# N910ME: 2017 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: 1208
- Year built: 2017
- Type: Fixed wing single engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: November 10, 2017
- Certificate issued: December 12, 2017
- Expires: December 31, 2027
- Mode S code: AC97C3
- Registered owners: [Plj700pv LLC](https://openairdocs.org/faa-owner/PLJ700PV%20LLC), [Pc700pv LLC](https://openairdocs.org/faa-owner/PC700PV%20LLC), [Mb700pv LLC](https://openairdocs.org/faa-owner/MB700PV%20LLC)
- Location: [King Of Prussia, PA](https://openairdocs.org/faa-place/PA/King%20Of%20Prussia)
- Owner type: Co-owned
- Owner's area on the map: 40.0949° N, 75.3857° W: Placed by OpenAirDocs at the center of ZIP code 19406, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=910ME
- Page: https://openairdocs.org/aircraft/N910ME

From the FAA registry file of October 22, 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/N910ME/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 N910ME.

## NTSB investigations on N910ME not matched to an aircraft (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB NYC05MA083](https://openairdocs.org/ntsb/NYC05MA083), May 13, 2005: Boeing 717-200 (N910ME), Union Star, MO, incident, no damage. Probable cause: A loss of reliable airspeed indication due to an accumulation of ice on the air data/pitot sensors. Contributing to the incident was the flight crew's improper response to the erroneous airspeed…

## FAA accident and incident reports

None matched to N910ME.

## Reports on N910ME not matched to an aircraft (1)

They name N910ME, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20050512007219I](https://openairdocs.org/incident/20050512007219I), May 12, 2005: Boeing 717200 (N910ME), Kirksville, MO, Minor damage. (-23) On 5/12/2005 midwest airlines flight 490, a/c N910ME, from Kansas city international airport (kmci) enroute to ronald reagan Washington national airport…

