# Service difficulty reports: Boeing 767-316F A list on [Boeing 767-316F](https://openairdocs.org/model/boeing-767-316f.md). Newest first. General aviation reporting is voluntary. Page 1 of 3 · 116 reports - [SDR 2025FA0000637](https://openairdocs.org/sdr/2025FA0000637.md): Window · open · Sep 6, 2025 · N542LA · Boeing 767316F · Flight Compartment Windows > RTO WAS CARRIED OUT AT APPROXIMATELY 120 KTS DUE TO A NOISE IN THE NO. 2 RH WINDOW DURING THE TAKEOFF ROLL. THE CREW LEFT THE RUNWAY AND AWAITED A DECREASE IN BRAKE TEMPERATURES BASED ON THE BRAKE COOLING SCHEDULE BEFORE RETURNING TO THE GATE. THE AIRCRAFT R - [SDR 2025FA0000416](https://openairdocs.org/sdr/2025FA0000416.md): Relay · burned · Jun 23, 2025 · N418LA · Boeing 767316F · Cargo/Baggage Doors > LATAM AIRCRAFT VISIT FOR HEAVY MAINTENANCE. DURING THE MAINTENANCE, THE PRODUCTION PERSONNEL REPORTED THAT INSIDE P33 PANEL FOUND SIGN OF BURN ON ONE OF THE STUDS OF MAIN CARGO DOOR LATCH RELAY K2218. - [SDR 2025F00066](https://openairdocs.org/sdr/2025F00066.md): Cowling · unlatched · Mar 17, 2025 · N418LA · Boeing 767316F · Nacelle/Pylon, Main Frame > ON FEBRUARY 17, AIRCRAFT N418LA OPERATING FLIGHT L7-1817 ON ROUTE MIA-VCP EXPERIENCED HIGH FUEL CONSUMPTION IN FLIGHT. THE CREW REPORTED: "EXCESSIVE FUEL CONSUMPTION VERSUS FPL CALCULATION > 2000 KG." IN THE MAINTENANCE LOG BOOK (MLB). UPON THE AIRCRAFT'S ARRI - [SDR IPXA2024081574300](https://openairdocs.org/sdr/IPXA2024081574300.md): Skin · dented · Aug 15, 2024 · N393UP · Boeing 767316F · Fuselage Main, Plate/Skin > DENT - SKIN, R/H FUSELAGE TAIL SECTION STA 1746-1767 S-38R ~ S39R (EVALUATE) OK TO WORK - [SDR IPXA2024081574434](https://openairdocs.org/sdr/IPXA2024081574434.md): Skin · dented · Aug 15, 2024 · N393UP · Boeing 767316F · Fuselage Main, Plate/Skin > DENT - SKIN, R/H FUSELAGE TAIL SECTION STA 1915.1 - 1923.5 (EVALUATE) OK TO WORK - [SDR 2LCF202407010059](https://openairdocs.org/sdr/2LCF202407010059.md): Clamp · loose · Jun 17, 2024 · N532LA · Boeing 767316F · Cabin Cooling System > AIRCRAFT N532LA HAD THE FOLLOWING REPORT IN FLIGHT AT 6000 FT ON JUNE 17TH “LOUD BANG AT 6000FT", CREW DID NOT REPORT ANY ENGINE PARAMETERS VARIATION NOR PRESSURIZATION FAULTS; HOWEVER THEY DECIDED TO RETURN TO MIA. ONCE THE AIRPLANE ARRIVED AT MIA, INSPECTION - [SDR 2024FA0000300](https://openairdocs.org/sdr/2024FA0000300.md): Idg · faulted · Mar 20, 2024 · N566LA · Boeing 767316F · AC Generator-Alternator > ON MARCH 20TH AT THE MIA BASE, AFTER THE PUSHBACK (02:56 LT) NEAR 100 KTS AN EICAS MESSAGE APPEARS FROM LH GEN DRIVE AND THE CAPTAIN IMMEDIATELY STOPS AND GENERATES REJECT TAKE OFF (RTO) WHICH FOR QRH REQUIRED THE AIRCRAFT TO RETURN FOR MAINTENANCE ACTIONS. MA - [SDR 2024FA0000299](https://openairdocs.org/sdr/2024FA0000299.md): Torque Shaft · out of position · Mar 4, 2024 · N532LA · Boeing 767316F · Cargo/Baggage Doors > ON MARCH 4TH AT THE SJO BASE, AFTER THE PUSHBACK NEAR 65 KTS, AN EICAS