# Service difficulty reports: N314FE, cancelled Jul 9, 2013

A list on [N314FE, cancelled Jul 9, 2013](https://openairdocs.org/deregistered/N314FE-2013-07-09.md).

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

- [SDR FDEA201203020739](https://openairdocs.org/sdr/FDEA201203020739.md): Anti-Ice Valve · failed · Mar 2, 2012 · N314FE · Doug MD1030F · Airfoil Anti/De-ice System
  > ON CLIMB OUT, RECEIVED LT WING ANTI-ICE DISAGREE. WING ANTI-ICE WAS CYCLED OFF-ON BUT SAME RESULT. TRIED A SECOND ON-OFF CYCLE AND SAME RESULT. ALSO RECEIVED NR 1 AIR SYSTEM MANIFOLD FAILURE ALERT. DUMPED 9000 POUNDS FUEL AND RETURNED TO SEA. R & R L
- [SDR FDEA201203020738](https://openairdocs.org/sdr/FDEA201203020738.md): Anti-Ice Valve · failed · Mar 2, 2012 · N314FE · Doug MD1030F · Airfoil Anti/De-ice System
  > ON CLIMB OUT, RECEIVED LEFT WING ANTI-ICE DISAGREE. WING ANTI-ICE WAS CYCLED OFF-ON BUT SAME RESULT. TRIED A SECOND ON-OFF CYCLE AND SAME RESULT. ALSO RECEIVED NR 1 AIR SYSTEM MANIFOLD FAILURE ALERT. DUMPED 9000 POUNDS FUEL AND RETURNED. R & R LEFT WING
- [SDR FDEA201109093812](https://openairdocs.org/sdr/FDEA201109093812.md): Support Fitting · cracked · Sep 9, 2011 · N314FE · Doug MD1030F · Fuselage Main, Structure
  > MAIN CARGO DOOR FRAME, CENTERING GUIDE, LOWER AFT SUPPORT FITTING CRACKED. FABRICATED & INSTALLED SUPPORT FITTING.
- [SDR FDEA201101070067](https://openairdocs.org/sdr/FDEA201101070067.md): Static Inverter · inoperative · Jan 7, 2011 · N314FE · Doug MD1030F · AC Inverter
  > EMERGENCY POWER TEST FAIL. TROUBLESHOT IAW FIM 24-24-00 FAULT D. FOUND STATIC INVERTER BAD. R & R STATIC INVERTER IAW AMM 24-24-01-2, OK FOR SERVICE.
- [SDR FDEA201005121519](https://openairdocs.org/sdr/FDEA201005121519.md): Wire Harness · damaged · May 12, 2010 · N314FE · Doug MD1030F · Engine Indicating System Wiring
  > ON CLIMB OUT OF ANC - NR3 ENGINE EGT GAGE FLUCTUATED WILDLY OUT OF 20,000 FT HIT 1020 GOT "ENG 3 EXCEEDANCE ALL ENG 3 OIL, TEM, PRESSURE SHOWED NORMAL DUMPED FUEL RETURNED TO DEPARTURE. ANC R EGT INDICATION NORMAL AFTER SHUTDOWN, VISUAL INSP OF HARNESS A
- [SDR FDEA201003040649](https://openairdocs.org/sdr/FDEA201003040649.md): Warning Light · illuminated · Mar 4, 2010 · N314FE · Doug DC1030F · Central Warning
  > AT CRUISE ALTITUDE 350, RECEIVED LEVEL 3 ALERT "AIR MANF 2 FAIL" COMPLIED WITH QRH AND PROCEEDED TO NEAREST SUITABLE KOKC FOUND SYSTEM TEST GOOD PER AMM 36-23-01-4.AS PRECAUTIONARY PERFORMED DECAY CHECK ON ALL 3 MANIFOLDS PER AMM 36-00-01-5.ALL MANIFOLDS
