# Service difficulty reports: GE CF6-6D1A

A list on [GE CF6-6D1A](https://openairdocs.org/engine/ge-cf6-6d1a.md).

Newest first. General aviation reporting is voluntary.

- [SDR FDEA201208313202](https://openairdocs.org/sdr/FDEA201208313202.md): Skin · misrepaired · Aug 31, 2012 · N10060 · Doug MD1010F · Leading Edge Devices
  > LEFT WING NR 7 SLAT UPPER SURFACE INBD UPPER EDGE MISREPAIRED. REPAIRED AS PER EA 8-5750-162580. REPAIR CLASSIFED MAJOR AS PER GMM 6-2-100 REV. 115
- [SDR FDEA201208293194](https://openairdocs.org/sdr/FDEA201208293194.md): Floor Support · corroded · Aug 29, 2012 · N10060 · Doug MD1010F · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR SUPPORT BS 1900 X =60 CORRODED. REMOVED AND REPLACED AS PER DRAWING AGA 7551 REVISION 5 AND AMM 20-50-02 REVISION 14.3. E.O. 8-5100-7-5001B2 PART 2. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.
- [SDR FDEA201208293190](https://openairdocs.org/sdr/FDEA201208293190.md): Strut · misrepaired · Aug 29, 2012 · N10060 · Doug MD1010F · Fuselage Miscellaneous Structure
  > AFT CARGO BAY STRUT, BS 1964 X = -56 MISREPAIRED. REPAIRED AS PER EA 8-5310-159893. REPAIR CLASSIFED MAJOR AS PER GMM 6-2- 100 REV. 115
- [SDR FDEA201208263173](https://openairdocs.org/sdr/FDEA201208263173.md): Floorbeam · misrepaired · Aug 26, 2012 · N10060 · Doug MD1010F · Fuselage Main, Floor Beam
  > CENTER CARGO BAY FLOORBEAM AT BS 1701, LBL 34 MISREPAIRED. FLOORBEAM REMOVED AND REPLACED IAW SRM 51-31-01, VOL.2, REV.99. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 115.
- [SDR FDEA201208213090](https://openairdocs.org/sdr/FDEA201208213090.md): Skin · misrepaired · Aug 21, 2012 · N10060 · Doug MD1010F · Fuselage Main, Plate/Skin
  > SKIN AFT OF CENTER CARGO DOOR CUTOUT AT BS 1801 TO 1821, BETWEEN LONGERON 41 RIGHT AND LONGERON 42 RT MISREPAIRED. CARRIED OUT REPAIR AS PER E.A.#8-5330-159882.
- [SDR FDEA201208213091](https://openairdocs.org/sdr/FDEA201208213091.md): Skin · misrepaired · Aug 21, 2012 · N10060 · Doug MD1010F · Fuselage Main, Plate/Skin
  > FUSELAGE INTERIOR SKIN AT BS 1851, BETWEEN LONGERON 37 AND 38 RT. REPAIRED EA 8-5330-159882. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.
- [SDR FDEA201208203081](https://openairdocs.org/sdr/FDEA201208203081.md): Skin · cracked · Aug 20, 2012 · N10060 · Doug MD1010F · Leading Edge Devices
  > LT WING L/E NR 3 SLAT UPPER SURFACE APPROX AT STATION XOS 515 FOUND WITH SCRATCHES. REPAIRED AS PER SRM 57-10-00 SHEET 1 TO SHEET 2 FIGURE 43 VOLUME 1 REVISION 99. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.
- [SDR FDEA201208203082](https://openairdocs.org/sdr/FDEA201208203082.md): Skin · misrepaired · Aug 20, 2012 · N10060 · Doug MD1010F · Ailerons
  > RT WING INBD AILERON UPPER SKIN MISREPAIRED. REPAIRED AS PER SRM 57-10-00 FIG.85 VOL.I REV.99 SHEET 2. REPAIR CLASSIFED MAJOR AS PER GMM 6-2-100 REV. 115.