MESSAGE APPEARS FROM AFT CARGO DOOR AND THE CAPTAIN IMMEDIATELY STOPS AND GENERATES REJECT TAKE OFF (RTO), WHICH DUE TO QRH REQUIRED THE AIRCRAFT TO RETURN FOR MAINTENANCE ACTIONS. THE MAI - [SDR 2023F00220](https://openairdocs.org/sdr/2023F00220.md): Unknown · unknown · Jul 7, 2023 · N536LA · Boeing 767316F · Cabin Pressure Control System > AT FLIGHT LEVEL 13600, 2 MINUTES PRIOR TO STARTING DESCENT MSTER WARNING AND EICAS MESSAGE CABIN ALTITUDE PRESENTED. CABIN ALTITUDE SELECTOR WAS SELECTEDTO MAN. DESCENT WAS INITIATED AND CABIN ALTITUDE WAS CONTROLLED MANUALLY DURING DESCEND UNTIL LANDING, NO - [SDR 2022F00439](https://openairdocs.org/sdr/2022F00439.md): Actuator · cracked · Oct 30, 2022 · N532LA · Boeing 767316F · Landing Gear Actuator > AFTER TAKE OFF FROM ZAZ AIRPORT, CREW HEARD A NOISE DURING LANDING GEAR RETRACTION, HOWEVER ALL CABIN INDICATIONS WERE NORMAL. DURING APPROACH TO JFK WHEN LANDING GEAR WAS SELECTED DOWN POSITION, RH MAIN LANDING GEAR INDICATION SHOWED NOT IN GREEN INDICATIO - [SDR 2LCF20210916001](https://openairdocs.org/sdr/2LCF20210916001.md): Engine · fractured · Sep 16, 2021 · N536LA · Boeing 767316F · Powerplant System > DURING CLIMB FROM FL310 TO FL330, THERE IS A SUDDEN LOSS OF N1 AND STRONG VIBRATION ON THE RIGHT ENGINE. THEREFORE, THE CREW CONSIDERS SEVERE DAMAGE; THE CREW SHUTS DOWN THE ENGINE, DECLARES AN EMERGENCY (MAYDAY) AND OPTS TO LAND IN KINGSTON. (JAMAICA). THE LA - [SDR 2LCF202109130007](https://openairdocs.org/sdr/2LCF202109130007.md): Unknown · unknown · Sep 7, 2021 · N418LA · Boeing 767316F · Flight Control System > ON SEPTEMBER 7TH, DURING THE DESCENT AND LANDING OF THE AIRCRAFT N418LA THAT WAS CARRYING OUT MIA-BOG ROUTE (L7-1806), THE CREW FELT A STRONG RESPONSE FROM THE AIRCRAFT TO PITCH UP AND LATER A BOUNCE LANDING, A CIRCUMSTANCE UNDER WHICH THE CREW TOOK THE DECISI - [SDR 2LCF2020102901](https://openairdocs.org/sdr/2LCF2020102901.md): Wheel · melted · Oct 29, 2020 · N532LA · Boeing 767316F · Wheel/Ski/Float > DURING THE N532LA TRANSIT SERVICE CHECK ON OCTOBER 29TH IN THE STATION OF QUITO (UIO), LOSS OF PRESSURE OCCURS IN THE WHEEL NR 1, AT THE MOMENT OF CHANGING IT, THE CORRESPONDING BEARING AND BRAKE WERE FOUND WITH DAMAGE. FOLLOWING THE PROCEDURE BY THE AMM, THE - [SDR 2LCF20190716002](https://openairdocs.org/sdr/2LCF20190716002.md): Eec · failed · Jul 16, 2019 · N418LA · Boeing 767316F · Fuel Control/Turbine Engines > AFTER TAKEOFF ON THE MIA - MVD ROUTE, A MESSAGE FROM THE LEFT ENGINE CONTROL WAS PRESENTED TO THE CREW. IN COMMUNICATION WITH THE MOC, THE CONVENIENCE OF RETURNING TO MIA WAS DETERMINED BECAUSE MVD DID NOT HAVE THE NECESSARY RESOURCES TO CORRECT THE FAIL. UPON - [SDR 2LCF20190719001](https://openairdocs.org/sdr/2LCF20190719001.md): Heat Exchanger · failed · Jun 17, 2019 · N536LA · Boeing 767316F · Cabin Cooling System > ON JUNE 15, THE AIRCRAFT FLEW ON THE MIA - ANF ROUTE, A REPORT BY LT BLEED DUCT LEAK IS PRESENTED, WHICH