# N86CH: 2010 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 PT6A-66 series](https://openairdocs.org/engine/pratt-whitney-canada-pt6a-66-series) (registry code 52118)
- 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: 543
- Year built: 2010
- Type: Fixed wing single engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: June 14, 2010
- Certificate issued: August 20, 2025
- Expires: August 31, 2032
- Mode S code: ABCCB8
- Registered owner: [Carlyle Air LLC](https://openairdocs.org/faa-owner/CARLYLE%20AIR%20LLC)
- Location: [Morristown, TN](https://openairdocs.org/faa-place/TN/Morristown)
- Owner type: LLC
- Owner's area on the map: 36.1751° N, 83.2570° W: Placed by OpenAirDocs at the center of ZIP code 37813, 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=86CH
- Page: https://openairdocs.org/aircraft/N86CH

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. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada PT6A-66 model are included.

## ADs that may apply (OpenAirDocs): 57 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 PT6A-66 series)

- [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
- [AD 2012-09-10](https://openairdocs.org/ad/2012-09-10): First stage sun gears · Pratt & Whitney Canada PT6A-110, PT6A-112, PT6A-114 and 12 more. Effective May 23, 2012
- [AD 97-04-12](https://openairdocs.org/ad/97-04-12): Compressor Bleed-off Valve · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 52 more. Effective Mar 14, 1997

### 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 68: https://openairdocs.org/aircraft/N86CH/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 N86CH.

## FAA accident and incident reports

None matched to N86CH.

## Reports on N86CH not matched to an aircraft (2)

They name N86CH, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19961006043299I](https://openairdocs.org/incident/19961006043299I), Oct 6, 1996: Bolkms BO105S (N86CH), Lafayette, LA. Narrative: the pilot detected a slight vibration in the tail rotor pedals and diverted to a nearby airport. Maintenance found failed bearing in the tail rotor…
- [Incident 19950120006189I](https://openairdocs.org/incident/19950120006189I), Jan 20, 1995: Bolkms BO105A (N86CH), Little Rock, AR. Narrative: the no. 1 engine turbine outlet temperature (tot) increased to 800 degrees in cruise flight. The pilot reduced the N2 RPM of the no. 1 engine,…

