# N65ML: 1981 Rockwell International NA-265-65 - Status: Valid registration - Airframe: [Rockwell International NA-265-65](https://openairdocs.org/model/rockwell-international-na-265-65) (registry code 7630107, 12 seats) - Engine: [Garrett TFE731 series](https://openairdocs.org/engine/garrett-tfe731-series) (registry code 29001) - Data sheets: [TCDS A2WE](https://openairdocs.org/tcds/A2WE) (Sabreliner Aviation LLC), [TCDS E6WE](https://openairdocs.org/tcds/E6WE) (Honeywell Aerospace US LLC) (OpenAirDocs) - Serial number: 465-69 - Year built: 1981 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Experimental, research and development - Airworthiness date: August 18, 2026 - Certificate issued: February 21, 2023 - Expires: February 28, 2030 - Mode S code: A88B7F - Registered owner: [Bae Systems Technology Solutions & Services Inc](https://openairdocs.org/faa-owner/BAE%20SYSTEMS%20TECHNOLOGY%20SOLUTIONS%20%26%20SERVICES%20INC) - Location: [Mojave, CA](https://openairdocs.org/faa-place/CA/Mojave) - Owner type: Corporation - Owner's area on the map: 35.0658° N, 118.2218° W: Placed by OpenAirDocs at the center of ZIP code 93501, within about 8 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=65ML - Page: https://openairdocs.org/aircraft/N65ML 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. The registry lists only the engine series, so ADs for every Garrett TFE731 model are included. ## ADs that may apply (OpenAirDocs): 49 in force ### Matched by airframe (Rockwell International NA-265-65) - [AD 2005-25-18](https://openairdocs.org/ad/2005-25-18): Wing center section · Sabreliner NA-265, NA-265-20, NA-265-30 and 5 more. Effective Jan 18, 2006 - [AD 2001-22-14](https://openairdocs.org/ad/2001-22-14): Fire Extinguishing System Bottle Cartridges · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 105 more. Effective Dec 10, 2001 - [AD 97-05-03 R1](https://openairdocs.org/ad/97-05-03-R1): Global Positioning Systems · BAE Systems Avro 146-RJ100A, BAe 146-200A, Jetstream Model 4101 and 27 more. Effective Apr 20, 1999 - [AD 97-04-15](https://openairdocs.org/ad/97-04-15): Fire Extinguisher Bottle Cartridges · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 24 more. Effective Mar 7, 1997 - [AD 96-25-12](https://openairdocs.org/ad/96-25-12): Auxiliary Power Units · BAE Systems HS 748 Series 2A, HS 748 Series 2B, 707-100 Long Body and 74 more. Effective Jan 13, 1997 - [AD 95-26-15 R1](https://openairdocs.org/ad/95-26-15-R1): Traffic Alert and Collision Avoidance Systems · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 159 more. Effective Dec 26, 1996 - [AD 94-01-05](https://openairdocs.org/ad/94-01-05): Traffic Alert and Collision Avoidance System II Processors · Airbus A340-211, A340-212, A340-213 and 85 more. Effective Feb 4, 1994 - [AD 92-27-16](https://openairdocs.org/ad/92-27-16): Hydraulic Pump · Sabreliner NA-265, NA-265-20, NA-265-30 and 5 more. Effective Jan 13, 1993 - [AD 82-26-02](https://openairdocs.org/ad/82-26-02): Vertical Floor Panel Inspection · Sabreliner NA-265-60 and NA-265-65. Effective Apr 13, 1983 - [AD 82-27-10](https://openairdocs.org/ad/82-27-10): Horizontal Stabilizer Trim Actuator · Sabreliner NA-265-65. Effective Jan 19, 1983 - [AD 82-10-02 R1](https://openairdocs.org/ad/82-10-02-R1): Flap Screwjack Inspection · Sabreliner NA-265-60 and NA-265-65 with STC SA687NW. Effective Sep 13, 1982 - [AD 