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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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 BOSDR 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. FINALLYSDR 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 RSDR 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 CRSDR 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. STICKSHAKESDR 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.SDR 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-SDR FDEA201304270868Beam · crackedFWD CARGO DOOR BALANCE BEAM CRACKED AND BROKEN. R & R FWD CARGO DOOR BEAM ASSY IAW CMM 52-31-03, STEP 21(D).SDR FDEA201304230836Doubler · crackedWHEEL WELL SUSPECT A CRACK ON LT KEEL BEAM BULKHEAD MACHINED DOUBLER. REMOVED AND REPLACED CRACKED DOUBLER AEA 0526U1SDR 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.SDR 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 SRMSDR 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 TISDR 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 TSDR 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 ANSDR 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 CONTISDR 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 STSDR FDEA200905201752Stiffener · crackedLT WING L/E FOUND STIFFENER WITH CRACK. REPAIRED AREA IAW SRM 57-00-01 FIG 10 VOL I.SDR FDEA200905061550Rib · crackedLT WING OUTBOARD FLAP FOUND CRACK ON OTBD FITTING. REPAIRED AREA IAW EA NR 8-5750-128520.SDR 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.SDR 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.SDR 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.SDR 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.SDR FDEA200902110503Skin · noneACFT DOOR PACK NR 2 EXTERNAL SKIN FOUND EXISTING FLUSH REPAIR. REPAIRED AREA IAW EA NR 8-5240-128516.SDR FDEA200901160218Frame · crackedAIR COND COMPT FOUND CRACK ON CAP FRAME, REPAIRED AREA IAW SRM 53-00-01 FIG 2, SHT 2, VOL I.SDR 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.SDR FDEA200812195229Stanchion · noneCTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126252.SDR FDEA200812195228Stanchion · noneCTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126251.SDR FDEA200812195230Frame · crackedDURING INSPECTION ON AVIONIC COMPT FOUND CRACK ON FRAME. REPAIRED FRAME IAW SRM 53-30-00 VOL I, FIG 5.SDR FDEA200812185221Stanchion · unknownCTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126245.SDR FDEA200812185220Stanchion · unknownCTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126246.SDR FDEA200812185219Stanchion · unknownCTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA NR 8-5310-126247.SDR FDEA200812185218Stanchion · unknownCTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126248.SDR FDEA200812185217Stanchion · unknownCTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126249.SDR FDEA200812185216Stanchion · unknownCTR CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPAIRED AREA IAW EA 8-5310-126250.SDR FDEA200812185223Frame · wornDURING INSPECTION ON AVIONIC COMPT FOUND DEEP WEAR ON FRAME. REPAIRED AREA IAW SRM 53-30-00 FIG 4 VOL I.SDR FDEA200812185222Frame · crackedDURING INSPECTION ON AVIONIC COMPT FOUND CRACK ON FRAME. REPAIRED FRAME IAW SRM 53-30-00 FIG 11 VOL I.SDR FDEA200812185215Web · crackedDURING INSPECTION NLG WW FOUND CRACK ON VERTICAL WEB. REPAIRED WEB IAW SRM 53-40-00 FIG 34 VOL I.SDR FDEA200812185214Web · crackedDURING INSPECTION NLG FOUND CRACK ON VERTICAL WEB. REPAIRED WEB IAW SRM 53-40-00 FIG 34, VOL I.SDR FDEA200812165178Frame · unknownAFT CARGO COMPARTMENT EXISTING REPAIR ON FRAME. REPLACED FRAME IAW DWG AJC7363.SDR 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.SDR 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.SDR 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.SDR FDEA200812035071Stanchion · unknownFWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPLACE STANCHION IAW DWG ADA3353.SDR FDEA200812035070Stanchion · unknownFWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPLACE STANCHION IAW DWG ADA3353.SDR FDEA200812035069Stanchion · unknownFWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPLACE STANCHION IAW DWG ADA3353.SDR FDEA200812035068Stanchion · unknownFWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. REPLACE STANCHION IAW DWG ADA3353.SDR FDEA200812035067Angle · crackedLT WING LEADING EDGE FOUND NR 1 CRACK ON TEE ANGLE. REPAIRED AREA IAW SRM 57-10-00 FIG 49 VOL I.SDR 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.SDR 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.SDR 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 VALVE
Back to N317FE, cancelled Feb 1, 2024