# Service difficulty reports: Aerospatiale/Atr ATR 72 202

A list on [Aerospatiale/Atr ATR 72 202](https://openairdocs.org/model/aerospatiale-atr-atr-72-202.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 12 · 579 reports

- [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 MTNA2025121500001](https://openairdocs.org/sdr/MTNA2025121500001.md): Engine · power loss · Dec 11, 2025 · N811FX · Aerosp ATR72202 · Engine (Turbine/Turboprop)
  > IN-FLIGHT ENGINE SHUTDOWN, FLIGHT 8850, TLH-MEM. ON THE VISUAL APPROACH TO RUNWAY 27 AT KMEM, THE CREW OBSERVED THE NO. 1 ENGINE TORQUE INDICATION BECOME ERRATIC, THEN DROP TO ZERO, ACCOMPANIED BY AN UNCOMMANDED LEFT ROLL. MEMORY ITEMS WERE ACCOMPLISHED, AND
- [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 CA190808012](https://openairdocs.org/sdr/CA190808012.md): Transmitter · leaking · Aug 8, 2019 · Aerosp ATR72202 · Engine Fuel Distribution
  > (CAN) FLIGHT SNAG - FLIGHT CREW REPORTED SIGNIFICANT FUEL LEAK COMING FROM #2 ENGINE. #2 ENGINE FUEL FLOW TRANSMITTER FOUND LEAKING FROM AROUND CANNON PLUG MATING SURFACE ON HOUSEING OF TRANSMITTER. SEE ATTACHED PICTURE WITH ARROW INDICATING REPORTED POINT OF
- [SDR CA190719010](https://openairdocs.org/sdr/CA190719010.md): Extinguisher · leaking · Jul 19, 2019 · Aerosp ATR72202 · Fire Bottle, Portable
  > (CAN) WHILE IN FLIGHT, CABIN PORTABLE FIRE EXTINGUISHER LOCATED BEHIND LAST ROW OF SEAT ON LH SIDE STARTED LEAKING EXTINGUISHING AGENT (HALON 1211). PLEASE NOTE THE PHOTO WHICH SHOWS THE O RING BETWEEN THE CYLINDER AND THE EXTINGUISHING HEAD/NOZZLE ASSY EXPOSE
- [SDR CA190617016](https://openairdocs.org/sdr/CA190617016.md): Horn · burned · Jun 15, 2019 · Aerosp ATR72202 · Airfoil Anti/De-ice System
  > (CAN) FLIGHT CREW REPORTED R ELEV. HORN HEAT FAULT WITH R ELEV. CB POPPING. MAINTENANCE INVESTIGATION: FOUND R ELEVATOR HORN HEATER BURNT. REPLACED R ELEVATOR HORN. STILL INOP. FURTHER INVESTIGATION FOUND RH ELEVATOR HORN HARNESS SHORTING OUT NEAR RH ELEVATOR
- [SDR CA190508005](https://openairdocs.org/sdr/CA190508005.md): Shaft · cracked · May 5, 2019 · Aerosp ATR72202 · Flight Compartment Equipment
  > (CAN) DURING A SCHEDULED INSPECTION OF THE SEAT AS PER CMM 25-11-21 `CHECK 1`, THE SEAT BACK PIVOT SPINE SHAFT WAS DISCOVERED TO BE CRACKED AROUND THE CENTER BOLT HOLE. THIS CAUSED EXCESS PLAY OF THE SEAT BACK. THE CRACKED SHAFT WAS DISCOVERED DURING THE INSPE
- [SDR CA190506010](https://openairdocs.org/sdr/CA190506010.md): Bearing · seized · May 2, 2019 · Aerosp ATR72202 · Wheel/Ski/Float
  > (CAN) DURING A SCHEDULED INSTALLATION OF A NOSE GEAR GRAVEL DEFLECTOR, THE R/H NLG WHEEL OUTER BEARING WAS DISCOVERED SEIZED. THE WHEEL WAS STILL ABLE TO ROTATE ON ITS AXIS, BUT DIFFICULT TO REMOVE FROM THE AXLE. AFTER REMOVAL OF THE WHEEL, SEVERE AXLE DAMAGE
