# Daher TBM 700 - Type: Aircraft model (FAA registry) - Registry code: 8682014 - Manufacturer (registry): DAHER AIRCRAFT SAS - Model: TBM 700 - Aircraft type: Fixed wing single engine - Category: Airplane - Engines: 1 · Turbo-prop - Seats: 8 - Weight class: Up to 12,499 lb - Certification: Type certificated - Data sheet: [TCDS A60EU](https://openairdocs.org/tcds/A60EU) (OpenAirDocs) - Holder: Daher Aircraft SAS - Registered aircraft: 31 - Page: https://openairdocs.org/model/daher-tbm-700 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [AD 2025-26-02](https://openairdocs.org/ad/2025-26-02): Vertical Stabilizer Structure · Daher Aerospace TBM 700. Effective Feb 12, 2026 - [AD 2025-02-08](https://openairdocs.org/ad/2025-02-08): Fire Protection System · DAHER AEROSPACE TBM 700. Effective Mar 19, 2025 - [AD 2025-01-04](https://openairdocs.org/ad/2025-01-04): TE Flap Control System; TE Flap Actuator · DAHER AEROSPACE TBM 700. Effective Mar 11, 2025 - [AD 2023-11-12](https://openairdocs.org/ad/2023-11-12): Emergency Exits · DAHER AEROSPACE TBM 700. Effective Jul 21, 2023 - [AD 2021-25-10](https://openairdocs.org/ad/2021-25-10): Engine Oil System (Airframe) · Daher Aerospace TBM 700. Effective Jan 24, 2022 - [AD 2021-24-13](https://openairdocs.org/ad/2021-24-13): Cabin Pressure Control System · Daher Aerospace TBM700. Effective Jan 12, 2022 - [AD 2017-15-15](https://openairdocs.org/ad/2017-15-15): Flight Controls · SOCATA TBM 700. Effective Sep 6, 2017 - [AD 2015-17-10](https://openairdocs.org/ad/2015-17-10): Landing gear · SOCATA TBM 700. Effective Sep 29, 2015 - [AD 2014-09-03](https://openairdocs.org/ad/2014-09-03): Stabilizers · SOCATA TBM 700. Effective Jun 5, 2014 - [AD 2014-06-06](https://openairdocs.org/ad/2014-06-06): Landing Gear · SOCATA TBM 700. Effective May 2, 2014 - [AD 2012-10-14](https://openairdocs.org/ad/2012-10-14): Landing gear · SOCATA TBM 700. Effective Jul 23, 2012 - [AD 2011-27-09](https://openairdocs.org/ad/2011-27-09): Flight Controls · SOCATA TBM 700. Effective Feb 15, 2012 - [AD 2011-23-03](https://openairdocs.org/ad/2011-23-03): Navigation · SOCATA TBM 700. Effective Dec 6, 2011 - [AD 2011-17-06](https://openairdocs.org/ad/2011-17-06): Flight Controls · SOCATA TBM 700. Effective Sep 19, 2011 - [AD 2011-02-02](https://openairdocs.org/ad/2011-02-02): Air Conditioning. · SOCATA TBM 700. Effective Mar 1, 2011 - [AD 2010-23-28](https://openairdocs.org/ad/2010-23-28): Oxygen · SOCATA TBM 700. Effective Dec 29, 2010 - [AD 2010-11-15](https://openairdocs.org/ad/2010-11-15): Fire Protection · SOCATA TBM 700. Effective Jul 6, 2010 - [AD 2010-07-07](https://openairdocs.org/ad/2010-07-07): Towing and Taxiing · SOCATA TBM 700. Effective May 7, 2010 - [AD 2009-24-15](https://openairdocs.org/ad/2009-24-15): Electric power · SOCATA TBM 700. Effective Jan 4, 2010 - [AD 2007-03-17 R1](https://openairdocs.org/ad/2007-03-17-R1): Fuselage · SOCATA TBM 700. Effective Sep 9, 2009 - [AD 2009-08-09](https://openairdocs.org/ad/2009-08-09): Wiring harness · SOCATA TBM 700. Effective May 20, 2009 - [AD 2008-19-10](https://openairdocs.org/ad/2008-19-10): Movement of the emergency landing gear by-pass selector. · SOCATA TBM 700. Effective Oct 23, 2008 - [AD 2008-17-09](https://openairdocs.org/ad/2008-17-09): Alternator · SOCATA TBM 700. Effective Sep 23, 2008 - [AD 2008-03-15](https://openairdocs.org/ad/2008-03-15): Pilot door · SOCATA TBM 700. Effective Mar 11, 2008 - [AD 2007-23-07](https://openairdocs.org/ad/2007-23-07): Main landing gear wheel · SOCATA TBM 700. Effective Nov 28, 2007 - [AD 2007-21-10](https://openairdocs.org/ad/2007-21-10): Upper access door · SOCATA TBM 700. Effective Nov 21, 2007 - [AD 2007-09-07](https://openairdocs.org/ad/2007-09-07): Nose landing gear (NLG) · SOCATA TBM 700. Effective Jun 4, 2007 - [AD 2007-06-14](https://openairdocs.org/ad/2007-06-14): Propeller