# N943CA: 2021 Compagnie Daher TBM 700

- Status: Valid registration
- Airframe: [Compagnie Daher TBM 700](https://openairdocs.org/model/compagnie-daher-tbm-700) (registry code 8682010, 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: 1401
- Year built: 2021
- Type: Fixed wing single engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: November 19, 2021
- Certificate issued: June 17, 2024
- Expires: June 30, 2031
- Mode S code: AD1880
- Registered owner: [Mccloud & Company LLC](https://openairdocs.org/faa-owner/MCCLOUD%20%26%20COMPANY%20LLC)
- Location: [Oakton, VA](https://openairdocs.org/faa-place/VA/Oakton)
- Owner type: LLC
- Owner's area on the map: 38.8938° N, 77.3302° W: Placed by OpenAirDocs at the center of ZIP code 22124, 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=943CA
- Page: https://openairdocs.org/aircraft/N943CA

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 (Compagnie Daher 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/N943CA/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 N943CA.

## FAA accident and incident reports

None matched to N943CA.

## 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 N943CA not matched to an aircraft (68, newest 50)

They name N943CA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR COMA0160959](https://openairdocs.org/sdr/COMA0160959), Dec 12, 2001: SKIN. DENTED. FUSELAGE SKIN FWD OF PAX DOOR FS 310.00 DENTED APPROXIMATELY .020 DEEP. FABBED REPAIR PARTS AND INSTALLED IAW CANADAIR REO 601R-53-21-180.
- [SDR COMA0160873](https://openairdocs.org/sdr/COMA0160873), Nov 4, 2001: WEB. CRACKED. ENGINE SUPPORT BEAM CRACKED AT THE LEFT AND RIGHT LOWER WEB ACCESS PANEL.CUT OUT DAMAGE AND INSTALLED REPAIR TO LEFT AND RIGHT LOWER WEB I/A/W REO 601R-53-61-36
- [SDR COMA0160872](https://openairdocs.org/sdr/COMA0160872), Nov 4, 2001: WEB. CRACKED. ENGINE SUPPORT BEAM CRACKED ON UPPER WEB.CUT OUT DAMAGE SECTION AND INSTALLED TEMPORARY REPAIR TO UPPER AND LOWER WEB. I/A/W REO 601R-53-61-345.
- [SDR COMA0160870](https://openairdocs.org/sdr/COMA0160870), Nov 4, 2001: PLANK. FAULTY. FLAW INDICATION WERE NOTED BY EDDY CURRENT METHOD AT LOWER WING SURFACE ACCESS OPENINGS AT 640 EB W/S 116.366, 640 CB W.S. 76.161 AND 640 EB W.S. 116.366, 540 A
- [SDR COMA0160871](https://openairdocs.org/sdr/COMA0160871), Oct 29, 2001: SKIN. CRACKED. OVERWING SKIN CRACKED ON FUSELAGE AT STA F.S.520.00 TO F.S. 528.7.REPAIRED BY REMOVING DAMAGE AND INSTALLING DOUBLERS I/A/W REO 601R-53-51-069.
- [SDR COMA0160856](https://openairdocs.org/sdr/COMA0160856), Oct 25, 2001: LAMP. INOPERATIVE. FLIGHT #5800 - EMERGENCY FLOOR PATH LIGHTING, ROWS 9 AFT, ARE INOPERABLE.REPLACED DAMAGED FLOOR PATH LIGHTING STIRP.
- [SDR COMA0160645](https://openairdocs.org/sdr/COMA0160645), Aug 28, 2001: LIGHT. FLIGHT #5780. DURING PRE-FLIGHT INSPECTION DISCOVERED THE FLOOR EMERGENCY LIGHTING BETWEEN ROWS 9 AND 13 TO BE INOPERATIVE.RE-CONNECTED AFFECTED FLOOR EMERGENCY
- [SDR COMA0160652](https://openairdocs.org/sdr/COMA0160652), Aug 26, 2001: RADOME. BURNED. FLIGHT #5628. DURING CRUSIE FLIGHT AIRCRAFT ENCOUNTERED A LIGHTNING STRIKE, CREW REPORTED SMOKE/BURNING SMELL IN CABIN AND GALLEY AREA. AIRCRAFT CONTINUED FLIGH
