Airframe Structural Components: 3T53069-103, 3T60005-103, 3T60067-103
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 3T53069-103 3T53069103 | 1560-00-989-2468 | Weight, Balance, Elevator | General Characteristics Item Description: Uranium, 5.250 in. lg, 1.600 in. W, 0.066 in. thk, 2 mtg holes 0.200 in. min, 0.206 in. max dia, 3.250 in. C to C, 0.37 lb weight | Lockheed Martin Corporation (98897) | |
| 3T53069-105 3T53069105 | 1560-00-989-2469 | Weight, Balance, Elevator | General Characteristics Item Description: Uranium, 4.250 in. lg, 1.600 in. W, 0.066 in. thk, 2 mtg holes 0.200 in. min, 0.206 in. max dia, 2.250 in. C to C, 0.030 lb weight | Lockheed Martin Corporation (98897) | |
| 3T53070-101 3T53070101 | 1560-00-989-2455 | Weight, Balance, Elevator | General Characteristics Item Description: Uranium, 3.660 in. lg, 1.350 in. W, 0.050 in. thk, 2 mtg holes 0.198 in. min, 0.204 in. max dia, 1.650 in. C to C, 0.17 lb weight | Lockheed Martin Corporation (98897) | |
| 3T53070-103 3T53070103 | 1560-00-989-2459 | Weight, Balance, Elevator | General Characteristics Item Description: Uranium, 4.940 in. lg, 1.350 in. W, 0.050 in. thk, 2 mtg holes 0.198 in. min, 0.204 in. max dia, 2.940 in. C to C, 0.23 lb weight | Lockheed Martin Corporation (98897) | |
| 3T53071-101 3T53071101 | 1560-00-989-2433 | Weight, Balance Elevator | General Characteristics Item Description: Uranium, 3.780 in. lg, 0.850 in. W, 0.060 in. thk, 2 mtg holes 0.200 in. min, 0.206 in. max dia, 1.780 in. C to C, 0.13 lb weight | Lockheed Martin Corporation (98897) | |
| 3T53071-103 3T53071103 | 1560-00-989-2445 | Weight, Balance Elevator | General Characteristics Item Description: Uranium, 4.750 in. lg, 0.850 in. W, 0.060 in. thk, 2 mtg holes 0.200 in. min, 0.206 in. max dia, 2.750 in. C to C, 0.16 lb weight | Lockheed Martin Corporation (98897) | |
| 3T53071-105 3T53071105 | 1560-00-989-2454 | Weight, Balance Elevator | General Characteristics Item Description: Uranium, 4.510 in. lg, 0.850 in. W, 0.060 in. thk, 2 mtg holes 0.200 in. min, 0.206 in. max dia, 2.510 in. C to C, 0.15 lb weight | Lockheed Martin Corporation (98897) | |
| 3T60005-103 3T60005103 | 1560-00-789-4681 | Cover, Access | Material: Aluminum alloy 2024 Material Document AND Classification: QQ-A-250/5, T3 fed spec single material response Surface Treatment: Chromate | Honeycomb Company of America Inc. (99115) Lockheed Martin Corporation (98897) Pratt & Whitney H A C Inc. (1N454) | |
| 3T60013-102 3T60013102 | 1560-00-789-9842 | Fairing, Skirt, Assembly | III End Item Identification: Aircraft model C141 | Lockheed Martin Corporation (98897) | |
| 3T60035-118 3T60035118 | 1560-00-738-3231 | Strip, Attaching, Bul | General Characteristics Item Description: Aluminum alloy, 2024-T42, QQ-A-362, 25.0 in. lg, 5.0 in. W0.080 in. thk | Lockheed Martin Corporation (98897) | |
| 3T60035-119 3T60035119 | 1560-00-738-3232 | Strip, Attachment | III End Item Identification: C-141A aircraft General Characteristics Item Description: Used on stub-bullet, forward; MATL-2024-O clad QQ-A-362 temper o; DIMENSION-24.000 in. lg, 2.000 in., 0.080 in. thk | Hughes Missile Systems Co. (14170) Lockheed Martin Corporation (98897) Raytheon Company (15090) | |
| 3T60035-120 3T60035120 | 1560-00-738-3233 | Strip, Attachment | III End Item Identification: C-141A aircraft General Characteristics Item Description: Used on stub-bullet, forward; MATL-2024-O clad QQ-A-362 temper o; DIMENSION-24.000 in. lg, 2.000 in. W, 0.080 in. thk | Lockheed Martin Corporation (98897) | |
| 3T60035-123 3T60035123 | 1560-00-074-4231 | Stub Assembly, Leading Edge | General Characteristics Item Description: Aluminum alloy, 2024-T3, QQ-A-362 | Lockheed Martin Corporation (98897) | |
| 3T60035-124 3T60035124 | 1560-00-074-4232 | Stub Assembly, Leading Edge | General Characteristics Item Description: Aluminum alloy, 2024-T3, QQ-A-362 | Lockheed Martin Corporation (98897) | |
| 3T60036-101 3T60036101 | 1560-00-066-7971 | Fairing, Aircraft | Aircraft Mission Design Series: C-141 | Lockheed Martin Corporation (98897) | |
| 3T60036-109 3T60036109 | 1560-00-066-7971 | Fairing, Aircraft | Aircraft Mission Design Series: C-141 | Lockheed Martin Corporation (98897) | |
| 3T60049-112 3T60049112 | 1560-00-911-2015 | Cover, Access | Material: Aluminum alloy 7075 Material Document AND Classification: QQ-A-250/12 fed spec single material response Hole Diameter: 0.193 inches minimum and 0.201 inches maximum | Lockheed Martin Corporation (98897) | |
| 3T60049-115 3T60049115 | 1560-00-911-2020 | Cover, Access | Material: Aluminum alloy 7075 Material Document AND Classification: QQ-A-250/12 fed spec single material response Hole Diameter: 0.193 inches minimum and 0.201 inches maximum | Lockheed Martin Corporation (98897) | |
| 3T60049-116 3T60049116 | 1560-00-911-2015 | Cover, Access | Material: Aluminum alloy 7075 Material Document AND Classification: QQ-A-250/12 fed spec single material response Hole Diameter: 0.193 inches minimum and 0.201 inches maximum | Lockheed Martin Corporation (98897) | |
| 3T60067-103 3T60067103 | 1560-01-271-5520 | Rib, Airfoil | III End Item Identification: C-141 Special Features: Consists of 1 rib, 40 nut; nha 3T00001 Aircraft Location: Aft bullet rib instl | Lockheed Martin Corporation (98897) |