# Service difficulty reports: Daher TBM 700

A list on [Daher TBM 700](https://openairdocs.org/model/daher-tbm-700.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 131 reports

- [SDR 2023FA0000290](https://openairdocs.org/sdr/2023FA0000290.md): Starter Gen · failed · May 25, 2023 · N848DB · Socata TBM700 · Starter-Generator
  > STARTER/GEN FAILURE IN FLIGHT FORCING PILOT TO DECLARE EMERGENCY LANDING. UPON INSPECTION, STARTER BEARING FOUND THROUGHOUT STARTER HOUSING, ALONG WITH STATOR WINDINGS AND OTHER FOD MATERIAL. SPLINED SHAFT WAS ALSO SHEARED.
- [SDR DGCA 23 3100](https://openairdocs.org/sdr/DGCA%2023%203100.md): Elevator · delaminated · Feb 7, 2023 · N940CS · Socata TBM700 · Elevator Control System
  > ELEVATOR LEADING EDGE DELAMINATION
- [SDR 2020FA0000379](https://openairdocs.org/sdr/2020FA0000379.md): Pump · bypassing · Aug 21, 2020 · N179NC · Socata TBM700 · Hydraulic System, Main
  > LANDING GEAR PUMP FAILURE. GEAR WOULD NOT GO DOWN. USED EMERGENCY HAND PUMP TO EXTEND THE GEAR.
- [SDR 2019FA0000129](https://openairdocs.org/sdr/2019FA0000129.md): Control Rod · detached · Apr 23, 2019 · N616CM · Socata TBM700 · Rudder Tab Control System
  > THE RUDDER TRIM TAB IS OPERATED BY AN ELECTRIC ACTUATOR AND CONNECTED BY A LOWER AND AN UPPER RUDDER TRIM TAB CONTROL ROD. AFTER RUDDER REMOVAL FOR ROUTINE INSPECTION, THE UPPER RUDDER TRIM CONTROL ROD DETACHED FROM THE ACTUATOR WHILE THE BEARING WAS STILL IN
- [SDR V94R2019022831002](https://openairdocs.org/sdr/V94R2019022831002.md): Roll Pin · backed out · Jan 29, 2019 · N700FP · Socata TBM700 · Autopilot System
  > ROLL PIN THAT HOLDS PINION GEAR ON SERVO DRIVESHAFT WORKED ITS WAY OUT SO THAT THE GEAR SLIPPED ON THE SHAFT AND THE SERVO WAS MECHANICALLY DISCONNECTED FROM THE FLIGHT CONTROLS. THE SYSTEM DID NOT PROVIDE ANY WARNING OF THIS FAILURE. IT IS ALSO LIKELY THAT
- [SDR 2018FA0000133](https://openairdocs.org/sdr/2018FA0000133.md): Generator · power loss · Apr 3, 2018 · N851TB · Socata TBM700 · AC Generator-Alternator
  > PILOT DIVERTED TO PMP DUE TO LOST POWER FROM MAIN GENERATOR.
- [SDR URZR20170117001](https://openairdocs.org/sdr/URZR20170117001.md): Wire · not reported · Jan 12, 2017 · N930X · Socata TBM700 · Air Conditioning System Wiring
  > THE PILOT CHANGED SWITCH POSITION FROM AUTO TO MAX DIFF AND EXPERIENCED LOSS OF BLEED AIR. PILOT WAS ALERTED BY A BLEED OFF MESSAGE, CABIN PRESSURE BEGAN TO DECREASE. INITIATED A DESCENT, RESET BLEED, STABILIZED PRESSURIZATION AND MADE UNEVENTFUL LANDING. WI
- [SDR 2016FA0000664](https://openairdocs.org/sdr/2016FA0000664.md): Valve · defective · Dec 21, 2016 · N693MA · Socata TBM700 · Passenger Oxygen System
  > DURING ANNUAL INSPECTION, A TEST OF THE PASSENGER OXYGEN MASK DROP IS REQUIRED. PASSENGER MASK DEPLOYED @10,500 FT INSTEAD OF THE 12,500 REQUIREMENT. REMOVED AND REPLACED ALTMETRIC VALVE WITH OVERHAULED UNIT.