80-05-02](https://openairdocs.org/ad/80-05-02): Safety Belt Assemblies · Gulfstream Aerospace G-1159, G-1159A, G-1159B and 17 more. Effective Feb 27, 1980 - [AD 75-04-05](https://openairdocs.org/ad/75-04-05): Engine Fuel Pressure Switches · Sabreliner NA-265, NA-265-20, NA-265-30 and 5 more. Effective Feb 18, 1975 - [AD 70-24-03](https://openairdocs.org/ad/70-24-03): Engine Fire Control Handle · Sabreliner NA-265, NA-265-20, NA-265-30 and 5 more. Effective Nov 28, 1970 - [AD 69-10-01](https://openairdocs.org/ad/69-10-01): Main Landing Gear Pistons · Sabreliner NA-265, NA-265-20, NA-265-30 and 5 more. Effective May 9, 1969 ### Matched by engine (Garrett TFE731 series) - [AD 2016-07-02](https://openairdocs.org/ad/2016-07-02): Failure of the interstage turbine transition duct · Honeywell International TFE731-4, TFE731-4R, TFE731-5AR and 2 more. Effective May 5, 2016 - [AD 2014-12-52](https://openairdocs.org/ad/2014-12-52): Engines · Honeywell International TFE731-20AR, TFE731-20BR, TFE731-20R and 11 more. Effective Jul 28, 2014 - [AD 2012-17-05](https://openairdocs.org/ad/2012-17-05): First stage low-pressure turbine (LPT1) rotor assembly · Honeywell International TFE731-4, TFE731-4R, TFE731-5 and 3 more. Effective Oct 2, 2012 - [AD 2010-06-11](https://openairdocs.org/ad/2010-06-11): Second stage low-pressure compressor rotor (LPCR) discs · Honeywell International TFE731-2, TFE731-2A, TFE731-2C and 16 more. Effective Apr 21, 2010 - [AD 2008-19-12](https://openairdocs.org/ad/2008-19-12): ITT duct · Honeywell International TFE731-4, TFE731-4R, TFE731-5 and 3 more. Effective Oct 27, 2008 - [AD 2008-02-19](https://openairdocs.org/ad/2008-02-19): High pressure (HP) turbine rotor assemblies · Honeywell International TFE731-20AR, TFE731-20BR, TFE731-20R and 15 more. Effective Mar 6, 2008 - [AD 2005-13-07](https://openairdocs.org/ad/2005-13-07): Turbine rotor discs. · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 12 more. Effective Jul 27, 2005 - [AD 2005-05-15](https://openairdocs.org/ad/2005-05-15): (LPT) stage 1 disks · Honeywell International TFE731-2, TFE731-2C, TFE731-3 and 5 more. Effective Apr 18, 2005 - [AD 2001-23-09](https://openairdocs.org/ad/2001-23-09): Fan Rotor Discs · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 14 more. Effective Dec 21, 2001 - [AD 2000-15-09](https://openairdocs.org/ad/2000-15-09): HPC Impeller · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 20 more. Effective Oct 10, 2000 - [AD 98-17-01 R1](https://openairdocs.org/ad/98-17-01-R1): Flex Fuel Tube · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 14 more. Effective Nov 29, 1999 - [AD 97-04-03](https://openairdocs.org/ad/97-04-03): First stage low pressure turbine (LPT) seal plates · Honeywell International TFE731-2A, TFE731-3C and TFE731-3CR. Effective May 5, 1997 - [AD 96-05-03](https://openairdocs.org/ad/96-05-03): Fan rotor disks · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 13 more. Effective Apr 2, 1996 - [AD 96-04-01](https://openairdocs.org/ad/96-04-01): Fan Rotor Assembly · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 12 more. Effective Mar 15, 1996 - [AD 95-07-02](https://openairdocs.org/ad/95-07-02): Low Pressure Turbine Disks · Honeywell International TFE731-3, TFE731-3A, TFE731-3AR and 3 more. Effective Jun 19, 1995 - [AD 94-23-05](https://openairdocs.org/ad/94-23-05): Honeywell International TFE731-3A and