# Service difficulty reports: N317FE, cancelled Feb 1, 2024 A list on [N317FE, cancelled Feb 1, 2024](https://openairdocs.org/deregistered/N317FE-2024-02-01.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 88 reports - [SDR FDEA201411263910](https://openairdocs.org/sdr/FDEA201411263910.md): Generator · contaminated · Nov 26, 2014 · N317FE · Doug MD1030F · AC Generator-Alternator > AFTER TAKEOFF LOST NR 1 GENERATOR THEN NR 3. STARTED APU, AND ABLE TO REGAIN BUSS 1 BUT NOT BUSS 3. MULTIPLE ALERTS, FOLLOWED QRH. RECEIVED NUMEROUS ALERTS AGAIN AT TOP OF DESCENT. LANDED WITHOUT INCIDENT. FOUND WATER ON MAIN DECK, LOOKED IN CAC FOUND BO - [SDR FDEA201409072502](https://openairdocs.org/sdr/FDEA201409072502.md): Gcu · failed · Sep 7, 2014 · N317FE · Doug MD1030F · AC Regulator > APPROX 1 MIN AFTER TAKEOFF, RUNWAY 36R, GEN 3 OFF. ALERT SHORTLY AFTER THAT GEN 1 OFF. ALERT ACCOMPLISHED GEN 3 DISCONNECTED AFTER GEN 3 FAIL ALERT, 10 SEC AFTER 1ST ALERT. GEN 1 RESET ONCE, BUT SUBSEQUENTLY FAILED AGAIN. GEN 1 DISCONNECT IAW QRH. FINALLY - [SDR FDEA201406121413](https://openairdocs.org/sdr/FDEA201406121413.md): Probe · blocked · Jun 12, 2014 · N317FE · Doug MD1030F · Pitot/Static System > FIRST OFFICERS’ AIRSPEED ERRATIC. HAD IAS MISCOMPARE CUE. RECEIVED WINDS HEAR DET FAIL, SEL ELEV FEEL MAN, SEL FLAP LIMIT OVRD. CAPTAIN`S SIDE NORMAL. PERFORMED INSPECTION OF PITOT PROBES, FOUND THE FIRST OFFICER`S PROBE TO BE BLOCKED. IAW MM 34-11-02-2 R - [SDR FDEA201405261197](https://openairdocs.org/sdr/FDEA201405261197.md): Skin · cracked · May 26, 2014 · N317FE · Doug MD1030F · Wing, Plate/Skin > DURING SERVICE CHECK FOUND POSSIBLE CRACK AT SLAT DRIVE MECH DOOR FWD INBD CORNER RT WING. PERFORMED HFEC, ON RT WING AT SLAT DRIVE MECH DOOR FWD INBD CORNER, TO VERIFY CRACK IAW NTM PT 6. TWO EACH CRACKS VERIFIED IN AREA. CUT OUT CRACK IAW SRM 57-10-00 CR - [SDR FDEA201310142498](https://openairdocs.org/sdr/FDEA201310142498.md): Sensor · malfunctioned · Oct 14, 2013 · N317FE · Doug MD1030F · Navigation System > AT FL 330, THROTTLES CAME TO IDLE, ACFT BEGAN A SLIGHT CLIMB, AND A "AUTOSLAT FAIL" ALERT. ANOTHER SLIGHT PITCH UP, AND CONFIGURATION PAGE SHOWED RT WING FLAPS TRYING TO EXTEND. INDICATION WAS WHITE BOXES BELOW RT WING, BUT NO NUMBERS INDICATING. STICKSHAKE - [SDR FDEA201305100971](https://openairdocs.org/sdr/FDEA201305100971.md): Web · cracked · May 10, 2013 · N317FE · Doug MD1030F · Nacelle/Pylon, Main Frame > HOLES OUT OF LIMITS ON WEB AUB7366-501. R & R UPPER PYLON SPAR WEB IAW DWG AUB7301 AND SRM 51-33-01, VOL. II INSTRUCTIONS. - [SDR FDEA201305100970](https://openairdocs.org/sdr/FDEA201305100970.md): Bulkhead · cracked · May 10, 2013 · N317FE · Doug MD1030F · Nacelle/Pylon, Bulkhead/Firewall > NR 1 ENGINE PYLON AFT BULKHEAD UPPER INBD CORNER FLANGE AREA INSIDE HAS A DISCONTINUITY INDICATION WHICH WAS CONFIRMED BEING CRACKED APPROX.5" BY VERIFYING WITH BOROSCOPE INSPECTION AS SEEN THROUGH THE FOOTBALL PANEL. R & R THE AFT PYLON BULKHEAD IAW EA 8- - [SDR FDEA201304270868](https://openairdocs.org/sdr/FDEA201304270868.md): Beam · cracked · Apr 27, 2013 · N317FE · Doug MD1030F · Cargo/Baggage Doors > FWD CARGO DOOR BALANCE