# N311RS: 1977 Lockheed 1329-25 JETSTAR II

- Status: Valid registration
- Airframe: [Lockheed 1329-25 JETSTAR II](https://openairdocs.org/model/lockheed-1329-25-jetstar-ii) (registry code 5263125, 12 seats)
- Engine: [Alliedsign TFE731 series](https://openairdocs.org/engine/alliedsign-tfe731-series) (registry code 02509)
- Data sheets: [TCDS 2A15](https://openairdocs.org/tcds/2A15) (Lockheed Martin Corporation) (OpenAirDocs)
- Serial number: 5222
- Year built: 1977
- Type: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: July 11, 2003
- Certificate issued: January 27, 2012
- Expires: January 31, 2028
- Mode S code: A34C10
- Registered owner: [Ken Sale Resources Inc](https://openairdocs.org/faa-owner/KEN%20SALE%20RESOURCES%20INC)
- Location: [Southlake, TX](https://openairdocs.org/faa-place/TX/Southlake)
- Owner type: Corporation
- Owner's area on the map: 32.9545° N, 97.1489° W: Placed by OpenAirDocs at the center of ZIP code 76092, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=311RS
- Page: https://openairdocs.org/aircraft/N311RS

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 Alliedsign TFE731 model are included.

## ADs that may apply (OpenAirDocs): 53 in force

### Matched by airframe (Lockheed 1329-25 JETSTAR II)

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2008-13-26](https://openairdocs.org/ad/2008-13-26): Nose landing gear (NLG) · Lockheed Martin 1329-23A, 1329-23D, 1329-23E and 1 more. Effective Aug 12, 2008
- [AD 2005-01-02](https://openairdocs.org/ad/2005-01-02): Front spar cap assembly of the lower vertical stabilizer · Lockheed Martin 1329-23A, 1329-23D, 1329-23E and 1 more. Effective Feb 9, 2005
- [AD 2002-15-02](https://openairdocs.org/ad/2002-15-02): Compressor Wheels · British Aerospace Regional Jetstream Series 3101, 234, Mystere-Falcon 20 - C5 and 22 more. Effective Aug 28, 2002
- [AD 99-19-17](https://openairdocs.org/ad/99-19-17): AFM - Limitation Section - Ice Protection System · Lockheed Martin 1329-23A, 1329-23D, 1329-23E and 1 more. Effective Dec 27, 1999
- [AD 98-07-21](https://openairdocs.org/ad/98-07-21): Engine Tailpipe V-Band Coupling · AiResearch TFE731-3-IE engines (UNC/CFC Acquisition STC SA2326SW). Effective May 18, 1998
- [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 91-11-13](https://openairdocs.org/ad/91-11-13): Empennage Pivot Fittings · Lockheed Martin 1329-23A, 1329-23D, 1329-23E and 1 more. Effective Jun 24, 1991
- [AD 87-16-01](https://openairdocs.org/ad/87-16-01): Fuel Line Shrouds and Drains · GTCP30-92 or GTCP30-92C auxiliary power unit (UNC/CFC Acquisition STC SA1043WE or 2 others). Effective Aug 26, 1987
- [AD 87-07-08](https://openairdocs.org/ad/87-07-08): APU Shutoff Valve · GTCP30-92 or GTCP30-92C auxiliary power unit (UNC/CFC Acquisition STC SA1043WE or SA3297WE). Effective May 1, 1987
- [AD 84-23-01](https://openairdocs.org/ad/84-23-01): Hardware, Fasteners · Lockheed Martin 1329-23A, 1329-23D, 1329-23E and 1 more. Effective Nov 26, 1984
- [AD 82-18-09](https://openairdocs.org/ad/82-18-09): Refueling System · Single point pressure fueling system (Rogerson ATS STC SA1851WE or 4 others). Effective Oct 4, 1982
- [AD 77-22-03](https://openairdocs.org/ad/77-22-03): Ring Segment - VHF Antenna · Lockheed Martin 1329-23A, 1329-23D, 1329-23E and 1 more. Effective Oct 28, 1977
- [AD 74-24-09](https://openairdocs.org/ad/74-24-09): Auxiliary Power Units · Airbus BAC 1-11 200 Series, BAC 1-11 400 Series, Auxiliary Power Units and 63 more. Effective Nov 19, 1975

