N317FE, cancelled Feb 1, 2024

Service difficulty reports · 88

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA201411263910Generator · contaminatedAFTER 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 BONov 26, 2014 · N317FE · Doug MD1030F · AC Generator-AlternatorSDR FDEA201409072502Gcu · failedAPPROX 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. FINALLYSep 7, 2014 · N317FE · Doug MD1030F · AC RegulatorSDR FDEA201406121413Probe · blockedFIRST 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 RJun 12, 2014 · N317FE · Doug MD1030F · Pitot/Static SystemSDR FDEA201405261197Skin · crackedDURING 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 CRMay 26, 2014 · N317FE · Doug MD1030F · Wing, Plate/SkinSDR FDEA201310142498Sensor · malfunctionedAT 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. STICKSHAKEOct 14, 2013 · N317FE · Doug MD1030F · Navigation SystemSDR FDEA201305100971Web · crackedHOLES OUT OF LIMITS ON WEB AUB7366-501. R & R UPPER PYLON SPAR WEB IAW DWG AUB7301 AND SRM 51-33-01, VOL. II INSTRUCTIONS.May 10, 2013 · N317FE · Doug MD1030F · Nacelle/Pylon, Main FrameSDR FDEA201305100970Bulkhead · crackedNR 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-May 10, 2013 · N317FE · Doug MD1030F · Nacelle/Pylon, Bulkhead/FirewallSDR FDEA201304270868Beam · crackedFWD CARGO DOOR BALANCE BEAM CRACKED AND BROKEN. R & R FWD CARGO DOOR BEAM ASSY IAW CMM 52-31-03, STEP 21(D).Apr 27, 2013 · N317FE · Doug MD1030F · Cargo/Baggage DoorsSDR FDEA201304230836Doubler · crackedWHEEL WELL SUSPECT A CRACK ON LT KEEL BEAM BULKHEAD MACHINED DOUBLER. REMOVED AND REPLACED CRACKED DOUBLER AEA 0526U1Apr 23, 2013 · N317FE · Doug MD1030F · Fuselage Main, BulkheadSDR FDEA201304230837Doubler · crackedWHEEL 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.Apr 23, 2013 · N317FE · Doug MD1030F · Fuselage Main, StructureSDR FDEA201209273479Structure · damagedRIGHT 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 SRMSep 27, 2012 · N317FE · Doug MD1030F · Elevator StructureSDR FDEA201207052488Transducer · failedSOON 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 TIJul 5, 2012 · N317FE · Doug MD1030F · Brake Anti-Skid SectionSDR FDEA201207052487Transducer · failedSOON 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 TJul 5, 2012 · N317FE · Doug MD1030F · Brake Anti-Skid SectionSDR FDEA201206262355Lead · malfunctionedDURING 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 ANJun 26, 2012 · N317FE · Doug MD1030F · Engine Indicating System WiringSDR FDEA200907292829Anti-Skid Sys · failedANTI-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 CONTIJul 29, 2009 · N317FE · Doug DC1030F · Brake Anti-Skid SectionSDR FDEA200907292814Computer · malfunctionedLOST 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 STJul 29, 2009 · N317FE · Doug DC1030F · Flight Management Computing Hardware SystemSDR FDEA200905201752Stiffener · crackedLT WING L/E FOUND STIFFENER WITH CRACK. REPAIRED AREA IAW SRM 57-00-01 FIG 10 VOL I.May 20, 2009 · N317FE · Doug DC1030F · Wing Miscellaneous StructureSDR FDEA200905061550Rib · crackedLT WING OUTBOARD FLAP FOUND CRACK ON OTBD FITTING. REPAIRED AREA IAW EA NR 8-5750-128520.May 6, 2009 · N317FE · Doug DC1030F · Wing, Rib/BulkheadSDR FDEA200904271424Skin · crackedDURING 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.Apr 27, 2009 · N317FE · Doug DC1030F · Horizontal Stabilizer, Plate/SkinSDR FDEA200903180956Skin · crackedRT WING LEADING EDGE FOUND CRACK ON SKIN L/E LOWER SIDE. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 SHT 2 VOL I.Mar 18, 2009 · N317FE · Doug DC1030F · Wing, Plate/SkinSDR FDEA200903090869Floorbeam · corrodedLOWER AFT COMPT LIGHT CORROSION ON UPPER SIDE FLOORBEAM AND ANGLE SUPPORT FLOOR. REPAIRED AREA IAW SRM 53-00-01 FIG 9 VOL I.Mar 9, 2009 · N317FE · Doug DC1030F · Fuselage Main, Floor BeamSDR FDEA200902190581Skin · looseLT 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.Feb 19, 2009 · N317FE · Doug DC1030F · Elevator, Plate/SkinSDR FDEA200902110503Skin · noneACFT DOOR PACK NR 2 EXTERNAL SKIN FOUND EXISTING FLUSH REPAIR. REPAIRED AREA IAW EA NR 8-5240-128516.Feb 11, 2009 · N317FE · Doug DC1030F · Fuselage Main, Plate/SkinSDR FDEA200901160218Frame · crackedAIR COND COMPT FOUND CRACK ON CAP FRAME, REPAIRED AREA IAW SRM 53-00-01 FIG 2, SHT 2, VOL I.Jan 16, 2009 · N317FE · Doug DC1030F · Fuselage Main, FrameSDR FDEA200901120154Seat Track · crackedMAIN 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.Jan 12, 2009 · N317FE · Doug