- [SDR COMA0160533](https://openairdocs.org/sdr/COMA0160533), Jul 28, 2001: SWITCH. MALFUNCTIONED. WING OVERHEAT MESSAGE.REPLACED THE BACKUP OVERHEAT SWITCH.
- [SDR COMA0160501](https://openairdocs.org/sdr/COMA0160501), Jul 26, 2001: CONTROL UNIT. FAILED. ON FINAL APPROACH INTO CVG THE PITCH TRIM CAUTION MESSAGE ACTIVATED.REPLACED THE MOTOR CONTROL UNIT.
- [SDR COMA0160500](https://openairdocs.org/sdr/COMA0160500), Jul 26, 2001: CONTROL UNIT. FAILED. ON FINAL APPROACH INTO CVG THE PITCH TRIM CAUTION MESSAGE ACTIVATED.REPLACED THE HORIZONTAL STABILIZER TRIM CONTROL UNIT.
- [SDR COMA0160354](https://openairdocs.org/sdr/COMA0160354), Mar 28, 2001: BEAM. CRACKED. VERTICAL BEAM AT RBL 27 AND LBL 27 FS 409.0 + 128 INBOARD LOWER FASTENERS CRACKED. REPAIRED BOTH BEAMS IAW WVAC EO 601R-53-2336C.
- [SDR COMA0160352](https://openairdocs.org/sdr/COMA0160352), Mar 26, 2001: POST. CRACKED. INBOARD AND OUTBOARD POSTS AT RBL 9 AND LBL 9 AT FS 559 ARE CRACKED AT APPROXIMATELY WL 45. CAUSE UNKNOWN. DAMAGED AREAS REMOVED AND REPAIRED IAW WVAC EO 601R-5
- [SDR COMA0160341](https://openairdocs.org/sdr/COMA0160341), Mar 26, 2001: ANGLE. CRACKED. THE ANGLES AT RBL 27 AND LBL 27 AND INTERCOSTALS AT BL36 (LT AND RT) AT FS 484 ARE CRACKED. REPAIRED LEFT AND RIGHT ANGLES AT RBL 27 AND LBL 27 INTERCOSTALS AT 
- [SDR COMA0160340](https://openairdocs.org/sdr/COMA0160340), Mar 26, 2001: ANGLE. CRACKED. VERTICAL J-ANGLE CLIP INSIDE CBP1 AT LBL 9 IS CRACKED. REPAIRED IAW WVAC EO 601R-53-2337A.
- [SDR COMA0160339](https://openairdocs.org/sdr/COMA0160339), Mar 26, 2001: ANGLE. CRACKED. THE ANGLES AT RBL 27 AND LBL 27 AND INTERCOSTALS AT BL 36 (LT AND RT) AT FS 484 ARE CRACKED. REPAIRED LEFT AND RIGHT ANGLES AT RBL 27 AND LBL 27 INTERCOSTAL AT 
- [SDR COMA0160136](https://openairdocs.org/sdr/COMA0160136), Jan 19, 2001: UNKNOWN. ODOR. STRONG ODOR OF FUEL IN CABIN WITH APU OPERATING. COULD NOT DUPLCIATE. INSPECTED APU. NO LEAKS OR DEFECTS NOTED.
- [SDR COMA0160071](https://openairdocs.org/sdr/COMA0160071), Jan 3, 2001: WINDSHIELD. FAILED. PILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD.
- [SDR COMA0160023](https://openairdocs.org/sdr/COMA0160023), Dec 31, 2000: SKIN. DENTED. TEMPORARY REPAIR ON FUSELAGE AFT AND BELOW CARGO DOOR.REPAIRED FOUR DENTS BETWEEN FS625 - 654.4 LT SIDE I/A/W W.V.A.C. E.O. 601R-53-2058.
- [SDR COMA0160011](https://openairdocs.org/sdr/COMA0160011), Dec 24, 2000: COMPUTER. MALFUNCTIONED. STALL FAIL CAUTION MESSAGE DURING T/O. RESET THE STALL COMPUTER.
- [SDR COMA0060947](https://openairdocs.org/sdr/COMA0060947), Nov 20, 2000: COMPUTER. MALFUNCTIONED. STALL FAIL MESSAGE DURING T/O. RESET STALL COMPUTER.
- [SDR COMA0060734](https://openairdocs.org/sdr/COMA0060734), Sep 9, 2000: LATCH. OUT OF ADJ. DOOR HANDLE CAUTION MESSAGE. ADJUSTED DOOR LATCH MECHANISM.
- [SDR COMA0060641](https://openairdocs.org/sdr/COMA0060641), Aug 9, 2000: STRAP. DAMAGED. CAPPING STRAP ON RBL 9 AT FS 409 AND 16 WAS CUT TO TRANSVERSE BEAM NOT TO S/B 601R-53-037 SPECIFICATIONS. STRAP SHOULD NOT HAVE BEEN CUT. REPAIRED CAPPING STRIP
