# Lockheed 382

- Type: Aircraft model (FAA registry)
- Registry code: 5264102
- Manufacturer (registry): LOCKHEED
- Model: 382
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 4 · Turbo-prop
- Seats: 3
- Weight class: 20,000 lb and over
- Cruise speed: 262 mph
- Certification: Type certificated
- Data sheet: [TCDS A1SO](https://openairdocs.org/tcds/A1SO) (OpenAirDocs)
- Holder: Lockheed Martin Corporation
- Registered aircraft: 0
- Page: https://openairdocs.org/model/lockheed-382

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 2024-01-02](https://openairdocs.org/ad/2024-01-02): Fuselage · Lockheed 382, 382B, 382E and 9 more. Effective Jan 24, 2024
- [AD 2023-22-06](https://openairdocs.org/ad/2023-22-06): Powerplant · Lockheed Martin 382, 382B, 382E and 8 more. Effective Nov 21, 2023
- [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 2023-09-13](https://openairdocs.org/ad/2023-09-13): Wings · Lockheed Martin 382, 382B, 382E and 7 more. Effective May 31, 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 2021-09-15](https://openairdocs.org/ad/2021-09-15): Wings · Coulson EC-130Q, C-130A, C-130A and 11 more. Effective Jun 1, 2021
- [AD 2019-25-20](https://openairdocs.org/ad/2019-25-20): Flight controls · Coulson EC-130Q, C-130A, C-130A and 11 more. Effective Feb 28, 2020
- [AD 2015-22-11](https://openairdocs.org/ad/2015-22-11): Wings · Lockheed Martin 382, 382B, 382E and 2 more. Effective Dec 28, 2015
- [AD 2015-18-02](https://openairdocs.org/ad/2015-18-02): Wings · Lockheed Martin 382, 382B, 382E and 2 more. Effective Sep 17, 2015
- [AD 2015-06-08](https://openairdocs.org/ad/2015-06-08): Wings · Lockheed Martin 382, 382B, 382E and 2 more. Effective May 14, 2015
- [AD 2015-05-08](https://openairdocs.org/ad/2015-05-08): Wings · Lockheed Martin 382, 382B, 382E and 2 more. Effective Apr 24, 2015
- [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 2012-06-09](https://openairdocs.org/ad/2012-06-09): Standard practices/structures · Lockheed Martin 382, 382B, 382E and 2 more. Effective May 15, 2012
- [AD 2011-15-02](https://openairdocs.org/ad/2011-15-02): Fuel · Lockheed Martin 382, 382B, 382E and 2 more. Effective Aug 19, 2011
- [AD 2009-11-03](https://openairdocs.org/ad/2009-11-03): Wings · Lockheed Martin 382, 382B, 382E and 2 more. Effective Jun 4, 2009
- [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 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 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 97-21-13](https://openairdocs.org/ad/97-21-13): AFM - Power Levers · Lockheed Martin 382, 382B, 382E and 2 more. Effective Nov 24, 1997
- [AD 97-05-07](https://openairdocs.org/ad/97-05-07): AFM Supplement 382-16 · Lockheed Martin 382, 382E and 382G. Effective Apr 4, 1997
- [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 96-24-14](https://openairdocs.org/ad/96-24-14): Main Landing Gear Brakes Inspection · Lockheed Martin 382, 382B, 382E and 2 more. Effective Jan 27, 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 94-26-15](https://openairdocs.org/ad/94-26-15): Outer Wing Assembly · Lockheed Martin 382, 382B, 382E and 2 more. Effective Feb 3, 1995