DC1030F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200812195229Stanchion · noneCTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126252.Dec 19, 2008 · N317FE · Doug DC1030F · Standard Practices/StructuresSDR FDEA200812195228Stanchion · noneCTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126251.Dec 19, 2008 · N317FE · Doug DC1030F · Standard Practices/StructuresSDR FDEA200812195230Frame · crackedDURING INSPECTION ON AVIONIC COMPT FOUND CRACK ON FRAME. REPAIRED FRAME IAW SRM 53-30-00 VOL I, FIG 5.Dec 19, 2008 · N317FE · Doug DC1030F · Fuselage Main, FrameSDR FDEA200812185221Stanchion · unknownCTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126245.Dec 18, 2008 · N317FE · Doug DC1030F · Standard Practices/StructuresSDR FDEA200812185220Stanchion · unknownCTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126246.Dec 18, 2008 · N317FE · Doug DC1030F · Standard Practices/StructuresSDR FDEA200812185219Stanchion · unknownCTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA NR 8-5310-126247.Dec 18, 2008 · N317FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR FDEA200812185218Stanchion · unknownCTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126248.Dec 18, 2008 · N317FE · Doug DC1030F · Standard Practices/StructuresSDR FDEA200812185217Stanchion · unknownCTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126249.Dec 18, 2008 · N317FE · Doug DC1030F · Standard Practices/StructuresSDR FDEA200812185216Stanchion · unknownCTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126250.Dec 18, 2008 · N317FE · Doug DC1030F · Standard Practices/StructuresSDR FDEA200812185223Frame · wornDURING INSPECTION ON AVIONIC COMPT FOUND DEEP WEAR ON FRAME. REPAIRED AREA IAW SRM 53-30-00 FIG 4 VOL I.Dec 18, 2008 · N317FE · Doug DC1030F · Fuselage Main, FrameSDR FDEA200812185222Frame · crackedDURING INSPECTION ON AVIONIC COMPT FOUND CRACK ON FRAME. REPAIRED FRAME IAW SRM 53-30-00 FIG 11 VOL I.Dec 18, 2008 · N317FE · Doug DC1030F · Fuselage Main, FrameSDR FDEA200812185215Web · crackedDURING INSPECTION NLG WW FOUND CRACK ON VERTICAL WEB. REPAIRED WEB IAW SRM 53-40-00 FIG 34 VOL I.Dec 18, 2008 · N317FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR FDEA200812185214Web · crackedDURING INSPECTION NLG FOUND CRACK ON VERTICAL WEB. REPAIRED WEB IAW SRM 53-40-00 FIG 34, VOL I.Dec 18, 2008 · N317FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR FDEA200812165178Frame · unknownAFT CARGO COMPARTMENT EXISTING REPAIR ON FRAME. REPLACED FRAME IAW DWG AJC7363.Dec 16, 2008 · N317FE · Doug DC1030F · Fuselage Main, FrameSDR FDEA200812155144Skin · crackedLT 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.Dec 15, 2008 · N317FE · Doug DC1030F · Wing, Plate/SkinSDR FDEA200812155142Skin · dentedEXT 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.Dec 15, 2008 · N317FE · Doug DC1030F · Fuselage Main, Plate/SkinSDR FDEA200812125124Rib · crackedLT 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.Dec 12, 2008 · N317FE · Doug DC1030F · Wing, Rib/BulkheadSDR FDEA200812035071Stanchion · unknownFWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPLACE STANCHION IAW DWG ADA3353.Dec 3, 2008 · N317FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR FDEA200812035070Stanchion · unknownFWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPLACE STANCHION IAW DWG ADA3353.Dec 3, 2008 · N317FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR FDEA200812035069Stanchion · unknownFWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPLACE STANCHION IAW DWG ADA3353.Dec 3, 2008 · N317FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR FDEA200812035068Stanchion · unknownFWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPLACE STANCHION IAW DWG ADA3353.Dec 3, 2008 · N317FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR FDEA200812035067Angle · crackedLT WING LEADING EDGE FOUND NR 1 CRACK ON TEE ANGLE. REPAIRED AREA IAW SRM 57-10-00 FIG 49 VOL I.Dec 3, 2008 · N317FE · Doug DC1030F · Wing Miscellaneous StructureSDR 08FDEA04938Skin · dentedDURING 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.Nov 20, 2008 · N317FE · Doug DC1030F · Wing, Plate/SkinSDR FDEA200810204445Pump · failedAT 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.Oct 20, 2008 · N317FE · Doug DC1030F · Hydraulic Pump (Electric/Engine), MainSDR 08FDEA04445Pump · failedAT 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 VALVEOct 20, 2008 · N317FE · Doug DC1030F · Hydraulic Pump (Electric/Engine), Main
Back to N317FE, cancelled Feb 1, 2024