- [SDR FDEA201002230494](https://openairdocs.org/sdr/FDEA201002230494.md): Clamp · loose · Feb 23, 2010 · N314FE · Doug DC1030F · Compressor Bleed Control
  > BASED ON MX REPORT, DECIDED TO GIVE A LITTLE EXTRA TIME FOR ACCELERATION. IT WAS NECESSARY TO GO FULL QUADRANT TO GET CLOSE TO TAKEOFF POWER. WHEN THE AUTOFLIGHT TILE WAS PRESSED ENG 1 AND 2 REACHED TAKEOFF POWER, ENG NR 3 WAS LAGGING ABOUT 15 PERCENT BELOW
- [SDR FDEA201001080044](https://openairdocs.org/sdr/FDEA201001080044.md): Throttle · malfunctioned · Jan 8, 2010 · N314FE · Doug DC1030F · Power Lever
  > AFTER TAKEOFF, DURING CLEAN-UP, THROTTLES WOULD CONTINUOUSLY RETARD DUE TO AN UPPER FOOT ON THE PFD LOWERING BELOW PRESENT AIRSPEED. EVEN WITH AUTO THROTTLES OFF, THE THROTTLES WOULD NOT STAY ADVANCED PROBABLY DUE TO THE AIRPLANE TRYING TO PROTECT ITSELF DUE T
- [SDR FDEA200911143954](https://openairdocs.org/sdr/FDEA200911143954.md): Spar Cap · cracked · Nov 14, 2009 · N314FE · Doug DC1030F · Horizontal Stabilizer, Spar/Rib
  > LT HORIZ STABILIZER L/E, FOUND 1EA CRACK 1,5" LONG ON UPPER FRONT SPAR CAP AT XE 115 REPAIRED IAW SRM 55-20-00 VOL 1, FIG9.
- [SDR FDEA200910063482](https://openairdocs.org/sdr/FDEA200910063482.md): Skin · dented · Oct 6, 2009 · N314FE · Doug DC1030F · Cargo/Baggage Doors
  > DURING INSP EXT FUSELAGE LWR SURFACE FOUND 1 EA DENT ON SKIN OF CTR CARGO DOOR 4"X2" DEEP.120". REPAIRED DENT IAW SRM 52-10-00, FIG 6, VOL I.
- [SDR FDEA200909233370](https://openairdocs.org/sdr/FDEA200909233370.md): Skin · dented · Sep 23, 2009 · N314FE · Doug DC1030F · Trailing Edge Flaps
  > RT WING INBD FLAP UPPER SKIN FOUND DEEP DENT AND OIL CANING 2.50 INCH X 1.50 INCH DEEP.055 INCH. REPAIRED AREA IAW SRM 57-10-00 FIG 85 SHT 1-4 VOL I.
- [SDR FDEA200908313170](https://openairdocs.org/sdr/FDEA200908313170.md): Door Frame · corroded · Aug 31, 2009 · N314FE · Doug DC1030F · Fuselage Main, Structure
  > INSPECTED UPPER CARGO DOOR JAMB STRUCTURE CORROSION ON UPPER DOOR JAMB. ACCOMPLISHED EA NR 8-5310-129649.
- [SDR FDEA200908102964](https://openairdocs.org/sdr/FDEA200908102964.md): Channel · corroded · Aug 10, 2009 · N314FE · Doug DC1030F · Fuselage Miscellaneous Structure
  > CTR CARGO COMPT REF EO 8-2550-7-2354 P2 STEP "E1" AFTER REMOVAL PARTS FOUND DEEP CORROSION ON CHANNEL. REPAIRED AREA IAW SRM 53-70-00 FIG 7 SHT 5 VOL I.
- [SDR FDEA200907282794](https://openairdocs.org/sdr/FDEA200907282794.md): Skin · cracked · Jul 28, 2009 · N314FE · Doug DC1030F · Wing, Plate/Skin
  > LT WING L/E FOUND CRACKED ON LOWER EXT SKIN L/E. REPAIRED AREA IAW SRM 57-10-00 FIG 68 SHT 2 VOL I.
