Lockheed Martin Aeronautics Company
Holds 8 type certificates (20 models). Holds 42 approved modifications, most of them for the Lockheed Martin Corp 382. FAA spelling: Lockheed Martin Aeronautics Company.
Type certificates 8
6A5Aircraft · 1049G-82, 1049C-55, 1049E-55, 1049F-55 (USAF C-121C), 1049D-55, 1049B-55 (Navy R7V-1) and 2 more
A-763Aircraft · 149-46, 649-79, 749A-79, 749-79, 649A-79, 49-46
TC 652Aircraft · 12-B
4A17Aircraft · 1649A-98
A-723Aircraft · 18
TC 590Aircraft · Electra 10-E
2A11Aircraft · 402-2
H5WEAircraft · L-286
Approved modifications 42 · newest first
Lockheed Martin Corp 382 22Boeing 747 3Lockheed 1329 2Boeing 757 1Mcdonnell Douglas DC-10 1Mcdonnell Douglas MD-11 1
2009-12-01SA5304NM-D · Reconfiguration of interior seating.This approval is limited to Boeing 747-273C, Serial No. 20651. · 747-200C Series
2009-12-01SA3447NM · Installation of a executive interior in the cabin compartment, modification of the flight station, and installation... · L-1011-385-3
2009-12-01SA5300NM-D · Conversion of L-1011 flight station and associated avionics from an Eastern Air Lines configuration to a Delta Air... · L-1011-385-1
2009-12-01ST00714CH · Installation of a Lockheed Martin Water Vapor Sensing System (WVSS). (757-200 PF SERIES) · 757-200, 757-200 Series, 757-200PF Series
2007-11-15SA1625WE · Pallet assembly provisions. · 382G, 382F, 382
2007-05-08SA8623SW · ONE-ONLY: Installation of an Executive Interior, S/N 293A-1249. · L-1011-385-3
2005-06-03SA2536WE · Modification and installation of aft cargo door; cargo loading and retention system; strengthened floor support... · 188A
2004-04-26SA4-1403 · Installation of a Lockheed Aircraft Service model 109C flight data recorder. · 188A, 188C
2004-04-26SA5315NM-D · Modification and installation of Hughes-Avicom video display unit consoles, P/N 612630 and 612640. · MD-11
2004-04-26SA5312NM-D · Installation of C & D Interiors video control center, P/N 8181001-101. · DC-10-30
2004-04-26SA1637WE · Installation of cargo door approximately 80 inches high by 144 inches long in left side of fuselage forebody. · 188C
2004-04-26SA1754WE · Installation of cargo doors, cargo floor and other changes. (188A, 188C Aircraft SN 1070 and higher are eligible.) · 188C, 188A
2004-04-26SA707EA · Relocation of cabin window right-side from fuselage station 217-236 to fuselage station 333-352. · 188C
2004-04-26SA5302NM-D · Reinforcement of Inertial Navigation System (INS) battery rack and installation of heavier batteries. · L-1011-385-3, L-1011-385-1-15, L-1011-385-1
2004-04-26SA3408NM · Installation of an 'executive' interior in the cabin compartment, modification of the flight station, and... · L-1011-385-3
2004-04-26SA5301NM-D · Installation of a satellite communication (SATCOM) system. · 747-400 Series
2004-04-26SA709EA · Installation of floor structure and miscellaneous modifications. Is approved only for its structural and electrical... · 188C
2004-04-26SA708EA · Installation of opening in fuselage right hand for emergency exit between fuselage station 226 and fuselage station... · 188C
2004-04-26SA5314NM-D · Modification and installation of Hughes-Avicom Video Display Unit Consoles, P/N 612630 and 612640. · 747-400 Series
1989-02-10ST374SO · Palletized cargo loading system per Lockheed Industrial Products top assy. dwg. 256-000. · 382, 382E
1989-02-10SA1231SO · Installation of four Type III emergency exits. (382G S/N 4880, 4883, 4886) · 382G
1989-02-10ST398SO · Installation of Allison 501-D22A engine(s) in the -6C and -10C versions of the Model 382B aircraft. · 382B
1989-02-10ST400SO · Installation of palletized cargo loading and restraint system. · 382G, 382B, 382
1989-02-10SA384SO · Installation of C-5A engine/EBU transportation dolly. · 382B, 382E
1989-02-10ST401SO · Installation of palletized cargo loading and restraint · 382B, 382E, 382G
1989-02-10ST368SO · Palletized cargo loading system. · 382B, 382
1989-02-10ST395SO · 100 inch increase in fuselage length, installation of Allison 501-D22A engines in lieu of 501-D22 engine, and... · 382B
1989-02-10ST425SO · Installation of 100 inch fuselage extension, (60 inches forward at F.S. 245 and 40 inches aft at F.S. 737). (382B... · 382B
1989-02-10ST441SO · Installation of a modified center and outer wing. · 382B
1989-02-10ST372SO · Air cargo container. · 382, 382B
1989-02-10ST531SO · Increase in maximum landing weight from 130,000 pounds to 135,000 pounds. (382B s/n 4209, 4234, 4248) (382E s/n 4222, 4300) · 382B, 382E
1989-02-10SA1973SW · Installation of Collins AP-105V autopilot. · 382B
1989-02-10ST524SO · Increase in maximum landing weight to 135,000 lbs. and maximum zero fuel weight to 128,790 lbs. With pylon tanks on... · 382F
1989-02-10ST407SO · Installation of palletized cargo loading and restraint system. · 382B, 382E, 382G
1989-02-10SA1126SO · Deletion of empennage de-icing provisions - removal of empennage de-icing boots. (1329-23A, -23D, -23E JETSTAR) · 1329-23A, 1329-23E, 1329-23D
1989-02-10SA1994SO · Installation of cargo handling system. · 382G
1989-02-10SA1056SO · Increase in zero fuel weight from126,790 lbs. to 128,790 lbs. With pylon tanks on and 125,000 lbs. To127,000 lbs.... · 382G
1989-02-10ST913SO · Installation of six 24-inch x 36-inch plug type doors in cargo compartment walls. · 382G
1989-02-10ST416SO · Installation of a Collins AP-104, autopilot, S/N 5136 and up. · 1329 Series
1989-02-10ST446SO · 180 inch increase in fuselage length, installation of Allison 501-D22A engines in lieu of 501-D22 engines, and... · 382B
1989-02-10ST439SO · Installation of palletized carrgo loading and restraint system. · 382G, 382F, 382E
1983-08-24ST521SO · Increase in maximum landing weight to 135,000 pounds and maximum zero fuel weight to 128,790 pounds with pylon tanks... · 382, 382E
Source: FAA Dynamic Regulatory System (type certificate data sheets, supplemental type certificates, technical standard order authorisations). An organisation's name is as the FAA spelled it on each record; related spellings are separate pages.