## 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 N86CH not matched to an aircraft (51, newest 50)

They name N86CH, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR HEEA079280](https://openairdocs.org/sdr/HEEA079280), May 16, 2002: INDICATOR. INACCURATE. HORIZON GYRO INDICATOR SHOWS 5 DEGREES LEFT BANK AND SOMETIMES 10 DEGREES NOSE DOWN IN LEVEL FLIGHT. REPLACED WITH SERVICEABLE PART.
- [SDR HEEA077040](https://openairdocs.org/sdr/HEEA077040), Oct 30, 2001: CONTROL UNIT. MALFUNCTIONED. LED READ OUT ARE UNREADABLE ON DISPLAY. REPLACED WITH SERVICEABLE PART.
- [SDR HEEA065399](https://openairdocs.org/sdr/HEEA065399), Dec 10, 1999: TRANSMITTER. FAILED. TRANSMITTER INOPERABLE.
- [SDR HEEA065394](https://openairdocs.org/sdr/HEEA065394), Dec 10, 1999: TRANSMITTER. FAILED. TRANSMITTER INOPERABLE.
- [SDR HEEA064646](https://openairdocs.org/sdr/HEEA064646), Oct 4, 1999: SEAL. PITTED. RECEIVING INSPECTION REVEALED PITTED AND SCRATCHED SEAL FACE. INSTALLED NEW PART.
- [SDR HEEA063427](https://openairdocs.org/sdr/HEEA063427), Aug 6, 1999: INDICATOR. FAILED. GAUGE READS NEGATIVE WHEN AIRCRAFT RUNNING.
- [SDR HEEA061796](https://openairdocs.org/sdr/HEEA061796), Apr 6, 1999: AUDIO CONTROL. FAILED. NO RECEPTION ON HEADSETS. PERFORMED PRELIMINARY INSPECTION AND FOUND SIDETONE LEVEL WEAK AND COULD NOT BE ADJUSTED TO MFG SPECS.
- [SDR HEEA060471](https://openairdocs.org/sdr/HEEA060471), Jan 25, 1999: INDICATOR. MALFUNCTIONED. SMALL NEEDLE OSCILLATES.
- [SDR HEEA060469](https://openairdocs.org/sdr/HEEA060469), Jan 25, 1999: TRANSMITTER. READS HIGH. PRESSURE TRANSMISSION CAUSING FLUCTUATIONS; READS HIGH OUT OF TOLERANCE ABOVE 16 PSI.
- [SDR HEEA0016755](https://openairdocs.org/sdr/HEEA0016755), Nov 6, 1998: INDICATOR. READS HIGH. EXHAUST TEMPERATURE INDICATION READS 15 HIGH.
- [SDR HEEA0016641](https://openairdocs.org/sdr/HEEA0016641), Nov 5, 1998: GYRO. MALFUNCTIONED. GYRO HAS INTERMITTENT OUTPUT TO HSI INDICATOR.
- [SDR HEEA0016138](https://openairdocs.org/sdr/HEEA0016138), Oct 8, 1998: HOUSING. LOOSE. ENGINE REMOVED DUE TO LOW POWER. UPON DISASSEMBLY OF ENGINE NOTED: DETACHED SPARE CAGE IN GEARBOX. GEARBOX DISASSEMBLY REVEALED: LOOSE P.T.O. CAGE IN GEARBOX HO
- [SDR HEEA0016137](https://openairdocs.org/sdr/HEEA0016137), Oct 8, 1998: COVER. LOOSE. ENGINE REMOVED DUE TO LOW POWER. UPON DISASSEMBLY OF ENGINE NOTED: DETACHED SPARE CAGE IN GEARBOX. GEARBOX DISASSEMBLY REVEALED: DETACHED SPARE CAGE AND LOOSE C
- [SDR HEEA0015545](https://openairdocs.org/sdr/HEEA0015545), Aug 14, 1998: VALVE. STICKING. BLEED AIR VALVE INTERMITTENTLY STICKS IN OPEN POSITION.
- [SDR HEEA0015061](https://openairdocs.org/sdr/HEEA0015061), Jun 30, 1998: TRANSDUCER. FAILED. TRANSDUCER PEGGING OUT, FUNCTION CHECK BAD, OUT OF TOLERANCE ON INCREASING PRESSURE.
- [SDR HEEA0014461](https://openairdocs.org/sdr/HEEA0014461), Jun 2, 1998: INDICATOR. ERRATIC. INDICATION ERRATIC.
- [SDR HEEA0014446](https://openairdocs.org/sdr/HEEA0014446), Jun 2, 1998: INDICATOR. FAULTY. NR 2 NR NEEDLE LAGS BEHIND AND IS RATCHETY.
