# Service difficulty reports: N810FX

A list on [N810FX](https://openairdocs.org/aircraft/N810FX.md).

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

- [SDR MTNA2026021700001](https://openairdocs.org/sdr/MTNA2026021700001.md): Metering Valve · unresponsive · Feb 16, 2026 · N810FX · Aerosp ATR72202 · Landing Gear Brake System
  > NORMAL BRAKING UNRESPONSIVE ON BOTH CAPT SIDE AND F/O SIDE. REPLACEMENT OF THE HYDRAULIC METERING VALVE (6027GG) IAW TASK ATR-A-32-42-50-02001-520A-A/720A-A. LEAK CHECK GOOD AND OPS CHECK GOOD
- [SDR MTNA20250616001](https://openairdocs.org/sdr/MTNA20250616001.md): Flex Hose · leaking · Jun 18, 2025 · N810FX · Aerosp ATR72202 · Crew Oxygen System
  > DURING PREFLIGHT OF FLIGHT 7500 MYR-CAE WITH AIRCRAFT N810FX, IT WAS DISCOVERED THAT THE F/O OXYGEN MASK WAS LEAKING. MAC MAINTENANCE TROUBLESHOT THE ISSUE TO THE OXYGEN LINE.
- [SDR MTNA20231227001](https://openairdocs.org/sdr/MTNA20231227001.md): Unknown · unknown · Dec 27, 2023 · N810FX · Aerosp ATR72202 · Engine Fuel and Control
  > AFTER TAKEOFF, LEAVING MAX RPM, RT ENGINE BEGAN SURGING. THE FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO GSP UNEVENTFULLY. CLEANED CANNON PLUG CONNECTIONS ON RT ENGINE ECU. PERFORMED ENGINE RUN. UNABLE TO REPLICATE ENGINE SURGING. NO FURTHER DEFECTS NOTE
- [SDR MTNA20230713001](https://openairdocs.org/sdr/MTNA20230713001.md): Unknown · unknown · Jul 13, 2023 · N810FX · Aerosp ATR72 · Crew Oxygen System
  > CAPT'S O2 MASK FAILS PREFLIGHT CHECK IN 100% MODE. MASK WILL NOT PRSSURIZE. REMOVED AND REPLACED CAPT'S O2 MASK BOX. LEAK AND OPS CHECKED GOOD.
- [SDR MTNA20210312001](https://openairdocs.org/sdr/MTNA20210312001.md): Roller · inoperative · Mar 12, 2021 · N810FX · Aerosp ATR72 · Landing Gear Brake System
  > DURING POST FLIGHT INSPECTION, FOUND EMERGENCY BRAKE DIFFICULT TO ENGAGE AND GRINDING. REMOVED AND REPLACED SPRING LOADED PIN ROLLER ON EMERGENCY BRAKE. OPS CHECKED GOOD.
- [SDR MTNA20160527002](https://openairdocs.org/sdr/MTNA20160527002.md): Floor Support · cracked · May 24, 2016 · N810FX · Aerosp ATR72202 · Fuselage Miscellaneous Structure
  > LT LONGITUDINAL FLOORBEAM IS CRACKED AT FRAME 23D. REMOVED BEAM, FABRICATED NEW BEAM FROM BAC 1518-344 7075-T6, PO 201739. ALODINED, PRIMED, AND INSTALLED NEW BEAM IAW M7 IPC SUP 53-00-00 AND SRM 51-21-17, 51-27-28, AND 51-25-01.
- [SDR MTNA20160527001](https://openairdocs.org/sdr/MTNA20160527001.md): Floor Support · damaged · May 24, 2016 · N810FX · Aerosp ATR72202 · Fuselage Miscellaneous Structure
  > LT LONGITUDINAL FLOORBEAM IS DAMAGED AT FRAME 23C. REMOVED BEAM, FABRICATED NEW BEAM FROM BAC 1518-344 7075-T6, PO 201739. ALODINED, PRIMED, AND INSTALLED NEW BEAM IAW M7 IPC SUPPLEMENT 53-00-00 AND SRM 51-21-17, 51-27-28, AND 51-25-01.
