N106FE
Service difficulty reports · 17
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 = 'N106FE' AND registry_match = 'registration' 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 = 'N106FE' AND registry_match = 'registration' 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 FDEA202601190069Web · dentedFLIGHT DECK, BS 246, LBL 26 DAMAGED ON WEB. REPAIRED FLOORBEAM WEB BS 246 REF EA H-5310-TO386201 ALONG WITH SRM 51-20- 01-0G, SRM 51-40-02-0G, SRM 51-70-13-0G, AND AMM 53-01-01-4 .MAJOR REPAIR.SDR FDEA202505050715Cover · deformedDURING POST FLIGHT CHECK FOUND L1 DOOR ESCAPE ROPE RETAINER COVER WAS DEFORMED. AMM 25-61-04-8 L1 DOOR ESCAPE ROPE RETAINER DEFORMED AMM: 25-61-04-8 ITEM IS TRANSFERED TO OIL FOR A/C DEPARTURE. REMOVED AND REPLACED L1 ENTRY DOOR EMERGENCY ESCAPE ROPESDR FDEA202505050714Hook And Loop · wornON ARRIVAL, CREW ENTRY DOOR UNABLE TO FULLY OPEN DUE TO ESCAPE ROPE DROP DOWN & ENTANGLE THE DOOR. AMM: 25-59-03-4 AMM: 25-61-04-402-014-001 NOTICED FEW VELCRO STRAPS IN THE CHANNEL NOT ATTACHED TO THE CHANNEL BODY. RE-FIT NEW VELCRO PER SMP AND REINSTALSDR FDEA202409121314Retainer · damagedCREW REPORTED, L1 DOOR ESCAPE ROPE RETAINER DEFORMED AMM 25-61-04-8. L1 DOOR ESCAPE ROPE RETAINER DEFORMED AND SEALED WITH CARGO PIT TAPE. PERFORMED GVI ON THE L1 DOOR JAMB. FOUND NO ADDITIONAL DAMAGE. RETAINER SEALED WITH CARGO PIT TAPE REF B767 AMM: 25-61SDR FDEA202312191948Fseu · failedON FINAL APPROACH INTO CAN WHEN SELECTING FLAPS 25 RECEIVED A LEADING EDGE, SLAT DISAGREE EICAS MESSAGE. EXECUTED MISSED APPROACH AND PERFORMED QRH PROCEDURE. UNEVENTFUL FLAPS 20 VREF 20 LANDING. LEFT FLIGHT CONTROLS, EXTENDED AND DEBRIEFED MAINTENANCE. SDR FDEA202304140647Wheel · damagedON TAKEOFF ROLL LOTS OF VIBRATION ABOVE 130. ON LANDING ROLL ABOVE 130 SAME VIBRATION. ON POSTFLIGHT MECHANIC SAID WE HAD #6 TIRE HAD BLOWN. NO STATUS MESSAGES PERIOD TO SHUTDOWN. REMOVED & REPLACED #6 MLG TIRE PER AMM 32-45-01-4. PERFORMED BURST TIRE CSDR FDEA202304030546Seat Track · damagedMEL 25-58-01-A MDC RESTRAINT ID503 INOP / SEAT TRACK DAMAGE. REPAIRED THE MAIN DECK CARGO DAMAGED SEAT TRACK PER B767 SRM53-00-52-2R REPAIR 9. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.SDR FDEA202209032170Relay · faultedUPON SELECTION OF FLAPS 1 ON ARRIVAL INTO CAN . LEADING EDGE SLAT DISAGREE EICAS.COMPLETED QRH 9.1.11"LEADING EDGE SLAT DISAGREE"DECLARED EMGERGENCY ,LANDED NORMALLY IAW QRH. PERFORMED FSEU BITE IAW FIM 27-51 FT809, NO HISTORY FAULT CODE FOUND. DUE AHM SHOSDR FDEA202203070435Engine · leakingPDIS 106 79-01 8034 07MAR22 PEN OPEN U LOGPAGES:2996686 RT ENGINE SHUTDOWN ON CLIMB-OUT DUE TO HIGH OIL TEMPERATURE, AS DIRECTED BY THE QRH. THIS WAS ACCOMPANIED BY LOW OIL PRESSURE AND LOW OIL QUANTITY. NO OTHER INDICATION WERE NOTED.SDR FDEA202203070434Engine · unknownPDIS 106 79-01 8034 07MAR22 PEN OPEN U LOGPAGES:2996686 RT ENGINE SHUTDOWN ON CLIMB-OUT DUE TO HIGH OIL TEMPERATURE, AS DIRECTED BY THE QRH. THIS WAS ACCOMPANIED BY LOW OIL PRESSURE AND LOW OIL QUANTITY. NO OTHER INDICATION WERE NOTED. FOUNDSDR FDEA202104130915Control Panel · inoperativeMDIS 106 33-50 7029 13APR21 MEM FACT U EMERGENCY LIGHT PANEL "UNARMED" LIGHT IS INOP. FACT 13APR21 19:03 MEM U RELAMPED PER B767 AMM 33-16-02-2 , NO HELP, IF YOU PRESS ON THE LIGHT ASSY IT WOULD ILLUMINATE. REMOVED & REPLACED THE PILOTS SDR FDEA2018110213080Display · malfunctionedAFTER TAKEOFF, FO MCDU FROZE ON THE LEGS PAGE. MCDU FROZE ON THE T/O PAGE, COULD NOT MANIPULATE ANY FMS FUNCTIONS ON EITHER. NO CIRCUIT BREAKERS TRIPPED. NO EICAS MESSAGES. MOCC ADVISE PULL L FMC E8, E9 R FMC E29, 30 SYSTEM RETURN NORMAL. PERFORMESDR FDEA201810202959Carabiner · missingFOUND RIGHT JUMP/SUPERNUMERARY SEAT MISSING CARABINER/D- RING 1 EA. REINSTALLED THE D RING OF THE ESCAPE HARNESSES AS PER AMM 22-61-03-2. CHECKED NORMAL.SDR FDEA201705201467Seal · failedAT FL 350 FIRST OFFICER HEARD A POP, FOLLOWED BY A HISS OF AIRFLOW ON AFT SEAL OF THE R2 WINDOW . NO FLUCTUATIONS IN PRESSURIZATION OR RATE ON PRESSURIZATION PANEL. REMOVED AND REPLACED THE R2 SLIDING WINDOW SEAL IAW AMM 56-11-11-4.SDR FDEA201602040456Slat · crackedNUMBER 5 SLAT HAS CRACK ON LOWER TE AT THE TELESCOPE DUCT. REPAIRED CRACK IAW SRM 57-43-01-2R FIG 201 TABLE 1 AND SRM 51-70-17 PAR 4 AND FIG 5 PG 38. ADJUSTED TAI DOOR IAW AMM 57-41-58-4. PERFORMED SATISFACTORY OP CHECK IAW B767 AMM 57-41-58-4. PERFORMED DVSDR FDEA201602010420Line · chafedRIGHT WING LE FIRE SUPPRESSION LINE WS 321, FOUND CHAFED THROUGH FROM SLAT TORQUE TUBE COUPLING NOT SECURED, MISSING BOLTS TO SECURE THE COUPLING. REF N00060, N00061, N00062. R & R RT WING LE FIRE SUPPRESSION LINE AT WS 321 IAW AMM 20-10-09.SDR FDEA201602010412Skin · damagedRIGHT WING INBD MAIN FLAP, OTBD END HAS COMPOSITE MATERIAL EXPOSED, COMPLIED WITH EA H 5750-T0323058. RT INBD MAIN FLAP - SKIN REPAIR - RSC. REPAIRED MAIN FLAP OB END IAW B767 SRM 57-53-01-2R AND 51-70-03-0G.
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