD. REMOVED EXISTING REPAIR, TRIMMED OUT DAMAGED AREA AND REPAIRED IAW SRM.
- [SDR 05FDEA02609](https://openairdocs.org/sdr/05FDEA02609.md): Rib · cracked · Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/Bulkhead
  > RT WING FIXED LEADING EDGE AT STA XORS 936 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER, FILLER AND DOUBLER REPAIR IAW SRM.
- [SDR 05FDEA02614](https://openairdocs.org/sdr/05FDEA02614.md): Rib · cracked · Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/Bulkhead
  > RT WING FIXED LEADING EDGE AT STA 750 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND REPAIR ANGLE.
- [SDR 05FDEA02615](https://openairdocs.org/sdr/05FDEA02615.md): Rib · cracked · Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/Bulkhead
  > RT WING FIXED LEADING EDGE AT STA XORS702 FOUND NR 1 RIB CRACKED. ACCOMPLISH FORMER REPAIR IAW SRM AND REPAIR ANGLE.
- [SDR 05FDEA02616](https://openairdocs.org/sdr/05FDEA02616.md): Rib · cracked · Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/Bulkhead
  > RT WING FIXED LEADING EDGE AT XORS 696 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND REPAIR ANGLE.
- [SDR 05FDEA02617](https://openairdocs.org/sdr/05FDEA02617.md): Rib · cracked · Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/Bulkhead
  > RT WING FIXED LEADING EDGE AT XORS 733 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM.
- [SDR 05FDEA02618](https://openairdocs.org/sdr/05FDEA02618.md): Rib · cracked · Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/Bulkhead
  > RT WING FIXED LEADING EDGE AT XORS 742 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM.
- [SDR 05FDEA02619](https://openairdocs.org/sdr/05FDEA02619.md): Rib · cracked · Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/Bulkhead
  > RT WING FIXED LEADING EDGE AT XORS 831 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM.
- [SDR 05FDEA02620](https://openairdocs.org/sdr/05FDEA02620.md): Rib · cracked · Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/Bulkhead
  > RT WING FIXED LEADING EDGE AT XORS 598 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR.
- [SDR 05FDEA02621](https://openairdocs.org/sdr/05FDEA02621.md): Rib · cracked · Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/Bulkhead
  > RT WING FIXED LEADING EDGE AT XORS 615 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR.
- [SDR 05FDEA02622](https://openairdocs.org/sdr/05FDEA02622.md): Rib · cracked · Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/Bulkhead
  > RT WING FIXED LEADING EDGE AT XORS 490 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR.
- [SDR 05FDEA02623](https://openairdocs.org/sdr/05FDEA02623.md): Rib · cracked · Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/Bulkhead
  > RT WING FIXED LEADING EDGE AT XORS 485 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR.
- [SDR 05FDEA02624](https://openairdocs.org/sdr/05FDEA02624.md): Rib · cracked · Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/Bulkhead
  > RT WING FIXED LEADING EDGE AT XORS 454 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM.
- [SDR 05FDEA02625](https://openairdocs.org/sdr/05FDEA02625.md): Rib · cracked · Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/Bulkhead
  > RT WING FIXED LEADING EDGE AT XORS 402 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR.
- [SDR 05FDEA02626](https://openairdocs.org/sdr/05FDEA02626.md): Rib · cracked · Aug 24, 2005 · N556FE · Doug DC1010 · Wing, Rib/Bulkhead
  > RT WING FIXED LEADING EDGE AT XORS 352 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR.
- [SDR 05FDEA02447](https://openairdocs.org/sdr/05FDEA02447.md): Skin · unknown · Aug 12, 2005 · N564FE · Doug DC1010 · Fuselage Main, Plate/Skin
  > FOUND REPAIR AT STA 1159 - 1139 LONGERON 41-48 RT. REPAIRED IAW FEDEX 8-5330-84091A.
- [SDR 05FDEA02449](https://openairdocs.org/sdr/05FDEA02449.md): Structure · corroded · Aug 12, 2005 · N564FE · Doug DC1010 · Wing, Center Box
  > CTR WING LWR BARREL STA 1216 LONGERON 48 REWORK OF CORROSION 40 PERCENT. MATERIAL LOSS TO STANDING LEG. CUT OUT CORRODED SECTION OF LONGERON IAW SRM 53-00-01 FIG 7 VOL I GN 16.