- [SDR MTNA20150403001](https://openairdocs.org/sdr/MTNA20150403001.md): Pan · damaged · Apr 3, 2015 · N810FX · Aerosp ATR72202 · Fuselage Miscellaneous Structure
  > AIRCRAFT HAD DAMAGE ON THE CARGO DOOR PAN. THE DAMAGE WAS REPAIRED IAW THE M7 DWG NR 72R47001-03 AND THE ACFT WAS RETURN TO SERVICE.
- [SDR MTNA20140225008H](https://openairdocs.org/sdr/MTNA20140225008H.md): Web · corroded · Feb 25, 2014 · N810FX · Aerosp ATR72202 · Fuselage Miscellaneous Structure
  > FOUND WEB, CORRODED OUT OF LIMITS. REPLACED WEB IAW SRM.
- [SDR MTNA20140225007H](https://openairdocs.org/sdr/MTNA20140225007H.md): Stringer · damaged · Feb 25, 2014 · N810FX · Aerosp ATR72202 · Fuselage Main, Longeron/Stringer
  > FOUND DAMAGE ON STRINGER 2R BETWEEN FRAME 21 AND 22 OUT OF LIMITS. REPAIRED DAMAGED STRINGER, IAW SRM.
- [SDR MTNA20140125006](https://openairdocs.org/sdr/MTNA20140125006.md): Stringer · damaged · Feb 25, 2014 · N810FX · Aerosp ATR72202 · Fuselage Main, Longeron/Stringer
  > FOUND DAMAGE ON STRINGER 1L BETWEEN FRAMES 23 AND 23A OUT OF LIMITS. REPLACED SECTION OF STRINGER, IAW SRM.
- [SDR MTNA20140224005](https://openairdocs.org/sdr/MTNA20140224005.md): Stringer · corroded · Feb 20, 2014 · N810FX · Aerosp ATR72202 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 20R BETWEEN FRAMES 32 AND 33. REPLACED SECTION OF STRINGER IAW INSTRUCTION DT/S-124/14-21175.
- [SDR MTNA20140127002](https://openairdocs.org/sdr/MTNA20140127002.md): Skin · corroded · Jan 27, 2014 · N810FX · Aerosp ATR72202 · Wing, Plate/Skin
  > RT WING LOWER SKIN INTERNAL CORROSION AT FEEDER PUMP BETWEEN RIBS 4/5 ON LOWER PANEL, PN S57112378-200. BLENDED CORROSION IAW SRI DT/S-7009/13-21067 IDENTIFIED AS MAJOR REPAIR, FINAL APPROVAL IS ATR STRUCTURAL REPAIR APPROVAL SHEET DT/S-7009/13.
- [SDR MTNA20140127003](https://openairdocs.org/sdr/MTNA20140127003.md): Stringer · corroded · Jan 23, 2014 · N810FX · Aerosp ATR72202 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 20R BETWEEN FRAMES 16-17. REPLACED SECTION OF STRINGER, PN S53371420206 IAW SRM.
- [SDR MTNA20140127001](https://openairdocs.org/sdr/MTNA20140127001.md): Seat Track · cracked · Jan 22, 2014 · N810FX · Aerosp ATR72202 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND LEFT SEAT TRACK AT FRAME 36 CRACKED, R & R SEAT TRACK IAW SRM.
- [SDR MTNA20131223048](https://openairdocs.org/sdr/MTNA20131223048.md): Floor Panel · corroded · Dec 20, 2013 · N810FX · Aerosp ATR72202 · Fuselage Floor Panel
  > FOUND CORROSION ON FLOOR PANEL 214BF, OUT OF LIMITS. REPLACED FLOOR PANEL IAW SRM.