BEAM CRACKED AND BROKEN. R & R FWD CARGO DOOR BEAM ASSY IAW CMM 52-31-03, STEP 21(D). - [SDR FDEA201304230836](https://openairdocs.org/sdr/FDEA201304230836.md): Doubler · cracked · Apr 23, 2013 · N317FE · Doug MD1030F · Fuselage Main, Bulkhead > WHEEL WELL SUSPECT A CRACK ON LT KEEL BEAM BULKHEAD MACHINED DOUBLER. REMOVED AND REPLACED CRACKED DOUBLER AEA 0526U1 - [SDR FDEA201304230837](https://openairdocs.org/sdr/FDEA201304230837.md): Doubler · cracked · Apr 23, 2013 · N317FE · Doug MD1030F · Fuselage Main, Structure > WHEEL WELL CRACKED ON RT KEEL BEAM BULKHEAD MACHINED DOUBLER AT BS 1386 AT X 31.5. R & R CRACKED DOUBLER AEA 0526U2, REF SRM 51-33-01, VOL 2. - [SDR FDEA201209273479](https://openairdocs.org/sdr/FDEA201209273479.md): Structure · damaged · Sep 27, 2012 · N317FE · Doug MD1030F · Elevator Structure > RIGHT ELEVATOR, AT GAP BETWEEN THE INNER AND OUTER ELEVATORS. DAMAGE TO THE T/E PIECE ON THE UPPER AND LOWER SURFACE THAT RUNS APPROX 10" FROM THE INNER EDGE TOWARDS THE OUTER EDGE RELATIVELY PARALLEL TO THE LONGITUDINAL AXIS OF THE ELEVATOR. REPAIRED IAW SRM - [SDR FDEA201207052488](https://openairdocs.org/sdr/FDEA201207052488.md): Transducer · failed · Jul 5, 2012 · N317FE · Doug MD1030F · Brake Anti-Skid Section > SOON AFTER GEAR EXTENSION, RECEIVED A LEVEL 2 'ANTISKID FAIL' ALERT. COMPLIED WITH QRH AND LANDED ACFT. DURING ROLL-OUT, TOWER REPORTED THAT AT LEAST 1 TIRE HAD FAILED. CALLED FOR CRASH TRUCK. THEY REPORTED NO SEVERE DAMAGE, BUT THAT WE HAD 2 FAILED TI - [SDR FDEA201207052487](https://openairdocs.org/sdr/FDEA201207052487.md): Transducer · failed · Jul 5, 2012 · N317FE · Doug MD1030F · Brake Anti-Skid Section > SOON AFTER GEAR EXTENSION, RECEIVED A LEVEL 2 'ANTISKID FAIL' ALERT. COMPLIED WITH QRH AND LANDED ACFT. DURING ROLL-OUT, TOWER REPORTED THAT AT LEAST ONE TIRE HAD FAILED. CALLED FOR CRASH TRUCK. THEY REPORTED NO SEVERE DAMAGE, BUT THAT WE HAD 2 FAILED T - [SDR FDEA201206262355](https://openairdocs.org/sdr/FDEA201206262355.md): Lead · malfunctioned · Jun 26, 2012 · N317FE · Doug MD1030F · Engine Indicating System Wiring > DURING CLIMBOUT ON A REDUCED POWER TAKEOFF, PASSING ABOUT 1500-2000 FT. RECEIVED A NR 1 ENGINE EXCEEDENCE WITH TEMP REACHING ABOUT 970. A MINUTE OR SO LATER RECEIVED A SIMILAR INDICATION WITH DIAL INDICATING A HIGHER TEMP, EVENTUALLY WITH A PEAK AT 1070C AN - [SDR FDEA200907292829](https://openairdocs.org/sdr/FDEA200907292829.md): Anti-Skid Sys · failed · Jul 29, 2009 · N317FE · Doug DC1030F · Brake Anti-Skid Section > ANTI-SKID FAIL ALERT AFTER T/O. WOULD NOT TEST AFTER RECYCLE TO OFF THEN ON. PEFORMED ANTI-SKID TEST, IAW 32-45-00-5. OPS CHECKS GOOD. NO HISTORY. OK FOR SERVICE. REMOVED AND REPLACED SKID CONTROL UNIT IAW MM 32-45-01-2. TEST SATISFACTORY. OK TO CONTI - [SDR FDEA200907292814](https://openairdocs.org/sdr/FDEA200907292814.md): Computer · malfunctioned · Jul 29, 2009 · N317FE · Doug DC1030F · Flight Management Computing Hardware System > LOST ALL TIME, FUEL AND ACFT WEIGHT PREDICTIONS FROM BOTH FMS NR 1 AND NR 2 WHILE ENROUTE. CHK NR 1 AND NR 2 VIA LAST LEG FAULT, NO FAULT REPORTED. PERFORMED R-T-S ON NR 1 AND NR 2 VIA, OPS CHK GOOD IAW MM 