control cables · SOCATA TBM 700. Effective Apr 20, 2007 - [AD 2007-06-04](https://openairdocs.org/ad/2007-06-04): Flap carriage rollpins · SOCATA TBM 700. Effective Apr 19, 2007 - [AD 2007-05-18](https://openairdocs.org/ad/2007-05-18): Pulley brackets · SOCATA TBM 700. Effective Apr 12, 2007 - [AD 2007-03-16](https://openairdocs.org/ad/2007-03-16): Excessive lateral play caused by a nonconforming washer · SOCATA TBM 700. Effective Mar 15, 2007 - [AD 2007-02-08](https://openairdocs.org/ad/2007-02-08): Master cylinder yoke failure · SOCATA TBM 700. Effective Feb 26, 2007 - [AD 2006-22-11](https://openairdocs.org/ad/2006-22-11): Initial elevator trim actuator greasing · SOCATA TBM 700. Effective Dec 1, 2006 - [AD 2005-20-24](https://openairdocs.org/ad/2005-20-24): VHF1 antenna mounting area · SOCATA TBM 700. Effective Nov 9, 2005 - [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005 - [AD 2003-26-06](https://openairdocs.org/ad/2003-26-06): Safety Belts and Restraint Systems · Anjou Aeronautique Safety Belts and Restraint Systems, AS332C, AS332L and 14 more. Effective Feb 17, 2004 - [AD 2002-09-11](https://openairdocs.org/ad/2002-09-11): Attaching Bolt/Screw Threads of Inboard, Central, and Outboard Carriages · SOCATA TBM 700. Effective Jun 20, 2002 - [AD 2002-03-03](https://openairdocs.org/ad/2002-03-03): Strainer Draining System in the Cabin Fuselage · SOCATA TBM 700. Effective Mar 29, 2002 - [AD 2001-23-17](https://openairdocs.org/ad/2001-23-17): GNS 430 units · Cessna 172, 182, 206 and 209 more. Effective Dec 28, 2001 - [AD 2001-23-06](https://openairdocs.org/ad/2001-23-06): Fuel Tank Air Vent Valves · SOCATA TBM 700. Effective Dec 27, 2001 - [AD 2001-06-05](https://openairdocs.org/ad/2001-06-05): Oil Breather Vent · SOCATA TBM 700. Effective May 11, 2001 - [AD 2001-04-07](https://openairdocs.org/ad/2001-04-07): Control Cable · SOCATA TBM 700. Effective Apr 13, 2001 - [AD 2000-26-19](https://openairdocs.org/ad/2000-26-19): Fuel Tank Air Vent Valve Hose · SOCATA TBM 700. Effective Feb 2, 2001 - [AD 2000-02-29](https://openairdocs.org/ad/2000-02-29): Airframe Pneumatic Deicing Boots · SOCATA TBM 700. Effective Mar 27, 2000 - [AD 98-24-04](https://openairdocs.org/ad/98-24-04): Flap Carriage · SOCATA TBM 700. Effective Dec 28, 1998 - [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. Effective Dec 22, 1998 - [AD 98-21-15](https://openairdocs.org/ad/98-21-15): Oxygen Generators · SOCATA TBM 700. Effective Nov 20, 1998 - [AD 98-12-02](https://openairdocs.org/ad/98-12-02): Elevator Trim Tab Fittings · SOCATA TBM 700. Effective Jul 17, 1998 - [AD 98-08-27](https://openairdocs.org/ad/98-08-27): Left-Hand Wheel Assembly · SOCATA TBM 700 with STC SA2786CE. Effective May 31, 1998 - [AD 98-04-04](https://openairdocs.org/ad/98-04-04): Starter Generator Mounting Adapter · SOCATA TBM 700. Effective Mar 24, 1998 Historical (superseded or no longer in force): - [AD 2009-23-12](https://openairdocs.org/ad/2009-23-12) (historical): Oxygen · SOCATA TBM 700. Effective Dec 18, 2009 - [AD 2009-13-05](https://openairdocs.org/ad/2009-13-05) (historical): Oxygen · SOCATA TBM 700. Effective Jul 9, 2009 - [AD 2008-19-06](https://openairdocs.org/ad/2008-19-06) (historical): Replacement of the pulley drive assembly by a new one of an improved design. · SOCATA TBM 700. Effective Oct 8, 2008 - [AD 2008-10-13](https://openairdocs.org/ad/2008-10-13) (historical): Alternator and vapour cycle cooling system · SOCATA TBM 700. Effective May 29, 2008 - [AD 2007-06-11](https://openairdocs.org/ad/2007-06-11) (historical): Vertical stabilizer attachment fitting · SOCATA TBM 700. Effective Apr 20, 2007 - [AD 2007-04-13](https://openairdocs.org/ad/2007-04-13) (historical): Main landing gear cylinders · SOCATA TBM 700. Effective Mar 23, 2007 - [AD 2007-04-08](https://openairdocs.org/ad/2007-04-08) (historical): Pilot