- [SDR MTNA20130409021](https://openairdocs.org/sdr/MTNA20130409021.md): Pin · out of limits · Apr 5, 2013 · N810FX · Aerosp ATR72202 · Main Landing Gear Attach Section
  > DISCOVERED A BASE METAL CHANGE THAT WAS OUT OF LIMITS ON LEFT MAIN LANDING GEAR AFT PINTLE PIN P/N D61000. THIS WAS DESCOVERED DURING AN ATTEMPT TO EXTEND THE TBO FOR THE LANDING GEAR COMPONENTS. THE LEFT LANDING GEAR ASSEMBLY IS GOING TO BE SENT TO AN OVERH
- [SDR MTNA20130409020](https://openairdocs.org/sdr/MTNA20130409020.md): Universal · out of limits · Apr 5, 2013 · N810FX · Aerosp ATR72202 · Main Landing Gear Attach Section
  > DISCOVERED A BASE METAL CHANGE THAT WAS OUT OF LIMITS ON RIGHT MAIN LANDING GEAR UNIVERSAL P/N D61036. THIS WAS DISCOVERED DURING AN ATTEMPT TO EXTEND THE TBO FOR THE LANDING GEAR COMPONENTS. THE RIGHT LANDING GEAR ASSEMBLY IS GOING TO BE SENT TO AN OVERHAUL
- [SDR MTNA20130409019](https://openairdocs.org/sdr/MTNA20130409019.md): Pin · out of limits · Apr 5, 2013 · N810FX · Aerosp ATR72202 · Main Landing Gear Attach Section
  > DISCOVERED A BASE METAL CHANGE THAT WAS OUT OF LIMITS ON RIGHT MAIN LANDING GEAR AFT PINTLE PIN PN D61000. THIS WAS DISCOVERED DURING AN ATTEMPT TO EXTEND THE TBO FOR THE LANDING GEAR COMPONENTS. THE RIGHT LANDING GEAR ASSEMBLY IS GOING TO BE SENT TO AN OVER
- [SDR MTNA0820120001](https://openairdocs.org/sdr/MTNA0820120001.md): Door · damaged · Aug 20, 2012 · N810FX · Aerosp ATR72202 · Cargo/Baggage Doors
  > DURING A INSPECTION THE CARGO DOOR ON AIRCRAFT 810FX WAS FOUND DAMAGED. THE AIRCRAFT WAS FERRIED TO THE MAINTENANCE HANGAR. THE CARGO DOOR WAS REPLACED IAW ART72 JIC 52-31-00 RAI 10000.
- [SDR MTNA0905001](https://openairdocs.org/sdr/MTNA0905001.md): Smoke Detector · false activation · May 27, 2009 · N810FX · Aerosp ATR72202 · Smoke Detection
  > WHILE EN ROUTE FROM MEM TO BHM A SMOKE WARNING LIGHT ILLUMINATED. THERE WAS NO SMOKE PRESENT. THE CREW DECLARED AN EMERGENCY AND RETURNED TO MEM. A SMOKE DETECTOR WAS REMOVED AND REPLACED AND THE SYSTEM CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR MTNA1208002](https://openairdocs.org/sdr/MTNA1208002.md): Smoke Detector · defective · Dec 19, 2008 · N810FX · Aerosp ATR72202 · Smoke Detection
  > ON CLIMBOUT OF MEM, THE NR 2 ZONE SMOKE DETECTOR LIGHT ILLUMINATED. NO SMOKE WAS FOUND. THE PILOT DID A PRECAUTIONARY TURNBACK INTO MEM. THE SMOKE DETECTOR WAS REMOVED AND REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR MTNA100802](https://openairdocs.org/sdr/MTNA100802.md): Structure · corroded · Oct 6, 2008 · N810FX · Aerosp ATR72202 · Wing Miscellaneous Structure