- [SDR FDEA201208203080](https://openairdocs.org/sdr/FDEA201208203080.md): Skin · misrepaired · Aug 20, 2012 · N10060 · Doug MD1010F · Trailing Edge Flaps
  > LT WING OTBD FLAP LOWER SKIN MISREPAIRED. REPAIRED AS PER SRM 57-10- 00 FIG.85 VOL.I REV.99. REPAIR CLASSIFED MAJOR AS PER GMM 6-2-100 REV. 115.
- [SDR FDEA201208183070](https://openairdocs.org/sdr/FDEA201208183070.md): Skin · misrepaired · Aug 18, 2012 · N10060 · Doug MD1010F · Leading Edge Devices
  > LEFT WING NR 4 SLAT STATION XOS 645 MISREPAIRED. REPAIR ACCOMPLISHED IAW EA 8-5750-159885. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION115.
- [SDR FDEA201208173042](https://openairdocs.org/sdr/FDEA201208173042.md): Frame · misrepaired · Aug 17, 2012 · N10060 · Doug MD1010F · Fuselage Main, Frame
  > FRAME AT BS 535, LONGERON 19 LT MISREPAIRED. REPAIRED IAW SRM 53-30-00 FIGURE 14 VOLUME I REVISION 99. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.
- [SDR FDEA201208173043](https://openairdocs.org/sdr/FDEA201208173043.md): Frame · misrepaired · Aug 17, 2012 · N10060 · Doug MD1010F · Fuselage Main, Frame
  > FRAME AT CABIN BS 535, LONGERON 23 RT MISREPAIRED. REPAIRED AS PER SRM 53-30-00 FIGURE 13 VOLUME I REVISION 99. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.
- [SDR FDEA201208173044](https://openairdocs.org/sdr/FDEA201208173044.md): Frame · misrepaired · Aug 17, 2012 · N10060 · Doug MD1010F · Fuselage Main, Plate/Skin
  > FRAME AT CABIN BS 535, L19R MISREPAIRED. REPAIRED AS PER SRM 53- 30-00 FIGURE 14 VOLUME 1 REVISION 99. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.
- [SDR FDEA201208173047](https://openairdocs.org/sdr/FDEA201208173047.md): Spar Cap · cracked · Aug 17, 2012 · N10060 · Doug MD1010F · Wing Spar
  > HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON LT WING REAR SPAR LOWER CAP AT XORS 345 FOUND 01 EA CRACK INDICATION ON INBD FORWARD HOLE AT 7 O'CLOCK POSITION FROM FORWARD LOOKING UP. APPROX 0.035 IN LENGTH STARTING FROM UPPER EDGE OF SECOND
- [SDR FDEA201208173048](https://openairdocs.org/sdr/FDEA201208173048.md): Spar Cap · cracked · Aug 17, 2012 · N10060 · Doug MD1010F · Wing Spar
  > HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON LT WING REAR SPAR LOWER CAP AT XORS 345 FOUND TWO CRACK INDICATIONS ON INBD CENTER HOLE AT 7 O'CLOCK AND 10 O'CLOCK POSITION FROM FORWARD LOOKING UP. APPROX 0.025 AND 0.187 INCH LENGTH RESPECTIVE
- [SDR FDEA201208173054](https://openairdocs.org/sdr/FDEA201208173054.md): Frame · misrepaired · Aug 17, 2012 · N10060 · Doug MD1010F · Fuselage Main, Plate/Skin
  > FRAME BS 535, L23L MISREPAIRED. REPAIRED IAW SRM 53-30-00 FIGURE 13 VOLUME I REVISION 99 AND E.A. 8-5310-159883. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.
