# N931MC: Socata TBM 700

- Status: Valid registration
- Airframe: [Socata TBM 700](https://openairdocs.org/model/socata-tbm-700) (registry code 8682000, 7 seats)
- Engine: [Pratt & Whitney Canada PT6A66D](https://openairdocs.org/engine/pratt-whitney-canada-pt6a66d) (registry code 52069)
- Data sheets: [TCDS A60EU](https://openairdocs.org/tcds/A60EU) (Daher Aircraft SAS), [TCDS E26NE](https://openairdocs.org/tcds/E26NE) (Pratt & Whitney Canada Corp.) (OpenAirDocs)
- Serial number: 1156
- Type: Fixed wing single engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: December 12, 2016
- Certificate issued: April 21, 2025
- Expires: April 30, 2032
- Mode S code: ACEA76
- Registered owner: [Sandcastle Stables LLC](https://openairdocs.org/faa-owner/SANDCASTLE%20STABLES%20LLC)
- Location: [Camden, DE](https://openairdocs.org/faa-place/DE/Camden)
- Owner type: LLC
- Owner's area on the map: 39.0847° N, 75.6274° W: Placed by OpenAirDocs at the center of ZIP code 19934, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=931MC
- Page: https://openairdocs.org/aircraft/N931MC

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 55 in force

### Matched by airframe (Socata TBM 700)

- [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

### Matched by engine (Pratt & Whitney Canada PT6A66D)

- [AD 2024-04-51](https://openairdocs.org/ad/2024-04-51): Turbine Section · Pratt & Whitney Canada PT6A-64, PT6A-66, PT6A-66A and 17 more. Effective Mar 28, 2024

### 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 66: https://openairdocs.org/aircraft/N931MC/ads.md

## Information bulletins (advisory) (17 in force)

- [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

## NTSB investigations

None matched to N931MC.

## FAA accident and incident reports

None matched to N931MC.

## Reports on N931MC not matched to an aircraft (6)

They name N931MC, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19980311005619I](https://openairdocs.org/incident/19980311005619I), Mar 11, 1998: Doug DC982 (N931MC), Kansas City, MO. Narrative: aircraft departed mci for msp, when pilot reported, unable to raise nose gear, main gears retracted easily, but nose gear did not. Aircraft landed…
- [Incident 19960513019439I](https://openairdocs.org/incident/19960513019439I), May 13, 1996: Doug DC982 (N931MC), Atlanta, GA, Minor damage. Narrative: after takeoff #2 engine failure at 1,000', aft's fired, EGT 700', n' 50%. Returned to atl.
- [Incident 19920116004379I](https://openairdocs.org/incident/19920116004379I), Jan 16, 1992: Doug DC982 (N931MC), Denver, CO. Pressurization problem en route. Masks deployed. Diverted for landing. Had two mask problems due to solenoid valve.
- [Incident 19860721041129I](https://openairdocs.org/incident/19860721041129I), Jul 21, 1986: Doug DC982 (N931MC), Houston, TX. After takeoff right main indicated unsafe. Recycled. Returned found faulty ground proximity card.
- [Incident 19850726046609I](https://openairdocs.org/incident/19850726046609I), Jul 26, 1985: Doug DC982 (N931MC), Houston, TX, Minor damage. Leading edge slat struck truck on taxiway. Crew unaware of strike. Damage discovered after 3 subsequent flights.
- [Incident 19831107069089I](https://openairdocs.org/incident/19831107069089I), Nov 7, 1983: Doug DC982 (N931MC), Lubbock, TX. Making a left turn from taxiway onto departure runway the turning radius was too short. Gear became stuck in mud.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N931MC not matched to an aircraft (27)