- [SDR FDEA200907282793](https://openairdocs.org/sdr/FDEA200907282793.md): Skin · cracked · Jul 28, 2009 · N314FE · Doug DC1030F · Leading Edge Devices
  > LT WING EXT STRUCTURE FOUND CRACKED ON LWR EXT SKIN L/E SLAT NR 4. REPAIRED AREA IAW SRM 57-00-01 FIG 4 SHT 2 & SRM 57-10-00 FIG 43 VOL I.
- [SDR FDEA200907202671](https://openairdocs.org/sdr/FDEA200907202671.md): Beam · cracked · Jul 20, 2009 · N314FE · Doug DC1030F · Fuselage Main, Structure
  > CTR CARGO BILGE INSP FOUND CRACK ON BEAM. REPAIRED AREA IAW SRM 53-00-01 FIG 9 SHT 9 VOL I.
- [SDR FDEA200907202670](https://openairdocs.org/sdr/FDEA200907202670.md): Hinge · nicked · Jul 20, 2009 · N314FE · Doug DC1030F · Wing, Control Surface Attach Fittings
  > LT WING INBD FLAP FOUND ON OUTBD HINGE "ON WING" INBD SIDE DEEP NICKS. REPAIRED AREA IAW SRM 57-20-00 FIG 17 SHT 1 VOL I.
- [SDR FDEA200907202668](https://openairdocs.org/sdr/FDEA200907202668.md): Angle · cracked · Jul 20, 2009 · N314FE · Doug DC1030F · Fuselage Miscellaneous Structure
  > UPPER INT. FUSELAGE COMPT "ZONE 312" DURING REPAIR ASSESSMENT WITH EO 8-5100-7- 5001-P2. FOUND CRACK ON ANGLE UPPER SIDE AFT VERTICAL BULKHEAD. REPAIRED CRACK IAW SRM 53-30-00 FIG 2B VOL I.
- [SDR FDEA200907132601](https://openairdocs.org/sdr/FDEA200907132601.md): Skin · cracked · Jul 13, 2009 · N314FE · Doug DC1030F · Trailing Edge Flaps
  > RT WING EXT SURFACE FOUND CRACK ON UPPER EXT SKIN OTBD FLAP. REPAIRED SKIN IAW SRM 57-10-00 FIG 85 VOL I.
- [SDR FDEA200907112584](https://openairdocs.org/sdr/FDEA200907112584.md): Skin · dented · Jul 11, 2009 · N314FE · Doug DC1030F · Trailing Edge Flaps
  > LT WING EXT FOUND 2 EA DENTS ON INBD FLAP LOWER EXT. SKIN LWR PNL. 1): 0.75 INCH X 0.50 INCH MAX DEEP 0.070 INCH. 2): 0.50 INCH X 0.50 INCH MAX DEEP 0.060 INCH. REPAIRED AREA IAW SRM 57-00-01 FIG 4 SHT 2 VOL I.
- [SDR FDEA200907112583](https://openairdocs.org/sdr/FDEA200907112583.md): Skin · dented · Jul 11, 2009 · N314FE · Doug DC1030F · Trailing Edge Flaps
  > LT WING EXT FOUND 1 EA DENT.75 INCH X 1 INCH MAX DEEP.060 INCH ON INBD FLAP LWR EXT. SKIN LWR PANEL. REPAIRED AREA IAW SRM 57-00-01 FIG 4 SHT 2 VOL I.
- [SDR FDEA200907012435](https://openairdocs.org/sdr/FDEA200907012435.md): Skin · loose · Jul 1, 2009 · N314FE · Doug DC1030F · Wing, Plate/Skin
  > RT WING EXT SURFACE FOUND NR 180 EA LOOSE FASTENERS ON UPPER EXT SKIN OUTBD FLAP. REPAIRED SKIN IAW SRM 57-10-00 FIG 85 & SRM 57-20-00 FIG 2 VOL I.
- [SDR FDEA200906262319](https://openairdocs.org/sdr/FDEA200906262319.md): Skin · cracked · Jun 26, 2009 · N314FE · Doug DC1030F · Wing, Plate/Skin
  > RT WING LWR EXT SURFACE FOUND CRACKS AND NR 100 EA LOOSE FASTENERS ON LWR EXT SKIN OTBD FLAP. REPAIRED AREA IAW SRM 57-10-00 FIG 7, SHT 3, VOL I.