31-43-01-5. PRECAUTIONARY PERFORMED, FIM 34-63-01 ST - [SDR FDEA200905201752](https://openairdocs.org/sdr/FDEA200905201752.md): Stiffener · cracked · May 20, 2009 · N317FE · Doug DC1030F · Wing Miscellaneous Structure > LT WING L/E FOUND STIFFENER WITH CRACK. REPAIRED AREA IAW SRM 57-00-01 FIG 10 VOL I. - [SDR FDEA200905061550](https://openairdocs.org/sdr/FDEA200905061550.md): Rib · cracked · May 6, 2009 · N317FE · Doug DC1030F · Wing, Rib/Bulkhead > LT WING OUTBOARD FLAP FOUND CRACK ON OTBD FITTING. REPAIRED AREA IAW EA NR 8-5750-128520. - [SDR FDEA200904271424](https://openairdocs.org/sdr/FDEA200904271424.md): Skin · cracked · Apr 27, 2009 · N317FE · Doug DC1030F · Horizontal Stabilizer, Plate/Skin > DURING INSPECTION OF HORIZONTAL STABILIZER CONSTANT AND CUTER SECTION SKIN PANELS FOUND NR 3 PANELS WITH CRACKS. REPAIRED AREA IAW EA NR 8-5510-126253 AND EA NR 8-5510-126254. - [SDR FDEA200903180956](https://openairdocs.org/sdr/FDEA200903180956.md): Skin · cracked · Mar 18, 2009 · N317FE · Doug DC1030F · Wing, Plate/Skin > RT WING LEADING EDGE FOUND CRACK ON SKIN L/E LOWER SIDE. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 SHT 2 VOL I. - [SDR FDEA200903090869](https://openairdocs.org/sdr/FDEA200903090869.md): Floorbeam · corroded · Mar 9, 2009 · N317FE · Doug DC1030F · Fuselage Main, Floor Beam > LOWER AFT COMPT LIGHT CORROSION ON UPPER SIDE FLOORBEAM AND ANGLE SUPPORT FLOOR. REPAIRED AREA IAW SRM 53-00-01 FIG 9 VOL I. - [SDR FDEA200902190581](https://openairdocs.org/sdr/FDEA200902190581.md): Skin · loose · Feb 19, 2009 · N317FE · Doug DC1030F · Elevator, Plate/Skin > LT OTBD ELEVATOR FOUND 150 LOOSE FASTENERS ON LWR SKIN T/E. REPAIRED T/E SECTION AND SKIN IAW DWG ALC7345 & SRM 55-10-00 FIG 8 VOL I. - [SDR FDEA200902110503](https://openairdocs.org/sdr/FDEA200902110503.md): Skin · none · Feb 11, 2009 · N317FE · Doug DC1030F · Fuselage Main, Plate/Skin > ACFT DOOR PACK NR 2 EXTERNAL SKIN FOUND EXISTING FLUSH REPAIR. REPAIRED AREA IAW EA NR 8-5240-128516. - [SDR FDEA200901160218](https://openairdocs.org/sdr/FDEA200901160218.md): Frame · cracked · Jan 16, 2009 · N317FE · Doug DC1030F · Fuselage Main, Frame > AIR COND COMPT FOUND CRACK ON CAP FRAME, REPAIRED AREA IAW SRM 53-00-01 FIG 2, SHT 2, VOL I. - [SDR FDEA200901120154](https://openairdocs.org/sdr/FDEA200901120154.md): Seat Track · cracked · Jan 12, 2009 · N317FE · Doug DC1030F · Fuselage, Seat/Cargo Attach Fittings > MAIN CABIN INSPECTION FLOOR PANEL AND SEAT TRACKS FOUND CRACKS ON TRACK. REPAIRED AREA IAW SRM 53-70-00 FIG 1, SHT 1 AND 2 VOL I. - [SDR FDEA200812195229](https://openairdocs.org/sdr/FDEA200812195229.md): Stanchion · none · Dec 19, 2008 · N317FE · Doug DC1030F · Standard Practices/Structures > CTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126252. - [SDR FDEA200812195228](https://openairdocs.org/sdr/FDEA200812195228.md): Stanchion · none · Dec 19, 2008 · N317FE · Doug DC1030F · Standard Practices/Structures > CTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126251. - [SDR FDEA200812195230](https://openairdocs.org/sdr/FDEA200812195230.md): Frame · cracked · Dec 19, 2008 · N317FE · Doug DC1030F · Fuselage Main, Frame > DURING INSPECTION