TFE731-3AR. Effective Dec 1, 1994 - [AD 94-07-03](https://openairdocs.org/ad/94-07-03): Turbine Nozzles · Honeywell International TFE731-2A, TFE731-3, TFE731-3A and 4 more. Effective Jun 6, 1994 - [AD 92-02-18](https://openairdocs.org/ad/92-02-18): Inflight Operation · Honeywell International TFE731-5BR. Effective Feb 10, 1993 - [AD 92-21-06](https://openairdocs.org/ad/92-21-06): Low Pressure Turbine (LPT) Rotor Disks · Honeywell International TFE731-2, TFE731-3, TFE731-3A and 2 more. Effective Nov 27, 1992 - [AD 90-24-06](https://openairdocs.org/ad/90-24-06): Thermocouple Lead Assemblies · Honeywell International TFE731-2, TFE731-2A, TFE731-3 and 8 more. Effective Nov 13, 1990 - [AD 90-03-04](https://openairdocs.org/ad/90-03-04): High Pressure Turbine Rotor Discs · Honeywell International TFE731-3, TFE731-3A, TFE731-3AR and 1 more. Effective Feb 22, 1990 - [AD 88-18-03](https://openairdocs.org/ad/88-18-03): High Pressure Turbine Rotor Disc · Honeywell International TFE731-3, TFE731-3A, TFE731-3AR and 1 more. Effective Jul 21, 1989 - [AD 86-03-01](https://openairdocs.org/ad/86-03-01): Turbine Interstage Transition Ducts · Honeywell International TFE731-2, TFE731-3, TFE731-3A and 4 more. Effective Feb 24, 1986 - [AD 82-23-03 R1](https://openairdocs.org/ad/82-23-03-R1): High Pressure Compressor Impellers · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 12 more. Effective Dec 9, 1983 - [AD 81-24-08](https://openairdocs.org/ad/81-24-08): Turbine Interstage Transition Ducts · Honeywell International TFE731-2, TFE731-3, TFE731-3A and 2 more. Effective Jan 6, 1982 - [AD 80-16-04](https://openairdocs.org/ad/80-16-04): Tie Rod · Honeywell International TFE731-2, TFE731-3 and TFE731-3R. Effective Aug 7, 1980 - [AD 78-22-10](https://openairdocs.org/ad/78-22-10): Low Pressure Rotor Thrust Ball Bearings · Honeywell International TFE731-2, TFE731-3 and TFE731-3R. Effective Nov 13, 1978 - [AD 75-07-10](https://openairdocs.org/ad/75-07-10): Transfer Gearbox Vertical Bevel Gear Bearing · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 12 more. Effective May 1, 1975 - [AD 74-23-05](https://openairdocs.org/ad/74-23-05): Fuel Pumps · Honeywell International TFE731-2. Effective Nov 14, 1974 - [AD 74-11-06](https://openairdocs.org/ad/74-11-06): Fuel Control Computer · Honeywell International TFE731-2. Effective Sep 23, 1974 - [AD 74-18-16](https://openairdocs.org/ad/74-18-16): Fuel Control Computer · Honeywell International TFE731-2. Effective Sep 6, 1974 - [AD 74-18-12](https://openairdocs.org/ad/74-18-12): Fuel Control Orifice Assembly · Honeywell International TFE731-2. Effective Sep 3, 1974 - [AD 74-13-09](https://openairdocs.org/ad/74-13-09): Fuel Pump Assemblies · Honeywell International TFE731-2. Effective Jul 31, 1974 - [AD 89-22-16](https://openairdocs.org/ad/89-22-16): Engine Acceleration or Deceleration · Honeywell International TFE731-2, TFE731-5, TFE731-5AR and 1 more ### Historical (superseded or no longer in force) - [AD 98-17-01](https://openairdocs.org/ad/98-17-01) (historical): Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 14 more. Effective Oct 13, 1998 - [AD 96-18-13](https://openairdocs.org/ad/96-18-13) (historical): Fan rotor disk · Honeywell International TFE731-2, TFE731-2A, TFE731-3 and 10 more. Effective Nov 12, 1996 - [AD 86-11-05](https://openairdocs.org/ad/86-11-05) (historical): Fan Rotor Discs · Honeywell