- [SDR FDEA200906262318](https://openairdocs.org/sdr/FDEA200906262318.md): Frame · worn · Jun 26, 2009 · N314FE · Doug DC1030F · Fuselage Main, Frame
  > DURING INSP LT AIR COND FOUND DEEP WEAR ON FRAME. REPAIRED AREA IAW SRM 53-30-00 FIG 4 & 4A VOL I.
- [SDR FDEA200906262317](https://openairdocs.org/sdr/FDEA200906262317.md): Frame · cracked · Jun 26, 2009 · N314FE · Doug DC1030F · Fuselage Main, Frame
  > DURING INSPECTION LT AIR COND FOUND CRACK ON FRAME. REPAIRED AREA IAW SRM 53-30-00 FIG 4 VOL I.
- [SDR FDEA200906262316](https://openairdocs.org/sdr/FDEA200906262316.md): Frame · worn · Jun 26, 2009 · N314FE · Doug DC1030F · Fuselage Main, Frame
  > DURING INSP AVIONIC COMPT BILGE AREA FOUND DEEP WEAR ON FRAME. REPAIRED AREA IAW SRM 53-30-00 FIG 4, VOL I.
- [SDR FDEA200906232239](https://openairdocs.org/sdr/FDEA200906232239.md): Membrane · cracked · Jun 23, 2009 · N314FE · Doug DC1030F · Fuselage Miscellaneous Structure
  > AFTER REMOVAL PANELS ON FLIGHT COMPT WITH OAN J/C 0600C210-1JR FOUND CRACK ON MEMBRANE. REPAIRED MEMBRANE IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.
- [SDR FDEA200906232238](https://openairdocs.org/sdr/FDEA200906232238.md): Membrane · cracked · Jun 23, 2009 · N314FE · Doug DC1030F · Fuselage Miscellaneous Structure
  > AFTER REMOVAL PANELS ON FLIGHT COMPT WITH OAN J/C 0600C210-1JR FOUND CRACK ON MEMBRANE. REPAIRED MEMBRANE IAW SRM 53-00-01, FIG 4, SHT 2, VOL I.
- [SDR FDEA200906122044](https://openairdocs.org/sdr/FDEA200906122044.md): Skin · cracked · Jun 12, 2009 · N314FE · Doug DC1030F · Horizontal Stabilizer, Plate/Skin
  > DURING INSP OF COSTANT SECTION STB, FOUND UP PANEL, INSP POSITION 3, WITH CRACK IN FLYABLE LIMITS, ACCOMPLISHED EA NR 8-5510-129688.
- [SDR 08FDEA03885](https://openairdocs.org/sdr/08FDEA03885.md): Line · leaking · Sep 15, 2008 · N314FE · Doug DC1030F · Hydraulic System, Main
  > CENTER GEAR FAILED TO EXTEND WITH GEAR HANDLE. RAN CHECK LIST, CENTER GEAR EXTENDED WHEN THE CENTER GEAR ALTERNATE EXTENSION HANDLE WAS PULLED. ON LANDING ROLLOUT HYD QUE ILLUMINATED, HYD SYS 3 ELEV ILLUMINATED. FOUND HYD LINE TO CENTER GEAR UNLOCK CYLINDE
- [SDR FDEA200807182982](https://openairdocs.org/sdr/FDEA200807182982.md): Engine · failed · Jul 18, 2008 · N314FE · Doug DC1030F · Engine (Turbine/Turboprop)
  > DURING DEPARTURE NR 1 ENGINE HAD LOUD BANG AND VIBRATION. NR 1 ENG TO IDLE AND THEN OIL QUANTITY WENT TO ZERO, NO N1. PERFROMED PHASE 1'S AND QRH PROCEDURE. RETURN TO MEM FOR ENGINE OUT LANDING. MX MEM - INSPECTED NR 1 ENGINE. FOUND OIL PUDDLED IN EXHAU
