# Service difficulty reports: N391FE, cancelled Oct 17, 2011

A list on [N391FE, cancelled Oct 17, 2011](https://openairdocs.org/deregistered/N391FE-2011-10-17.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR 06FDEA02929](https://openairdocs.org/sdr/06FDEA02929.md): Landing Gear · collapsed · Jul 28, 2006 · N391FE · Doug DC1010 · Main Landing Gear
  > LEFT MAIN LANDING GEAR COLLAPSED ON LANDING AT MEM. NO WRITE UP AT THIS TIME. UNDER NTSB INVESTIGATION. AIRCRAFT DESTROYED, BEYOND ECONOMICAL REPAIR.
- [SDR 06FDEA2929](https://openairdocs.org/sdr/06FDEA2929.md): Landing Gear · collapsed · Jul 28, 2006 · N391FE · Doug MD1010F · Main Landing Gear
  > LT MAIN LANDING GEAR COLLAPSED ON LANDING AT MEM. NO WRITE UP AT THIS TIME. UNDER NTSB INVESTIGATION.
- [SDR 06FDEA0066](https://openairdocs.org/sdr/06FDEA0066.md): Engine · damaged · Jan 7, 2006 · N391FE · Doug DC1010F · Engine (Turbine/Turboprop)
  > ON T/O ROLL AT ORD AT ABOUT 120KT, RECEIVED ENGINE FAIL ALERT ON NR 2 ENG, NOTED EGT EXCEEDANCE AT 1052DEG, REJECTED. CLEARED RUNWAY, QRH. SHUTDOWN NR 2 ENGINE ON TAXIWAY. RETURNED TO RAMP. DUE TO THE FOD DAMAGE DONE TO THE FAN AND METAL IN THE TAIL PIPE W
- [SDR 05FDEA03312](https://openairdocs.org/sdr/05FDEA03312.md): Tube · loose · Oct 7, 2005 · N391FE · Doug MD1010F · Engine Controls
  > DURING DESCENT THRU FL200, NOTICED NR 2 ENGINE WOULD NOT SPOOL UP FOR LEVEL OFF. N1 REMAINED AT LESS THAN 35 N1, N2 60 PERCENT. NR 2 THROTTLE HAD A VERY LIGHT TRAVEL FORCE AND FELT DISCONNECTED. ACCOMPLISHED RED TABS AND SHUT DOWN ENGINE DUE TO ENGINE BEI
- [SDR 05FDEA02127](https://openairdocs.org/sdr/05FDEA02127.md): Bracket · broken · Jul 28, 2005 · N391FE · Doug MD1010F · Trailing Edge Flap Control System
  > COMPLY WITH EA 8-2750-82100A FLIGHT CONTROL-FLAP-REPLACMENT OF FLAP CONTROL BRACKET. COMPLIED WITH EA 8-2750-82100A. FLIGHT CONTROL FLAP REPLACMENT OF LWR CONTROL BRACKET.
- [SDR 05FDEA01713](https://openairdocs.org/sdr/05FDEA01713.md): Seal · damaged · Jun 28, 2005 · N391FE · Doug MD1010F · Nacelle/Pylon Miscellaneous Structure
  > COMPLY WITH EA 8-5410-82094. NACELLES/PYLON-REPLACEMENT OF DAMAGED PYLON FAIRING SEAL. CLOSING ACTION ON 06/27/05, ON N/R S00083.COMPLIED WITH EA8-5410-82094.
- [SDR 05FDEA01682](https://openairdocs.org/sdr/05FDEA01682.md): Access Panel · cracked · Jun 24, 2005 · N391FE · Doug MD1010F · Nacelle/Pylon, Plate/Skin
  > NR 1 PYLON FUEL LINE INSIDE ACCESS PANEL 517CT HAS IMPROPER STOP DRILL INSIDE RADIUS OF WELD. CRACK APPEARS TO HAVE PROPAGATED ONTO THE WELD. REMOVED AND REINSTALLED AFTER REPAIR PER TRAVELER T5/522336 NR 1 PYLON FUEL LINE INSIDE ACCESS 517CT IAW MM 20-50-
- [SDR 05FDEA01681](https://openairdocs.org/sdr/05FDEA01681.md): Fuel Line · cracked · Jun 24, 2005 · N391FE · Doug MD1010F · Engine Fuel Distribution
  > NR 3 ENGINE FUEL LINE CRACKED ABOVE PYLON AT CONNECTING BRACKET UNDER PANEL 617CT. REMOVED AND REINSTALLED AFTER REPAIR PER TRAVLER T5/527309, NR 3 ENGINE PYLON. MAIN FUEL LINE AT PANEL 617CT IAW MM 20-50-01-2. LEAK CHECK GOOD IAW MM 28-00-02-2.