- [SDR CA190418009](https://openairdocs.org/sdr/CA190418009.md): Tube · damaged · Apr 16, 2019 · Aerosp ATR72202 · Engine Fuel Distribution
  > (CAN) AIRCRAFT TOOK OFF AT 11:54 UTC 16/APR/2019. A FEW MINUTES INTO THE FLIGHT IT WAS DISCOVERED THAT THE #2 ENGINE HAD AN EXCESSIVE FUEL FLOW AND FUEL COULD BE SEEN COMING OUT OF THE #2 ENGINE DRAIN MANIFOLD. THE AIRCRAFT STARTED TO RETURN TO AND ON THE DESC
- [SDR CA190322005](https://openairdocs.org/sdr/CA190322005.md): Stringer · corroded · Mar 22, 2019 · Aerosp ATR72202 · Fuselage Main, Longeron/Stringer
  > (CAN) (*SUP*) RHS STRINGER 16 PN S53671386-210 CORRODED AT MULTIPLE LOCATIONS. STRINGER 16 ORDERED AND RECEIVED FROM VENDOR. SHEET METAL TECHNICIAN NOTICED THAT THE PART RECEIVED HAVE THE RIGHT PN AND CERTIFICATION BUT IT WAS BENT ON THE WRONG SIDE. TYPE CERTI
- [SDR CA180706019](https://openairdocs.org/sdr/CA180706019.md): Nut · loose · Jul 5, 2018 · Aerosp ATR72202 · Accessory Gearboxes
  > (CAN) WHILE EN-ROUTE, THE CREW RECEIVED A LOW OIL PRESSURE WARNING ON THE CCAS (CENTRAL CREW ALERTING SYSTEM) FOR THE NR 1 (PORT) ENGINE. IMMEDIATELY ALONG WITH THIS WARNING, THE ENGINE APPEARED TO FLAME OUT ACCORDING TO THE CAPTAIN DURING AN INTERVIEW. THIS
- [SDR MTNA20171003002H](https://openairdocs.org/sdr/MTNA20171003002H.md): Floorbeam · cracked · Oct 2, 2017 · N821FX · Aerosp ATR72202 · Fuselage Main, Floor Beam
  > FLOORBEAM CRACKED AND CORRODED AT FRAME 16 LT SIDE.
- [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 CA160322003](https://openairdocs.org/sdr/CA160322003.md): Compressor · leaking · Feb 24, 2016 · Aerosp ATR72202 · Turbine Engine Compressor Section
  > (CAN) SHORTLY AFTER TAKEOFF, THE CREW OBSERVED A SMOKE INDICATION AND DECIDED TO RETURN TO THE AIRPORT. NO EMERGENCY WAS DECLARED AND THE ACFT LANDED WITHOUT FURTHER INCIDENT. AN INSPECTION REVEALED THAT AN OIL LEAK IN THE ENGINE COMPRESSOR HAD MIGRATED TO
- [SDR CA160125018](https://openairdocs.org/sdr/CA160125018.md): Tube · cracked · Jan 23, 2016 · Aerosp ATR72202 · Turbine Engine Oil System
  > (CAN) ENGINE NR 1, LT HAD EVIDENCE OF A POSSIBLE OIL LEAK. UPON INVESTIGATION A CRACK IN THE OIL PRESSURE TUBE ASSEMBLY CONNECTING THE REAR INLET TO THE ACCESSORY GEARBOX WAS DISCOVERED. REFER TO ATTACHED EMM PN 3037334, CHAPTER 72-01-50, FIGURE 16, ITEM 10 A
- [SDR CA160119028](https://openairdocs.org/sdr/CA160119028.md): Regulator · damaged · Jan 19, 2016 · Aerosp ATR72202 · Turbine Engine Oil System
  > (CAN) AIRCRAFT EXPERIENCED AN OIL PRESSURE FLUCTUATION OF THE NR 1 ENGINE. THE NR 1 ENGINE WAS SHUTDOWN IN FLIGHT AND THE FLIGHT LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE INVESTIGATED THE OIL PRESSURE FLUCTUATION AND DETERMINED A T-FITTING ON THE NR 1 ENGI