- [SDR 08FDEA02982](https://openairdocs.org/sdr/08FDEA02982.md): Engine · failed · Jul 18, 2008 · N314FE · Doug DC1030F · Engine (Turbine/Turboprop)
  > DURING DEPARTURE NR 1 ENGINE HAD LOUD BANG AND VIBRATION. NR 1 ENG TO IDLE AND THEN OIL QUANTITY WENT TO ZERO, NO N1. PERFORMED PHASE 1'S AND QRH PROCEDURE. RETURN TO MEM FOR ENGINE OUT LANDING. MX MEM, INSPECTED NR 1 ENGINE. FOUND OIL PUDDLED IN EXHAUS
- [SDR 03FDEA00337](https://openairdocs.org/sdr/03FDEA00337.md): Anti-Ice System · inoperative · Mar 19, 2003 · N314FE · Doug DC1030 · Windshield/Door Rain/Ice Removal
  > RIGHT WINDSHIELD ANTI/ICE INOPERATIVE LIGHT ILLUMINATED SHORTLY AFTER TAKE OFF. REMOVED AND REPLACED RIGHT WINDSHIELD IAW M.M. 56-11-00-2. REMOVED AND REPLACED WINDSHIELD ANTI/ICE CONTROLLER IAW MM 30-41-01-2. GROUND OPS CHECK NORMAL.
- [SDR 02FDEA00383](https://openairdocs.org/sdr/02FDEA00383.md): Transmitter · leaking · Jun 6, 2002 · N314FE · Doug DC1030 · Hydraulic Pressure Sensor
  > AFTER 2+15 OF FLT HYD SYS 3 ELEV OFF LIGHT ILLUMINATED. PERFORMED RED TABS, WITH FLUID DOWN TO 4.5 GALS. WHEN ENG 3 HYD PUMPS TURNED BACK ON, STARTED TO SLOWLY DECREASE TO 3.5 GALS. ENG HYD PUMPS TURNED OFF WITH QTY HOLDING AT 3.5 GALS. ON LANDING APPROX,
- [SDR 02FDEA00355](https://openairdocs.org/sdr/02FDEA00355.md): Seal · split · May 19, 2002 · N314FE · Doug DC1030 · Hydraulic Pressure Sensor
  > HYD SYS 3 ELEV OFF LIGHT ILLUMINATED. PRESSURE WAS NORMAL, QTY ABOUT 4.5 GALS. RAN RED TABS. LANDED AT TJSJ. HYD LEAK CONFIRMED BY COMPANY MX AFTER LANDING. UPON EXAMINATION, FOUND LEAK TO BE COMING FROM NR 3 HYD PRESSURE XMITTER. REMOVED XMITTER AND FOU
- [SDR 02FDEA00219](https://openairdocs.org/sdr/02FDEA00219.md): Periseal · failed · Mar 26, 2002 · N314FE · Doug DC1030F · Pneumatic Distribution System
  > AFTER T/O NR 3 PNEU MANIFOLD FAIL LIGHT ILLUMINATED. REMOVED AND REPLACED PERISEALS PER SMP.
- [SDR 01FDEA00025](https://openairdocs.org/sdr/01FDEA00025.md): Sensor · damaged · Jan 17, 2001 · N314FE · Doug DC1030F · Landing Gear Position and Warning
  > AFT T/O AND LAND GEAR UP S/O PNL IND RED UNSAFE NOSE GEAR. RECYCLED LG AND NOSE RED UNSAFE LIGHT ON EXT AND RETRACTION. *S/D* REPLACED DAMAGED NOSE GEAR LOCKED SENSOR PER A/W/D 32-61-04 PG 1 D1-79 AND S/M/P CHAP 20 MM 32-61-03-2. OPS CK NORMAL.
- [SDR 00FDEA00782](https://openairdocs.org/sdr/00FDEA00782.md): Tire · disintegrated · Nov 19, 2000 · N314FE · Doug DC1030F · Brake
  > 00-317 NR 3 & 4 TIRE REQUIRES REPLACEMENT DUE TO DISINTEGRATION ON T/O OUT OF CDG. R&R NR 3, 4, 7, 8 TIRES, & DAMAGED PANELS 152PT, 152MT, 152NT, PER MM 20-21-01-2.