door locking stop-fittings · SOCATA TBM 700. Effective Mar 23, 2007 - [AD 2007-03-17](https://openairdocs.org/ad/2007-03-17) (historical): Loose rivets on frames C18 BIS and C19 · SOCATA TBM 700. Effective Mar 15, 2007 - [AD 2002-19-01](https://openairdocs.org/ad/2002-19-01) (historical): Flight Control System · SOCATA TBM 700. Effective Oct 29, 2002 - [AD 2001-05-03](https://openairdocs.org/ad/2001-05-03) (historical): Flap Attaching Bolts/Screws · EADS SOCATA TBM 700. Effective Apr 27, 2001 - [AD 99-07-11](https://openairdocs.org/ad/99-07-11) (historical): Outboard Hinge Fittings of Horizontal Stabilizer · SOCATA TBM 700. Effective Apr 16, 1999 All 65: https://openairdocs.org/model/daher-tbm-700/ads.md ## Information bulletins (advisory) (17) - [SAIB CE-16-12](https://openairdocs.org/saib/CE-16-12): AUTO FLIGHT - Autopilot. Issued Jan 25, 2016 - [SAIB CE-07-07](https://openairdocs.org/saib/CE-07-07): Anchor Nuts. Issued Oct 27, 2006 - [SAIB CE-06-61](https://openairdocs.org/saib/CE-06-61): . Issued Aug 11, 2006 - [SAIB CE-06-60](https://openairdocs.org/saib/CE-06-60): . Issued Aug 11, 2006 - [SAIB CE-05-62](https://openairdocs.org/saib/CE-05-62): . Issued Jun 27, 2005 - [SAIB CE-04-61](https://openairdocs.org/saib/CE-04-61): . Issued Apr 12, 2004 - [SAIB CE-04-27](https://openairdocs.org/saib/CE-04-27): . Issued Dec 4, 2003 - [SAIB CE-04-26](https://openairdocs.org/saib/CE-04-26): . Issued Dec 4, 2003 - [SAIB CE-04-25](https://openairdocs.org/saib/CE-04-25): . Issued Dec 4, 2003 - [SAIB CE-04-20](https://openairdocs.org/saib/CE-04-20): . Issued Nov 20, 2003 - [SAIB CE-04-19](https://openairdocs.org/saib/CE-04-19): . Issued Nov 14, 2003 - [SAIB CE-04-16](https://openairdocs.org/saib/CE-04-16): . Issued Nov 12, 2003 - [SAIB CE-03-01](https://openairdocs.org/saib/CE-03-01): . Issued Oct 8, 2002 - [SAIB CE-02-44](https://openairdocs.org/saib/CE-02-44): . Issued Sep 4, 2002 - [SAIB CE-02-27](https://openairdocs.org/saib/CE-02-27): . Issued Apr 16, 2002 - [SAIB CE-01-02](https://openairdocs.org/saib/CE-01-02): . Issued Nov 3, 2000 - [SAIB ACE-98-37](https://openairdocs.org/saib/ACE-98-37): . Issued Jun 18, 1998 ## Registered aircraft (31) - [N128BJ](https://openairdocs.org/aircraft/N128BJ): [Transatlantic Deliveries Trust](https://openairdocs.org/faa-owner/TRANSATLANTIC%20DELIVERIES%20TRUST), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N 1671 - [N243F](https://openairdocs.org/aircraft/N243F): [Afs LLC](https://openairdocs.org/faa-owner/AFS%20LLC), [Prairieville, LA](https://openairdocs.org/faa-place/LA/Prairieville), S/N 1650 - [N318XA](https://openairdocs.org/aircraft/N318XA): [Transatlantic Deliveries Trust](https://openairdocs.org/faa-owner/TRANSATLANTIC%20DELIVERIES%20TRUST), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N 1661 - [N332](https://openairdocs.org/aircraft/N332): [Transatlantic Deliveries Trust](https://openairdocs.org/faa-owner/TRANSATLANTIC%20DELIVERIES%20TRUST), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N 1656 - [N37CV](https://openairdocs.org/aircraft/N37CV): S/N 1684, N-number assigned (import), not yet registered - [N37TA](https://openairdocs.org/aircraft/N37TA): S/N 1685, N-number assigned (import), not yet registered - [N444H](https://openairdocs.org/aircraft/N444H): [Transatlantic Deliveries Trust](https://openairdocs.org/faa-owner/TRANSATLANTIC%20DELIVERIES%20TRUST), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N 1670 - [N44MD](https://openairdocs.org/aircraft/N44MD): [Transatlantic Deliveries Trust](https://openairdocs.org/faa-owner/TRANSATLANTIC%20DELIVERIES%20TRUST), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N 1669 - [N72SW](https://openairdocs.org/aircraft/N72SW): [Watery Domestic LLC](https://openairdocs.org/faa-owner/WATERY%20DOMESTIC%20LLC), [Telluride, CO](https://openairdocs.org/faa-place/CO/Telluride), S/N 