# N71KM: 2018 Lockheed Martin 382J - Status: Valid registration - Airframe: [Lockheed Martin 382J](https://openairdocs.org/model/lockheed-martin-382j) (registry code 5264153, 2 seats) - Engine: [Rolls-Royce AE-2100D3](https://openairdocs.org/engine/rolls-royce-ae-2100d3) (registry code 54143) - Data sheets: [TCDS A1SO](https://openairdocs.org/tcds/A1SO) (Lockheed Martin Corporation), [TCDS TE1CH](https://openairdocs.org/tcds/TE1CH) (Rolls-Royce Corporation) (OpenAirDocs) - Serial number: 5854 - Year built: 2018 - Type: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: March 9, 2023 - Certificate issued: September 9, 2020 - Expires: September 30, 2027 - Mode S code: A97AA1 - Registered owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=71KM - Page: https://openairdocs.org/aircraft/N71KM 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): 18 in force ### Matched by airframe (Lockheed Martin 382J) - [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 2024-01-02](https://openairdocs.org/ad/2024-01-02): Fuselage · Lockheed 382, 382B, 382E and 9 more. Effective Jan 24, 2024 - [AD 2023-11-10](https://openairdocs.org/ad/2023-11-10): Fuselage · Lockheed Martin 382, 382B, 382E and 9 more. Effective Jul 11, 2023 - [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 2014-17-02](https://openairdocs.org/ad/2014-17-02): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Sep 9, 2014 - [AD 2008-14-10](https://openairdocs.org/ad/2008-14-10): Upper engine mount bolts · Lockheed Martin 382, 382B, 382E and 3 more. Effective Jul 22, 2008 - [AD 99-25-04](https://openairdocs.org/ad/99-25-04): Floor to Ring Fittings · Lockheed Martin 382, 382B, 382E and 3 more. Effective Jan 7, 2000 - [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 95-07-03](https://openairdocs.org/ad/95-07-03): Auxiliary Power Units · Allliedsignal Aerospace Auxiliary Power Units, 707-100 Long Body, 707-100B Long Body and 46 more. Effective May 3, 1995 - [AD 79-18-12](https://openairdocs.org/ad/79-18-12): Auxiliary Power Units · Airbus BAC 1-11 200 Series, BAC 1-11 400 Series, Manufacturing Company Auxiliary Power Units and 46 more. Effective Oct 8, 1979 ### Matched by engine (Rolls-Royce AE-2100D3) - [AD 2022-01-04](https://openairdocs.org/ad/2022-01-04): Turbine Engine Compressor Section · Rolls-Royce Deutschland AE 2100D3. Effective Feb 2, 2022 - [AD 2020-20-04](https://openairdocs.org/ad/2020-20-04): Turbine Engine Reduction Gear · Rolls-Royce AE 2100D3. Effective Oct 14, 2020 - [AD 2018-17-04](https://openairdocs.org/ad/2018-17-04): Turbine section · Rolls-Royce AE 2100D2A, AE 2100D3 and AE 3007A2. Effective Sep 21, 2018 - [AD 2015-02-08](https://openairdocs.org/ad/2015-02-08): Turbine wheels · Rolls-Royce AE 2100D2, AE 2100D2A, AE 2100D3 and 11 more. Effective Mar 11, 2015 - [AD 2009-11-04](https://openairdocs.org/ad/2009-11-04): Propeller gearbox (PGB) · Rolls-Royce AE 2100D2, AE 2100D2A, AE 2100D3 and 1 more. Effective Jun 26, 2009 - [AD 2006-25-13](https://openairdocs.org/ad/2006-25-13): Compressor cone shaft assemblies · Rolls-Royce AE 2100D3. Effective Dec 29, 2006 - [AD 2001-17-31](https://openairdocs.org/ad/2001-17-31): Second Stage High Pressure Turbine Wheel · Rolls-Royce AE 2100A, AE 2100C, AE 2100D3 and 2 more. Effective Oct 5, 2001 - [AD 99-03-09](https://openairdocs.org/ad/99-03-09): Turbine wheel failure · Rolls-Royce AE 2100A, AE 2100C and AE 2100D3. Effective Feb 19, 1999 ### Historical (superseded or no longer in force) - [AD 2013-18-09](https://openairdocs.org/ad/2013-18-09) (historical): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Oct 3, 2013 - [AD 74-08-09 R2](https://openairdocs.org/ad/74-08-09-R2) (historical): Waste Receptacles · Aero Spacelines 377, 377MG, 377SGT and 268 more. Effective Jul 29, 1996 ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N71KM. ## FAA accident and incident reports None matched to N71KM. ## 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 11VB202206230001](https://openairdocs.org/sdr/11VB202206230001), Jun 16, 2022: BOLT. MISSING. DURING THE 600HR TORQUE CHECK OF THE BL61R OF FS345E RING SEGMENT FASTENERS, FOUND THAT RING SEGMENT FS345E-245, BL61R, ANGLE RING SPLICE P/N 341950 IS MISSING ## STCs that may be installed (OpenAirDocs) (4) 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 Martin 382J) - [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 SA02365CH](https://openairdocs.org/stc/SA02365CH): Installation of NASI Supplemental Air-Conditioning System. National Aircraft Service Inc - [STC ST01307WI-D](https://openairdocs.org/stc/ST01307WI-D): Modification of a Collins TVI-920/TVI-920D Vertical Speed/TCAS Indicator installation. Rockwell Collins Inc ### Approved for the engine (Rolls-Royce AE-2100D3) - [STC SE00888CH](https://openairdocs.org/stc/SE00888CH): Install a Wind Gust Brake Kit. Rolls-Royce Corporation ## Earlier aircraft with N71KM The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N71KM before. - [Cancelled 2013-07-23](https://openairdocs.org/deregistered/N71KM-2013-07-23): Murray Kevin D MODIFIED PITTS, S/N KM-1, built 1981. Registration expired, pending cancellation. Owner: [Murray Kevin D](https://openairdocs.org/faa-owner/MURRAY%20KEVIN%20D), [Moneta, VA](https://openairdocs.org/faa-place/VA/Moneta) ## Related - Other Lockheed Martin 382J aircraft: https://openairdocs.org/model/lockheed-martin-382j/aircraft.md - The Rolls-Royce AE-2100D3 engine: https://openairdocs.org/engine/rolls-royce-ae-2100d3.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.