Airframe Structural Components: 377321-1, 377359-9, 37745
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
377321-1 3773211 | 1560-00-765-1706 | Latch, Wheel, Rudder Control | III End Item Identification: Aircraft model C130 | Lockheed Martin Corporation (98897) | |
377322-1 3773221 | 1560-00-734-9844 | Brace, Pedal Adjustment | General Characteristics Item Description: Aluminum alloy, 2024-T3, QQ-A-250/5, 3.750 in. l, 3.670 in. W, 3.100 in. H, 0.071 in. thk matl | Lockheed Martin Corporation (98897) | |
377323-1 3773231 | 1560-00-734-9845 | Inboard Brace, Co Pi | Lockheed Martin Corporation (98897) | ||
377356-17 37735617 | 1560-00-801-2610 | Duct Assembly, Wheel Well | III End Item Identification: Aircraft model C-130A | Lockheed Martin Corporation (98897) | |
377359-1 3773591 | 1560-00-823-8556 | Bracket Assembly, Support, Seat St | General Characteristics Item Description: Aluminum alloy, 2024-0, QQ-A-250/5, ht to T4 condition, 5.340 in. l, 3.780 in. W, with attached socket | Lockheed Martin Corporation (98897) | |
377359-9 3773599 | 1560-00-823-8556 | Bracket Assembly, Support, Seat St | General Characteristics Item Description: Aluminum alloy, 2024-0, QQ-A-250/5, ht to T4 condition, 5.340 in. l, 3.780 in. W, with attached socket | Lockheed Martin Corporation (98897) | |
377362-1 3773621 | 1560-00-771-3544 | Fitting, Intercostal | III End Item Identification: Aircraft model C130 General Characteristics Item Description: 5.800 in. O/a lg, 1.700 in. O/a W, 1.500 in. O/a H, 1 mtg hole 0.687 in. min, 0.694 in. max dia | Lockheed Martin Corporation (98897) | |
377362-3 3773623 | 1560-00-771-3544 | Fitting, Intercostal | III End Item Identification: Aircraft model C130 General Characteristics Item Description: 5.800 in. O/a lg, 1.700 in. O/a W, 1.500 in. O/a H, 1 mtg hole 0.687 in. min, 0.694 in. max dia | Aero Components Inc. (59213) Lockheed Martin Corporation (98897) | |
377365-1 3773651 | 1560-00-980-8595 | Bracket Assembly, Ru | Lockheed Martin Corporation (98897) | ||
377366-1 3773661 | 1560-00-806-7165 | Bracket Assembly | A and M Aerospace Inc. (6Z800) Aero Engineering & Manufacturing (17772) Lockheed Martin Aeroparts Inc. (0A489) Lockheed Martin Corporation (98897) Vought Aircraft Industries Inc. (93221) | ||
377367-1 3773671 | 1560-00-806-7162 | Support, Structural Component, Air | III End Item Identification: Acft model C-130 Special Features: C/O bracket P/N 352043-1, bushing P/N 377049-1 | Lockheed Martin Corporation (98897) | |
377371-1 3773711 | 1560-00-317-6686 | Pan, Flap link | III End Item Identification: Aircraft model C130 | Lockheed Martin Corporation (98897) | |
377372-1 3773721 | 1560-00-084-0130 | Pan, Flap link, Inboard | General Characteristics Item Description: Aluminum alloy, 2024-0, QQ-A-250/5, 0.050 in. thk matl, 6.830 in. l, 3.040 in. W, 0.720 in. deep, applicable to C130 acft | Aero Components Inc. (59213) Airborne Technologies Inc. (58730) International Precision Inc. (3H683) Lockheed Martin Corporation (98897) | |
377372-2 3773722 | 1560-00-084-0129 | Pan, Flap link, Inboard | General Characteristics Item Description: Aluminum alloy, 2024-0, QQ-A-250/5, 0.050 in. thk matl, 6.830 in. l, 3.040 in. W, 0.720 in. deep, applicable to C130 acft | Lockheed Martin Corporation (98897) | |
377376-3 3773763 | 1560-01-021-8428 | Pan Assembly, Cargo Light | III End Item Identification: Aircraft model C-130 | Lockheed Martin Corporation (98897) | |
377404-1 3774041 | 1560-01-564-5989 | Support, Structural Component, Air | Lockheed Martin Corporation (98897) | ||
377420-1 3774201 | 1560-00-501-0584 | Stop Assembly, Spring | General Characteristics Item Description: Steel 1095 annealed, MIL-S-7947 condition a | Lockheed Martin Corporation (98897) | |
377432-1 3774321 | 1560-00-874-2897 | Support, Checkout Va | Lockheed Martin Corporation (98897) | ||
377433-1 3774331 | 1560-00-874-2896 | Bracket, Pin Retainer | General Characteristics Item Description: 2.000 in. l, 1.720 in. W, 1.188 in. H | Lockheed Martin Corporation (98897) | |
37745 | 1560-00-361-0809 | Tank, Fuel, Aircraft | Special Features: Crash resistant, operating temp range M25 deg to 135 deg F, fuel usedin tank MIL-T-5624 grades JP-4 and JP-5 | American Fuel Cell and Coated (05476) |