RETURNS THE AIRCRAFT TO THE MIA STATION; LT PRSOV WAS REPLACED. AFTER THIS EVENT ON JUNE 16, THE AIRCRAFT MADE THE MIA - ANF -SCL FLIGHT, PRESENTING IN THI - [SDR 2LCF201902152001](https://openairdocs.org/sdr/2LCF201902152001.md): Warning Message · false activation · Feb 12, 2019 · N418LA · Boeing 767316F · Leading Edge Slat Control System > AFTER TAKEOFF, WAS PRESENTED WITH EICAS MESSAGE 27 90 14 00 LE SLAT ASYM, WHICH FORCED THE CREW TO RETURN THE AIRCRAFT TO DEPARTURE. AFTER THE RETURN OF THE AIRCRAFT, CARRIED OUT IN THE FIM TASK 27-81 FAULT TREE 809. THE CLEANING IS PERFORMED AND THE SENSOR - [SDR 2LCF201812110006](https://openairdocs.org/sdr/2LCF201812110006.md): Bolt · loose · Dec 6, 2018 · N536LA · Boeing 767316F · Leading Edge Slat Actuator > MESSAGE OF WARNING FLAP SHOWN, WITH AUDIBLE ALARM AND ACTIVATION OF MASTER WARNING; REJECTED TAKE OFF WAS MADE AND AFTER LEAVING THE TRACK IT WAS PRESENTED IN THE EICAS "MSG OF LE SLAT DESAGREE", THE AIRCRAFT RETURNED TO THE PLATFORM TO GENERATE THE REPORT AN - [SDR 2LCF2018111607003](https://openairdocs.org/sdr/2LCF2018111607003.md): Idg · malfunctioned · Nov 7, 2018 · N532LA · Boeing 767316F · AC Generator-Alternator > DURING T/O FROM UIO STATION, SHOWED "L GEN DRIVE LIGHT " AND MSG "L GEN OFF". PERFORMED LIST. APU STARTED AND OPERATED NORMAL, AND LH GEN DICONNECTED. FLIGHT CONTINUED AND THEN NOTED STATUS MSG APU OIL QTY (ADD). 10 MINUTES LATER, APU FAILED SHOWING EICAS MS - [SDR UIEA2018072801568](https://openairdocs.org/sdr/UIEA2018072801568.md): Warning System · false activation · Jul 27, 2018 · N1381A · Boeing 767316F · Cabin Cooling System > FWD EQUIPMENT VALVE EICAS MESSAGE. PERFORMED TROUBLESHOOTING IAW FIM 21-58 F/T 986 WAS UNABLE TO DUPLICATE EICAS MESSAGE SYSTEM TEST OK NO FAULTS AT THIS TIME. - [SDR 2LCF201807174002](https://openairdocs.org/sdr/2LCF201807174002.md): Coupler · failed · Jul 14, 2018 · N532LA · Boeing 767316F · HF Communications System > DURING THE CRUISE PHASE ON THE MIA - AMS ROUTE, THERE WERE FAULTS IN THE TRANSMISSION AND RECEPTION BY THE HF SYSTEM. THE CREW DECIDED TO RETURNED THE AIRCRAFT TO MIA STATION. AFTER THAT THE WIRING WAS CHECKED AND THE LT AND RT COUPLERS OF THE HF ANTENNAS WERE - [SDR L2CF2019F00030](https://openairdocs.org/sdr/L2CF2019F00030.md): Hf Comm · malfunctioned · Jul 14, 2018 · N532LA · Boeing 767316F · HF Communications System > DURING THE CRUISE PHASE ON THE MIA - AMS ROUTE, THERE WERE FAULTS IN THE TRANSMISSION AND RECEPTION BY THE HF SYSTEM. THE CREW DECIDED TO RETURNED THE AIRCRAFT TO MIA STATION; AFTER THAT THE WIRING WAS CHECKED AND THE LT AND RT COUPLERS OF THE HF ANTENNAS WERE - [SDR 2LCF20180711001](https://openairdocs.org/sdr/2LCF20180711001.md): Relay · failed · Jul 11, 2018 · N418LA · Boeing 767316F · DC Generating System > DURING THE CLIMB PHASE OF THE MIA - SCL ROUTE, THE CREW WAS PRESENTED WITH SEVERAL EICAS MESSAGES THAT FORCED THE CREW TO DECLARE EMERGENCY AND RETURN TO