1646 - [N775CE](https://openairdocs.org/aircraft/N775CE): [Transatlantic Deliveries Trust](https://openairdocs.org/faa-owner/TRANSATLANTIC%20DELIVERIES%20TRUST), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N 1676 - [N876DT](https://openairdocs.org/aircraft/N876DT): S/N 1680, N-number assigned (import), not yet registered - [N922GG](https://openairdocs.org/aircraft/N922GG): [Transatlantic Deliveries Trust](https://openairdocs.org/faa-owner/TRANSATLANTIC%20DELIVERIES%20TRUST), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N 1673 - [N963FA](https://openairdocs.org/aircraft/N963FA): S/N 1682, N-number assigned (import), not yet registered - [N980BK](https://openairdocs.org/aircraft/N980BK): [537r LLC](https://openairdocs.org/faa-owner/537R%20LLC), [Lake Havasu City, AZ](https://openairdocs.org/faa-place/AZ/Lake%20Havasu%20City), S/N 1648 - [N980CK](https://openairdocs.org/aircraft/N980CK): [As Aviation LLC](https://openairdocs.org/faa-owner/AS%20AVIATION%20LLC), [Hartland, WI](https://openairdocs.org/faa-place/WI/Hartland), S/N 1644 - [N980DV](https://openairdocs.org/aircraft/N980DV): [Transatlantic Deliveries Trust](https://openairdocs.org/faa-owner/TRANSATLANTIC%20DELIVERIES%20TRUST), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N 1672 - [N980EY](https://openairdocs.org/aircraft/N980EY): [Transatlantic Deliveries Trust Trustee](https://openairdocs.org/faa-owner/TRANSATLANTIC%20DELIVERIES%20TRUST%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N 1658 - [N980FP](https://openairdocs.org/aircraft/N980FP): [Elj Northwest Inc](https://openairdocs.org/faa-owner/ELJ%20NORTHWEST%20INC), [Aurora, OR](https://openairdocs.org/faa-place/OR/Aurora), S/N 1653 - [N980GP](https://openairdocs.org/aircraft/N980GP): [Spyglass Capital Holdings LLC](https://openairdocs.org/faa-owner/SPYGLASS%20CAPITAL%20HOLDINGS%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N 1649 - [N980GT](https://openairdocs.org/aircraft/N980GT): S/N 1681, N-number assigned (import), not yet registered - [N980MR](https://openairdocs.org/aircraft/N980MR): [Equipment Services Corp](https://openairdocs.org/faa-owner/EQUIPMENT%20SERVICES%20CORP), [Wahpeton, ND](https://openairdocs.org/faa-place/ND/Wahpeton), S/N 1645 - [N980NE](https://openairdocs.org/aircraft/N980NE): [Transatlantic Deliveries Trust Trustee](https://openairdocs.org/faa-owner/TRANSATLANTIC%20DELIVERIES%20TRUST%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N 1677 - [N980NP](https://openairdocs.org/aircraft/N980NP): [Innovation Transportation Inc](https://openairdocs.org/faa-owner/INNOVATION%20TRANSPORTATION%20INC), [South Chesterfield, VA](https://openairdocs.org/faa-place/VA/South%20Chesterfield), S/N 1652 - [N980PL](https://openairdocs.org/aircraft/N980PL): [Transatlantic Deliveries Trust](https://openairdocs.org/faa-owner/TRANSATLANTIC%20DELIVERIES%20TRUST), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N 1675 - [N980PR](https://openairdocs.org/aircraft/N980PR): [Transatlantic Deliveries Trust](https://openairdocs.org/faa-owner/TRANSATLANTIC%20DELIVERIES%20TRUST), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N 1665 - [N980SA](https://openairdocs.org/aircraft/N980SA): [960 Inc Trustee](https://openairdocs.org/faa-owner/960%20INC%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N 1655 - [N980SM](https://openairdocs.org/aircraft/N980SM): [Muncie Aviation Co](https://openairdocs.org/faa-owner/MUNCIE%20AVIATION%20CO), [Muncie, IN](https://openairdocs.org/faa-place/IN/Muncie), S/N 1663 - [N980SN](https://openairdocs.org/aircraft/N980SN): [Anazco Trans Air LLC](https://openairdocs.org/faa-owner/ANAZCO%20TRANS%20AIR%20LLC), [Warren, NJ](https://openairdocs.org/faa-place/NJ/Warren), S/N 1651 - [N980TH](https://openairdocs.org/aircraft/N980TH): [Transatlantic Deliveries