- [AD 92-10-14](https://openairdocs.org/ad/92-10-14): AFM Changes - Cabin Pressure · Lockheed Martin 382, 382B, 382E and 2 more. Effective Jun 29, 1992
- [AD 89-16-09](https://openairdocs.org/ad/89-16-09): Nose Landing Gear Strut Assembly · Lockheed Martin 382, 382B, 382E and 2 more. Effective Sep 7, 1989
- [AD 88-09-03](https://openairdocs.org/ad/88-09-03): Control Column Base · Lockheed Martin 382, 382B, 382E and 2 more. Effective Jun 7, 1988
- [AD 88-10-06](https://openairdocs.org/ad/88-10-06): Wing Panel Risers · Lockheed Martin 382, 382B, 382E and 2 more. Effective May 25, 1988
- [AD 88-10-05](https://openairdocs.org/ad/88-10-05): Wing Panel Doublers · Lockheed Martin 382, 382B, 382E and 2 more. Effective May 25, 1988
- [AD 87-18-04](https://openairdocs.org/ad/87-18-04): Circuit Breaker Panels · Lockheed Martin 382, 382B, 382E and 2 more. Effective Sep 17, 1987
- [AD 85-23-03](https://openairdocs.org/ad/85-23-03): Fire Estinguisher Squib Insp. · Lockheed Martin 382, 382B, 382E and 2 more. Effective Nov 24, 1985
- [AD 81-12-02](https://openairdocs.org/ad/81-12-02): Longerons · Lockheed Martin 382, 382B, 382E and 2 more. Effective Jun 5, 1981
- [AD 79-05-05](https://openairdocs.org/ad/79-05-05): Throttle Cables · Lockheed Martin 382, 382B, 382E and 2 more. Effective Jan 2, 1980
- [AD 79-25-06](https://openairdocs.org/ad/79-25-06): Window Latch Catches · Lockheed Martin 382, 382B, 382E and 2 more. Effective Dec 19, 1979
- [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
- [AD 79-03-04](https://openairdocs.org/ad/79-03-04): Ballscrew Assembly in MLG · Lockheed Martin 382, 382B, 382E and 2 more. Effective Feb 5, 1979
- [AD 74-12-06](https://openairdocs.org/ad/74-12-06): Outer Wing Beam Cap · Lockheed Martin 382, 382B, 382E and 2 more. Effective Dec 8, 1978
- [AD 75-17-04](https://openairdocs.org/ad/75-17-04): Main Frames · Lockheed Martin 382, 382B, 382E and 2 more. Effective Apr 21, 1978
- [AD 75-19-02](https://openairdocs.org/ad/75-19-02): Wing Beam Caps · Lockheed Martin 382, 382B, 382E and 2 more. Effective Mar 20, 1978
- [AD 75-18-04](https://openairdocs.org/ad/75-18-04): Outer Wing Lower Panels · Lockheed Martin 382, 382B, 382E and 2 more. Effective Mar 20, 1978
- [AD 75-18-03](https://openairdocs.org/ad/75-18-03): Outer Wing Spar Cap · Lockheed Martin 382, 382B, 382E and 2 more. Effective Mar 20, 1978
- [AD 76-09-11](https://openairdocs.org/ad/76-09-11): Crank Arm or Servo Valve Assembly · Lockheed Martin 382, 382B, 382E and 2 more. Effective May 14, 1976
- [AD 75-17-35](https://openairdocs.org/ad/75-17-35): Propeller Torque Check · Lockheed Martin 382, 382B, 382E and 2 more. Effective Aug 13, 1975
- [AD 74-24-08](https://openairdocs.org/ad/74-24-08): Engine Throttle Cables · Lockheed Martin 382, 382B, 382E and 2 more. Effective Nov 27, 1974
- [AD 74-24-04](https://openairdocs.org/ad/74-24-04): Lower Center Wing · Lockheed Martin 382, 382B, 382E and 2 more. Effective Nov 20, 1974
- [AD 67-18-03](https://openairdocs.org/ad/67-18-03): Engine Mount Truss · Lockheed Martin 382 and 382B. Effective Mar 12, 1973
- [AD 68-03-03](https://openairdocs.org/ad/68-03-03): Wing Lower Surface · Lockheed Martin 382 and 382B. Effective Feb 10, 1968

Historical (superseded or no longer in force):