- [SDR 2016FA0000665](https://openairdocs.org/sdr/2016FA0000665.md): Valve · no test · Dec 20, 2016 · N850VT · Socata TBM700 · Passenger Oxygen System
  > DURING ANNUAL INSPECTION, A FUNCTIONAL CHECK OF THE OXYGEN MASKS WAS PERFORMED. THE OXYGEN MASKS DROPPED AT 105000 FT INSTEAD OF 125. ALTIMETRIC VALVE REPLACED
- [SDR 2016FA0000657](https://openairdocs.org/sdr/2016FA0000657.md): Fuel Control · malfunctioned · Dec 14, 2016 · N850VT · Socata TBM700 · Fuel Control/Turbine Engines
  > ENGINE SLOW TO START, HANGING AT 33 PERCENT 50+ SECONDS TO START. CHANGED ACFT BATTERY SAME RESULTS. CALIBRATED FCU STARTS AT 38 SECONDS.
- [SDR 2016FA0000618](https://openairdocs.org/sdr/2016FA0000618.md): Fuel Control · malfunctioned · Dec 10, 2016 · N585GC · Socata TBM700 · Fuel Control/Turbine Engines
  > SLOW STARTS. RE-CALIBRATE FCU.
- [SDR 2016FA0000611](https://openairdocs.org/sdr/2016FA0000611.md): Fuel Control · malfunctioned · Dec 10, 2016 · N213RE · Socata TBM700 · Fuel Control/Turbine Engines
  > ENGINE SURGES IN MAX REVERSE. FCU TO RECALIBRATE.
- [SDR 2016FA0000610](https://openairdocs.org/sdr/2016FA0000610.md): Fuel Control · malfunctioned · Dec 10, 2016 · N213RE · Socata TBM700 · Fuel Control/Turbine Engines
  > MAX REVERSE FAILED CHECK. RE-CALIBRATE FCU.
- [SDR 2016FA0000609](https://openairdocs.org/sdr/2016FA0000609.md): Fuel Control · malfunctioned · Dec 10, 2016 · N8EG · Socata TBM700 · Fuel Control/Turbine Engines
  > AFTER RECEIPT OF FCU AFTER RE-CALIBRATION ENGINE WILL START NORMALLY BUT WILL NOT MAKE MAX REVERSE CHECK. SEND OUT FOR RE-CAL.
- [SDR 2016FA0000608](https://openairdocs.org/sdr/2016FA0000608.md): Fuel Control · malfunctioned · Dec 10, 2016 · N8EG · Socata TBM700 · Fuel Control/Turbine Engines
  > ENGINE HANGS DURING START BELOW 40%. SEND FOR RE-CALIBRATION.
- [SDR 2016FA0000625](https://openairdocs.org/sdr/2016FA0000625.md): Fuel Control · malfunctioned · Nov 19, 2016 · N700GQ · Socata TBM700 · Fuel Control/Turbine Engines
  > ITT LIGHT WHEN GOING INTO MAX REVERSE. RECALIBRATE FCU.
- [SDR 2016FA0000623](https://openairdocs.org/sdr/2016FA0000623.md): Fuel Control · abnormal · Oct 17, 2016 · N700G · Socata TBM700 · Fuel Control/Turbine Engines
  > MAX ITT LIGHT WHEN GOING INTO MAX REVERSE. RE-CALIBRATE FCU.
- [SDR 2016FA0000622](https://openairdocs.org/sdr/2016FA0000622.md): Fuel Control · malfunctioned · Aug 16, 2016 · Socata TBM700 · Fuel Control/Turbine Engines
  > ENGINE STARTING WARM. RE-CALIBRATE FCU.
- [SDR 2016FA0000621](https://openairdocs.org/sdr/2016FA0000621.md): Fuel Control · malfunctioned · Jul 26, 2016 · Socata TBM700 · Fuel Control/Turbine Engines
  > ENGINE STATING WARM. RE-CALIBRATE FCU.
- [SDR 2016FA0000620](https://openairdocs.org/sdr/2016FA0000620.md): Fuel Control · malfunctioned · Mar 25, 2016 · Socata TBM700 · Fuel Control/Turbine Engines
  > ENGINE STARTS WARM. RE-CALIBRATE FCU.
