# Lockheed 1329-23D - Type: Aircraft model (FAA registry) - Registry code: 5263108 - Manufacturer (registry): LOCKHEED - Model: 1329-23D - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 4 · Turbo-jet - Seats: 8 - Weight class: 20,000 lb and over - Cruise speed: 371 mph - Certification: Type certificated - Data sheet: [TCDS 2A15](https://openairdocs.org/tcds/2A15) (OpenAirDocs) - Holder: Lockheed Martin Corporation - Registered aircraft: 0 - Page: https://openairdocs.org/model/lockheed-1329-23d 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 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 75-06-05 R2](https://openairdocs.org/ad/75-06-05-R2): Fuselage Main Frames · Lockheed Martin 1329-23A, 1329-23D and 1329-23E. Effective Dec 21, 1983 - [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 - [AD 68-09-02](https://openairdocs.org/ad/68-09-02): Wing Skin Risers · Lockheed Martin 1329-23A, 1329-23D and 1329-23E. Effective Nov 19, 1968 - [AD 68-08-07](https://openairdocs.org/ad/68-08-07): Airspeed and Altimeter Systems · Lockheed Martin 1329-23A, 1329-23D and 1329-23E. Effective Apr 19, 1968 - [AD 65-22-02](https://openairdocs.org/ad/65-22-02): Horizontal Stabilizer Trim System · Lockheed Martin 1329-23A and 1329-23D. Effective Sep 29, 1965 - [AD 65-19-04](https://openairdocs.org/ad/65-19-04): Landing Gear Emergency System · Lockheed Martin 1329-23A and 1329-23D. Effective Sep 25, 1965 - [AD 65-14-05](https://openairdocs.org/ad/65-14-05): Engine Detector Electrical Systems · Lockheed Martin 1329-23A and 1329-23D. Effective Jun 26, 1965 - [AD 65-14-04](https://openairdocs.org/ad/65-14-04): Rudder Cable Inspection · Lockheed Martin 1329-23A and 1329-23D. Effective Jun 26, 1965 - [AD 65-13-05](https://openairdocs.org/ad/65-13-05): Elevator Counterweight Attach Bolts · Lockheed Martin 1329-23A and 1329-23D. Effective Jun 13, 1965 - [AD 63-17-04](https://openairdocs.org/ad/63-17-04): Airspeed Limits · Lockheed Martin 1329-23A and 1329-23D. Effective Jul 25, 1963 ## Registered aircraft None registered with this model now. ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (3) As reported by operators and repair stations, by the model named in the report. - [SDR 98ZZZX1070](https://openairdocs.org/sdr/98ZZZX1070), Mar 2, 1998: PUMP. FAILED. FUEL PUMP DRIVE SPLINE WORN TO THE POINT THAT THE SPLINES NO LONGER MADE CONTACT CAUSING THE ENGINE TO SHUT DOWN. - [SDR CA971231023](https://openairdocs.org/sdr/CA971231023), Dec 11, 1997: CASTING. CRACKED. (CAN) DURING INSPECTION, FOUND RT AILERON COUNTERWEIGHT CASTING ATTACH CRACKED THROUGH BETWEEN 2 BOLTS. REPLACED. PART TC: 5,513. - [SDR 98ZZZX236](https://openairdocs.org/sdr/98ZZZX236), Dec 1, 1997: AILERON. CRACKED. DOING 12-MONTH PERIODIC INSPECTION, FOUND RT AILERON COUNTERWEIGHT CASTING ATTACHMENT CRACKED THROUGH BETWEEN 2 BOLTS. INCLUDED: PART CATALOGUE, PAGE 2-62, ITEM ## STCs that may be installed (OpenAirDocs) (230, first 50) 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 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 SA4018WE](https://openairdocs.org/stc/SA4018WE): Installation of on-board air stairs. Dow Aero Logistics LLC. Lists 1329 Series - [STC SA1664WE](https://openairdocs.org/stc/SA1664WE): Installation of Sperry SP-40C auto flight control system and SPI-73B Sperry instrumentation system. Honeywell International Inc - [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 SA1525SW](https://openairdocs.org/stc/SA1525SW): Installation of TRAMM BT1 600 nickel cadmium battery temperature indicator. FoxCart GSE, LLC - [STC SA374CE](https://openairdocs.org/stc/SA374CE): Installation of Hoskins Twilighter Mk III Supplemental Lighting System in accordance with FAA sealed Hoskins Top Drawing No. 10-0031. BF Goodrich Aerospace - [STC SA996EA](https://openairdocs.org/stc/SA996EA): Installation of Shaw Aero fuel filler cap P/Ns 457-2, -266, -370, 431, -9R, -125, -1251. Parker Hannifin Fluid Systems Division - [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 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 ST02038CH-D](https://openairdocs.org/stc/ST02038CH-D): Installation of Honeywell N1 Digital Electronic Engine Controls (DEEC). Standard Aero - [STC SA918SW](https://openairdocs.org/stc/SA918SW): Installation of Teledyne avionics normalized angle of attack indicating system. Aerosonic Corporation - [STC SA2751SW](https://openairdocs.org/stc/SA2751SW): Installation of Tracor Model 7640A Omega navigation system. Hawker Beechcraft Services Inc - [STC ST01312WI-D](https://openairdocs.org/stc/ST01312WI-D): Reduced Vertical Separation Minimum (RVSM) non-group (individual) airworthiness approval of specific Lockheed Martin Model 1329-23 aircraft in accordance with Kohlman Systems Research (KSR) Master Drawing List Jetstar 1329-23, Drawing No. MDL 1009, Rev. OR, dated January 06, 2005, or later FAA approved revision. Kohlman Systems Research Inc - [STC ST01360WI](https://openairdocs.org/stc/ST01360WI): Reduced Vertical Separation Minimum (RVSM) non-group airworthiness approval of specific Lockheed Martin Corporation Model 1329-23 Jetstar aircraft. Kohlman Systems Research Inc - [STC ST00914WI-D](https://openairdocs.org/stc/ST00914WI-D): Installation of Dual IS&S Air Data/Altimeter System along with a two-inch standby pneumatic altimeter. Duncan Aviation Inc - [STC ST02037CH](https://openairdocs.org/stc/ST02037CH): Installation of Michelin main landing gear tires. World Harvest Church - [STC SA61NE](https://openairdocs.org/stc/SA61NE): Installation of Garrett AiResearch GTCP36-100(H) auxiliary power unit. PATS Aircraft LLC - [STC SA880EA](https://openairdocs.org/stc/SA880EA): Installation of Solar T-62T-39 gas turbine auxiliary power unit. PATS Aircraft LLC - [STC SA1052EA](https://openairdocs.org/stc/SA1052EA): Installation of Solar gas turbine auxiliary power unit T-62T-40C. PATS Aircraft LLC. Lists 1329 Series - [STC SA2262SW](https://openairdocs.org/stc/SA2262SW): Modification of hydraulic brake system. L-3 Communications Integrated Systems LP - [STC ST01379SE](https://openairdocs.org/stc/ST01379SE): Non-group approval for Reduced Vertical Separation Minimum. AeroMech Incorporated All 230: https://openairdocs.org/model/lockheed-1329-23d/stcs.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.