- [SDR HEEA0013824](https://openairdocs.org/sdr/HEEA0013824), Apr 2, 1998: POWER SUPPLY. FAILED. STROBE LIGHT INOPERATIVE.
- [SDR HEEA0013823](https://openairdocs.org/sdr/HEEA0013823), Apr 2, 1998: RPM WARNING BOX. FAILED. ROTOR LIGHTS INOPERATIVE.
- [SDR HEEA0013820](https://openairdocs.org/sdr/HEEA0013820), Apr 2, 1998: RPM WARNING BOX. MALFUNCTION. AUDIO HORN BEEPS LOW.
- [SDR HEEA0013731](https://openairdocs.org/sdr/HEEA0013731), Apr 2, 1998: INDICATOR. FAILED. ROTOR NEEDLE READS ABOUT 3% HIGHER THAN N2 NEEDLES.
- [SDR HEEA0013667](https://openairdocs.org/sdr/HEEA0013667), Mar 30, 1998: GEARBOX COVER. LEAKING. ENGINE REMOVED DUE TO AFT T/M LEAK. INSPECTION REVEALED: LEAKING AT COVER AFT T/M BORE.
- [SDR HEEA0013282](https://openairdocs.org/sdr/HEEA0013282), Mar 4, 1998: INDICATOR. HANGS. SINGLE RPM NEEDLE HANGS 10% WHEN MOTORING ENGINE.
- [SDR HEEA0013181](https://openairdocs.org/sdr/HEEA0013181), Mar 4, 1998: ALTIMETER. FAILED. RADAR ALTIMETER NEEDLE WON'T REVOLVE IN REVOLVE MODE.
- [SDR HEEA0012510](https://openairdocs.org/sdr/HEEA0012510), Jan 6, 1998: INVERTER. FAILED. INVERTER FAILED. NO POWER TO 110 VAC.
- [SDR HEEA0012489](https://openairdocs.org/sdr/HEEA0012489), Jan 6, 1998: POWER SUPPLY. FAILED. POWER SUPPLY INOPERATIVE. NO OUTLET WORKS, SMALL RATTLE INSIDE.
- [SDR HEEA0012488](https://openairdocs.org/sdr/HEEA0012488), Jan 6, 1998: POWER SUPPLY. FAILED. POWER SUPPLY INOPERATIVE LIGHTS ARE OUT.
- [SDR HEEA0011685](https://openairdocs.org/sdr/HEEA0011685), Oct 22, 1997: OIL COOLER. LEAKING. NR 2 ENGINE OIL COOLER LEAKING.
- [SDR HEEA0011559](https://openairdocs.org/sdr/HEEA0011559), Oct 16, 1997: GEAR BOX ASSY. LOW OIL PRESS. GEAR BOX ASSY LOW OIL PRESSURE.
- [SDR HEEA0011437](https://openairdocs.org/sdr/HEEA0011437), Oct 10, 1997: CARTRIDGE. DEFECTIVE. PUMP RUNS INTERMITTENTLY.
- [SDR HEEA0011241](https://openairdocs.org/sdr/HEEA0011241), Oct 7, 1997: TRANSCEIVER. MALFUNCTION. SEGMENTS OF LETTERS INTERMITTENTLY DISAPPEAR. FOUND UNIT DISPLAY TO FLUTTER AND GO DIM INTERMITTENTLY AFTER WARMED UP. REMOVED SMALL METAL FLAKES FROM DISPLAY B
- [SDR HEEA0010752](https://openairdocs.org/sdr/HEEA0010752), Aug 19, 1997: INDICATOR. ERRATIC. TEMP INDICATOR ERRATIC INDICATION. TIME SINCE REPAIR 14:40.
- [SDR HEEA0010498](https://openairdocs.org/sdr/HEEA0010498), Jul 16, 1997: VALVE. STICKING. VALVE STICKING.
- [SDR HAIHEEA9579](https://openairdocs.org/sdr/HAIHEEA9579), Apr 24, 1997: FUEL TANK. CRACKED. FOUR UNBONDED SNAPS, CRACKED SEAMS AND WORN MATERIAL AT SNAP LOCATION.
- [SDR HEEA978937](https://openairdocs.org/sdr/HEEA978937), Jan 29, 1997: TANK. LEAKING. TANK LEAKING.
- [SDR HEEA978884](https://openairdocs.org/sdr/HEEA978884), Jan 14, 1997: ELT. MALFUNCTION. ELT ACTIVATES IN FLIGHT.
- [SDR HEEA968539](https://openairdocs.org/sdr/HEEA968539), Nov 22, 1996: BEARING. FAILED. BEARING INNER RACE CAME COMPLETELY OUT OF BEARING. INSTALLED SERVICEABLE P/C LINK. ONE P/C LINK SCRAPPED CAUSED BY BEARING FAILURE.
- [SDR HEEA968320](https://openairdocs.org/sdr/HEEA968320), Oct 14, 1996: TRANSMITTER. FAILED. TRANSMITTER UNRELIABLE.