- [AD 2019-18-09](https://openairdocs.org/ad/2019-18-09) (historical): Wings · Coulson EC-130Q, C-130A, C-130A and 11 more. Effective Oct 11, 2019
- [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 2011-09-04](https://openairdocs.org/ad/2011-09-04) (historical): Wings · Lockheed Martin 382, 382B, 382E and 2 more. Effective Jun 22, 2011
- [AD 2011-09-03](https://openairdocs.org/ad/2011-09-03) (historical): Wings · Lockheed Martin 382, 382B, 382E and 2 more. Effective May 26, 2011
- [AD 2008-20-01](https://openairdocs.org/ad/2008-20-01) (historical): Fuel tank systems · Lockheed Martin 382, 382B, 382E and 2 more. Effective Nov 3, 2008
- [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
- [AD 96-12-20](https://openairdocs.org/ad/96-12-20) (historical): Upper Truss Mounts · Lockheed Martin 382, 382B, 382E and 2 more. Effective Jul 15, 1996

## Information bulletins (advisory) (1)

- [SAIB NM-09-03](https://openairdocs.org/saib/NM-09-03): Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations. Issued Dec 11, 2008

## Registered aircraft

None registered with this model now.

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports (1)

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.

- [Incident 19880822054889I](https://openairdocs.org/incident/19880822054889I), Aug 22, 1988: Lkheed 382G (N912SJ), Indianapolis, IN. Precautionary shut down of NR3 engine after oil loss. Found bad o ring at accessory drive oil pump.

## Service difficulty reports (3)

As reported by operators and repair stations, by the model named in the report.

- [SDR 2023FA0000379](https://openairdocs.org/sdr/2023FA0000379), Jul 25, 2023: BRACKET. BROKEN. DURING THE MAINTENANCE DOWNLOAD AND DEBRIEF OF THE AIRPLANE THE MAINTENANCE TECHNICIAN OBSERVED THE FOLLOWING FAULT CODES: 4610744 BAU II NO. 3 BUILT-IN TEST FA
- [SDR 2017FA0000649](https://openairdocs.org/sdr/2017FA0000649), Dec 18, 2017: HUB. CRACKED. DURING PROPELLER RE-INSTALLATION AFTER AND ENGINE CHANGE. A 2" CRACK WAS VISUALLY NOTED FORWARD SURFACE OF THE PROPELLER HUB (BARREL HALF). THE RII INSPECTOR NO
- [SDR NQ3R20130104001](https://openairdocs.org/sdr/NQ3R20130104001), Jan 4, 2013: THRUST BEARING. BRINELLED. DURING O/H AND REPAIR CYCLES TO VALVE HOUSINGS, IT WAS NOTICED THAT AN INCREASED RATE OF GOVERNOR BEARING FAILURE IS OCCURRING. A SUBSEQUENT INDEPENDENT ENGINEE