- [SDR CA160203006](https://openairdocs.org/sdr/CA160203006.md): Fitting · leaking · Jan 18, 2016 · Aerosp ATR72202 · Turbine Engine Oil System
  > (CAN) DURING CRUISE, THE CREW OBSERVED OIL PRESSURE FLUCTUATIONS AND ELECTED TO SHUT THE ENGINE DOWN. AN UNEVENTFUL SINGLE ENGINE LANDING WAS THEN ACCOMPLISHED AT DESTINATION. POST FLIGHT INSPECTION FOUND AND OIL LEAK FROM DAMAGED THREADS ON ONE OF THE FITTING
- [SDR CA20163006](https://openairdocs.org/sdr/CA20163006.md): Fitting · leaking · Jan 18, 2016 · Aerosp ATR72202 · Turbine Engine Oil System
  > (CAN) DURING CRUISE, THE CREW OBSERVED OIL PRESSURE FLUCTUATIONS AND ELECTED TO SHUT THE ENGINE DOWN. AN UNEVENTFUL SINGLE ENGINE LANDING WAS THEN ACCOMPLISHED AT DESTINATION. POST FLIGHT INSPECTION FOUND AND OIL LEAK FROM DAMAGED THREADS ON 1 OF THE FITTING
- [SDR CA150917005](https://openairdocs.org/sdr/CA150917005.md): O-Ring · worn · Sep 3, 2015 · Aerosp ATR72202 · Turbine Engine Oil System
  > (CAN) FIGHT CREW RECEIVED A SMOKE WARNING FOLLOWING TAKEOFF. THE ACFT RETURNED TO THE AIRPORT WITHOUT INCIDENT. INVESTIGATION REVEALED THAT THE O-RINGS ON THE NL PROBES HAD DETERIORATED AND WERE ALLOWING OIL FUMES/VAPOR INTO THE ACFT BLEED SYSTEM. O-RING PN
- [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 CA141222004](https://openairdocs.org/sdr/CA141222004.md): Altimeter · malfunctioned · Dec 18, 2014 · Aerosp ATR72202 · Altimeter, Barometric/Encoder
  > (CAN) WHILE CLIMBING THROUGH 10`000 FT. THE F/O`S ALTIMETER "OFF" FLAG APPEARED IN VIEW, AND THE ALTIMETER WAS FROZEN. WHEN DESCENDING THROUGH 10000 FT. THE ALTIMETER FLAG DISAPPEARED AND WORKED NORMALLY FOR REMAINDER OF FLIGHT.
- [SDR CA141126007](https://openairdocs.org/sdr/CA141126007.md): Actuator · failed · Nov 25, 2014 · Aerosp ATR72202 · Rudder Tab Control System
  > (CAN) DURING CLIMB OUT CREW NOTED RUDDER TRIM WAS NOT RESPONDING TO INPUTS. SWITCH TRIED IN BOTH DIRECTIONS WITH NO EFFECT ON RUDDER TRIM OR GAUGE INDICATION.
- [SDR MTNA201407180001](https://openairdocs.org/sdr/MTNA201407180001.md): Line · failed · Jul 18, 2014 · N811FX · Aerosp ATR72202 · Hydraulic System, Main
  > AFTER BLOCK OUT OF FLIGHT THE COPILOTS BRAKE WAS FOUND TO BE INOPERATIVE. REPLACED HYDRAULIC LINES. CHECKED GOOD & ACFT RETURN TO SERVICE.
- [SDR MTNA070920140001](https://openairdocs.org/sdr/MTNA070920140001.md): Line · leaking · Jul 9, 2014 · N811FX · Aerosp ATR72202 · Hydraulic System, Main
  > DURING BRAKE CHECK FOR TAXI, THE LT BRAKE PEDAL ON THE COPILOTS SIDE WAS INOPERATIVE. TROUBLESHOT & A HYD LEAK WAS FOUND. THE LINE WAS REPAIRED IAW AMM 20-23-13. LEAK & OPERATIONS CHECKED GOOD IAW JIC 32-42-00 OPT 10000.