- [SDR 2016FA0000624](https://openairdocs.org/sdr/2016FA0000624.md): Fuel Control · malfunctioned · Jan 24, 2016 · N220NA · Socata TBM700 · Fuel Control/Turbine Engines
  > ENGINE STARTING WARM AND SLOW STARTS. RE-CALIBRATE FCU.
- [SDR 2016FA0000619](https://openairdocs.org/sdr/2016FA0000619.md): Fuel Control · malfunctioned · Jan 15, 2016 · N850GS · Socata TBM700 · Fuel Control/Turbine Engines
  > ENGINE SLOW TO START. RE-CALIBRATE FCU.
- [SDR 2016FA0000617](https://openairdocs.org/sdr/2016FA0000617.md): Fcu · malfunctioned · Sep 21, 2015 · N777FX · Socata TBM700 · Fuel Control/Turbine Engines
  > HIGH TEMPS DURING START. RE-CLAIBRATE FCU.
- [SDR 2016FA0000615](https://openairdocs.org/sdr/2016FA0000615.md): Fuel Control · malfunctioned · Sep 9, 2015 · N622PK · Socata TBM700 · Fuel Control/Turbine Engines
  > MAX ITT LIGHT COMES ON WHEN PULLING INTO MAX REVERSE. RE-CALIBRATE FCU.
- [SDR 2016FA0000616](https://openairdocs.org/sdr/2016FA0000616.md): Fcu · malfunctioned · Aug 18, 2015 · N773TC · Socata TBM700 · Fuel Control/Turbine Engines
  > ENGINE START TEMPS EXCESSIVE. RECALIBRATE FCU.
- [SDR 2016FA0000614](https://openairdocs.org/sdr/2016FA0000614.md): Fuel Control · malfunctioned · Aug 7, 2015 · N773TC · Socata TBM700 · Fuel Control/Turbine Engines
  > FAILED MAX REVERSE CHECK. RE-CALIBRATED FCU.
- [SDR 2016FA0000613](https://openairdocs.org/sdr/2016FA0000613.md): Fuel Control · malfunctioned · Jul 1, 2015 · N418A · Socata TBM700 · Fuel Control/Turbine Engines
  > ENGINE IS SLOW TO START AND DOES NOT MAKE MAX REVERSE CHECK. RECALIBRATED THE FCU.
- [SDR 2016FA0000612](https://openairdocs.org/sdr/2016FA0000612.md): Fuel Control · malfunctioned · May 28, 2015 · N900TK · Socata TBM700 · Fuel Control/Turbine Engines
  > ENGINE IS SLOW TO START. RECALIBRATED THE FCU.
- [SDR 2016FA0000595](https://openairdocs.org/sdr/2016FA0000595.md): Fuel Control · out of limits · May 5, 2015 · N753BD · Socata TBM700 · Fuel Control/Turbine Engines
  > MANUAL OVER RIDE LOWER THAN 40 PERCENT AND FUEL FLOW LOWER THAN 60 PERCENT. FUEL CONTROL UNIT CONTACTING STOPS.
- [SDR 2016FA0000599](https://openairdocs.org/sdr/2016FA0000599.md): Fuel Control · out of adjust · Jan 14, 2015 · N850PK · Socata TBM700 · Fuel Control/Turbine Engines
  > DEAD BAND ADJUSTMENT SCREW IS AFT OF THE FLIGHT IDLE ROLLER. RE-CALIBRATED FUEL CONTROL UNIT.
- [SDR 2016FA0000598](https://openairdocs.org/sdr/2016FA0000598.md): Fuel Control · out of adjust · Dec 12, 2014 · N700WE · Socata TBM700 · Fuel Control/Turbine Engines
  > AIRCRAFT WILL NOT MAKE MAX REVERSE. RE-CALIBRATED FUEL CONTROL UNIT.
- [SDR 2016FA0000597](https://openairdocs.org/sdr/2016FA0000597.md): Fuel Control · abnormal · Dec 8, 2014 · N700HK · Socata TBM700 · Fuel Control/Turbine Engines
  > ENGINE IS SLOW TO START AND NOT MAKING MAX REVERSE. CALIBRATED FUEL CONTROL UNIT.