### Matched by engine (Alliedsign TFE731 series)

- [AD 2019-05-07](https://openairdocs.org/ad/2019-05-07): Turbine Engine Compressor Section · Honeywell International TFE731-20AR, TFE731-20BR, TFE731-20R and 4 more. Effective Apr 25, 2019
- [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 2012-16-14](https://openairdocs.org/ad/2012-16-14): LPT2 rotor blades · Honeywell International TFE731-20AR, TFE731-20BR, TFE731-20R and 5 more. Effective Oct 1, 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 99-07-19](https://openairdocs.org/ad/99-07-19): Tube and Fuel Flow Meter Mounting Bracket · Honeywell International TFE731-40R. Effective Apr 21, 1999
- [AD 98-10-15](https://openairdocs.org/ad/98-10-15): Fuel Line · Honeywell International TFE731-40R. Effective May 19, 1998
- [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 2017-20-01](https://openairdocs.org/ad/2017-20-01) (historical): Turbine Engine Compressor Section · Honeywell International TFE731-20 and TFE731-40. Effective Nov 2, 2017
- [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 N311RS.

## FAA accident and incident reports

None matched to N311RS.

## 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) (260, 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 (Lockheed 1329-25 JETSTAR II)

- [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 ST00155DE-D](https://openairdocs.org/stc/ST00155DE-D): Installation of TCAS 791 TCAS I System. 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 ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc
- [STC ST01930LA](https://openairdocs.org/stc/ST01930LA): Installation of Sandel Avionics SN4500 Electronic Horizontal Situation Indicator (EHSI). Sandel Avionics LLC
- [STC SA4018WE](https://openairdocs.org/stc/SA4018WE): Installation of on-board air stairs. Dow Aero Logistics LLC. Lists 1329 Series
- [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 SA2-1574](https://openairdocs.org/stc/SA2-1574): Change SP-40 Autopilot heading and radio control data from the copilot's R-4A Course Indicator and #2 VHF Navigation system to the pilot's R-4A Course Indicator and #1 VHF Navigation system. Associated Air Center, Inc. - c/o CT Corporation System
- [STC SA535SW](https://openairdocs.org/stc/SA535SW): Relocation and use of miniature switches in fuel flow system. Associated Air Center, Inc. - c/o CT Corporation System
- [STC SA548SW](https://openairdocs.org/stc/SA548SW): Installation of a Flight Recorder System. Associated Air Center, Inc. - c/o CT Corporation System
- [STC SA602SW](https://openairdocs.org/stc/SA602SW): Installation of a hinged instrument panel in a Lockheed Model 1329 aircraft. Associated Air Center, Inc. - c/o CT Corporation System. Lists 1329 Series
- [STC SA762SW](https://openairdocs.org/stc/SA762SW): Smith servo altimeter system. Associated Air Center, Inc. - c/o CT Corporation System. Lists 1329 Series
- [STC SA769SW](https://openairdocs.org/stc/SA769SW): Collins 329P-1D peripheral commander Indicating System. Associated Air Center, Inc. - c/o CT Corporation System. Lists 1329 Series
- [STC SA345SW](https://openairdocs.org/stc/SA345SW): Installation of Bendix Doppler radar navigation system. Associated Air Center, Inc. - c/o CT Corporation System
- [STC SA536SW](https://openairdocs.org/stc/SA536SW): Installation of a Litton low range radio altimeter system. Associated Air Center, Inc. - c/o CT Corporation System