Trust](https://openairdocs.org/faa-owner/TRANSATLANTIC%20DELIVERIES%20TRUST), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N 1674 - [N980VH](https://openairdocs.org/aircraft/N980VH): S/N 1683, N-number assigned (import), not yet registered - [N980VM](https://openairdocs.org/aircraft/N980VM): [Menasha, WI](https://openairdocs.org/faa-place/WI/Menasha), S/N 1654, Registration pending ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (131, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 2023FA0000290](https://openairdocs.org/sdr/2023FA0000290), May 25, 2023: STARTER GEN. FAILED. STARTER/GEN FAILURE IN FLIGHT FORCING PILOT TO DECLARE EMERGENCY LANDING. UPON INSPECTION, STARTER BEARING FOUND THROUGHOUT STARTER HOUSING, ALONG WITH STATOR W - [SDR DGCA 23 3100](https://openairdocs.org/sdr/DGCA%2023%203100), Feb 7, 2023: ELEVATOR. DELAMINATED. ELEVATOR LEADING EDGE DELAMINATION - [SDR 2020FA0000379](https://openairdocs.org/sdr/2020FA0000379), Aug 21, 2020: PUMP. BYPASSING. LANDING GEAR PUMP FAILURE. GEAR WOULD NOT GO DOWN. USED EMERGENCY HAND PUMP TO EXTEND THE GEAR. - [SDR 2019FA0000129](https://openairdocs.org/sdr/2019FA0000129), Apr 23, 2019: CONTROL ROD. DETACHED. 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 INSP - [SDR V94R2019022831002](https://openairdocs.org/sdr/V94R2019022831002), Jan 29, 2019: ROLL PIN. BACKED OUT. 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 TH - [SDR 2018FA0000133](https://openairdocs.org/sdr/2018FA0000133), Apr 3, 2018: GENERATOR. POWER LOSS. PILOT DIVERTED TO PMP DUE TO LOST POWER FROM MAIN GENERATOR. - [SDR URZR20170117001](https://openairdocs.org/sdr/URZR20170117001), Jan 12, 2017: WIRE. NOT REPORTED. 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 DEC - [SDR 2016FA0000664](https://openairdocs.org/sdr/2016FA0000664), Dec 21, 2016: VALVE. DEFECTIVE. 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 AN - [SDR 2016FA0000665](https://openairdocs.org/sdr/2016FA0000665), Dec 20, 2016: VALVE. NO TEST. 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), Dec 14, 2016: FUEL CONTROL. MALFUNCTIONED. 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), Dec 10, 2016: FUEL CONTROL. MALFUNCTIONED. SLOW STARTS. RE-CALIBRATE FCU. - [SDR 2016FA0000611](https://openairdocs.org/sdr/2016FA0000611), Dec 10, 2016: FUEL CONTROL. MALFUNCTIONED. ENGINE SURGES IN MAX REVERSE. FCU TO RECALIBRATE. - [SDR 2016FA0000610](https://openairdocs.org/sdr/2016FA0000610), Dec 10, 2016: FUEL CONTROL. MALFUNCTIONED. MAX REVERSE FAILED CHECK. RE-CALIBRATE FCU. - [SDR 2016FA0000609](https://openairdocs.org/sdr/2016FA0000609), Dec 10, 2016: FUEL CONTROL. MALFUNCTIONED. 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), Dec 10, 2016: FUEL CONTROL. MALFUNCTIONED. ENGINE HANGS DURING START BELOW 40%. SEND FOR RE-CALIBRATION. - [SDR 2016FA0000625](https://openairdocs.org/sdr/2016FA0000625), Nov 19, 2016: FUEL CONTROL. MALFUNCTIONED. ITT LIGHT WHEN GOING INTO MAX REVERSE. RECALIBRATE FCU. - [SDR 2016FA0000623](https://openairdocs.org/sdr/2016FA0000623), Oct 17, 2016: FUEL CONTROL. ABNORMAL. MAX ITT LIGHT WHEN GOING INTO MAX REVERSE. RE-CALIBRATE FCU. - [SDR 2016FA0000622](https://openairdocs.org/sdr/2016FA0000622), Aug 16, 2016: FUEL CONTROL. MALFUNCTIONED. ENGINE STARTING WARM. RE-CALIBRATE FCU. - [SDR 2016FA0000621](https://openairdocs.org/sdr/2016FA0000621), Jul 26, 2016: FUEL CONTROL. MALFUNCTIONED. ENGINE STATING WARM. RE-CALIBRATE FCU. - [SDR 2016FA0000620](https://openairdocs.org/sdr/2016FA0000620), Mar 25, 2016: FUEL CONTROL. MALFUNCTIONED. ENGINE STARTS WARM. RE-CALIBRATE FCU. - [SDR 2016FA0000624](https://openairdocs.org/sdr/2016FA0000624), Jan 24, 2016: FUEL CONTROL. MALFUNCTIONED. ENGINE STARTING WARM AND SLOW STARTS. RE-CALIBRATE FCU. - [SDR 2016FA0000619](https://openairdocs.org/sdr/2016FA0000619), Jan 15, 2016: FUEL