MIA. THE MESSAGES THAT APPEARED WERE "AUTOPILOT, AUTO THROTTLE, YAW DAMPER, FMC, LT REV. INSULATION VALVE" - [SDR 2LCF2019F00026](https://openairdocs.org/sdr/2LCF2019F00026.md): Relay · failed · Jul 11, 2018 · N418LA · Boeing 767316F · DC Generating System > DURING THE CLIMB PHASE OF THE MIA - SCL ROUTE, THE CREW WAS PRESENTED WITH SEVERAL EICAS MESSAGES THAT FORCED THE CREW TO DECLARE EMERGENCY AND RETURN TO MIA. THE MESSAGES THAT APPEARED WERE "AUTOPILOT, AUTO THROTTLE, YAW DAMPER, FMC, LT REV INSULATION VALVE". - [SDR FDEA201711153241](https://openairdocs.org/sdr/FDEA201711153241.md): Adc · inoperative · Nov 15, 2017 · N68079 · Boeing 767316F · Altimeter, Barometric/Encoder > DURING CLIMB OUT, PASSING 12,000 FT, RECEIVED AN ALT DISAGREE AMBER EICAS. ALSO, INTERMITTENT IAS DISAGREE. RAN QRH AND LEVELED AT FL260. CAPTAIN`S ALTIMETER AT 14,000 FT AND F/O'S SHOWED 13,750 FT. CAPTAIN`S ALTIMETER AT FL 240, F/O'S INDICATED FL 237. - [SDR FDEA201710293101](https://openairdocs.org/sdr/FDEA201710293101.md): Panel · missing · Oct 29, 2017 · N68078 · Boeing 767316F · Nacelle/Pylon, Plate/Skin > OVAL PANEL MISSING ON RT ENG NR 2 PYLON OB SIDE. IPC REF 54-53-01-16 ITEM 100. - [SDR UIEA2017101901980](https://openairdocs.org/sdr/UIEA2017101901980.md): Adc · failed · Oct 17, 2017 · N1381A · Boeing 767316F · Air Data Computer > DURING CLIMB THRU FL 180, LT ADC FAILED. REMOVED AND REPLACEDTHE LT ADC COMPUTER IAW AMM 34-12-01. OPS CHECKED NORMAL, PITOT STATIC LEAK CHECKED ACCOMPLISHED IAW AMM 34-11-00, NO DEFECTS NOTED. REMOVED AND REPLACED RT ADC COMPUTER IAW AMM 34-12-01, OPS CHE - [SDR UIEA2017081501484](https://openairdocs.org/sdr/UIEA2017081501484.md): Skin · damaged · Oct 8, 2017 · N1381A · Boeing 767316F · Fuselage Main, Plate/Skin > AFT UPPER FUSELAGE AT APPROXIMATELY BS 1432, BETWEEN STRINGERS 18R TO 19R, FOUND WITH PREVIOUSLY BLEND OUT. AREA REPAIRED IAW SRM 53-00-01-2R-6, REPAIR 6, FIGURE 201, REV 104. REPAIR CLASSIFIED AS MAJOR. - [SDR UIEA2017081701493](https://openairdocs.org/sdr/UIEA2017081701493.md): Rub Strip · cracked · Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main Frame > NR 2 NACELLE EXTERIOR SURFACE, FWD UPPER WEAR STRIPS FOUND CRACKED. THE WEAR STRIPS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 29. - [SDR UIEA2017081701494](https://openairdocs.org/sdr/UIEA2017081701494.md): Support · cracked · Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon Miscellaneous Structure > NR 2 NACELLE INTERIOR SURFACE FWD SUPPORT FOUND CRACKED LOCATED IN THE UPPER SECTION. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 29. - [SDR UIEA2017082101516](https://openairdocs.org/sdr/UIEA2017082101516.md): Skin · worn · Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Plate/Skin > NR 2 NACELLE FAIRING SKIN INTERIOR SURFACE UPPER AFT CUTOUT SECTION FOUND WORN. THE FAIRING SKIN WAS REPAIRED IAW SRM 54-42-01-2R-5, REPAIR 5, REV 29. - [SDR UIEA2017082101517](https://openairdocs.org/sdr/UIEA2017082101517.md): Skin · worn · Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Plate/Skin > NR 1 NACELLE FAIRING SKIN FOUND WORN. THE FAIRING SKIN WAS REPAIRED IAW SRM 54-42-01-2R-5, REPAIR 5, REV 29. - [SDR UIEA2017082101518](https://openairdocs.org/sdr/UIEA2017082101518.md): Skin · worn · Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Plate/Skin > NR 1 NACELLE FAIRING SKIN INTERIOR SURFACE UPPER AFT CUTOUT SECTION FOUND WORN. THE FAIRING SKIN WAS REPAIRED IAW SRM 54-42-01-2R-5, REPAIR 5, REV 29. - [SDR UIEA2017082101519](https://openairdocs.org/sdr/UIEA2017082101519.md): Skin · worn · Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Plate/Skin > NR 2 NACELLE FAIRING SKIN INTERIOR SURFACE UPPER AFT CUTOUT SECTION FOUND WORN. THE FAIRING SKIN WAS REPAIRED IAW SRM 54-42-01-2R-5, REPAIR 5, REV 29. - [SDR UIEA2017082301527](https://openairdocs.org/sdr/UIEA2017082301527.md): Seal · damaged · Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main Frame > NR 1 NACELLE FAIRING UPPER EDGE FWD STRIP SEAL FOUND DAMAGED. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 29. - [SDR UIEA2017082301528](https://openairdocs.org/sdr/UIEA2017082301528.md): Seal · damaged · Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main Frame > NR 1 NACELLE FAIRING UPPER EDGE AFT STRIP SEAL FOUND DAMAGED. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 29. - [SDR UIEA2017082301529](https://openairdocs.org/sdr/UIEA2017082301529.md): Stop · missing · Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main Frame > NR 1 NACELLE FAIRING UPPER EDGE FLIPPER DOOR AFT STOP FOUND MISSING. A NEW STOP WAS INSTALLED IAW SRM 51-40-02, REV 29. - [SDR UIEA2017082401534](https://openairdocs.org/sdr/UIEA2017082401534.md): Skin · scratched · Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Plate/Skin > NR 1 NACELLE SKIN SCRATCHED. REPAIRED IAW SRM 54-42-01-2R-7, REPAIR 7, REV 29. - [SDR UIEA2017082401539](https://openairdocs.org/sdr/UIEA2017082401539.md): Rub Strip · worn · Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main Frame > NR 1 NACELLE FAIRING INTERIOR SURFACE AFT UPPER EDGE RUB STRIP FOUND WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 29. - [SDR UIEA2017082401540](https://openairdocs.org/sdr/UIEA2017082401540.md): Rub Strip · worn · Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main Frame > NR 1 NACELLE FAIRING INTERIOR SURFACE AFT UPPER EDGE RUB STRIP FOUND WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 29. - [SDR UIEA2017082401541](https://openairdocs.org/sdr/UIEA2017082401541.md): Rub Strip · worn · Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main Frame > NR 2 NACELLE FAIRING INTERIOR SURFACE AFT UPPER EDGE RUB STRIP FOUND WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 29. - [SDR UIEA2017082701556](https://openairdocs.org/sdr/UIEA2017082701556.md): Screw · damaged · Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main Frame > NR 1 