They name N931MC, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR 9807289304](https://openairdocs.org/sdr/9807289304), Apr 25, 1998: SPLICE. BROKEN. DURING LINE CHECK, FOUND FLOOR TRACK LIGHT AFT OF SEAT ROW 1CD WITH BROKEN WIRE SPLICE. MAINTENANCE REPAIRED WIRING, OPERATIONAL CHECK NORMAL.
- [SDR 9804139304](https://openairdocs.org/sdr/9804139304), Mar 10, 1998: STRUT. CONTAMINATED. AIRCRAFT FAILED TO SHIFT FROM GROUND MODE TO FLIGHT MODE AFTER TAKEOFF. FLIGHT WAS RETURNED TO MCI AND LANDED WITHOUT INCIDENT. MAINTENANCE CONFIRMED CONTAMINAT
- [SDR 9801349304](https://openairdocs.org/sdr/9801349304), Jan 22, 1998: SLIDE. LOW PRESSURE. DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EVACUATION SLIDE BOTTLE PRESSURE LOW. REPLACED SLIDE.
- [SDR 9718749304](https://openairdocs.org/sdr/9718749304), Oct 2, 1997: BATTERY PACK. DISCHARGED. DURING LINE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE IN THE TAILCONE AREA. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL.
- [SDR 9718539304](https://openairdocs.org/sdr/9718539304), Oct 1, 1997: OIL FILTER. DIRTY. DURING TAXI, THE LEFT ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED. CREW SHUT DOWN THE LEFT ENGINE AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE LEFT ENGINE 
- [SDR 9712729304](https://openairdocs.org/sdr/9712729304), Jun 27, 1997: BATTERY  PACK. DISCHARGED. DURING LINE INSPECTION, FOUND SEAT ROW 3 THROUGH 9 EMERGENCY OVERHEAD LIGHTS INOPERATIVE. REPLACED BATTERIES AND POWER SUPPLY, OPERATIONAL CHECK OK.
- [SDR 9712589304](https://openairdocs.org/sdr/9712589304), Jun 24, 1997: OIL TEMP BULB. FAILED. DURING CLIMB, APU OIL TEMP HIGH LIGHT ANNUNCIATED. PLACED NR 2 ENGINE GENERATOR ON MEL. APU WAS SHUT DOWN. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. REPLACED THE 
- [SDR 9706389304](https://openairdocs.org/sdr/9706389304), Mar 24, 1997: BATTERY. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 15 THROUGH 19 INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.
- [SDR 9707689304](https://openairdocs.org/sdr/9707689304), Feb 23, 1997: PT 7 LINE. ICED UP. AS TAKEOFF POWER WAS APPLIED, THE RIGHT ENGINE EPR INDICATION DID NOT RESPOND. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE FOUND THE RIGHT ENGINE
- [SDR 9622419304](https://openairdocs.org/sdr/9622419304), Oct 20, 1996: SLIDE. DEPLOYED. AFT TAILCONE EVACUATION SLIDE INADVERTANTLY DEPLOYED. REPLACED SLIDE.
- [SDR 9621399304](https://openairdocs.org/sdr/9621399304), Oct 2, 1996: LONGERON. CORRODED. DURING H-CHECK, FOUND CORROSION ON LONGERON 22L AT FS 1287 AND 1309. REPAIRED LONGERON (P/N S-1242886) PER EA 93-110348.
- [SDR 9621389304](https://openairdocs.org/sdr/9621389304), Oct 2, 1996: DOUBLER. CRACKED. DURING H-CHECK, FOUND CRACKS IN THE FS 1079 -1089 WINDOW RINGPAN LEFT SIDE. REPAIRED RINGPAN (P/N 5912285) PER EA 93-110339.
- [SDR 9621369304](https://openairdocs.org/sdr/9621369304), Oct 1, 1996: CUSP. CORRODED. DURING H-CHECK, FOUND CORROSION ON THE LEFT CUSP AT FS 200. REPAIRED CUSP (P/N 9923666-3) PER EA 93-109586.
- [SDR 9621359304](https://openairdocs.org/sdr/9621359304), Oct 1, 1996: LONGERON. CORRODED. DURING H-CHECK, FOUND CORROSION ON LONGERON 29L AT FS 480. REPAIRED LONGERON (P/N 3936478-503) PER EA 93-110321.
- [SDR 9621349304](https://openairdocs.org/sdr/9621349304), Oct 1, 1996: LONGERON. CORRODED. DURING H-CHECK, FOUND CORROSION ON THE LONGERON 26L FROM FS 229 - 399. REPAIRED LONGERON (P/N 5936434-29) PER EA 93-110340.
- [SDR 9620499304](https://openairdocs.org/sdr/9620499304), Sep 22, 1996: FITTING. CORRODED. DURING H-CHECK, FOUND CORROSION IN THE AFT CARGO DOOR CUTOUT OF THE AFT LOWER CORNER FS 1211 FRAME FITTING. REPLACED FITTING (P/N 5936469-1) PER SRM 51-01, PAR 