## 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 N910ME not matched to an aircraft (21)

They name N910ME, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR MWEA090515001](https://openairdocs.org/sdr/MWEA090515001), May 15, 2009: CABLE. DAMAGED. TAILCONE AND SLIDE FAILED TO DEPLOY USING AFT PRESSURE BULKHEAD DOOR EMERGENCY RELEASE SYSTEM. ADJUSTED RETAINING CLIPS ON INTERIOR RELEASE PINS TO OBTAIN 30 LB
- [SDR MWEA090012](https://openairdocs.org/sdr/MWEA090012), Apr 21, 2009: GASPER FAN. DEFECTIVE. ELECTRICAL ODOR FROM FORWARD CABIN DURING AIRCRAFT BOARDING. PASSENGERS WERE DISEMBARKED AS A PRECAUTION. THE GASPER FAN IN THE LEFT CONDITIONED AIR DISTRIBUTIO
- [SDR MWE2008F00036](https://openairdocs.org/sdr/MWE2008F00036), Aug 30, 2008: BATTERY PACK. INOPERATIVE. BOTH LT AND RT EXTERIOR EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED OVERWING EMERGENCY BATTERY PACK. (K)
- [SDR MWE2008F00000](https://openairdocs.org/sdr/MWE2008F00000), Jun 28, 2008: BATTERY PACK. INOPERATIVE. TWO LIGHT INOPERATIVE ON TAILCONE SLIDE EMERGENCY LIGHT. REPLACED BATTERY PACK ASSEMBLY. (K)
- [SDR MWEA080076](https://openairdocs.org/sdr/MWEA080076), May 21, 2008: CONTROL UNIT. MALFUNCTIONED. AT 35,000 FEET RIGHT FIRE DETECTOR FAIL CAME ON INTERMITTENTLY. LIGHT WOULD COME ON FOR NO LONGER THAN 2 SECONDS, THEN GO OFF. REMOVED AND REPLACED FDCU FOR RIG
- [SDR MWEA080034](https://openairdocs.org/sdr/MWEA080034), Feb 20, 2008: BATTERY PACK. DISCHARGED. LEFT AND RIGHT EXTERIOR EMERGENCY LIGHTS ARE NOT ILLUMINATING. REMOVED AND REPLACED EMERGENCY BATTERY PACK.
- [SDR MWEA070293](https://openairdocs.org/sdr/MWEA070293), Nov 8, 2007: PAN. CRACKED. AFT CARGO DOOR INNER PAN CRACKED AT FORWARD CRANK GUIDE. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA070292](https://openairdocs.org/sdr/MWEA070292), Nov 8, 2007: PAN. CRACKED. AFT CARGO DOOR OUTER PAN HAS A CRACK LOCATED AT THE FORWARD SIDE BY CRANK GUIDE. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA070234](https://openairdocs.org/sdr/MWEA070234), Oct 4, 2007: CHANNEL. CRACKED. RIGHT THRUST REVERSER UPPER BUCKET AFT ZEE CHANNEL IS CRACKED ON INBOARD SIDE AT STATION 36. CUT OUT DAMAGE AND FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA070098](https://openairdocs.org/sdr/MWEA070098), Apr 25, 2007: SWITCH. INOPERATIVE. INTERNAL TAIL CONE RELEASE LIGHT SWITCH DID NOT ACTUATE AFTER TAIL CONE WAS RELEASED FOR TEST FUNCTION. REMOVED AND REPLACED INTERNAL TAIL CONE LOCKING SWITCH.
- [SDR MWEA060179](https://openairdocs.org/sdr/MWEA060179), Aug 23, 2006: DIMMER. SMOKE. VISIBLE SMOKE AND ACRID SMELL POURED FROM THE HOUSING AROUND THE MASK. FOUND INSTRUMENT AND PEDESTAL LIGHT DIMMER BOX SHOWING SIGNS OF INTERNAL COMPONENT BURN A
- [SDR MWEA050141](https://openairdocs.org/sdr/MWEA050141), Dec 22, 2005: DISPLAY. FAILED. NUMBER TWO DISPLAY UNIT FAILED AND CABIN WAS FILLED WITH SMOKE. REMOVED AND REPLACED NUMBER TWO DISPLAY UNIT.
- [SDR MWEA050133](https://openairdocs.org/sdr/MWEA050133), Dec 5, 2005: STRUT. LOW. NOSE LANDING GEAR UNSAFE LIGHT STAYED ON. FOUND STRUT LOW, SERVICED STRUT.
- [SDR MWEA050058](https://openairdocs.org/sdr/MWEA050058), Jun 25, 2005: WIRE. UNSECURE. SEAT 13D EMERGENCY EXIT ROW DOOR HAS A WIRE HANGING OUT OF LOWER PANEL. RESECURED WIRE.
- [SDR MWEA060230](https://openairdocs.org/sdr/MWEA060230), May 12, 2005: CONTROL COLUMN. DISCONNECTED. RUDDER LIMIT FAULT ON ENGINE AND ALERT DISPLAY AND CONTROL COLUMN DISCONNECTED. PERFORMED FAULT ISLOATION MANUAL TASK OR RETURNED TO SERVICE WORK, LIGHTNING STR
- [SDR MWEA050043](https://openairdocs.org/sdr/MWEA050043), May 12, 2005: SKIN. LIGHTNING STRIKE. LIGHTNING STRIKE DAMAGE TO TAILCONE BOTTOM RIGHT EDGE. NO OTHER INFORMATION AT THIS TIME WAITING FOR FIX.
- [SDR MWEA040161](https://openairdocs.org/sdr/MWEA040161), Sep 10, 2004: THROTTLE. FAILED. AUTO THROTTLES FAILED TO ADVANCE, SET POWER MANUALLY, THEN V SPEED INDICATIONS WERE LOST. PERFORMED RETURN TO SERVICE TEST, FOR FLIGHT CONTROL COMPUTER AND ENGI
- [SDR MWEA040028](https://openairdocs.org/sdr/MWEA040028), Mar 20, 2004: COMPUTER. INTERMITTENT. LOW SPEED HIGH PROTECTION CAME ON TOGETHER AND STICK SHAKER. PERFORMED ADJUSTMENT TEST OF NUMBER 1 FLIGHT CONTROL COMPUTER AND NR 2 FLIGHT CONTROL COMPUTER STAL
- [SDR MWEA030495](https://openairdocs.org/sdr/MWEA030495), Dec 20, 2003: CHARGER. FAILED. ENGINE STARTED AND GENERATOR CAME ON LINE ALERTS BUS TIE LEFT AND RIGHT LOCKOUT EMERGENCY POWER ON BUS AC GROUND SPEED OFF ILLUMINATED. REMOVED AND REPLACED EME
- [SDR MWEA030450](https://openairdocs.org/sdr/MWEA030450), Nov 20, 2003: MODULE. INOPERATIVE. GROUND SPOILER WOULD NOT ARM. REMOVED AND REPLACED SPEED BRAKE MODULE.
- [SDR MWEA030449](https://openairdocs.org/sdr/MWEA030449), Nov 20, 2003: WARNING SYSTEM. FALSE INDICATION. GROUND SPOILER WOULD NOT ARM. PERFORMED RETURN TO SERVICE TEST. ALL TEST PASSED, OK FOR SERVICE.

## 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 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 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 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/N910ME/stcs.md

## 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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