- [SDR 05FDEA01657](https://openairdocs.org/sdr/05FDEA01657.md): Door · cracked · Jun 22, 2005 · N391FE · Doug MD1010F · Leading Edge Devices
  > RT WING NR 8 SLAT TRACK DOOR HAS CRACK AND WORN. REMOVED AND REPLACED NR 8 SLAT TRACK DOOR IAW MM 57-21-01--2 AND OPS CHECKED GOOD IAW MM 27-80-01-4.
- [SDR 05FDEA01594](https://openairdocs.org/sdr/05FDEA01594.md): Support Fitting · corroded · Jun 13, 2005 · N391FE · Doug MD1010F · Wing, Control Surface Attach Fittings
  > COMPLY WITH EA 8-5750-55487, WINGS - FLAP VANE SUPPORT CORROSION REWORK (RIGHT OUTBOARD FLAP). COMPLIED WITH EA 8-5750-55487.
- [SDR 05FDEA01496](https://openairdocs.org/sdr/05FDEA01496.md): Stiffener · gouged · May 31, 2005 · N391FE · Doug MD1010F · Nacelle/Pylon Miscellaneous Structure
  > COMPLY WITH EA 8-7254-89506 ENGINE - TURBINE - TMF STRUT NR 1 STIFFENER GOUGE REPAIR. COMPLIED WITH EA 8-7254-89506.
- [SDR 04FDEA03482](https://openairdocs.org/sdr/04FDEA03482.md): Proximity Sensor · out of adjust · Dec 24, 2004 · N391FE · Doug MD1010F · Landing Gear Position and Warning
  > AFTER T/O RAISED LANDING GEAR, BOTH PRI AND SEC IND SHOWED LT GEAR NOT UP AND LOCKED. NOTED NO UNUSUAL VIB OR CONT INPUT. C/W QRH AND LOWERED THEN RAISED LANDING GEAR. ALL IND WERE LEFT MAIN GEAR NOT UP AND LOCKED. DECIDED TO RETURN TO RAMP. CTR GAVE US A
- [SDR 04FDEA02436](https://openairdocs.org/sdr/04FDEA02436.md): Control Unit · malfunctioned · Aug 11, 2004 · N391FE · Doug MD1010F · Battery/Charger System
  > IN CRUISE FLIGHT RECEIVED BATTERY DISCHARGING ALERT, BATTERY VOLTAGE WAS 29V. DIVERTED TO TPA. AFTER LANDING GOT: BATTERY CHARGER INOP ALERT. FACT: TROUBLESHOT PER FIM 24-30-01. REMOVED AND REPLACED EPCU PER MM 24-08-01-4. PERFORMED RTS PER MM 24-08-01-
- [SDR 04FDEA01161](https://openairdocs.org/sdr/04FDEA01161.md): Flap · malfunctioned · May 7, 2004 · N391FE · Doug DC1010 · Trailing Edge Flap Control System
  > ON FLAP RETRACTION AFTER T/O, GOT A FLAP DISAGREE LEVEL 2 ALERT. CONFIG PAGE SHOWED FLAPS STILL AT 18 DEG T/O SETTING. ACCOMPLISHED QRH PROCEDURES WITH RESULTS OF INABILITY TO RAISE OR LOWER FLAPS AT ALL. LANDED AT FLAPS 18 DEG/ EXT. CONFIG PAGE SHOWED FLA
- [SDR 03FDEA01977](https://openairdocs.org/sdr/03FDEA01977.md): Attach Fitting · cracked · Nov 24, 2003 · N391FE · Doug DC1010 · Trailing Edge Flap Actuator
  > REMOVE I/B FLAP ACTUATOR CYLINDER ATTACH FITTING STEP'S 1 THRU 8 LEFT SIDE. REMOVED AND INSTALLED FLAP ACTUATOR IAW MM 25-52-01-2 AND ACCOMPLISHED EO 8-5720- 7-2302 STEP NR 1 THRU NR 8 LEFT SIDE FLAP ACTUATOR CYLINDER ATTACH FITTING REPLACEMENT.
- [SDR 03FDEA01978](https://openairdocs.org/sdr/03FDEA01978.md): Attach Fitting · cracked · Nov 24, 2003 · N391FE · Doug DC1010 · Trailing Edge Flap Actuator
  > REMOVE I/B FLAP ACTUATOR CYLINDER ATTACH FITTING STEP'S 1 THRU 8 RIGHT SIDE. REMOVED FLAP ACTUATOR AND INSTALLED IAW MM 27-52-01-2 AND ACCOMPLISHED EO 8-5720- 7-2302 STEP NR 1 THRU NR 8 RIGHT SIDE I/B FLAP ACTUATOR CYLINDER ATTACH FITTING REPLACEMENT.