CONTROL. MALFUNCTIONED. ENGINE SLOW TO START. RE-CALIBRATE FCU. - [SDR 2016FA0000617](https://openairdocs.org/sdr/2016FA0000617), Sep 21, 2015: FCU. MALFUNCTIONED. HIGH TEMPS DURING START. RE-CLAIBRATE FCU. - [SDR 2016FA0000615](https://openairdocs.org/sdr/2016FA0000615), Sep 9, 2015: FUEL CONTROL. MALFUNCTIONED. MAX ITT LIGHT COMES ON WHEN PULLING INTO MAX REVERSE. RE-CALIBRATE FCU. - [SDR 2016FA0000616](https://openairdocs.org/sdr/2016FA0000616), Aug 18, 2015: FCU. MALFUNCTIONED. ENGINE START TEMPS EXCESSIVE. RECALIBRATE FCU. - [SDR 2016FA0000614](https://openairdocs.org/sdr/2016FA0000614), Aug 7, 2015: FUEL CONTROL. MALFUNCTIONED. FAILED MAX REVERSE CHECK. RE-CALIBRATED FCU. - [SDR 2016FA0000613](https://openairdocs.org/sdr/2016FA0000613), Jul 1, 2015: FUEL CONTROL. MALFUNCTIONED. ENGINE IS SLOW TO START AND DOES NOT MAKE MAX REVERSE CHECK. RECALIBRATED THE FCU. - [SDR 2016FA0000612](https://openairdocs.org/sdr/2016FA0000612), May 28, 2015: FUEL CONTROL. MALFUNCTIONED. ENGINE IS SLOW TO START. RECALIBRATED THE FCU. - [SDR 2016FA0000595](https://openairdocs.org/sdr/2016FA0000595), May 5, 2015: FUEL CONTROL. OUT OF LIMITS. 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), Jan 14, 2015: FUEL CONTROL. OUT OF ADJUST. DEAD BAND ADJUSTMENT SCREW IS AFT OF THE FLIGHT IDLE ROLLER. RE-CALIBRATED FUEL CONTROL UNIT. - [SDR 2016FA0000598](https://openairdocs.org/sdr/2016FA0000598), Dec 12, 2014: FUEL CONTROL. OUT OF ADJUST. AIRCRAFT WILL NOT MAKE MAX REVERSE. RE-CALIBRATED FUEL CONTROL UNIT. - [SDR 2016FA0000597](https://openairdocs.org/sdr/2016FA0000597), Dec 8, 2014: FUEL CONTROL. ABNORMAL. ENGINE IS SLOW TO START AND NOT MAKING MAX REVERSE. CALIBRATED FUEL CONTROL UNIT. - [SDR CA141024008](https://openairdocs.org/sdr/CA141024008), Oct 5, 2014: OIL SYSTEM. LOW PRESSURE. (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 AIRPLAN - [SDR 2014FA0000536](https://openairdocs.org/sdr/2014FA0000536), Aug 11, 2014: CABIN PRESSURE. MALFUNCTIONED. 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 A - [SDR 2016FA0000596](https://openairdocs.org/sdr/2016FA0000596), Aug 9, 2014: FUEL CONTROL. ABNORMAL. ENGINE IS SLOW TO START. FUEL CONTROL UNIT HAD TO BE RE-CALIBRATED. - [SDR CA140721003](https://openairdocs.org/sdr/CA140721003), Jun 25, 2014: ENGINE. VIBRATION. (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 WHE - [SDR 2014FA0000294](https://openairdocs.org/sdr/2014FA0000294), Apr 10, 2014: STRUCTURE. CONTAMINATED. HORIZONTAL STABILIZER STRUCTURE COMPROMISED BY APPARENT WATER DAMAGE CREATING CRACKS AND CORROSION. DEFECTS WITHIN THE PRIMARY STRUCTURE OF THE HORIZONTAL STABI - [SDR CA131007007](https://openairdocs.org/sdr/CA131007007), Sep 22, 2013: FUEL CONTROL. MALFUNCTIONED. (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 P - [SDR RL8R2013FA0000544](https://openairdocs.org/sdr/RL8R2013FA0000544), Aug 28, 2013: ROLL PIN. LOOSE. 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), Aug 28, 2013: ROLL PIN. LOOSE. 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), Aug 28, 2013: ROLL PIN. LOOSE. 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), Aug 28, 2013: ROLL PIN. LOOSE. 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), Aug 28, 2013: ROLL PIN. LOOSE. 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), May 15, 2013: ENGINE. MAKING METAL. (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 - [SDR CA130502001](https://openairdocs.org/sdr/CA130502001), Apr 28, 2013: ENGINE. POWER LOSS. (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. TH - [SDR RL8R2014030700151](https://openairdocs.org/sdr/RL8R2014030700151), Mar 13, 2013: CARRIAGE. DAMAGED. INBD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FLAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOS - [SDR RL8R2014030700150](https://openairdocs.org/sdr/RL8R2014030700150), Mar 13, 2013: CARRIAGE. DAMAGED. INBD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FLAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOS - [SDR 2014FA0000149](https://openairdocs.org/sdr/2014FA0000149), Mar 13, 2013: INSERT. LOOSE. INBD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FLAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOS - [SDR 2013FA0000283](https://openairdocs.org/sdr/2013FA0000283), Mar 13, 2013: INSERT. LOOSE. INBOARD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT L - [SDR 2013FA0000282](https://openairdocs.org/sdr/2013FA0000282), Mar 13, 2013: INSERT. LOOSE. INBD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOSS All 131: https://openairdocs.org/model/daher-tbm-700/reports.md ## STCs that may be installed (OpenAirDocs) (84, first 50) Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc - [STC SA01844WI](https://openairdocs.org/stc/SA01844WI): Installation of Garmin GFC 600 Automatic Flight Control System. Garmin International Inc - [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies - [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC - [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc - [STC SA12408LA](https://openairdocs.org/stc/SA12408LA): Description of Type Design Change: Installation of Dedicated Gas Generator Case drain. Blackhawk Modifications, LLC - [STC SA11158SC](https://openairdocs.org/stc/SA11158SC): Demonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS). Liberty Partners Inc - [STC SA12179DE](https://openairdocs.org/stc/SA12179DE): Replacement of the original Pratt and Whitney PT6A-64 engine with a Pratt and Whitney PT6A-66D engine. Blackhawk Modifications LLC - [STC SA12024SE](https://openairdocs.org/stc/SA12024SE): Installation of Ram Air Cowling. American Aviation Inc - [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc - [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc - [STC SA09887AC](https://openairdocs.org/stc/SA09887AC): Installation of an Avionica MK-III mini Quick Access Recorder (QAR) and optional 4G or LTE Avionica Cellular Module (avCM. Aircraft Systems and Manufacturing Inc - [STC SA01572CH](https://openairdocs.org/stc/SA01572CH): Installation of a Honeywell KMH 880 and KTA 870 Multi-hazard Awareness and Traffic Advisory system. Amphenol Cable and Interconnect Technologies Inc - [STC SA03316CH](https://openairdocs.org/stc/SA03316CH): Activation of an 802.11 a/b/g/n WiFi System. Elliott Aviation Technical Products Development Inc - [STC SA01596SE](https://openairdocs.org/stc/SA01596SE): Installation of Butterfield Industries Oil Residue Collection System, kit P/N BI 3401-1. Raisbeck Engineering Inc - [STC SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH - [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems Inc - [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC - [STC SA09856AC](https://openairdocs.org/stc/SA09856AC): Installation of BendixKing Aerowave 100 In-flight Data Link System for non-essential, non-required aircraft Cabin Systems & Equipments. Honeywell International Inc (Bendix King) - [STC SA11174SC PAGE 2](https://openairdocs.org/stc/SA11174SC%20PAGE%202): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King) - [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC - [STC SA02075SE](https://openairdocs.org/stc/SA02075SE): Installation of a Mid-Continent MD835( ) Lithium Ion Battery. Mid-Continent Instrument Co. Inc - [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc - [STC SA04514NY](https://openairdocs.org/stc/SA04514NY): Single/Dual Transponder System ADS-B Upgrade. Scandinavian Avionics Design ApS - [STC SA00930WI-D](https://openairdocs.org/stc/SA00930WI-D): Installation of Bendix/King KMD 550/850 Multi-Function Display (MFD) system and optional Bendix/King KGP 560 General Aviation Enhanced ground proximity warning system (GA-EGPWS). Honeywell International Inc - [STC SA2328CE-D](https://openairdocs.org/stc/SA2328CE-D): Installation of the Bendix/King KLN 88 Loran C system. Honeywell International Inc - [STC SA01522WI-D](https://openairdocs.org/stc/SA01522WI-D): SERIAL NUMBERS up to and including 433 Excluding 269: Installation of the alternate part number EFS 40 SG 465 Symbol Generator. Honeywell International Inc - [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit. Med-Pac Inc - [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc - [STC SA8107SW](https://openairdocs.org/stc/SA8107SW): Installation of Electrically Powered vapor cycle Air Conditioning System utilizing freon 12 or R134A refrigerant. Air Comm Corporation - [STC SA00344BO PAGE 2](https://openairdocs.org/stc/SA00344BO%20PAGE%202): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies - [STC SA02486LA](https://openairdocs.org/stc/SA02486LA): Replacement of Socata Leading Edge Assemblies and Pneumatic Deicer. SMR Technologies Inc - [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine - [STC SA04263NY](https://openairdocs.org/stc/SA04263NY): Installation of Gogo Business Aviation ATG System. Maxcraft Avionics Ltd - [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation - [STC SA02153LA-D PAGE 2](https://openairdocs.org/stc/SA02153LA-D%20PAGE%202): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc - [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation - [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation - [STC SA2786CE](https://openairdocs.org/stc/SA2786CE): Installation of fuselage shell upholstery panels, window shade assemblies, cabinets, table, and seat upholstery. Textron Aviation Inc - [STC SA00352BO PAGE 2](https://openairdocs.org/stc/SA00352BO%20PAGE%202): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation - [STC SA02119SE PAGE 2](https://openairdocs.org/stc/SA02119SE%20PAGE%202): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc - [STC SA01969SE](https://openairdocs.org/stc/SA01969SE): Installation of a Mid-Continent MD302 Standby Attitude Module. Mid-Continent Instruments and Avionics - [STC SA01229SE PAGE 2](https://openairdocs.org/stc/SA01229SE%20PAGE%202): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc - [STC SA02442AK PAGE 2](https://openairdocs.org/stc/SA02442AK%20PAGE%202): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC - [STC SA01933LA-D PAGE 2](https://openairdocs.org/stc/SA01933LA-D%20PAGE%202): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA03931AT-D](https://openairdocs.org/stc/SA03931AT-D): Installation of a Modified Battery Heat Shield. Socata North America Inc - [STC SA02121SE](https://openairdocs.org/stc/SA02121SE): Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic System. Garmin International Inc - [STC SA00269BO](https://openairdocs.org/stc/SA00269BO): Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ), Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1, and Avidyne Mounting Tray P/N 700-00034-000. Avidyne Corporation - [STC SA02717NY PAGE 2](https://openairdocs.org/stc/SA02717NY%20PAGE%202): Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module. VoiceFlight Systems LLC All 84: https://openairdocs.org/model/daher-tbm-700/stcs.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Socata TBM 700](https://openairdocs.org/model/socata-tbm-700): 643 registered aircraft, registry code 8682000 - [Compagnie Daher TBM 700](https://openairdocs.org/model/compagnie-daher-tbm-700): 314 registered aircraft, registry code 8682010 - [EADS Socata TBM 700](https://openairdocs.org/model/eads-socata-tbm-700): 12 registered aircraft, registry code 8682004 - [Compagnie Daher TBM-700 C1](https://openairdocs.org/model/compagnie-daher-tbm-700-c1): 0 registered aircraft, registry code 8680213 --- 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.