- [SDR HEEA966871](https://openairdocs.org/sdr/HEEA966871), Mar 22, 1996: INDICATOR. DEFECTIVE. FLAG IS NOT GOING BEHIND MASK AFTER TESTING. SENT TO ALLIED SIGNAL AVIONICS FOR INSPECTION AND REPAIR.
- [SDR HEEA966702](https://openairdocs.org/sdr/HEEA966702), Feb 20, 1996: INDICATOR. ERRATIC. UNIT WILL NOT TEST PROPERLY AND NEEDLE HAS A ERRATIC INDICATION. TIME SINCE REPAIR 0:00.
- [SDR HEEA966701](https://openairdocs.org/sdr/HEEA966701), Feb 20, 1996: TRANSMITTER. ERRATIC. TRANSMITTER UNIT WILL NOT TEST PROPERLY AND NEEDLE HAS A ERRATIC INDICATION. TIME SINCE REPAIR 0:00.
- [SDR HEEA966532](https://openairdocs.org/sdr/HEEA966532), Jan 26, 1996: TANK. PEELING. MAIN FUEL TANK,PEELING INSIDE.
- [SDR HEEA955654](https://openairdocs.org/sdr/HEEA955654), Aug 31, 1995: INDICATOR. DEFECTIVE. #1 NEEDLE LAGS BY APPROXIMATELY 3%.
- [SDR HEEA955633](https://openairdocs.org/sdr/HEEA955633), Aug 25, 1995: CARTRIDGE. DEFECTIVE. UNIT STOPPED RUNNING. INSPECTED BY ACCESSORY SHOP AND RAN ON TEST BENCH. UNIT RAN SLOW AND NOISY. IT DID NOT RUN FAST ENOUGH TO INDICATE FLOW ON THE FLOW METER 
- [SDR HEEA955432](https://openairdocs.org/sdr/HEEA955432), Jul 24, 1995: CARTRIDGE. DEFECTIVE. FUEL CARTRIDGE CAUSED CIRCUIT BREAKER TO EXTEND (POP).
- [SDR HEEA955051](https://openairdocs.org/sdr/HEEA955051), May 19, 1995: POWER SUPPLY. INOPERATIVE. POWER SUPPLY INOPERATIVE.
- [SDR HEEA954823](https://openairdocs.org/sdr/HEEA954823), Apr 20, 1995: BLADE. CRACKED. NOSE AND NECK SHELLS CRACKED.
- [SDR HEEA954636](https://openairdocs.org/sdr/HEEA954636), Mar 24, 1995: ENGINE ASSY. OBSTRUCTED. #1 ENGINE T.O.T. INCREASED TO 800 DEGREES CELCIUS IN CRUISE. FOUND AN APPROXIMATELY 4 X 4 INCH PIECE OF CHAFE TAPE OBSTRUCTING THE INLET. REPAIRED ENGINE AND RE
- [SDR HEEA954625](https://openairdocs.org/sdr/HEEA954625), Mar 23, 1995: WINDSHIELD. MIS MFG. DURING INITIAL FIT OF WINDSHIELD ON AIRFRAME, FOUND WINDOW TO HAVE IMPROPER FORM AND FIBERGLASS EDGING TOO THICK TO ALLOW PROPER FIT ON AIRFRAME.
- [SDR HEEA954624](https://openairdocs.org/sdr/HEEA954624), Mar 23, 1995: WINDSHIELD. MIS MFG. WINDSHIELD CRACKED DURING INSTALLATION AT UPPER INBOARD CORNER. FOUND WINDOW TO HAVE IMPROPER FORM AND FIBERGLASS EDGING TOO THICK TO ALLOW PROPER FIT ON AIRFRA

All 51: https://openairdocs.org/aircraft/N86CH/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (86, 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 86: https://openairdocs.org/aircraft/N86CH/stcs.md

## Earlier aircraft with N86CH

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N86CH before.

- [Cancelled 2008-02-07](https://openairdocs.org/deregistered/N86CH-2008-02-07): Bell 206B, S/N 3590. Exported to Germany. Owner: [Xxx, OK](https://openairdocs.org/faa-place/OK/Xxx)
- [Cancelled 1988-05-19](https://openairdocs.org/deregistered/N86CH-1988-05-19): Bell 206L-3, S/N 51149. N-number assigned, not yet registered

## Related

- Other Socata TBM 700 aircraft: https://openairdocs.org/model/socata-tbm-700/aircraft.md
- The Pratt & Whitney Canada PT6A-66 series engine: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-66-series.md

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