- [SDR FDEA201208163021](https://openairdocs.org/sdr/FDEA201208163021.md): Seat Track · corroded · Aug 16, 2012 · N10060 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK RT CURVE SEAT TRACK AT BS 1962, X = -107.25 FOUND CORRODED. REPAIRED AS PER SRM 53-70-00, FIGURE 1 VOLIME I, REVISION 99 AND EA 8-5310-159881. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.
- [SDR FDEA201208163020](https://openairdocs.org/sdr/FDEA201208163020.md): Skin · misrepaired · Aug 16, 2012 · N10060 · Doug MD1010F · Fuselage Main, Plate/Skin
  > FORWARD CARGO DOOR CUTOUT EXTERIOR SKIN BS 959, BETWEEN LONGERON 40 - 41 RT MISREPAIRED. CARRIED OUT REPAIR AS PER 53-50-00 FIG.26 VOL.I REV.99. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV.115
- [SDR FDEA201208153003](https://openairdocs.org/sdr/FDEA201208153003.md): Skin · misrepaired · Aug 15, 2012 · N10060 · Doug MD1010F · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN BS 1775 TO 1786, BETWEEN L45 - 46 L MISREPAIRED. CARRIED OUT REPAIR AS PER EA 8-5330-159889 PART 1. REPAIR CLASSIFED MAJOR AS PER GMM 6-2-100 REV. 115.
- [SDR FDEA201208153004](https://openairdocs.org/sdr/FDEA201208153004.md): Skin · misrepaired · Aug 15, 2012 · N10060 · Doug MD1010F · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN BS 1790 - 1801, BETWEEN L44 - 45 L MISREPAIRED. CARRIED OUT REPAIR AS PER EA 8-5330-159889 PART 1. REPAIR CLASSIFED MAJOR AS PER GMM 6-2-100 REV 115.
- [SDR FDEA201208153005](https://openairdocs.org/sdr/FDEA201208153005.md): Skin · dented · Aug 15, 2012 · N10060 · Doug MD1010F · Elevator, Plate/Skin
  > RIGHT INBD ELEVATOR LOWER SURFACE INBD T/E WEDGE FOUND DENTED. REPAIRED IAW SRM 55-33-00, FIG 2, VOLUME I, REV 99. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.
- [SDR FDEA201208142981](https://openairdocs.org/sdr/FDEA201208142981.md): Skin · misrepaired · Aug 14, 2012 · N10060 · Doug MD1010F · Trailing Edge Flaps
  > RT WING INBD FLAP UPPER SKIN STATION XIFH 217 MISREPAIRED. REPAIRED IAW SRM 57-10-00, FIG 85, VOL.1, REV 99 AND EA NR 8-5750-162369. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.
- [SDR FDEA201208142982](https://openairdocs.org/sdr/FDEA201208142982.md): Skin · dented · Aug 14, 2012 · N10060 · Doug MD1010F · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE EXTERIOR SKIN FOUND DENT AT STATION 1995, LONGERON 39 LT. DENT EXCEEDED LIMITS IAW SRM 53-20-00, FIGURE 13, VOL 1, REV 99 CARRIED OUT REPAIR IAW SRM 53-20-00, FIG 6, SHEET 16, VOL 1, REV 99. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.
- [SDR FDEA201208142983](https://openairdocs.org/sdr/FDEA201208142983.md): Skin · misrepaired · Aug 14, 2012 · N10060 · Doug MD1010F · Trailing Edge Flaps
  > RT WING INBD FLAP T/E UPPER SKIN XIFH 207 MISREPAIRED. REPAIRED IAW SRM 57-10-00, FIG 85, VOL 1, REV 99 AND EA 8-5750-162369. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.