- [STC SA561SW](https://openairdocs.org/stc/SA561SW): Modification of glare shield for quick removal. Associated Air Center, Inc. - c/o CT Corporation System
- [STC SA783SW](https://openairdocs.org/stc/SA783SW): Installation of Bar extension equipment shelf. Associated Air Center, Inc. - c/o CT Corporation System. Lists 1329 Series
- [STC SA827SW](https://openairdocs.org/stc/SA827SW): Installation of a Fairchild Model 5424-502 flight data recorder. Associated Air Center, Inc. - c/o CT Corporation System. Lists 1329 Series
- [STC SA828SW](https://openairdocs.org/stc/SA828SW): Installation of Fairchild A100 cockpit voice recorder. Associated Air Center, Inc. - c/o CT Corporation System. Lists 1329 Series
- [STC SA844SW](https://openairdocs.org/stc/SA844SW): Installation of Consolidated Electrodynamic Corporation Advanced Airborne Vibration Monitor System. Associated Air Center, Inc. - c/o CT Corporation System
- [STC SA876SW](https://openairdocs.org/stc/SA876SW): Bulkhead modification. Associated Air Center, Inc. - c/o CT Corporation System
- [STC SA877SW](https://openairdocs.org/stc/SA877SW): Pedestal modification. Associated Air Center, Inc. - c/o CT Corporation System
- [STC SA879SW](https://openairdocs.org/stc/SA879SW): Hinged instrument panel and modification to control column. Associated Air Center, Inc. - c/o CT Corporation System. Lists 1329 Series
- [STC SA883SW](https://openairdocs.org/stc/SA883SW): Mounting bracket antenna tuner. Associated Air Center, Inc. - c/o CT Corporation System. Lists 1329 Series
- [STC SA884SW](https://openairdocs.org/stc/SA884SW): Hoskins power supply support. Associated Air Center, Inc. - c/o CT Corporation System. Lists 1329 Series
- [STC SA885SW](https://openairdocs.org/stc/SA885SW): Bulkhead coax fitting and VHF or FM antenna. Associated Air Center, Inc. - c/o CT Corporation System
- [STC SA887SW](https://openairdocs.org/stc/SA887SW): Installation of "L" Band Antenna. Associated Air Center, Inc. - c/o CT Corporation System
- [STC SA900SW](https://openairdocs.org/stc/SA900SW): Installation of Skyphone antenna. Associated Air Center, Inc. - c/o CT Corporation System
- [STC SA902SW](https://openairdocs.org/stc/SA902SW): Installation of Howell Autotemp Indicators. Associated Air Center, Inc. - c/o CT Corporation System
- [STC SA904SW](https://openairdocs.org/stc/SA904SW): Installation of Mach Airspeed Warning Switch. Associated Air Center, Inc. - c/o CT Corporation System
- [STC ST00366WI](https://openairdocs.org/stc/ST00366WI): Installation of Keddeg Company P/N 21BC115 Coalescer Assembly. Purolator Facet, Inc
- [STC ST02406LA](https://openairdocs.org/stc/ST02406LA): Installation of TCAS version 7.1. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC SA1525SW](https://openairdocs.org/stc/SA1525SW): Installation of TRAMM BT1 600 nickel cadmium battery temperature indicator. FoxCart GSE, LLC
- [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 ST01399LA](https://openairdocs.org/stc/ST01399LA): Installation of Honeywell TCAS 2000/Dual Mode S ATC Transponder Systems. Limited to installation on Lockheed 1329-25, serial number 5213. Lockheed Sales & Rentals Inc
- [STC ST01095CH-D](https://openairdocs.org/stc/ST01095CH-D): Installation of an Allied Signal CAS-67A Traffic Alert and Collision Avoidance System (TCAS II). Installed per ElectroSonics Drawing ES1329-205075-01, Rev. 2, dated 09-20-00 or later FAA approved revision. Standard Aero
