# Morane-Saulnier MS760B - Type: Aircraft model (FAA registry) - Registry code: 5910106 - Manufacturer (registry): MORANE-SAULNIER - Model: MS760B - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-jet - Seats: 4 - Weight class: Up to 12,499 lb - Cruise speed: 258 mph - Certification: Type certificated - Data sheet: [TCDS 7A3](https://openairdocs.org/tcds/7A3) (OpenAirDocs) - Holder: Jet Set Aviation Holdings SAS - Registered aircraft: 2 - Page: https://openairdocs.org/model/morane-saulnier-ms760b Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [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 ## Registered aircraft (2) - [N207MJ](https://openairdocs.org/aircraft/N207MJ): [Tej Jet Inc](https://openairdocs.org/faa-owner/TEJ%20JET%20INC), [Greenwich, CT](https://openairdocs.org/faa-place/CT/Greenwich), built 1966, S/N 02 - [N999PJ](https://openairdocs.org/aircraft/N999PJ): [Tej Jet Of Del LLC](https://openairdocs.org/faa-owner/TEJ%20JET%20OF%20DEL%20LLC), [Greenwich, CT](https://openairdocs.org/faa-place/CT/Greenwich), S/N 89 ## NTSB investigations (3) 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 CHI08CA249](https://openairdocs.org/ntsb/CHI08CA249), Aug 9, 2008: Morane-Saulnier MS-760/B (N69X), St Paul, MN, substantial damage. Probable cause: Restriction of the elevator controls due to the presence of the seat belt buckled around the co-pilot control stick. An additional cause was the failure of the pilot to verify that the flight… - [NTSB LAX97FA059](https://openairdocs.org/ntsb/LAX97FA059), Nov 30, 1996: Morane-Saulnier MS760 II (N2TE), Irvine, CA, destroyed, 3 fatal. Probable cause: The pilot's failure to maintain an adequate airspeed margin while maneuvering in a steep banked turn to the landing runway, which resulted in an inadvertent stall/spin. Factors in the accident were:… - [NTSB MIA72DKJ06](https://openairdocs.org/ntsb/MIA72DKJ06), Jul 16, 1971: M-Saulnier MS-760 (N760X), Huntsville, AL, incident, minor damage ## FAA accident and incident reports (11) 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. - [Accident 20080809846349A](https://openairdocs.org/incident/20080809846349A), Aug 9, 2008: Mnslnr MS760B (N69X), St Paul, MN, Substantial damage. (-23) The co-pilot's seat belt had been previously wrapped around the co-pilot's control stick, a situation that went undetected by the pilot on this flight.… - [Incident 20061218027609I](https://openairdocs.org/incident/20061218027609I), Dec 18, 2006: Mnslnr MS760B (N760X), Spokane, WA, Minor damage. (-23) N760X gear would not extend. The pilot tried the emergency extension system which also failed. The pilot elected to land gear up, and gently settled the… - [Accident 19961130036869A](https://openairdocs.org/incident/19961130036869A), Nov 30, 1996: Mnslnr MS760 (N2TE), Santa Ana, CA, Destroyed, 3 fatal. Departed boarding ladder attached. Overshot runway alignment. Wake upset. Rolled inverted. Hit bldg. Spacing inadeq - [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 19960201002319I](https://openairdocs.org/incident/19960201002319I), Feb 1, 1996: Mnslnr MS760B (N760R), Alamogordo, NM. Narrative: the nose tire of the aircraft involved failed on takeoff just prior to V-1. The takeoff was aborted and the aircraft came to a stop approximately… - [Incident 19910202008329I](https://openairdocs.org/incident/19910202008329I), Feb 2, 1991: Mnslnr MS760A (N760PJ), Dallas, TX, Minor damage. As pilot recovered from stall maneuver the canopy blew off. Diverted and landed safely. - [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. - [Incident 19870302024329I](https://openairdocs.org/incident/19870302024329I), Mar 2, 1987: Mnslnr MS760B (N69X), Fairmont, MN, Minor damage. The canopy separated from the aircraft after level off. Canopy release levers had not been reset or safetied. - [Incident 19850612044409I](https://openairdocs.org/incident/19850612044409I), Jun 12, 1985: Mnslnr MS760B (N5879), Kansas City, MO, Minor damage. Nose gear collapsed on landing rollout after unsafe light. Probable improper over center rigging. - [Incident 19850112007429I](https://openairdocs.org/incident/19850112007429I), Jan 12, 1985: Mnslnr MS760B (N5878), Bethany, OK, Minor damage. Canopy separated from aircraft striking occupants. Canopy came to rest in rear seat. Safe landing. - [Incident 19840921063719I](https://openairdocs.org/incident/19840921063719I), Sep 21, 1984: Mnslnr MS760B (N760T), Tucson, AZ, Minor damage. Hard landing caused collapse of nose gear and damage to left main. ## STCs that may be installed (OpenAirDocs) (31) Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [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 --- 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.