- [SDR FDEA201208142990](https://openairdocs.org/sdr/FDEA201208142990.md): Skin · misrepaired · Aug 14, 2012 · N10060 · Doug MD1010F · Trailing Edge Flaps
  > RT WING INBD FLAP T/E UPPER SKIN XIFH 237 MISREPAIRED. REPAIRED IAW SRM 57-10-00, FIG 85, VOL 1, REV 99 AND EA 8-5750-162369. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115
- [SDR FDEA201208142992](https://openairdocs.org/sdr/FDEA201208142992.md): Skin · misrepaired · Aug 14, 2012 · N10060 · Doug MD1010F · Elevator Structure
  > RIGHT OTBD ELEVATOR LOWER SURFACE MISREPAIRED. REPAIRED IAW SRM 55-10-00, FIG 8, VOL 1, REV 99 & EO 8-5100-7-5001B2, PART 2. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.
- [SDR FDEA201208142994](https://openairdocs.org/sdr/FDEA201208142994.md): Skin · misrepaired · Aug 14, 2012 · N10060 · Doug MD1010F · Trailing Edge Flaps
  > LEFT WING INBD FLAP LOWER SURFACE APPROX STATION XIFH 201 MISREPAIRED. REPAIRED IAW EA 8-5750-159899, STEP 1 AND STEP 7. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.
- [SDR FDEA201208142993](https://openairdocs.org/sdr/FDEA201208142993.md): Skin · misrepaired · Aug 14, 2012 · N10060 · Doug MD1010F · Elevator, Plate/Skin
  > LEFT INBD ELEVATOR LOWER SURFACE T/E WEDGE MISREPAIRED. REPAIRED AS PER SRM 55-30-00 FIG.2 VOL.I REV.99. REPAIR CLASSIFED MAJOR AS PER GMM 6-2-100 REV. 115.
- [SDR FDEA201208132964](https://openairdocs.org/sdr/FDEA201208132964.md): Skin · misrepaired · Aug 13, 2012 · N10060 · Doug MD1010F · Cargo/Baggage Doors
  > FORWARD CARGO DOOR LOWER AFT CORNER EXTERIOR SKIN MISREPAIRED. REPAIRED IAW EA NR 8-5230-159887. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.
- [SDR FDEA201208132969](https://openairdocs.org/sdr/FDEA201208132969.md): Skin · misrepaired · Aug 13, 2012 · N10060 · Doug MD1010F · Elevator, Plate/Skin
  > RIGHT INBD ELEVATOR UPPER SURFACE MISREPAIRED. REPAIRED IAW SRM 55-10-00, FIG 8, VOL 1, REV 99. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.
- [SDR FDEA201208132965](https://openairdocs.org/sdr/FDEA201208132965.md): Frame · misrepaired · Aug 13, 2012 · N10060 · Doug MD1010F · Fuselage Main, Frame
  > FRAME MISREPAIRED AT CENTER WHEEL WELL BS 1381, LONGERON 52. REPAIRED IAW SRM 53-30-00, FIG 4 VOLUME I, REV 99. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.
- [SDR FDEA201208132967](https://openairdocs.org/sdr/FDEA201208132967.md): Skin · misrepaired · Aug 13, 2012 · N10060 · Doug MD1010F · Elevator, Plate/Skin
  > LEFT ELEVATOR UPPER SKIN STATION XE 142 MISREPAIRED. REPAIRED IAW SRM 55-10-00, FIG 8, VOL I, REV 99. REPAIR CLASSIFED MAJOR IAW GMM 6-2-100 REV 115.
- [SDR FDEA201208132968](https://openairdocs.org/sdr/FDEA201208132968.md): Skin · misrepaired · Aug 13, 2012 · N10060 · Doug MD1010F · Elevator, Plate/Skin
  > LEFT ELEVATOR UPPER SKIN STATION XE 233 MISREPAIRED. REPAIRED IAW SRM 55-10-00, FIG 8, VOL I, REV 99. REPAIR CLASSIFED MAJOR IAW GMM 6-2-100 REV 115.
- [SDR FDEA201208112942](https://openairdocs.org/sdr/FDEA201208112942.md): Skin · misrepaired · Aug 11, 2012 · N10060 · Doug MD1010F · Leading Edge Devices
  > RT WING NR 1 SLAT UPPER SKIN STATION XIS 168.66 MISREPAIRED. REPAIRED IAW EA NR 8-5750-159897. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.