- [SDR 03FDEA01975](https://openairdocs.org/sdr/03FDEA01975.md): Spar Cap · damaged · Nov 21, 2003 · N391FE · Doug DC1010 · Horizontal Stabilizer, Spar/Rib
  > NR S 15 COMPLY WITH EA8-5510-73851. STABILIZER HORIZONTAL ELONGATED HOLE IN HORIZONTAL STAB UPPER REAR SPAR CAP AD 52-22-10. COMPLIED WITH EA8-5510-73851.
- [SDR 03FDEA01919](https://openairdocs.org/sdr/03FDEA01919.md): Structure · corroded · Nov 17, 2003 · N391FE · Doug DC1010 · Cargo/Baggage Doors
  > COMPLY WITH EA 8-5310-73850 FUSELAGE - CORROSION ON LWR AFT CARGO DOOR LWR RAIL EXTENSION. CLOSING ACTION ON 11/17/03, ON N/R S00011. COMPLIED WITH EA 8-5310-73850.
- [SDR 01FDEA00795](https://openairdocs.org/sdr/01FDEA00795.md): Engine · shutdown · Aug 31, 2001 · N391FE · Doug DC1010 · Engine (Turbine/Turboprop)
  > INFLT SHUTDOWN OF NR 2 ENG IN DESCENT THROTTLES RETARDED.
- [SDR 01FDEA00718](https://openairdocs.org/sdr/01FDEA00718.md): Arm · cracked · Aug 14, 2001 · N391FE · Doug DC1010 · Rudder Control System
  > CAPT'S RUDDER PEDAL TORQUE TUBE ARM ASSY CRACKED AT I/B SIDE INPUT ROD ATTACH POINT RT RUDDER PEDAL. *S/D* REMOVED AND REPLACED RT ARM ASSY PER DAC CMM 27-21-02.
- [SDR 00FDEA00036](https://openairdocs.org/sdr/00FDEA00036.md): Fastener · corroded · Jan 26, 2000 · N391FE · Doug DC1010F · Wing Miscellaneous Structure
  > SNRM #N00581 - RIGHT WING LWR SKIN SURFACE DOUBLER STRAP AT BS XOR & 264 & INNER REAR SPAR APPROX. HAS A CORRODED SHEARED FASTENER. ** S/D ** REMOVED FASTENER, EDDY CURRENTED SURFACE INSP WAS COMPLIED WITH. INSTALL & TORQUED BOLT PER DPS 3.67-60 & MM 20-5
- [SDR 99FDEA00032](https://openairdocs.org/sdr/99FDEA00032.md): Spar Web · cracked · Feb 1, 1999 · N391FE · Doug DC1010F · Wing Spar
  > NR 129 - RT WING REAR SPAR WEB HAS CRACK EMANATING INBD FROM RADIUS OF APU FUEL PUMP HOLE. CRACK APPROX 2.5 INCHES IN LENGTH VER BY NDT. STOP DRILLED CRACK AND PLUG HOLE IAW SRM 51-00-02 AND 53-00-01 WEB DOUBLER INSTALL PER EA 8-5710-40417.
- [SDR 98FDEA00204](https://openairdocs.org/sdr/98FDEA00204.md): Frame · cracked · Feb 17, 1998 · N391FE · Doug DC1010F · Fuselage Main, Frame
  > STA 459 Z=-78, X=-63 A CRACK WAS FOUND ON THE FRAME LT SIDE. REF NRC NR N 2064. REPAIRED FRAME IAW SRM 53-30-00 FIG 5.
- [SDR 98FDEA00140](https://openairdocs.org/sdr/98FDEA00140.md): Frame · cracked · Feb 17, 1998 · N391FE · Doug DC1010F · Fuselage Main, Frame
  > VCE: N2103 - AT STA NR 459 Z= -78, X = - 63 A CRACK WAS FOUND ON THE FRAME (RT SIDE). REF NRC NR N2064. REPAIRED FRAME IAW SRM 53-30-00, FIG 5.
- [SDR 97FDEA00490](https://openairdocs.org/sdr/97FDEA00490.md): Clip · cracked · Jul 30, 1997 · N391FE · Doug DC1010 · Wing Miscellaneous Structure
  > AT STA XORS - 402, STRINGER NR 37, FOUND CLIP CRACKED ON RIGHT WING LOWER SURFACE. *S/D* REMOVED AND REPLACED CLIP (REF DWG ARB 0807), PER SRM 51-31-01.
- [SDR 97FDEA00489](https://openairdocs.org/sdr/97FDEA00489.md): Clip · cracked · Jul 30, 1997 · N391FE · Doug DC1010 · Wing Miscellaneous Structure
  > AT XORS - 402, STRINGER NR 36, FOUND CLIP CRACKED ON RIGHT WING LOWER SURFACE. *S/D* REMOVED AND REPLACED CLIP (REF DWG ARB 0807), PER SRM 51-31-01.

## 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 n_number = 'N391FE' AND deregistration_id = 'N391FE-2011-10-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N391FE-2011-10-17/reports

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