NACELLE NOSE COWL HOIST POINT SCREWS FOUND DAMAGED. THE SCREWS WERE REMOVED AND REPLACED IAW AMM 20-11-00, REV 122. - [SDR UIEA2017082701557](https://openairdocs.org/sdr/UIEA2017082701557.md): Screw · damaged · Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main Frame > NR 2 NACELLE NOSE COWL HOIST POINT SCREWS FOUND DAMAGED. THE SCREWS WERE REMOVED AND REPLACED IAW AMM 20-11-00, REV 122. - [SDR UIEA2017082801564](https://openairdocs.org/sdr/UIEA2017082801564.md): Channel · worn · Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main Frame > NR 2 NACELLE HAT CHANNEL ATTACH STOP FOUND WORN. THE HAT CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 29. - [SDR UIEA2017082801565](https://openairdocs.org/sdr/UIEA2017082801565.md): Bracket · worn · Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main Frame > NR 2 NACELLE DOOR HOLD OPEN ROD STOW PIN ADAPTER AND BRACKET FOUND WORN. THE STOW PIN SUPPORT ADAPTER AND BRACKETS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 29. - [SDR UIEA2017082801566](https://openairdocs.org/sdr/UIEA2017082801566.md): Bracket · worn · Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main Frame > NR 2 NACELLE DOOR HOLD OPEN ROD STOW PIN ADAPTER AND BRACKET FOUND WORN. THE STOW PIN SUPPORT ADAPTER AND BRACKET WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 29. - [SDR UIEA2017083001584](https://openairdocs.org/sdr/UIEA2017083001584.md): Seal · torn · Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main Frame > NR 2 NACELLE FWD SEAL FOUND TORN. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 29. - [SDR UIEA2017083001585](https://openairdocs.org/sdr/UIEA2017083001585.md): Rub Strip · cracked · Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main Frame > NR 1 NACELLE RUB STRIP FOUND CRACKED AT THE 9 TO 11 O'CLOCK POSITIONS. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 29. - [SDR UIEA2017090401594](https://openairdocs.org/sdr/UIEA2017090401594.md): Skin · corroded · Oct 8, 2017 · N1381A · Boeing 767316F · Fuselage Main, Plate/Skin > CORROSION FOUND THE SKIN BS 1197+19, STRINGER 36R. REPAIRED IAW SRM 53-00-01-2R-12, REPAIR 12, DETAIL IV, FIGURE 201. - [SDR UIEA2017090501603](https://openairdocs.org/sdr/UIEA2017090501603.md): Seal · torn · Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main Frame > NR 1 NACELLE INTERIOR SURFACE, UPPER FWD SEAL FOUND TORN. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 29. - [SDR UIEA2017090601605](https://openairdocs.org/sdr/UIEA2017090601605.md): Plate · worn · Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main Frame > NR 2 NACELLE PLATE WORN. THE PLATE WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 29. Next page: https://openairdocs.org/model/boeing-767-316f/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 aircraft_model_key = '767316F' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/boeing-767-316f/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.