  > FOUND CORROSION INSIDE LEFT FUEL FEEDER TANK BETWEEN RIBS 4 AND 5. THERE WERE SEVERAL AREAS FROM STIFFENER 1 TO STIFFENER 10. CORROSION REMOVED AS PER SRM ATR72 CH 51-21-42. APPLIED TREATMENT TO NEUTRALIZE ANY HEDDIN CORROSION. PERFORMED FINAL BLEND OUT IA
- [SDR MAC060802](https://openairdocs.org/sdr/MAC060802.md): Pitot Tube · obstructed · May 20, 2008 · N810FX · Aerosp ATR72202 · Pitot/Static System
  > ON TAKEOFF ROLL, THE ANNUNCIATOR ILLUMINATED. ON CROSS CHECK THE F/O`S AIRSPEED INDICATOR INDICATED ZERO. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. THE NR 2 PITOT TUBE WAS REMOVED AND REPLACED THE SYSTEM CHECKED AND THE AIRCRAFT WAS RET
- [SDR MAC060801](https://openairdocs.org/sdr/MAC060801.md): Indicator · inoperative · May 20, 2008 · N810FX · Aerosp ATR72202 · Airspeed/Mach Indicator
  > ON TAKEOFF ROLL, THE ANNUNCIATOR ILLUMINATED. ON CROSS CHECK THE F/O`S AIRSPEED INDICATOR INDICATED ZERO. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. THE F/O`S AIRSPEED INDICATOR WAS REPLACED AND OPS CHECK NORMAL. RETURNED AIRCRAFT TO SE
- [SDR MAC020803](https://openairdocs.org/sdr/MAC020803.md): Master Cylinder · defective · Feb 14, 2008 · N810FX · Aerosp ATR72202 · Master Cylinder/Brake Valve
  > AFTER ARRIVAL, THE PILOT REPORTED THE CAPT SIDE RIGHT BRAKE INOPERATIVE. THE MASTER CYLINDER WAS REPLACED AND THE BRAKE LOW PRESSURE SIDE WAS BLED.
- [SDR MAC020805](https://openairdocs.org/sdr/MAC020805.md): Filter · clogged · Feb 7, 2008 · N810FX · Aerosp ATR72202 · Aircraft Fuel Filter/Strainer
  > ON DEPARTURE FROM MEM-BHM FLT 8375, THE NR 1 ENGINE FUEL CLOG LIGHT ILLUMINATED. THE PIC DECIDED TO RETURN TO MEM. MAINTENANCE WAS NOT AVAILABLE IN BHM. MAINTENANCE REPLACED THE HP FUEL PUMP INLET FILTER. THE SYSTEM TESTED GOOD AND THE A/C WAS RETURNED TO
- [SDR MAC020802](https://openairdocs.org/sdr/MAC020802.md): Metering Valve · malfunctioned · Feb 3, 2008 · N810FX · Aerosp ATR72202 · Landing Gear Brake System
  > DURING TAXI ON INITIAL BRAKE CHECK, LOW RIGHT BRAKE PRESSURE WAS DISCOVERED ON BOTH THE PIC AND SIC SIDES. THE A/C RETURNED TO THE GATE. THE BRAKE METERING VALVE WAS REPLACED.
- [SDR MAC110701](https://openairdocs.org/sdr/MAC110701.md): Frame · corroded · Oct 18, 2007 · N810FX · Aerosp ATR72202 · Fuselage Main, Frame
  > DURING INSPECTION, CORROSION WAS FOUND ON FRAME 39 AT BL 0 REQUIRING A FRAME REPAIR. THE CORROSION ORIGINATED FROM A BLUE WATER SPILL AT SOMETIME IN THE PAST. THE LAV WAS PREVIOUSLY REMOVED DURING A RECONFIGURATION OF THE A/C. THIS IS AN ISOLATED CASE AND H

## 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 = 'N810FX' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N810FX/reports

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