# Service difficulty reports: N106FE A list on [N106FE](https://openairdocs.org/aircraft/N106FE.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR FDEA202601190069](https://openairdocs.org/sdr/FDEA202601190069.md): Web · dented · Jan 19, 2026 · N106FE · Boeing 7673S2F · Fuselage Miscellaneous Structure > FLIGHT 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 FDEA202505050715](https://openairdocs.org/sdr/FDEA202505050715.md): Cover · deformed · May 5, 2025 · N106FE · Boeing 7673S2F · Emergency Equipment > DURING 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 ROPE - [SDR FDEA202505050714](https://openairdocs.org/sdr/FDEA202505050714.md): Hook And Loop · worn · May 5, 2025 · N106FE · Boeing 7673S2F · Emergency Equipment > ON 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 REINSTAL - [SDR FDEA202409121314](https://openairdocs.org/sdr/FDEA202409121314.md): Retainer · damaged · Sep 12, 2024 · N106FE · Boeing 7673S2F · Emergency Equipment > CREW 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: 25-61 - [SDR FDEA202312191948](https://openairdocs.org/sdr/FDEA202312191948.md): Fseu · failed · Dec 19, 2023 · N106FE · Boeing 767300 · Leading Edge Slat Control System > ON 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 FDEA202304140647](https://openairdocs.org/sdr/FDEA202304140647.md): Wheel · damaged · Apr 14, 2023 · N106FE · Boeing 767300 · Wheel/Ski/Float > ON 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 C - [SDR FDEA202304030546](https://openairdocs.org/sdr/FDEA202304030546.md): Seat Track · damaged · Apr 3, 2023 · N106FE · Boeing 767300 · Fuselage Main, Structure > MEL 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 FDEA202209032170](https://openairdocs.org/sdr/FDEA202209032170.md): Relay · faulted · Sep 3, 2022 · N106FE · Boeing 7673S2F · Leading Edge Slat Control System > UPON 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 SHO - [SDR FDEA202203070435](https://openairdocs.org/sdr/FDEA202203070435.md): Engine · leaking · Mar 7, 2022 · N106FE · Boeing 767300 · Engine Oil System (Airframe Furnished) > PDIS 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 FDEA202203070434](https://openairdocs.org/sdr/FDEA202203070434.md): Engine · unknown · Mar 7, 2022 · N106FE · Boeing 767300 · Engine Oil System (Airframe Furnished) > PDIS 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. FOUND - [SDR FDEA202104130915](https://openairdocs.org/sdr/FDEA202104130915.md): Control Panel · inoperative · Apr 13, 2021 · N106FE · Boeing 7673S2F · Emergency Lighting > MDIS 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 FDEA2018110213080](https://openairdocs.org/sdr/FDEA2018110213080.md): Display · malfunctioned · Nov 1, 2018 · N106FE · Boeing 7673S2F · Flight Management Computing Hardware System > AFTER 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. PERFORME - [SDR FDEA201810202959](https://openairdocs.org/sdr/FDEA201810202959.md): Carabiner · missing · Oct 20, 2018 · N106FE · Boeing 7673S2F · Emergency Equipment > FOUND 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 FDEA201705201467](https://openairdocs.org/sdr/FDEA201705201467.md): Seal · failed · May 20, 2017 · N106FE · Boeing 7673S2F · Flight Compartment Windows > AT 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 FDEA201602040456](https://openairdocs.org/sdr/FDEA201602040456.md): Slat · cracked · Feb 4, 2016 · N106FE · Boeing 7673S2F · Leading Edge Devices > NUMBER 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 DV - [SDR FDEA201602010420](https://openairdocs.org/sdr/FDEA201602010420.md): Line · chafed · Feb 1, 2016 · N106FE · Boeing 7673S2F · Extinguishing System > RIGHT 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 FDEA201602010412](https://openairdocs.org/sdr/FDEA201602010412.md): Skin · damaged · Feb 1, 2016 · N106FE · Boeing 7673S2F · Trailing Edge Flaps > RIGHT 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. ## 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 = 'N106FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N106FE/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.