- [SDR CA140602036](https://openairdocs.org/sdr/CA140602036.md): Starter Gen · malfunctioned · May 30, 2014 · Aerosp ATR72202 · Starter-Generator
  > (CAN) DURING INITIAL DESCENT, ALL COCKPIT DISPLAYS & INSTRUMENTS STARTED FLUCTUATING RAPIDLY. BUS 1 FAILED INTERMITTENTLY. BOTH ENGINES STARTED FLUCTUATING, POWER CHANGES WERE FELT BY THE CREW. EMERGENCY DECLARED, VISUAL LANDING CARRIED OUT, BOTH ENGINES RU
- [SDR MTNA20140520013](https://openairdocs.org/sdr/MTNA20140520013.md): Skin Panel · corroded · May 20, 2014 · N811FX · Aerosp ATR72202 · Wing, Plate/Skin
  > FOUND LT WING LOWER SKIN PANEL INTERNAL CORROSION AT JET PUMP SUPPORT SEATING BETWEEN RIBS 4 & 5, STIFFENERS 8 - 9. REPAIRED IAW SRI DT S-2157 14-21832 DATED 4/11/2014. APPROVED DATA IS SHEET DO TS-2644 10 5790.
- [SDR MTNA20140521015](https://openairdocs.org/sdr/MTNA20140521015.md): Housing · corroded · May 19, 2014 · N811FX · Aerosp ATR72202 · Wing Miscellaneous Structure
  > FOUND PANEL 622CT HOUSING CORRODED OUT OF LIMITS ON REMOVABLE PANEL PN S57112322201. REPAIRED IAW SRI DT S-2001 14-21784 ISSUE A DATED 4/5/2014. APPROVED DATA IS SRAS DT S-200114 8440.
- [SDR MTNA20140521014](https://openairdocs.org/sdr/MTNA20140521014.md): Panel · corroded · May 19, 2014 · N811FX · Aerosp ATR72202 · Wing, Plate/Skin
  > FOUND PANEL 521DT & 522CT HOUSINGS CORRODED OUT OF LIMITS ON REMOVABLE PANEL PN S57112322200. REPAIRED IAW SRI DT S-2001 14-21784 ISSUE A DATED 4/5/2014. APPROVED DATA IS SRAS DT S-2001 14 8440.
- [SDR MTNA20140518012](https://openairdocs.org/sdr/MTNA20140518012.md): Crease Beam · corroded · May 15, 2014 · N811FX · Aerosp ATR72202 · Fuselage Main, Structure
  > FOUND CREASE BEAM PN S53373000226 CORRODED OUT OF LIMITS. REPLACED WEB IAW SRM.
- [SDR MTNA20140518011](https://openairdocs.org/sdr/MTNA20140518011.md): Crease Beam · corroded · May 15, 2014 · N811FX · Aerosp ATR72202 · Fuselage Main, Structure
  > FOUND CREASE BEAM WEB PN S53374000204 CORRODED OUT OF LIMITS. REPLACED WEB IAW SRM.
- [SDR MTNA20140518010](https://openairdocs.org/sdr/MTNA20140518010.md): Crease Beam · corroded · May 15, 2014 · N811FX · Aerosp ATR72202 · Fuselage Main, Structure
  > FOUND CREASE BEAM WEB PN S53374000228 CORRODED BEYOND LIMITS. REPLACED WEB IAW SRM.
- [SDR MTNA20140509009](https://openairdocs.org/sdr/MTNA20140509009.md): Pan · dented · May 9, 2014 · N811FX · Aerosp ATR72202 · Cargo/Baggage Doors
  > FOUND DENTS IN AFT CARGO DOOR FRAME PANS PN S52176204202, S52176204206 & S51276204208 TO BE OUT OF LIMITS. REPAIRED IAW DWG 72R47000-07 DATED 3/31/2014.