- [SDR FDEA201208112944](https://openairdocs.org/sdr/FDEA201208112944.md): Skin · misrepaired · Aug 11, 2012 · N10060 · Doug MD1010F · Leading Edge Devices
  > LEFT WING NR 5 SLAT LOWER SKIN XORS 640 MISREPAIRED. REPAIRED IAW SRM 57-10-00, FIG 31, VOL 1, REV 99 AND EA 8-5750-159896. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 115,
- [SDR FDEA201208112945](https://openairdocs.org/sdr/FDEA201208112945.md): Skin · misrepaired · Aug 11, 2012 · N10060 · Doug MD1010F · Leading Edge Devices
  > LT WING L/E NR 7 SLAT LOWER SURFACE STATION XOS 900 MISREPAIRED. REPAIR AS PER EA 8-5750-162583. REPAIR CLASSIFED MAJOR AS PER GMM 6-2-100 REV. 115
- [SDR FDEA201208092903](https://openairdocs.org/sdr/FDEA201208092903.md): Bulkhead · cracked · Aug 9, 2012 · N10060 · Doug MD1010F · Fuselage Main, Bulkhead
  > CENTER LANDING GEAR WHEEL WELL LT VERTICAL BULKHEAD FOUND CRACKED AT BS 1492. REPAIRED IAW EA 8-5310-159894. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.
- [SDR FDEA201208092904](https://openairdocs.org/sdr/FDEA201208092904.md): Structure · deformed · Aug 9, 2012 · N10060 · Doug MD1010F · Cargo/Baggage Doors
  > CENTER CARGO DOOR FORWARD LOWER CORNER FOUND DEFORMED. DEFORMED AREA TRIMMED OUT AND REPAIR CARRIED OUT EA 8-5230-159880. THIS REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.
- [SDR FDEA201208092917](https://openairdocs.org/sdr/FDEA201208092917.md): Skin · misrepaired · Aug 9, 2012 · N10060 · Doug MD1010F · Trailing Edge Flaps
  > LT WING INBD FLAP UPPER SKIN STATION XIFH 133 MISREPAIRED. REPAIR ACCOMPLISHED IAW EA 8-5750-159899, STEP 1 & 2. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.
- [SDR FDEA201009303804](https://openairdocs.org/sdr/FDEA201009303804.md): Skin · dented · Sep 30, 2010 · N40061 · Doug MD1010F · Air Conditioning Doors
  > NR 1 AIRCON COMPARTMENT DOOR - FOUND DENT MARK. REPAIRED AS PER EA 8-5240-143736. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 111.
- [SDR FDEA201009093332](https://openairdocs.org/sdr/FDEA201009093332.md): Longeron · corroded · Sep 9, 2010 · N40061 · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > LOWER FUSELAGE - STA 1521, LONGERON 32L FOUND EXFOLIATION CORROSION. LONGERON REPAIRED IAW EA NR 8-5310-132479. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.
- [SDR FDEA201009093333](https://openairdocs.org/sdr/FDEA201009093333.md): Support Fitting · cracked · Sep 9, 2010 · N40061 · Doug MD1010F · Fuselage Main, Structure
  > CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSP ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLES A, B, C AND D. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II REVISION 96 AND EXISTING REPAIR DOUBLER AND TRIP
- [SDR FDEA201009093334](https://openairdocs.org/sdr/FDEA201009093334.md): Skin · damaged · Sep 9, 2010 · N40061 · Doug MD1010F · Wing, Plate/Skin
  > RIGHT WING NR 3 SLAT TRACK DOOR CUTOUT FOUND DAMAGED. REPAIR CARRIED OUT AS PER SRM 57-00-01 FIG 1A VOLUME I REVISION 96. REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISION 111.
