# N207MJ: 1966 Morane-Saulnier MS760B

- Status: Valid registration
- Airframe: [Morane-Saulnier MS760B](https://openairdocs.org/model/morane-saulnier-ms760b) (registry code 5910106, 4 seats)
- Engine: [Turbomeca MARBORE IIC](https://openairdocs.org/engine/turbomeca-marbore-iic) (registry code 60004)
- Data sheets: [TCDS 7A3](https://openairdocs.org/tcds/7A3) (Jet Set Aviation Holdings SAS), [TCDS E-302](https://openairdocs.org/tcds/E-302) (Turbomeca S.A.) (OpenAirDocs)
- Serial number: 02
- Year built: 1966
- Type: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, utility
- Airworthiness date: December 11, 1987
- Certificate issued: May 6, 1996
- Expires: April 30, 2027
- Mode S code: A1AD20
- Registered owner: [Tej Jet Inc](https://openairdocs.org/faa-owner/TEJ%20JET%20INC)
- Location: [Greenwich, CT](https://openairdocs.org/faa-place/CT/Greenwich)
- Owner type: Corporation
- Owner's area on the map: 41.0376° N, 73.6243° W: Placed by OpenAirDocs at the center of ZIP code 06830, 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=207MJ
- Page: https://openairdocs.org/aircraft/N207MJ

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): 4 in force

### Matched by airframe (Morane-Saulnier MS760B)

- [AD 2007-05-05](https://openairdocs.org/ad/2007-05-05): Limitations Section of the Airplane Flight Manual (AFM) · SOCATA - Groupe Aerospatiale M.S. 760 (Paris I), M.S. 760B (Paris II) and M.S. 760.A (Paris IA). Effective Apr 9, 2007
- [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 76-06-07](https://openairdocs.org/ad/76-06-07): Inflight Fire · SOCATA - Groupe Aerospatiale M.S. 760B (Paris II). Effective Mar 25, 1976
- [AD 66-08-05](https://openairdocs.org/ad/66-08-05): Rudder Control System Rod · SOCATA - Groupe Aerospatiale M.S. 760 (Paris I), M.S. 760.A (Paris IA) and M.S. 760B (Paris II). Effective Apr 16, 1966

### Matched by engine (Turbomeca MARBORE IIC)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N207MJ.

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19960810026639I](https://openairdocs.org/incident/19960810026639I), Aug 10, 1996: Mnslnr MS760B (N207MJ), Bridgeport, CT, Minor damage. Narrative: on 08/10/96 an instructor providing dual instruction to his student for the purpose of obtaining a type rating in the morane saulnier (MS76)…
- [Incident 19901226066009I](https://openairdocs.org/incident/19901226066009I), Dec 26, 1990: Mnslnr MS760B (N207MJ), Halifax, CN. Canadian officials reported this aricraft performing aerobatics in voilation of regulations.

## 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.

## STCs that may be installed (OpenAirDocs) (31)

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 (Morane-Saulnier MS760B)

- [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 SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA02254AK](https://openairdocs.org/stc/SA02254AK): Installation of "Single Screen", "2 or 3 Screen", "Dual Screen", or "4 or 6 screen". Genesys Aerosystems Inc
- [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 SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International 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 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 SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA02428SE](https://openairdocs.org/stc/SA02428SE): Installation of an Air Stream Switch for an electric time recording device on non-pressurized aircraft. Henry F Rogers/David E Polley
- [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 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 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 SA01933LA-D PAGE 1](https://openairdocs.org/stc/SA01933LA-D%20PAGE%201): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA02717NY PAGE 2](https://openairdocs.org/stc/SA02717NY%20PAGE%202): Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module. VoiceFlight Systems LLC
- [STC SA01692SE](https://openairdocs.org/stc/SA01692SE): Installation of a Garmin GMX 200 Multi-Function Display. Garmin International Inc
- [STC SA01487SE-D](https://openairdocs.org/stc/SA01487SE-D): Installation of a GDL 69 or GDL 69A XM Satellite Receiver. Garmin International Inc
- [STC SA00243BO](https://openairdocs.org/stc/SA00243BO): Installation of Centurion Consulting, Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100), or without roll steering (p/n 0025-5200). Icarus Avionics, LLC
- [STC SA02018SE-D](https://openairdocs.org/stc/SA02018SE-D): Provisions installation of Garmin GPS/XM Antennas in accordance with FAA Approved Model List (AML) SA02018SE-D, dated January 4, 2011, or later FAA approved revision, and FAA Approved GPS/XM Antenna STC Master Drawing List, Document No.: 005-00638-01, Revision 1 , approved on January 4, 2011, or later FAA approved revision. Garmin International Inc
- [STC SA2311SW](https://openairdocs.org/stc/SA2311SW): Install Bendix FCS-810 Automatic Flight Control System. Airline Fueling Inc
- [STC SA01473SE](https://openairdocs.org/stc/SA01473SE): Installation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote Transponde. Garmin AT Inc
- [STC SA01695SE](https://openairdocs.org/stc/SA01695SE): Installation of an antenna. Garmin AT Inc
- [STC SA01487SE](https://openairdocs.org/stc/SA01487SE): Installation of a GDL 69 or GDL 69A XM Satellite Receiver in accordance with Garmin Supplemental Type Certificate Master Data List, P/N 005-C0217-00, Revision A, dated December 20, 2004, or later FAA approved revision. Garmin AT Inc
- [STC SA02154AK](https://openairdocs.org/stc/SA02154AK): Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display, P/N 430-0270-500. Garmin AT Inc
- [STC SA02217AK](https://openairdocs.org/stc/SA02217AK): Installation of Garmin AT Model GDL90 UAT Data Link System, in accordance with Garmin AT, Inc., GDL 90 UAT Master Data List, P/N 560-0278-01, Revision A, dated November 12, 2004, or later FAA approved revision. Garmin AT Inc
- [STC SA2537WE](https://openairdocs.org/stc/SA2537WE): Installation of modified fuel system. Aviation Research Corporation
- [STC SA2554WE](https://openairdocs.org/stc/SA2554WE): Installation of antiskid power brake system, new main landing gear legs and Goodyear wheels and brakes. Aviation Research Corporation
- [STC SA2751WE](https://openairdocs.org/stc/SA2751WE): Installation of rear seat assembly, P/N N76091. Aviation Research Corporation
- [STC SA8907SW-D](https://openairdocs.org/stc/SA8907SW-D): Installation of S-TEC System 55 two axis automatic flight guidance system, Model ST-564, with optional automatic electric trim system. S-TEC Corporation
- [STC SA02153LA-D](https://openairdocs.org/stc/SA02153LA-D) (historical): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc
- [STC SA02153LA](https://openairdocs.org/stc/SA02153LA) (historical): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin AT Inc
- [STC SA01933LA](https://openairdocs.org/stc/SA01933LA) (historical): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin AT Inc

## Related

- Other Morane-Saulnier MS760B aircraft: https://openairdocs.org/model/morane-saulnier-ms760b/aircraft.md
- The Turbomeca MARBORE IIC engine: https://openairdocs.org/engine/turbomeca-marbore-iic.md

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.