- [SDR COMA0060640](https://openairdocs.org/sdr/COMA0060640), Aug 9, 2000: SPLICE. MISDRILLED. WHILE PERFORMING S/B 601R-53-037 P/N 601R31030-77 FS 409 SPLICE PLATE WAS DRILLED UPSIDE DOWN NOT TO WVAC EO 601R-53-1563 SPECIFICATIONS LBL 9. DRILLED AND INST
- [SDR COMA0060635](https://openairdocs.org/sdr/COMA0060635), Aug 7, 2000: STRAP. MISMANUFACTURED. WHILE PERFORMING TITANIUM FLOORBEAM S/B 601R-53-037 REV A CAPPING STRAP P/N 601R31030-77/S WAS MANUFACTURED INCORRECTLY AT RBL 9. REPAIRED 601R3103-77 CAPPING S
- [SDR COMA0060634](https://openairdocs.org/sdr/COMA0060634), Aug 7, 2000: STRAP. MISMANUFACTURED. WHILE PERFORMING TITANIUM FLOORBEAM S/B 601R-53-037 REV A FOUND CAPPING STRAP LBL 9 P/N 601R31030-77S IS MANUFACTURED INCORRECTLY. REPAIRED 601R31030-77 CAPPING
- [SDR COMA0060633](https://openairdocs.org/sdr/COMA0060633), Aug 7, 2000: ANGLE. MISINSTALLED. WHILE PERFORMING TITANIUM FLOORBEAM S/B 601R-53-037 REV A FOUND LBL 9 ATTACH BRACKETS FOR TRANSVERSE BEAMS REQUIRE SHIMMING TO MAINTAIN SUFFICIENT EDGE DISTANCE
- [SDR COMA0060632](https://openairdocs.org/sdr/COMA0060632), Aug 7, 2000: ANGLE. MISREPAIRED. WHILE PERFORMING TITANIUM FLOORBEAM S/B 601R-53-037 REV A FOUND RBL 9 TO HAVE SHORT EO ON ANGLE BRACKETS AT THREE POSITIONS FS 280, 349 AND 364 TO A/C CONFIGURA
- [SDR COMA0060636](https://openairdocs.org/sdr/COMA0060636), Aug 6, 2000: THRESHOLD. CORRODED. PASSENGER DOOR SUPPORT THRESHOLD P/N 601R31527-221 AT FS 310.0 TO FS 349.0 LHS FS CORRODED. PERFORMED A MAJOR REPAIR BY REPLACING CORRODED THRESHOLD P/N 601R315
- [SDR COMA0060455](https://openairdocs.org/sdr/COMA0060455), May 25, 2000: LIGHT. INOPERATIVE. AFT SECTION OF EMERGENCY FLOOR LIGHTS IS INOPERABLE. SECURED LOOSE CONNECTION IN LIGHT STRIP. SYSTEM OPERATIONAL.
- [SDR COMA0060355](https://openairdocs.org/sdr/COMA0060355), Apr 18, 2000: WINDSHIELD. FAILED. CO-PILOTS SIDE WINDOW SHATTERED. REPLACED WINDOW.
- [SDR COMA9960632](https://openairdocs.org/sdr/COMA9960632), Oct 16, 1999: SKIIN. CRACKED. 2 CRACKS DETECTED IN THE LOWER HORIZONTAL SURFACE LT LOWER WING ACCESS HOLE AT 540AB. BLENDED OUT DAMAGED AREAS, ROTO-PEENED, ALODINED IAW BOMBARDIER REO 601R-5
- [SDR COMA9960631](https://openairdocs.org/sdr/COMA9960631), Oct 16, 1999: SKIN. CRACKED. CRACK DETECTED IN THE LOWER HORIZONTAL SURFACE OF LT LOWER WING ACCESS HOLE AT 540EB. BLENDED OUT DAMAGED AREA, ROTO-PEENED AND ALODINED IAW BOMBARDIER REO 601R
- [SDR COMA9960630](https://openairdocs.org/sdr/COMA9960630), Oct 16, 1999: SKIN. CRACKED. CRACK DETECTED IN THE LOWER HORIZONTAL SURFACE OF RT LOWER WING ACCESS HOLE AT 640EB. BLENDED OUT DAMAGE AREA, ROTO-PEENED ALODINED IAW BOMBARDIER REO 601R-57-2
- [SDR COMA9960526](https://openairdocs.org/sdr/COMA9960526), Sep 14, 1999: BULB. FAILED. ELECTRICAL ODOR IN THE AREA OF CABIN SEATING ROWS 2 AND 3 DURING FLIGHT. AIRCRAFT RETURNED TO CVG. REPLACED CEILING LIGHT BULBS ABOVE SEATS 2 AND 3.
- [SDR COMA9960507](https://openairdocs.org/sdr/COMA9960507), Sep 12, 1999: ANGLE. CHAFED. PANEL 411AL CHAFED BY FASTENER MID FRAME OUTBOARD EDGE LEFT HAND ENGINE PYLON. PERFORMED MAJOR REPAIR SMOOTHED CHAFE ON (P/N 601-37004-133) AND FABED NEW SUPPOR