International TFE731-2, TFE731-3 and TFE731-3R ## Information bulletins (advisory) (1 in force) - [SAIB NE-06-70](https://openairdocs.org/saib/NE-06-70): . Issued Sep 25, 2006 ## NTSB investigations None matched to N65ML. ## FAA accident and incident reports None matched to N65ML. ## Service difficulty reports (1) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UVVR2017031500044](https://openairdocs.org/sdr/UVVR2017031500044), Jan 12, 2017: SKIN. CORRODED. CORROSION WAS DISCOVERED AT LT UPPER WING PLANK BETWEEN WING STATION 146.4 TO 159.0. ## STCs that may be installed (OpenAirDocs) (107, 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 (Rockwell International NA-265-65) - [STC ST01305WI-D](https://openairdocs.org/stc/ST01305WI-D): Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision. Rockwell Collins Inc - [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc - [STC ST11216DS](https://openairdocs.org/stc/ST11216DS): Installation of automatic dependent surveillance-broadcast (ADS-B) out on Part 25 aircraft. BHE & Associates Ltd - [STC ST00106WI](https://openairdocs.org/stc/ST00106WI): Installation of a BFGoodrich model TCAS791 traffic alert and collision avoidance system (TCAS) I. Acron Aviation Inc - [STC ST03424CH](https://openairdocs.org/stc/ST03424CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC - [STC ST04183AT](https://openairdocs.org/stc/ST04183AT): Installation of the Honeywell CAS-100 Traffic Alert and Collision Avoidance System (TCAS), Version 7.1, and the ACSS NXT-800 Mode S Transponder with associated hardware. Woven Electronics LLC - [STC SA2698SO](https://openairdocs.org/stc/SA2698SO): Installation of provisions for a CAS-81 TCAS. Honeywell International Inc - [STC SA2734SO](https://openairdocs.org/stc/SA2734SO): Installation of a CAS-81 TCAS II. Honeywell International Inc - [STC ST00445WI-D](https://openairdocs.org/stc/ST00445WI-D): Installation of Honeywell Enhanced Ground Proximity Warning System. Limited to installation on NA-265-65, serial number 465-58 ONLY. Honeywell International Inc - [STC ST00715WI-D](https://openairdocs.org/stc/ST00715WI-D): Installation of provisions for AlliedSignal AIRSAT 1 IRIDIUM Aeronautical Satelite Communication System. Honeywell International Inc - [STC ST00093WI-D](https://openairdocs.org/stc/ST00093WI-D): ONE-ONLY STC, S/N 465-58: Installation of hte Bendix/King CAS 66A TCAS I System. Honeywell International Inc - [STC ST01343CH-D](https://openairdocs.org/stc/ST01343CH-D): Installation of AlliedSignal CAS-67A Traffic Alert and Collision Avoidance System (TCAS II) incorporating MOPS Change 7. Airplane must be previously equipped with STC ST333CH-D. Honeywell International Inc - [STC ST01344CH-D](https://openairdocs.org/stc/ST01344CH-D): Installation of dual Honeywell enhanced GNS-XLS Flight Management System. Aircraft must have STC ST335CH-D installed. Honeywell International Inc - [STC SA2073CE-D](https://openairdocs.org/stc/SA2073CE-D): Installation of Bendix/King EFS-10 electronic flight instrument sys (5 tube) dual KFC-400 automatic flight control sys, dual KAD-480 air data sys, dual KNS-660 flight mgmt sys, KHF-950HF Comm System and MLS-21 microwave landing system. Honeywell International Inc - [STC SA2311CE-D](https://openairdocs.org/stc/SA2311CE-D): ONE-ONLY STC, SN 465-058: Installation of Bendix/King CAS 80A Traffic Alert and Collision Avoidance