- [SDR FDEA201009053278](https://openairdocs.org/sdr/FDEA201009053278.md): Beam · damaged · Sep 5, 2010 · N40061 · Doug MD1010F · Fuselage Main, Structure
  > CABIN - L3 MED PLUG NR4 DOOR BEAM SUPPORT BRACKET FOUND DAMAGED. DAMAGED SUPPORT BRACKET AT CABIN L3 MED PLUG NR4 DOOR REMOVED IAW SRM 51-31-01 REV 96, VOLUME II. NEW SUPPORT BRACKET FABRICATED IAW DWG ADA3752, REV E AND INSTALLED IAW EA 8-5210-132476 TITLE:
- [SDR 04FDEA03018](https://openairdocs.org/sdr/04FDEA03018.md): Connector · loose · Nov 2, 2004 · N394FE · Doug MD11F · Turbine Engine System Wiring
  > AFTER SETTING MAX PWR AND ABOVE 90 KTS T/O ROLL RECEIVED ENG FAIL LIGHT, NR 1 ENG ROLLED BACK. REJECTED T/O. FOUND FIREWALL CONNECTOR NR P1-8002 NOT PROPERLY SECURED ON THE NR 1 PYLON. INSPECTED PLUG, NO DEFECTS NOTED. SECURED CONNECTOR. OPERATED ENGINE
- [SDR 2001F00260](https://openairdocs.org/sdr/2001F00260.md): Engine · failed · Aug 3, 2001 · N571RY · Doug DC1010 · Engine (Turbine/Turboprop)
  > DURING CLIMB-OUT FROM HNL, CREW NOTED AIRCRAFT VIBRATION FOLLOWED BY NR 2 ENGINE FAILURE. COMPLIED WITH EMERGENCY PROCEDURES CHECK LIST FOR ENGINE SHUT DOWN. JETTISONED FUEL. RETURNED TO HNL AND LANDED WITHOUT INCIDENT. EMERGENCY WAS DECLARED AND EQUIPMENT
- [SDR 00FDEA00728](https://openairdocs.org/sdr/00FDEA00728.md): Engine · inoperative · Oct 21, 2000 · N40061 · Doug DC1010F · Engine (Turbine/Turboprop)
  > NR 2 ENGINE FLAMED OUT NOTICED WHEN ENGINE ANTI-ICE TURN ON AND NR 2 A/I DISAGREE LIGHT CAME ON. *S/D* REMOVED AND REPLACED LINE ENGINE, OPS CK OK.
- [SDR 99ZZZM734](https://openairdocs.org/sdr/99ZZZM734.md): Engine · failed · Oct 7, 1999 · N571SC · Doug DC1010 · Engine (Turbine/Turboprop)
  > FLT 102 - LAX - NR 1 ENGINE EXHAUST GAS TEMPERATURE CAUTION LIGHT CAME ON EARLY ON CLIMB-OUT, NR 1 THRUST HAD TO BE REDUCED TO MAINTAIN EXHAUST GAS TEMPERATURE LIMITS. REPLACED NR 1 ENGINE DUE TO BOROSCOPE DAMAGE FOUND. (M)
- [SDR 99ZZZX805](https://openairdocs.org/sdr/99ZZZX805.md): Engine · malfunctioned · Jan 22, 1999 · N572SC · Doug DC1010 · Engine (Turbine/Turboprop)
  > DELIVERY FLIGHT, POST-HEAVY MAINTENANCE, A POST-TROUBLE FREE 4 HOUR TEST FLIGHT, NR 3 ENGINE CONSUMPTION 3 QUARTS/HOUR AT 95 PERCENT N1. OIL WAS EXITING ENGINE AT CENTRAL JET PIPE BREATHER. ENGINE WAS REMOVED AND SENT FOR INVESTIGATION. ENGINE CYCLES: 18,22

## 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 = 'CF66D1A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/ge-cf6-6d1a/reports

---
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