- [SDR 9621189304](https://openairdocs.org/sdr/9621189304), Sep 19, 1996: SKIN. CRACKED. DURING H-CHECK, FOUND A CRACK IN THE LEFT AFT SERVICE DOOR SKIN AT THE HOLD OPEN HOOK. REPAIRED SKIN (P/N 5937601-3) PER EA 93-110332.
- [SDR 9616349304](https://openairdocs.org/sdr/9616349304), Jul 28, 1996: SEAL. FAILED. DURING CLIMB MSP-IND, A FLIGHT ATTENDANT HEARD A LOUD BANGING NOISE OUTSIDE OF THE AFT GALLEY SERVICE DOOR. RETURNED TO MSP WITHOUT FURTHER INCIDENT. REPLACED U
- [SDR 9614359304](https://openairdocs.org/sdr/9614359304), Jun 29, 1996: CEILING PANEL. OUT OF POSITION. DURING A-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DEPLOY THE TAILCONE USING THE AFT ENTRY DOOR. ALSO, FOUND THAT THE CEILING PANEL INTERFERED WITH THE 
- [SDR 9613769304](https://openairdocs.org/sdr/9613769304), Jun 23, 1996: POWER PACK. INOPERATIVE. DURING LINE CHECK, FOUND EMERGENCY EXIT SIGN AT ROW 20 RIGHT INOPERATIVE. REPLACED POWER PACK AND LIGHT ASSEMBLY, OPERATIONAL CHECK OK.
- [SDR 9612649304](https://openairdocs.org/sdr/9612649304), Jun 8, 1996: BATTERY PACK. DISCHARGED. DURING LINE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE AT AFT OVERWING EXITS. REPLACED BATTERY PACKS, OPERATIONAL CHECK OK.
- [SDR 9610679304](https://openairdocs.org/sdr/9610679304), May 13, 1996: TURBINE. FAILED. NR 2 ENGINE EXPERIENCED A CONTAINED TURBINE FAILURE DURING CLIMB-OUT. FLIGHT RETURNED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NR 2 ENGINE ASSEM
- [SDR 9610149304](https://openairdocs.org/sdr/9610149304), May 3, 1996: BATTERIES. DISCHARGED. DURING LINE CHECK, FOUND EMERGENCY LIGHTS IN CABIN CEILING INOPERATIVE FROM ROWS 20 - 25. REPLACED BATTERIES AND OPERATIONAL CHECK GOOD.
- [SDR 9602949304](https://openairdocs.org/sdr/9602949304), Feb 1, 1996: BATTERY PACK. DISCHARGED. DURING LINE CHECK, MAINTENANCE FOUND FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK AND CHECKED GOOD.
- [SDR 9521969304](https://openairdocs.org/sdr/9521969304), Dec 30, 1995: COFFEE MAKER. MALFUNCTIONED. EN ROUTE MSP-ATL, SMOKE BEGAN EMANATING FROM THE COFFEE MAKER AREA. GALLEY POWER WAS EXTINGUISHED AND SMOKE DISSIPATED SHORTLY THEREAFTER. FLIGHT CONTINUED TO D
- [SDR 9508319304](https://openairdocs.org/sdr/9508319304), May 16, 1995: DOOR JAMB. CORRODED. DURING PERIODIC CHECK, FOUND CORROSION ON THE MID CARGO LOWER DOOR JAMB BEAM. REPAIRED BEAM P/N 5936038-1 PER EA 93-98421.
- [SDR 9503039304](https://openairdocs.org/sdr/9503039304), Feb 22, 1995: PRESS CONTROL. MALFUNCTIONED. AIRCRAFT WOULD NOT PRESSURIZE WITH PRIMARY SYSTEM AFTER TAKEOFF. SWITCHED TO STANDBY AND SYSTEM WORKED NORMALLY. TRANSFER LOCKOUT AND STANDBY ON LIGHTS ILLUMINA

## STCs that may be installed (OpenAirDocs) (84, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Socata TBM 700)

- [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/aircraft/N931MC/stcs.md

## Earlier aircraft with N931MC

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N931MC before.

- [Cancelled 2010-01-12](https://openairdocs.org/deregistered/N931MC-2010-01-12): Cessna T182T, S/N T18208931. Exported to Switzerland. Owner: [Atlantic Ferry Service Inc](https://openairdocs.org/faa-owner/ATLANTIC%20FERRY%20SERVICE%20INC), [Waterloo, IA](https://openairdocs.org/faa-place/IA/Waterloo)

## Related

- Other Socata TBM 700 aircraft: https://openairdocs.org/model/socata-tbm-700/aircraft.md
- The Pratt & Whitney Canada PT6A66D engine: https://openairdocs.org/engine/pratt-whitney-canada-pt6a66d.md

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