System. Honeywell International Inc - [STC ST00791WI](https://openairdocs.org/stc/ST00791WI): Installation of AlliedSignal Avionics, Inc., KAD-481 adaptor module, part number 065-05041-28E1 (software part number 125-00981-00E1). Approved for installation on NA-265-65, serial number 465-58 ONLY. Honeywell International Inc - [STC ST333CH-D](https://openairdocs.org/stc/ST333CH-D): Installation of a Bendix/King CAS67A TCAS II System with dual MST-67 Mode S Transponders installed per Garrett Aviation Services. Honeywell International Inc - [STC ST335CH-D](https://openairdocs.org/stc/ST335CH-D): Installation of Dual AlliedSignal Aerospace, Global Wulfsberg GNS-XLS Flight Management. Honeywell International Inc - [STC ST01553WI](https://openairdocs.org/stc/ST01553WI): Installation of the Honeywell MKV EGPWS with RAAS and Monitor Functions or the Honeywell MKV-A EGPWS with RAAS and Monitor Functions. Honeywell International Inc - [STC ST02635LA](https://openairdocs.org/stc/ST02635LA): Modification to replace the existing Mode S Transponder system with the ACSS NXT-600 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC SA4991SW](https://openairdocs.org/stc/SA4991SW): Installation of freon air conditioning. Air Comm Corporation - [STC ST00790DE](https://openairdocs.org/stc/ST00790DE): Installation of BendixKing CAS 67B Traffic Alert and Collision Avoidance System (TCAS) II Version 7.1. Peregrine - [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC ST00347BO](https://openairdocs.org/stc/ST00347BO): Modification to upgrade a BendixKing CAS 67A TCAS II system to CAS 67B TCAS II Change 7.1. Pro Star Aviation, LLC - [STC ST00373BO](https://openairdocs.org/stc/ST00373BO): Installation of Rockwell Collins TDR-94D Transponders with ADS-B Out. Pro Star Aviation, LLC - [STC ST00105AT](https://openairdocs.org/stc/ST00105AT): Installation of a replacement coalescer filter. Purolator Facet, Inc - [STC ST00304WI](https://openairdocs.org/stc/ST00304WI): Installation of Keddeg Company 21BC113 coaleser assembly. Purolator Facet, Inc - [STC ST02632LA](https://openairdocs.org/stc/ST02632LA): Modification to replace the existing Mode S Transponder system with ACSS NXT-700 Mode S Transponder with ADS-B Out and optionally install ACSS NXG-900 GPS as a position source for ADS-B Out. Aviation Communications and Surveillance Systems - [STC ST02609LA](https://openairdocs.org/stc/ST02609LA): Modification to replace the existing Mode S Transponder system with ACSS NXT-700 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC SA4407SW](https://openairdocs.org/stc/SA4407SW): Installation of emergency brake pressure indication system. Centurion Investments - [STC SA1357GL](https://openairdocs.org/stc/SA1357GL): Install air ambulance stretcher P/N 125 using installation kit P/N 805. Paul/ Lanna Egan LLC - [STC ST00881WI-D](https://openairdocs.org/stc/ST00881WI-D): Modification of a TCAS II system installation to Change 7.0 or Change 7.1. Rockwell Collins Inc - [STC ST04238AT](https://openairdocs.org/stc/ST04238AT): Upgrade of Honeywell Traffic Collision Avoidance Systems II (TCAS II) Processor Software from TCAS II Version 7.0 to TCAS II Version 7.1. Aviation Partners Group Inc - [STC SA1537CE](https://openairdocs.org/stc/SA1537CE): Installation of Solar Model T-62T-40C auxiliary power unit(APU). Sabreliner Aviation LLC - [STC SA1603CE](https://openairdocs.org/stc/SA1603CE): Installation