Airframe Structural Components: 3P49013-101, 3P60502-101, 3P61500-108
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 3P49013-101 3P49013101 | 1560-00-052-8329 | Elbow, Hose, Air Duct | General Characteristics Item Description: Fiberglass, laminated, 6 ply, 0.060 in. wall thk, 90.0 deg, 5.250 in. radius bend, 3.380 in. id, 26.250 in. lg, plain end 1ST leg, single outside bead, 8.250 in. lg 2ND leg | Lockheed Martin Corporation (98897) | |
| 3P49014-101 3P49014101 | 1560-00-052-8330 | Duct, Fuel Pump Cooling | III End Item Identification: Aircraft model C-141 General Characteristics Item Description: Glass fabric, laminated | Lockheed Martin Corporation (98897) | |
| 3P49017-111 3P49017111 | 1560-00-052-8335 | Cover, Dust, Exhaust | III End Item Identification: Aircraft model no. C-141 | Lockheed Martin Corporation (98897) | |
| 3P53061-101A 3P53061101A | 1560-01-097-3799 | Stiffener, Skin | III End Item Identification: C-5A acft General Characteristics Item Description: Matl T1-6AL-4V annealed MIL-T-9046 per DS30009; 3.370 in. lg 2.020 in. w; used on pylon apron station 127.0; titanium alloy material; do not use cadmium plated tools on this item Criticality Code Justification: TEXT | Lockheed Martin Services Inc. (1WL60) | |
| 3P60502-101 3P60502101 | 1560-00-069-7866 | Fairing Assembly, Access | General Characteristics Item Description: Aluminum alloy, QQ-A-250-5 | Lockheed Martin Corporation (98897) | |
| 3P60503-101 3P60503101 | 1560-00-759-7083 | Fairing, Aircraft | Aircraft Mission Design Series: C-141 Material: Aluminum alloy Material Document and Classification: QQ-A-250/5 fed spec single material response | Lockheed Martin Corporation (98897) Rohr Inc. (51563) | |
| 3P60504-101 3P60504101 | 1560-00-759-7084 | Fairing, Aircraft | Aircraft Mission Design Series: C-141 Material: Aluminum alloy Material Document and Classification: QQ-A-250/5 fed spec single material response | Lockheed Martin Corporation (98897) | |
| 3P60504-113 3P60504113 | 1560-01-267-9551 | Former, Aircraft | III End Item Identification: C-141 | Lockheed Martin Corporation (98897) | |
| 3P60504-114 3P60504114 | 1560-01-267-9550 | Former, Aircraft | III End Item Identification: C-141 | Lockheed Martin Corporation (98897) | |
| 3P60504-116 3P60504116 | 1560-01-295-7805 | Support, Structural Component, Air | Aircraft Mission Design Series: C-141 Special Features: U/a: angle Aircraft Location: Pylon, leading edge | Lockheed Martin Corporation (98897) | |
| 3P60504-119 3P60504119 | 1560-01-137-2637 | Support, Structural Component, Air | Aircraft Mission Design Series: C-141 Special Features: Opposite to P/N 3P60504-120 Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 3P60504-120 3P60504120 | 1560-01-137-2638 | Support, Structural Component, Air | Aircraft Mission Design Series: C-141 Special Features: Opposite to P/N 3P60504-119 Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 3P60504-121 3P60504121 | 1560-01-137-2639 | Support, Structural Component, Air | Aircraft Mission Design Series: C-141 Special Features: U/a:retainer Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 3P60504-127 3P60504127 | 1560-01-293-2709 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-141 Special Features: T42 clad; doubler Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 3P61000-101 3P61000101 | 1560-00-789-4668 | Fairing, Aircraft | Aircraft Mission Design Series: C-130 Material: Aluminum alloy Material Document and Classification: QQ-A-250/5 fed spec single material response | Aero Components Inc. (59213) Lockheed Martin Corporation (98897) | |
| 3P61000-135 3P61000135 | 1560-01-134-4549 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-141B Special Features: Opposite to P/N 3P61000-136 Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 3P61000-136 3P61000136 | 1560-01-134-4548 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-141B Material: Aluminum alloy 2024 Aircraft Location: Fairing-trailing edge, inboard pylon | Lockheed Martin Corporation (98897) | |
| 3P61100-101 3P61100101 | 1560-00-789-4669 | Fairing, Aircraft | Aircraft Mission Design Series: C-141 Material: Aluminum alloy Material Document and Classification: QQ-A-250/5 fed spec single material response | Lockheed Martin Corporation (98897) | |
| 3P61500-107 3P61500107 | 1560-01-269-3583 | Support, Structural Component, Air | Aircraft Mission Design Series: C-141 | Lockheed Martin Corporation (98897) | |
| 3P61500-108 3P61500108 | 1560-01-269-4100 | Support, Structural Component, Air | Aircraft Mission Design Series: C-141 Overall Length: 3.000 inches nominal Overall Width: 1.000 inches nominal | Lockheed Martin Corporation (98897) |