- [SDR CA140429004](https://openairdocs.org/sdr/CA140429004.md): Control Unit · failed · Apr 25, 2014 · Aerosp ATR72202 · AC Power Distribution System
  > (CAN) DURING APPROACH, THE ACFT LOST COMPLETE POWER "ELECTRICAL" TO THE INSTRUMENT PANEL FOR ABOUT "5 SEC". DURING THAT TIME MANY RELAYS WERE CONSTANTLY CYCLING "ON & OFF". BOTH CPT EFIS SCREEN AND ADC WERE LOST. SOME OF THE WARNINGS WERE "TOO LOW GEAR". E
- [SDR CA140409006](https://openairdocs.org/sdr/CA140409006.md): Wire Harness · failed · Apr 7, 2014 · Aerosp ATR72202 · Turbine Engine System Wiring
  > (CAN) DURING CLIMB OUT THROUGH 5000 FT, CREW NOTED A TORQUE DROP OF 5 PERCENT ON ENGINE NR 2. ALL OTHER ENGINE PARAMETERS STABLE. CREW COULD HEAR A CHANGE FROM THE ENGINE AS WELL AS FEEL THE ACFT YAW. THIS HAPPENED TWICE DURING THE CLIMBOUT AND THEN ENGINE
- [SDR CA140408006](https://openairdocs.org/sdr/CA140408006.md): Valve · failed · Apr 4, 2014 · Aerosp ATR72202 · Trailing Edge Flap Control System
  > (CAN) DURING APPROACH TO RWY, FLAP 30 WAS SELECTED AND INDICATING. THE FLAP INDICATOR POSITION NEEDLE APPEARED TO RETRACT SLIGHTLY, APPROXIMATELY 1 DEGREE, FOLLOWED BY THE "EXTEND" FLAG, INDICATOR NEEDLE MOVED BACK TO 30 AND EXTEND FLAG WENT OUT. THIS CYCLE R
- [SDR CA140403003](https://openairdocs.org/sdr/CA140403003.md): Elt · false activation · Apr 1, 2014 · Aerosp ATR72202 · Emergency Locator Beacon
  > (CAN) ELT ACTIVATED WHILE ON GROUND, REASON UNKNOWN.
- [SDR CA140403002](https://openairdocs.org/sdr/CA140403002.md): Elt · false activation · Mar 16, 2014 · Aerosp ATR72202 · Emergency Locator Beacon
  > (CAN) ELT ACTIVATED WHILE ON GROUND, REASON UNKNOWN.
- [SDR CA140306009](https://openairdocs.org/sdr/CA140306009.md): Elt · false activation · Feb 27, 2014 · Aerosp ATR72202 · Emergency Locator Beacon
  > (CAN) ELT ACTIVATED WHILE ON THE GROUND, REASON UNKNOWN.
- [SDR CA140228004](https://openairdocs.org/sdr/CA140228004.md): Elt · malfunctioned · Feb 27, 2014 · Aerosp ATR72202 · Emergency Locator Beacon
  > (CAN) ELT ACTIVATED WHILE ON THE GROUND, REASON UNKNOWN.
- [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 CA140123002](https://openairdocs.org/sdr/CA140123002.md): Indicator · inoperative · Jan 23, 2014 · Aerosp ATR72202 · Engine BMEP/Torque Indicating
  > (CAN) WHEN POWER WAS ADVANCED FOR TAKEOFF THE NR 1 ENGINE TORQUE INDICATOR NEEDLE DID NOT INCREASE AND WAS READING APPROXIMATELY 5 PERCENT.
- [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 CA140123001](https://openairdocs.org/sdr/CA140123001.md): Torque Sensor · fluctuates · Jan 22, 2014 · Aerosp ATR72202 · Engine BMEP/Torque Indicating
  > (CAN) NR 1 ENGINE TORQUE NEEDLE FLUCTUATED VERY SLIGHTLY BUT CONTINUOUSLY DURING CLIMB AND CRUISE. FLUCTUATION OCCURRED WHEN POWER LEVER WAS BOTH IN AND OUT OF THE NOTCH POSITION.
- [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.

Next page: https://openairdocs.org/model/aerospatiale-atr-atr-72-202/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 = 'ATR72202'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/aerospatiale-atr-atr-72-202/reports

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