- [SDR 00FDEA00729](https://openairdocs.org/sdr/00FDEA00729.md): Controller · malfunctioned · Oct 21, 2000 · N314FE · Doug DC1030F · Leading Edge Slat Control System
  > DURING CLIMB HAD UNCOMMANDED AUTO SLAT EXTENSION.
- [SDR 00FDEA00307](https://openairdocs.org/sdr/00FDEA00307.md): Valve · failed · May 1, 2000 · N314FE · Doug DC1030F · Cabin Cooling System
  > LOUD BANG FROM REAR OF A/C PRESS BUMP FELT. REMOVED AND REPLACED AIR CONDITIONING SYS AIR CK VALVE IN REF TO AMM 21-22-03-2. OPS CK NORM.
- [SDR 00FDEA0025](https://openairdocs.org/sdr/00FDEA0025.md): Connector · failed · Jan 18, 2000 · N314FE · Doug DC1030F · Hydraulic Pump (Electric/Engine), Main
  > NR 751 - RT W/W FWD INBD ELECT HYD PUMP CANNON PLUG WAS A SHORTED WIRE. PUMP HAD 2 EA SHORT WIRES CAUSING ELECTRICAL FIRE.
- [SDR 00FDEA00025](https://openairdocs.org/sdr/00FDEA00025.md): Connector · failed · Jan 18, 2000 · N314FE · Doug DC1030F · Hydraulic Pump (Electric/Engine), Main
  > NR 751 - RT W/W FWD INBD ELECT HYD PUMP CANNON PLUG WAS A SHORTED WIRE. PUMP HAD 2 EA SHORT WIRES CAUSING ELECTRICAL FIRE. REPLACED WIRE HARNESS, PLUG CONNECTOR PER WD/M 29-21-01, 29-21-02. REPLACED HYD PUMP AND ELECT MOTOR PER MM 29-21-01-2. OPS AND LEAK
- [SDR 99FDEA00013](https://openairdocs.org/sdr/99FDEA00013.md): Transmitter · failed · Jan 14, 1999 · N314FE · Doug DC1030F · Trailing Flap Position Indicating System
  > 99-0013 - ON T/O FLAP LIMIT CHANNEL INOP AND SELECT FLAP LIMIT OVERRIDE LIGHT ILL IN READ 10 DEG LT SIDE AND 4 DEG RT SIDE. FOUND LT OTBD FLAP POS TRANSMITTER BAD. REMOVED AND REPLACED SAME PER MM 27-54-03-2. OPS CK GOOD. FOUND DUPLEX ACTUATOR INOP MM 27-5
- [SDR 98FDEA00692](https://openairdocs.org/sdr/98FDEA00692.md): Temp Gauge · inop · Nov 10, 1998 · N314FE · Doug DC1030F · Hydraulic Indicating System
  > NR 3 HYDRAULIC TEMP HAD SLOWLY INCREASED IN TEMP AFTER T/O. TEMP 108C, NO TEMP LIGHT, PRESS TO TEST WAS OK. REMOVED AND REPLACED HYDRAULIC GAUGE AFTER TROUBLESHOOTING, RAN SYS, OK FOR SERVICE MM 29-33-01.
- [SDR 97FDEA00907](https://openairdocs.org/sdr/97FDEA00907.md): Control Unit · failed · Dec 19, 1997 · N314FE · Doug DC1030F · Landing Gear Retraction/Extension System
  > 97-0260 - ON T/O CTR AND RT GEAR RED LIGHTS WERE SLOW TO EXTINGUISH, LEFT GEAR LIGHT WENT FROM EXTINQUISHED TO RED RECYCLE GEAR AND ALL LIGHTS EXTINGUISHED. ON LANDING, ALL GEAR LIGHTS AND WARNING HORNS INDICATED UNSAFE, RECYCLED GEAR AND INITIALLY LEFT AND R

## 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 = 'N314FE' AND deregistration_id = 'N314FE-2013-07-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N314FE-2013-07-09/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.