- [STC ST00523WI-D](https://openairdocs.org/stc/ST00523WI-D): Installation of an AlliedSignal Avionics, Inc., GNS-XIs Flight Management System (Dual). Duncan Aviation Inc
- [STC ST00970WI-D](https://openairdocs.org/stc/ST00970WI-D): Installation of a Collins AHS-3000A Attitude Heading Reference System (AHRS). Duncan Aviation Inc
- [STC ST01059WI-D](https://openairdocs.org/stc/ST01059WI-D): Installation of Honeywell MK VII Enhanced Ground Proximity Warning System (EGPWS). Duncan Aviation Inc
- [STC ST01240WI-D](https://openairdocs.org/stc/ST01240WI-D): Installation of Universal Avionics Terrain Awareness and Warning System (TAWS). Duncan Aviation Inc
- [STC ST01312WI](https://openairdocs.org/stc/ST01312WI): Vertical Separation Minimum (RVSM) non-group (individual) airworthiness approval of specific Lockheed Martin Model 1329-23 aircraft. Kohlman Systems Research Inc
- [STC ST01082SE](https://openairdocs.org/stc/ST01082SE): Group approval for Reduced Vertical Separation Minimum are contained in AeroMech Document No AMI-QD-JS-0019, dated May 10, 2002, or later FAA-approved revisions. AeroMech Incorporated
- [STC ST01360SE](https://openairdocs.org/stc/ST01360SE): ONE ONLY STC, S/N 5213: Non-Group approval for Reduced Vertical Separation Minimum are contained in AeroMech Document No AMI-QD-JS-0023, Rev. A, dated February 1, 2008, or later FAA-approved revisions. AeroMech Incorporated
- [STC ST02038CH-D](https://openairdocs.org/stc/ST02038CH-D): Installation of Honeywell N1 Digital Electronic Engine Controls (DEEC). Standard Aero
- [STC ST1360SE](https://openairdocs.org/stc/ST1360SE): ONE ONLY STC. SN 5213: Non-Group approval for Reduced Vertical Separation Minimum are contained in AeroMech Document No AMI-QD-JS-0023, Rev. A, dated February 1, 2008, or later FAA-approved revisions. AeroMech Incorporated
- [STC SA3371WE](https://openairdocs.org/stc/SA3371WE): Installation of Teledyne angle of attack system. Aerosonic Corporation
- [STC SA2751SW](https://openairdocs.org/stc/SA2751SW): Installation of Tracor Model 7640A Omega navigation system. Hawker Beechcraft Services Inc
- [STC SA2752SW](https://openairdocs.org/stc/SA2752SW): Installation of Sperry TERN-100 navigation system. Hawker Beechcraft Services Inc
- [STC SA2753SW](https://openairdocs.org/stc/SA2753SW): Installation of Delco Carousel IVA inertial navigation system. Hawker Beechcraft Services Inc
- [STC ST459CH-D](https://openairdocs.org/stc/ST459CH-D): Installation of an AllliedSignal Aerospace TFE731-3D-1(F,K) Turbofan Engine. Honeywell International Inc

All 260: https://openairdocs.org/aircraft/N311RS/stcs.md

## Earlier aircraft with N311RS

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N311RS before.

- [Cancelled 1999-10-21](https://openairdocs.org/deregistered/N311RS-1999-10-21): Starck Robert L AURIGA, S/N 028. Owner: [Camp Excelsior](https://openairdocs.org/faa-owner/CAMP%20EXCELSIOR), [Chattanooga, TN](https://openairdocs.org/faa-place/TN/Chattanooga)

## Related

- Other Lockheed 1329-25 JETSTAR II aircraft: https://openairdocs.org/model/lockheed-1329-25-jetstar-ii/aircraft.md
- The Alliedsign TFE731 series engine: https://openairdocs.org/engine/alliedsign-tfe731-series.md

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