- [SDR CA141024008](https://openairdocs.org/sdr/CA141024008.md): Oil System · low pressure · Oct 5, 2014 · Socata TBM700 · Engine Oil Indicating System
  > (CAN) WHILE ENROUTE, HAD AN INDICATION OF LOW OIL PRESSURE. THE PILOT WAS UNABLE TO LAND. WHILE MANEUVERING FOR A FORCED LANDING ON A FOOTBALL FIELD THE AIRPLANE COLLIDED WITH TREES THAT SEPARATED THE RT WING. THE AIRPLANE CAME TO REST UPRIGHT ON THE FO
- [SDR 2014FA0000536](https://openairdocs.org/sdr/2014FA0000536.md): Cabin Pressure · malfunctioned · Aug 11, 2014 · N331GL · Socata TBM700 · Cabin Pressure Control System
  > DURING CRUISE, WHILE AT FL310, CABIN PRESSURE BEGAN TO RISE AS CONFIRMED BY THE G1000 ELECTRONIC GAUGES FOR CABIN ALT, ROC AND DIFF PRESSURE. AT 10,300' CABIN ALTITUDE THE CABIN ALTITUDE CAS MESSAGE APPEARED. WHEN THE CABIN ALTITUDE REACHED APPROXIMATELY 10,5
- [SDR 2016FA0000596](https://openairdocs.org/sdr/2016FA0000596.md): Fuel Control · abnormal · Aug 9, 2014 · N327MM · Socata TBM700 · Fuel Control/Turbine Engines
  > ENGINE IS SLOW TO START. FUEL CONTROL UNIT HAD TO BE RE-CALIBRATED.
- [SDR CA140721003](https://openairdocs.org/sdr/CA140721003.md): Engine · vibration · Jun 25, 2014 · Socata TBM700 · Engine (Turbine/Turboprop)
  > (CAN) AFTER TAKEOFF, THE PILOT NOTICED A VIBRATION HAD COME BACK AFTER THE ENGINE WAS REINSTALLED. THE PILOT MENTIONED THAT THIS VIBRATION HAD NOT BEEN FELT WHEN THE RENTAL ENGINE WAS INSTALLED.
- [SDR 2014FA0000294](https://openairdocs.org/sdr/2014FA0000294.md): Structure · contaminated · Apr 10, 2014 · N356F · Socata TBM700 · Horizontal Stabilizer Structure
  > HORIZONTAL STABILIZER STRUCTURE COMPROMISED BY APPARENT WATER DAMAGE CREATING CRACKS AND CORROSION. DEFECTS WITHIN THE PRIMARY STRUCTURE OF THE HORIZONTAL STABILIZER. HONEYCOMB CORE CONTAMINATED WITH WATER INTRUSION.
- [SDR CA131007007](https://openairdocs.org/sdr/CA131007007.md): Fuel Control · malfunctioned · Sep 22, 2013 · Socata TBM700 · Fuel Control/Turbine Engines
  > (CAN) DURING FLIGHT, THE ENGINE TQ STAYED AT 72.7 PERCENT AND THE ENGINE ITT WAS 752. IT REMAINED BELOW 72.7 PERCENT EVEN WHEN THE MANUAL OVERRIDE USED TO 100 PERCENT TORQUE. THE FCU WAS REMOVED FOR INVESTIGATION.
- [SDR RL8R2013FA0000544](https://openairdocs.org/sdr/RL8R2013FA0000544.md): Roll Pin · loose · Aug 28, 2013 · N700MX · Socata TBM700 · Ailerons
  > DURING A ROUTINE ANNUAL INSPECTION, THE LT INBD AILERON MOUNTING PIVOT POINT ROLL PIN WAS FOUND TO BE LOOSE AND WORKING.
- [SDR RL8R2013FA0000543](https://openairdocs.org/sdr/RL8R2013FA0000543.md): Roll Pin · loose · Aug 28, 2013 · N702GS · Socata TBM700 · Ailerons
  > DURING A ROUTINE ANNUAL INSPECTION, THE LT & RT INBD AILERON MOUNTING PIVOT POINT ROLL PINS WERE FOUND TO BE LOOSE AND WORKING.
- [SDR RL8R2013FA0000542](https://openairdocs.org/sdr/RL8R2013FA0000542.md): Roll Pin · loose · Aug 28, 2013 · N700ZZ · Socata TBM700 · Ailerons
  > DURING A ROUTINE ANNUAL INSPECTION, THE LT & RT INBD AILERON MOUNTING PIVOT POINTS ROLL PINS WERE FOUND TO BE LOOSE AND WORKING.