- [SDR COMA9960506](https://openairdocs.org/sdr/COMA9960506), Sep 12, 1999: FRAME. CRACKED. FRAME AT FS 718.00 RHS HAS TWO CRACKS. ONE CRACK IS IN THE RADIUS EXTENDING APPROXIMATELY 2 ABOVE STRINGER II IN THE FLANGE ATTACHING TO THE SKIN AND THE OTHER 
- [SDR COMA9960502](https://openairdocs.org/sdr/COMA9960502), Sep 12, 1999: FRAME. CRACKED. FRAME AT FS 718.00 LHS HAS TWO CRACKS. ONE CRACK IS IN THE RADIUS EXTENDING APPROXIMATELY 4 ABOVE STRINGER II IN THE FLANGE ATTACHING TO THE SKIN AND THE OTHER 
- [SDR COMA9960422](https://openairdocs.org/sdr/COMA9960422), Aug 7, 1999: DEPLOY SYS. MALFUNCTIONED. ADG DEPLOYED DURING FLIGHT. DEFERRED THE ADG AUTO DEPLOY SYSTEM.
- [SDR COMA9960360](https://openairdocs.org/sdr/COMA9960360), Jul 11, 1999: WIRE HARNESS. LOOSE. AFTER TAKEOFF, RIGHT ENGINE ROLLED BACK AND THEN SURGED 10 PERCENT. SECURED LOOSE WIRING HARNESS AT FUEL CONTROL UNIT.
- [SDR COMA9960289](https://openairdocs.org/sdr/COMA9960289), Jun 21, 1999: COWL. CRACKED. DURING MAINTENANCE SEVERAL CRACKS WERE FOUND ON INLET COWL AFT BULKHEAD OF RIGHT ENGINE. ENGINE INLET COWL WAS REPLACED.
- [SDR COMA9960056](https://openairdocs.org/sdr/COMA9960056), Feb 3, 1999: STRIKER SEAL. CRACKED. PASSENGER DOOR STRIKER SEAL DAMAGED BY BOTTOM AFT LATCH PIN. REPAIRED DAMAGE TO PAX DOOR STRIKER SEAL PER REO 601R-52-11-008.
- [SDR COMA9960034](https://openairdocs.org/sdr/COMA9960034), Jan 15, 1999: FUEL CONTROL. MALFUNCTION. NR 1 ENGINE LAGS NR 2 DURING TAKEOFF. REPLACED THE LEFT ENGINE FUEL CONTROL.
- [SDR COMA9860021](https://openairdocs.org/sdr/COMA9860021), Jan 22, 1998: TCAS. MALFUNCTIONED. AIRCRAFT SUSTAINED NEGATIVE 'GS' FOR 5 SECONDS DUE TO TCAS RA COMMAND, (FALSE WARNING). COMPLIED WITH TURBULANCE AND HARD LANDING INSPECTIONS. NO DAGMAGE NOTES.
- [SDR COMA9860007](https://openairdocs.org/sdr/COMA9860007), Jan 11, 1998: TRANSFORMER. OUT OF ADJUST. UPON GEAR EXTENSION, RECEIVED STEERING CAUTION MESSAGE. ADJUSTED THE ROTARY VARIABLE DIFFERENTIAL TRANSFORMER.
- [SDR COMA9760251](https://openairdocs.org/sdr/COMA9760251), Dec 17, 1997: STEERING. MALFUNCTIONED. STEERING INOP MESSAGE WHEN LANDING GEAR LOWERED. COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK OF NWS SYSTEM WAS NORMAL.
- [SDR COMA9760219](https://openairdocs.org/sdr/COMA9760219), Nov 6, 1997: FUSE. BLOWN. SERVICE DOOR EMERGENCY LIGHT IS INOP. REPLACED POWER SUPPLY FUSE F2.
- [SDR COMA9760216](https://openairdocs.org/sdr/COMA9760216), Nov 5, 1997: LAMP. FAILED. LEFT HAND OVERWING EMERGENCY LIGHT IS INOP. REPLACED BULB.
- [SDR COMA976020](https://openairdocs.org/sdr/COMA976020), Oct 22, 1997: FLAP LEVER. MALFUNCTION. FLAPS FAILED AT 20 DEGREES AFTER TAKEOFF. REPLACED THE FLAP CONTROL HANDLE.
- [SDR COMA9760177](https://openairdocs.org/sdr/COMA9760177), Sep 19, 1997: RETRACT MECH. MALFUNCTIONED. FLAPS FAILED AT 20 DEGREES. COULD NOT DUPLICATE DISCREPANCY. OPERATONAL CHECK OF FLAP SYSTEM NORMAL, NO FAULTS FOUND.

All 68: https://openairdocs.org/aircraft/N943CA/unmatched-reports.md

## 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 (Compagnie Daher 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/N943CA/stcs.md

## Related

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

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