ON AVIONIC COMPT FOUND CRACK ON FRAME. REPAIRED FRAME IAW SRM 53-30-00 VOL I, FIG 5. - [SDR FDEA200812185221](https://openairdocs.org/sdr/FDEA200812185221.md): Stanchion · unknown · Dec 18, 2008 · N317FE · Doug DC1030F · Standard Practices/Structures > CTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126245. - [SDR FDEA200812185220](https://openairdocs.org/sdr/FDEA200812185220.md): Stanchion · unknown · Dec 18, 2008 · N317FE · Doug DC1030F · Standard Practices/Structures > CTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126246. - [SDR FDEA200812185219](https://openairdocs.org/sdr/FDEA200812185219.md): Stanchion · unknown · Dec 18, 2008 · N317FE · Doug DC1030F · Fuselage Miscellaneous Structure > CTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA NR 8-5310-126247. - [SDR FDEA200812185218](https://openairdocs.org/sdr/FDEA200812185218.md): Stanchion · unknown · Dec 18, 2008 · N317FE · Doug DC1030F · Standard Practices/Structures > CTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126248. - [SDR FDEA200812185217](https://openairdocs.org/sdr/FDEA200812185217.md): Stanchion · unknown · Dec 18, 2008 · N317FE · Doug DC1030F · Standard Practices/Structures > CTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126249. - [SDR FDEA200812185216](https://openairdocs.org/sdr/FDEA200812185216.md): Stanchion · unknown · Dec 18, 2008 · N317FE · Doug DC1030F · Standard Practices/Structures > CTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126250. - [SDR FDEA200812185223](https://openairdocs.org/sdr/FDEA200812185223.md): Frame · worn · Dec 18, 2008 · N317FE · Doug DC1030F · Fuselage Main, Frame > DURING INSPECTION ON AVIONIC COMPT FOUND DEEP WEAR ON FRAME. REPAIRED AREA IAW SRM 53-30-00 FIG 4 VOL I. - [SDR FDEA200812185222](https://openairdocs.org/sdr/FDEA200812185222.md): Frame · cracked · Dec 18, 2008 · N317FE · Doug DC1030F · Fuselage Main, Frame > DURING INSPECTION ON AVIONIC COMPT FOUND CRACK ON FRAME. REPAIRED FRAME IAW SRM 53-30-00 FIG 11 VOL I. - [SDR FDEA200812185215](https://openairdocs.org/sdr/FDEA200812185215.md): Web · cracked · Dec 18, 2008 · N317FE · Doug DC1030F · Fuselage Miscellaneous Structure > DURING INSPECTION NLG WW FOUND CRACK ON VERTICAL WEB. REPAIRED WEB IAW SRM 53-40-00 FIG 34 VOL I. - [SDR FDEA200812185214](https://openairdocs.org/sdr/FDEA200812185214.md): Web · cracked · Dec 18, 2008 · N317FE · Doug DC1030F · Fuselage Miscellaneous Structure > DURING INSPECTION NLG FOUND CRACK ON VERTICAL WEB. REPAIRED WEB IAW SRM 53-40-00 FIG 34, VOL I. - [SDR FDEA200812165178](https://openairdocs.org/sdr/FDEA200812165178.md): Frame · unknown · Dec 16, 2008 · N317FE · Doug DC1030F · Fuselage Main, Frame > AFT CARGO COMPARTMENT EXISTING REPAIR ON FRAME. REPLACED FRAME IAW DWG AJC7363. - [SDR FDEA200812155144](https://openairdocs.org/sdr/FDEA200812155144.md): Skin · cracked · Dec 15, 2008 · N317FE · Doug DC1030F · Wing, Plate/Skin > LT WING SLATS, FOUND CRACK AND NR 10 FASTENERS U/S ON CORNER SKIN INTERNAL SIDE SLAT NR 2. REPAIRED AREA IAW SRM 57-10-00 FIG 31, VOL I. - [SDR FDEA200812155142](https://openairdocs.org/sdr/FDEA200812155142.md): Skin · dented · Dec 15, 2008 · N317FE · Doug DC1030F · Fuselage Main, Plate/Skin > EXT FUSELAGE LWR SURFACE FOUND DEEP DENT ON SKIN 1 INCH BY 1 INCH DEEP.078 INCH. REPAIRED AREA IAW SRM 53-20-00, VOL I, FIG 6, SHT 3-4. - [SDR FDEA200812125124](https://openairdocs.org/sdr/FDEA200812125124.md): Rib · cracked · Dec 12, 2008 · N317FE · Doug DC1030F · Wing, Rib/Bulkhead > LT WING LEADING EDGE, FOUND CRACK AND RIVETS U/S ON ANGLE SUPPORT REFUEL PANEL. REPAIRED RIB IAW SRM57-00-01 VOL I, FIG 10, SHT 1,3,4. - [SDR FDEA200812035071](https://openairdocs.org/sdr/FDEA200812035071.md): Stanchion · unknown · Dec 3, 2008 · N317FE · Doug DC1030F · Fuselage Miscellaneous Structure > FWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPLACE STANCHION IAW DWG ADA3353. - [SDR FDEA200812035070](https://openairdocs.org/sdr/FDEA200812035070.md): Stanchion · unknown · Dec 3, 2008 · N317FE · Doug DC1030F · Fuselage Miscellaneous Structure > FWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPLACE STANCHION IAW DWG ADA3353. - [SDR FDEA200812035069](https://openairdocs.org/sdr/FDEA200812035069.md): Stanchion · unknown · Dec 3, 2008 · N317FE · Doug DC1030F · Fuselage Miscellaneous Structure > FWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPLACE STANCHION IAW DWG ADA3353. - [SDR FDEA200812035068](https://openairdocs.org/sdr/FDEA200812035068.md): Stanchion · unknown · Dec 3, 2008 · N317FE · Doug DC1030F · Fuselage Miscellaneous Structure > FWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPLACE STANCHION IAW DWG ADA3353. - [SDR FDEA200812035067](https://openairdocs.org/sdr/FDEA200812035067.md): Angle · cracked · Dec 3, 2008 · N317FE · Doug DC1030F · Wing Miscellaneous Structure > LT WING LEADING EDGE FOUND NR 1 CRACK ON TEE ANGLE. REPAIRED AREA IAW SRM 57-10-00 FIG 49 VOL I. - [SDR 08FDEA04938](https://openairdocs.org/sdr/08FDEA04938.md): Skin · dented · Nov 20, 2008 · N317FE · Doug DC1030F · Wing, Plate/Skin > DURING INSPECTION RT WING LWR SURFACE FOUND SCRATCH 22 INCHES LONG AND DEEP DENT 3 INCHES BY 3 INCHES DEEP.161 INCH ON LWR SKIN OF OUTBD AILERON. DAMAGE IS "NOT/FLIGHT AIRCRAFT STRIKE DAMAGE". REPAIRED AREA IAW SRM 57-10-00 VOL I FIG 2 SHT 2 NOTE 8. - [SDR FDEA200810204445](https://openairdocs.org/sdr/FDEA200810204445.md): Pump · failed · Oct 20, 2008 · N317FE · Doug DC1030F · Hydraulic Pump (Electric/Engine), Main > AT CRUISE FLT, NR 2 HYDRAULIC QTY AND PRESSURE WENT TO ZER0. NO HIGH TEMP INDICATED. COMPLIED WITH QRH AND RETURNED TO MEMPHIS. REMOVED AND REPLACED 2/1 NON-REV MOTOR PUMP SHUTOFF VALVE. - [SDR 08FDEA04445](https://openairdocs.org/sdr/08FDEA04445.md): Pump · failed · Oct 20, 2008 · N317FE · Doug DC1030F · Hydraulic Pump (Electric/Engine), Main > AT CRUISE FLT, NR 2 HYDRAULIC QTY AND PRESSURE WENT TO ZER0. NO HIGH TEMP INDICATED. COMPLIED WITH QRH AND RETURNED TO MEMPHIS. REMOVED AND REPLACED 2/1 NON-REV MOTOR PUMP SHUTOFF VALVE Next page: https://openairdocs.org/deregistered/N317FE-2024-02-01/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 n_number = 'N317FE' AND deregistration_id = 'N317FE-2024-02-01' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N317FE-2024-02-01/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.