## STCs that may be installed (OpenAirDocs) (29)

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 ST02495LA](https://openairdocs.org/stc/ST02495LA): Installation of a multipurpose hatch system. R4 Integration Inc
- [STC SA733CE](https://openairdocs.org/stc/SA733CE): Installation of cargo pallets. Telair US LLC
- [STC ST427SO](https://openairdocs.org/stc/ST427SO): Installation of cargo rail system. Telair US LLC
- [STC ST03595AT](https://openairdocs.org/stc/ST03595AT): Installation of a LED Anticollision Lights. B/E Aerospace Inc
- [STC ST03595T](https://openairdocs.org/stc/ST03595T): Installation of a LED Anticollision Lights. Woven Electronics, LLC
- [STC ST01635WI-D](https://openairdocs.org/stc/ST01635WI-D): Modification of Rockwell Collins, Inc. VHF-4000 and VHF-4000E installations. Rockwell Collins Inc
- [STC SA3132NM](https://openairdocs.org/stc/SA3132NM): Installation of a de-icing system on the Hamilton Standard P/N 554654 propeller spinner. ROBERT W. MURRAY
- [STC SA3407NM](https://openairdocs.org/stc/SA3407NM): Installation of a de-icing system on the Hamilton Standard P/N 560501 propeller spinner afterbody. ROBERT W. MURRAY
- [STC ST01202WI-D](https://openairdocs.org/stc/ST01202WI-D): Modification of an existing FAA approved Collins TPR-720, TPR-900 or TPR-901 Mode S transponder installation in Part 25 Aircraft using Collins Drawing Index as listed on AML No. ST01202WI-D, latest FAA approved revision. Rockwell Collins Inc
- [STC ST01256WI-D](https://openairdocs.org/stc/ST01256WI-D): Modification of a Collins TPR-720, TPR-900 or TPR-901 Mode S Transponder System installation with an ATC/TCAS Control Panel to an Elementary Surveillance Compliant Collins TPR-901 Mode S Transponder System installation with a Flight ID/ATC/TCAS Control Panel in accordance with Collins Drawing Index as listed on AML No. ST01256WI-D, Revision -, or later FAA approved revision. Rockwell Collins Inc
- [STC ST00435CH-D](https://openairdocs.org/stc/ST00435CH-D): Installation of a Collins TCAS-94 Traffic Alert and Collision Avoidance System (TCAS-II) system. Duncan Aviation Inc
- [STC ST434CH-D](https://openairdocs.org/stc/ST434CH-D): Installation of Dual Trimble TNL8100 GPS Navigation Systems. Duncan Aviation Inc
- [STC SA1625WE](https://openairdocs.org/stc/SA1625WE): Pallet assembly provisions. Lockheed Martin Aeronautics Company
- [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
- [STC SA1371GL](https://openairdocs.org/stc/SA1371GL): Installation of Norton Radome Kit No. 4853CX. Saint-Gobain Performance Plastics Corp
- [STC ST09130SC](https://openairdocs.org/stc/ST09130SC): Replacement of core assembly in Airesearch heat exchanger P/N 118440. Limco-Airepair, Inc
- [STC ST09345SC](https://openairdocs.org/stc/ST09345SC): Installation of a dual independent UNS-1Msp navigation management system. New Systems
- [STC ST555CH](https://openairdocs.org/stc/ST555CH): Approve operation at runway gradients up to 8 %. Southern Air Transport
- [STC ST435CH-D](https://openairdocs.org/stc/ST435CH-D): Installation of a Collins TCAS-94 traffic alert and collision avoidance system (TCAS-II) system. Duncan Aviation
- [STC SA4857NM](https://openairdocs.org/stc/SA4857NM): Modification replaces Airesearch metal shaft coupling P/N 3300065-1 with Elco P/N 2241901, non-metallic coupling. Turbine Engine Consultants, Ltd
- [STC ST368SO](https://openairdocs.org/stc/ST368SO): Palletized cargo loading system. Lockheed Martin Aeronautics Company
- [STC ST372SO](https://openairdocs.org/stc/ST372SO): Air cargo container. Lockheed Martin Aeronautics Company
- [STC ST374SO](https://openairdocs.org/stc/ST374SO): Palletized cargo loading system per Lockheed Industrial Products top assy. dwg. 256-000. Lockheed Martin Aeronautics Company
- [STC ST400SO](https://openairdocs.org/stc/ST400SO): Installation of palletized cargo loading and restraint system. Lockheed Martin Aeronautics Company
- [STC ST407SO](https://openairdocs.org/stc/ST407SO): Installation of palletized cargo loading and restraint system. Lockheed Martin Aeronautics Company
- [STC ST521SO](https://openairdocs.org/stc/ST521SO): Increase in maximum landing weight to 135,000 pounds and maximum zero fuel weight to 128,790 pounds with pylon tanks on and 127,000 pounds with pylon tanks off. Lockheed Martin Aeronautics Company
- [STC SA3793WE](https://openairdocs.org/stc/SA3793WE): Installation of Tracor 7640A ONS. Transinternational Airlines

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Lockheed 382 44C (C130K)](https://openairdocs.org/model/lockheed-382-44c-c130k): 1 registered aircraft, registry code 526021A

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