- [SDR 05FDEA01680](https://openairdocs.org/sdr/05FDEA01680.md): Engine · malfunctioned · Jun 24, 2005 · N565FE · Doug MD1010F · Engine Indicating System
  > NR 1 ENGINE REMAINED AT FLIGHT IDLE DURING DESCENT AND WOULD NOT FOLLOW THROTTLE. N1 AND N2 SLOWLY STARTED DECAYING UNTIL GEN, AIR, HYDRAULIC ALERTS STARTED COMING ON. EGT WAS BELOW OTHER ENGINES 150-200 DEG FF WAS APPROX 500 PPH. FIRST NOTED PROBLEM FL220
- [SDR 05FDEA00287](https://openairdocs.org/sdr/05FDEA00287.md): Engine · vibration · Feb 14, 2005 · N399FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > AT FL 340 EXPERIENCED NR 1 ENGINE VIBRATION, N1 ROLLED BACK TO 34%, N2 62% FF 690 LBS. EXECUTED ENG FIRE SEVERE DAMAGE CHECKLIST, FUEL DUMP ABOUT 3000 LBS, DECLARED EMERGENCY LANDING 18C. INSPECTED INTAKE AND EXHAUST. NO DEFECTS NOTED. BOROSCOPE INSPECTE
- [SDR HALA0100292](https://openairdocs.org/sdr/HALA0100292.md): Fcu · malfunctioned · Dec 11, 2001 · N128AA · Doug DC1010 · Fuel Control/Turbine Engines
  > FLT 481 - PPT - NR 3 ENGINE FLAMED OUT ON APPROACH. ENGINE HAD BEEN AT IDLE POWER 5 MINUTES. REMOVED AND REPLACED FUEL CONTROL. OPS AND LEAK CHECK GOOD. (M)
- [SDR HALA0100204](https://openairdocs.org/sdr/HALA0100204.md): Mec · failed · Aug 8, 2001 · N135AA · Doug DC1010 · Fuel Control/Turbine Engines
  > FLT 938 - INBOUND TO ANC, HAD NR 2 ENGINE QUIT AT 15,000 FT, ATTEMPTED RESTART, NO SUCCESS. DECLARED EMERGENCY. REMOVED AND REPLACED MEC AND FUEL PUMP. TRIM RUN CHECKS OK. (M)
- [SDR CNMA200100029](https://openairdocs.org/sdr/CNMA200100029.md): Bearing · failed · Aug 6, 2001 · N360AX · Doug DC1010 · Turbine Engine Accessory Drive
  > DURING CLIMBOUT #3 ENGINE OIL STRAINER CLOGGED LIGHT CAME ON AND THROTTLE WAS REDUCED AND LIGHT WENT OUT. SHORTLY THERE AFTER OIL QTY DROPPED TO "0" AND ENGINE WAS SHUT DOWN PER COM PROCEDURES. ACCOMPLISHED FUEL DUMP INFLIGHT. REMOVED AND REPLACED RADIAL MID
- [SDR CNMA200100025](https://openairdocs.org/sdr/CNMA200100025.md): Lever · stuck · Jun 6, 2001 · N450AX · Doug DC1010 · Power Lever
  > AT FLIGHT LEVEL 360 NR 2 ENG THROTTLE BECAME JAMMED AT A POWER SETTING OF 94 PERCENT N1. REPEATED ATTEMPTS WERE MADE TO FREE THROTTLE LEVER, NONE SUCCESSFUL. AFTER ENGINE SHUTDOWN N1 READ 10-13 PERCENT, N2 READ.7 TO 0 PERCENT 2 ENGINE. APPROACH AND LANDING
- [SDR CNMA200100012](https://openairdocs.org/sdr/CNMA200100012.md): Filter · clogged · Apr 14, 2001 · N450AX · Doug DC1010 · Turbine Engine Oil System
  > NR 2 ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED IN FLIGHT. PERFORMED OIL STRAINER CLOG LIGHT ABNORMAL CHECKLIST. CLOG LIGHT REMAINED ILLUMINATED. ENGINE WAS SHUTDOWN BY FLIGHT CREW. MX REPLACED OIL STRAINER FILTER AND OIL CLOG LIGHT SWITCH.
- [SDR AALA20001213](https://openairdocs.org/sdr/AALA20001213.md): Engine · failed · Jul 22, 2000 · N133AA · Doug DC1010 · Engine (Turbine/Turboprop)
  > SFO - FLT 39 - DURING TAKEOFF, IN EXCESS OF 100 KNOTS, THE NR 2 ENGINE FAIL LIGHT ILLUMINATED, REJECTED TAKEOFF, ENGINE NR 2 FLAMED OUT AFTER CLEARING THE RUNWAY. REMOVED AND REPLACED NR 2 ENGINE. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
- [SDR 00FDEA00124](https://openairdocs.org/sdr/00FDEA00124.md): Engine · malfunctioned · Mar 1, 2000 · N375FE · Doug DC1010 · Engine (Turbine/Turboprop)
  > ON ROTATION AIRCREW HEARD LOUD NOISE, SEEMING TO ORIGINATE FROM LEFT SIDE OF A/C. NR 1 EGT AMBER O/H LIGHT ILLUM ON LANDING (AFT LAND). MEM TOWER SAW 2-3 ORANGE FLAMES COMING OUT OF NR 1 ENGINE. REPLACED ENGINE.
- [SDR AALA990882](https://openairdocs.org/sdr/AALA990882.md): Fuel Control · defective · Jun 16, 1999 · N133AA · Doug DC1010 · Fuel Control/Turbine Engines
  > LAX - FLT 162 - DURING APPROACH LAX AT APPROX 1,006 FEET, THE NR 1 ENGINE FLAMED OUT. FUEL PRESSURE WAS ZERO. FUEL PUMPS WERE ON, HAD 5200 LBS OF FUEL IN NR 1 TANK. ENGINE RELIT AT ABOUT 100 FEET AGL. LANDED LAX WITHOUT INCIDENT. REPLACED MAIN ENGINE FUEL
- [SDR HALA9900079](https://openairdocs.org/sdr/HALA9900079.md): Engine · failed · Mar 19, 1999 · N171AA · Doug DC1010 · Engine (Turbine/Turboprop)
  > GEN 3 OFF AND GEN FAIL LIGHTS BOTH ILLUMINATED AND NR 3 AC LOAD INDICATED ZERO. NR 3 CSD OIL PRESS LOW LIGHT ILLUMINATED CSD OIL OUTLET TEMP NORMAL AND RISE TEMP NORMAL FOLLOWED BY INCREASE IN OUTLET TEMP AFTER SEVERAL MINUTES. OUTLET TEMP REDUCED AFTER CSD

Next page: https://openairdocs.org/engine/ge-cf6-6k/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 = 'CF66K'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/ge-cf6-6k/reports

---
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