of Collins FPC-75 ground proximity warning system. Sabreliner Aviation LLC - [STC SA1604CE](https://openairdocs.org/stc/SA1604CE): Installation of Collins DNS-61B inertial navigation system. Sabreliner Aviation LLC - [STC SA1917CE](https://openairdocs.org/stc/SA1917CE): Installation of Puritan-Bennett "sweep on, low profile" quick donning crew mask and regulator assembly. Sabreliner Aviation LLC - [STC SA2143CE](https://openairdocs.org/stc/SA2143CE): Installation of a modified entry step system for the entrance door. Sabreliner Aviation LLC - [STC SA2199CE](https://openairdocs.org/stc/SA2199CE): Installation of Universal Navigation Corporation UNS-1 Jr. Navigation Management System. Sabreliner Aviation LLC - [STC SA2545CE](https://openairdocs.org/stc/SA2545CE): Installation of Fairchild Model GA-100 cockpit voice recorder system. Sabreliner Aviation LLC - [STC SA2640CE](https://openairdocs.org/stc/SA2640CE): tallation of Global-Wulfsberg GNS-500A Series 5 Navigation System with VLF, Omega and GPS Sensors. Sabreliner Aviation LLC - [STC SA2649CE](https://openairdocs.org/stc/SA2649CE): Installation of dual Global-Wulfsberg GNS-500A Series 5 navigation systems with VLF, Omega, GPS and Loran C sensors. Sabreliner Aviation LLC - [STC SA2759CE](https://openairdocs.org/stc/SA2759CE): Installation of Fairchild Model A100A Cockpit Voice Recorder. Sabreliner Aviation LLC - [STC ST00007WI](https://openairdocs.org/stc/ST00007WI): Installation of Collins TCAS-94 (TCAS II), TDR-94D (dual) Mode S transponder system, TWR-850 turbulence weather radar, VHF-72 COM's, VIR-32 NAV's, DME-42's, Dual CTL-22, and Dual CTL-32 controls. Sabreliner Aviation LLC - [STC ST00119WI](https://openairdocs.org/stc/ST00119WI): Installation of a Bendix TCAS I. Sabreliner Aviation LLC - [STC ST00262WI](https://openairdocs.org/stc/ST00262WI): Installation of a Trimble TNL-2100T (I/O) GPS Navigation System. Sabreliner Aviation LLC - [STC ST00456WI](https://openairdocs.org/stc/ST00456WI): Installation of an AlliedSignal Avionics Inc., MARK VI Ground Proximity Warning System. Sabreliner Aviation LLC - [STC ST00535WI](https://openairdocs.org/stc/ST00535WI): Installation of an AlliedSignal Avionics Inc., GNS-XLS Flight Management System (Dual). Sabreliner Aviation LLC - [STC ST00552WI](https://openairdocs.org/stc/ST00552WI): Installation of a Universal Avionics Systems UNS-1D with GPS and a UNS-1MSP with GPS Navigation Management Systems. Sabreliner Aviation LLC - [STC ST00603WI](https://openairdocs.org/stc/ST00603WI): Installation of dual Universal Navigation Corp UNS-1 Msp. Navigation Management Systems with dual GPS. Sabreliner Aviation LLC All 107: https://openairdocs.org/aircraft/N65ML/stcs.md ## Earlier aircraft with N65ML The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N65ML before. - [Cancelled 1997-12-08](https://openairdocs.org/deregistered/N65ML-1997-12-08): Sikorsky S-76A, S/N 760080. Exported to Brazil. Owner: [First Security Bank Na Trustee](https://openairdocs.org/faa-owner/FIRST%20SECURITY%20BANK%20NA%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) ## Related - Other Rockwell International NA-265-65 aircraft: https://openairdocs.org/model/rockwell-international-na-265-65/aircraft.md - The Garrett TFE731 series engine: https://openairdocs.org/engine/garrett-tfe731-series.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.