- [SDR RL8R2013FA0000541](https://openairdocs.org/sdr/RL8R2013FA0000541.md): Roll Pin · loose · Aug 28, 2013 · N144JT · Socata TBM700 · Ailerons
  > DURING A ROUTINE ANNUAL INSPECTION, THE LT AND RT AILERON MOUNTING PIVOT POINT ROLL PINS WERE FOUND TO BE LOOSE AND WORKING.
- [SDR RL8R2013FA0000540](https://openairdocs.org/sdr/RL8R2013FA0000540.md): Roll Pin · loose · Aug 28, 2013 · N701AV · Socata TBM700 · Ailerons
  > DURING A ROUTINE ANNUAL INSPECTION, THE LT AILERON MOUNTING PIVOT POINT ROLL PINS WERE FOUND TO BE LOOSE AND WORKING.
- [SDR CA130603004](https://openairdocs.org/sdr/CA130603004.md): Engine · making metal · May 15, 2013 · Socata TBM700 · Engine (Turbine/Turboprop)
  > (CAN) THE PILOT REPORTED THAT 5 MINUTES AFTER TAKEOFF DURING CLIMB HE FELT A SLIGHT VIBRATION AND THE OIL PRESSURE WENT MOMENTARILY IN TO THE YELLOW RANGE. THE PILOT MADE RIGHT TURN TO RETURN TO HOME BASE WITH THE LOP WARNING LLUMINATED AND A GROWL NOISE BEING
- [SDR CA130502001](https://openairdocs.org/sdr/CA130502001.md): Engine · power loss · Apr 28, 2013 · Socata TBM700 · Engine (Turbine/Turboprop)
  > (CAN) SHORTLY AFTER T/O, A LOSS OF ENGINE POWER OCCURRED AND THE A/C MADE A FORCED WHEELS UP LANDING IN AN OPEN FIELD. NO ONE ON BOARD WAS SERIOUSLY INJURED. THE A/C SUFFERED DAMAGE TO THE PROPELLER AND LOWER FUSELAGE. OFFER OF ASSISTANCE WILL BE MADE TO THE D
- [SDR RL8R2014030700151](https://openairdocs.org/sdr/RL8R2014030700151.md): Carriage · damaged · Mar 13, 2013 · N702AV · Socata TBM700 · Trailing Edge Flaps
  > INBD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FLAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOSS OF FLAP OR WORSE. REQUIRES REPAIR TO FLAP END AND INSTALLATION OF NEW FLAP CARRIAGE INSERTS. TH
- [SDR RL8R2014030700150](https://openairdocs.org/sdr/RL8R2014030700150.md): Carriage · damaged · Mar 13, 2013 · N700WK · Socata TBM700 · Trailing Edge Flaps
  > INBD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FLAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOSS OF FLAP OR WORSE. REQUIRES REPAIR TO FLAP END AND INSTALLATION OF NEW FLAP CARRIAGE INSERTS. TH
- [SDR 2014FA0000149](https://openairdocs.org/sdr/2014FA0000149.md): Insert · loose · Mar 13, 2013 · N700WK · Socata TBM700 · Trailing Edge Flaps
  > INBD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FLAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOSS OF FLAP OR WORSE. REQUIRES REPAIR TO FLAP END AND INSTALLATION OF NEW FLAP CARRIAGE INSERTS. TH
- [SDR 2013FA0000283](https://openairdocs.org/sdr/2013FA0000283.md): Insert · loose · Mar 13, 2013 · N702AV · Socata TBM700 · Trailing Edge Flaps
  > INBOARD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOSS OF FLAP OR WORSE. REQUIRES REPAIR TO FLAP END AND INSTALLATION OF NEW FLAP CARRIAGE INSERTS.
- [SDR 2013FA0000282](https://openairdocs.org/sdr/2013FA0000282.md): Insert · loose · Mar 13, 2013 · N700WK · Socata TBM700 · Trailing Edge Flaps
  > INBD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOSS OF FLAP OR WORSE. REQUIRES REPAIR TO FLAP END AND INSTALLATION OF NEW FLAP CARRIAGE INSERTS. THI

Next page: https://openairdocs.org/model/daher-tbm-700/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 = 'TBM700'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/daher-tbm-700/reports

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