Airframe Structural Components: 3F23052-101, 3F23055-110, 3F28059-113
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 3F23052-101 3F23052101 | 1560-01-118-1040 | Fitting, Air Refueling | III End Item Identification: C141B acft General Characteristics Item Description: Matl 7075-T7351 QQ-A-250/12; usedon rear adaptor, aerial refueling | Lockheed Martin Corporation (98897) | |
| 3F23055-105 3F23055105 | 1560-01-118-5296 | Skin, Aircraft | Aircraft Mission Design Series: C-141B Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5 fed spec single material response | Lockheed Martin Corporation (98897) | |
| 3F23055-106 3F23055106 | 1560-01-118-5297 | Skin, Aircraft | Aircraft Mission Design Series: C-141B Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5 T42 fed spec single material response | Lockheed Martin Corporation (98897) | |
| 3F23055-107 3F23055107 | 1560-01-118-5298 | Skin, Aircraft | Aircraft Mission Design Series: C-141B Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5 T3 fed spec single material response | Lockheed Martin Corporation (98897) | |
| 3F23055-109 3F23055109 | 1560-01-118-5265 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-141B Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5 T42 fed spec single material response | Lockheed Martin Corporation (98897) | |
| 3F23055-110 3F23055110 | 1560-01-118-5266 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-141B Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5 T42 fed spec single material response | Lockheed Martin Corporation (98897) | |
| 3F23056-101 3F23056101 | 1560-01-118-1039 | Fitting Assembly, Canted | III End Item Identification: C141B acft General Characteristics Item Description: C/O 1 ea fitting P/N 3F23051-101, 1 ea fitting P/N 3F23052-101, 1 ea fitting P/N 3F23032-101, 1 ea fitting assy P/N 3C00508-101, 1 ea 3C00508-102, used on fuselage station 442.50 | Lockheed Martin Corporation (98897) | |
| 3F23058-101 3F23058101 | 1560-01-073-9453 | Fitting, Emergency Exit Release | III End Item Identification: C-141 acft General Characteristics Item Description: 3.630 in. lg, 0.790 in. thk, 7075-T7351 QQ-A-250/12 | Lockheed Martin Corporation (98897) | |
| 3F23061-103 3F23061103 | 1560-01-073-9454 | Panel Assembly, Fairing | III End Item Identification: C-141 acft | Lockheed Martin Corporation (98897) | |
| 3F23062-103 3F23062103 | 1560-01-073-6348 | Panel Assembly, Fairing | III End Item Identification: Acft C-141 General Characteristics Item Description: Consists of skin 1, doubler 4, frame 3 | Lockheed Martin Corporation (98897) | |
| 3F23063-103 3F23063103 | 1560-01-073-6354 | Panel Assembly, Fairing | III End Item Identification: Acft C-141 General Characteristics Item Description: Consists of frame 3, doubler 3, skin 1 | Lockheed Martin Corporation (98897) | |
| 3F23063-113 3F23063113 | 1560-01-097-2395 | Panel Assembly, Fairing | III End Item Identification: C-141 acft General Characteristics Item Description: C/O skin, doublers 3, frames 3; matl al alloy, 2024-T3 clad; used on fuselage station 548.00E to 557.10E | Lockheed Martin Corporation (98897) | |
| 3F23064-101 3F23064101 | 1560-01-118-5271 | Support, Structural Component, Air | III End Item Identification: C141B acft Special Features: Matl 2024-0 clad QQ-A-250/5 T42; used on fuselage station 404.00 | Lockheed Martin Corporation (98897) | |
| 3F23065-103 3F23065103 | 1560-01-118-5264 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-141B Special Features: Cond 0, T42 Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 3F23065-123 3F23065123 | 1560-01-073-6349 | Panel Assembly, Fairing | III End Item Identification: Acft C-141 General Characteristics Item Description: Panel 20.000 in. W, 19.000 in. lg, 0.100 in. thk, 2024-O clad QQ-A-250/5 1, nut(dome) 2 | Lockheed Martin Corporation (98897) | |
| 3F23067-101 3F23067101 | 1560-01-073-6350 | Collar, Emergency Exit Release | III End Item Identification: Acft C-141 General Characteristics Item Description: Matl 2024-T351 al alloy rod, spec QQ-A-225/6, size 0.625 in. dia, 1.000 in. lg | Lockheed Martin Corporation (98897) | |
| 3F23068-101 3F23068101 | 1560-01-073-6351 | Rod, Emergency Exit Release | III End Item Identification: Acft C-141 General Characteristics Item Description: Stock 0.438 in. dia, 5.000 in. lg, matl MIL-S-6758 cond F-4 125 ksi min | Lockheed Martin Corporation (98897) | |
| 3F23069-101 3F23069101 | 1560-01-073-6352 | Rod, Emergency Exit Release, Aft | III End Item Identification: Acft C-141 General Characteristics Item Description: Stock 0.1875 in. dia, 7.000 in. lg, matl per MIL-S-6758 cond F-4 125 ksi min | Lockheed Martin Corporation (98897) | |
| 3F28059-112 3F28059112 | 1560-00-269-5187 | Support, Structural Component, Air | Aircraft Mission Design Series: C-141 | Lockheed Martin Corporation (98897) | |
| 3F28059-113 3F28059113 | 1560-00-261-6132 | Support, Structural Component, Air | Aircraft Mission Design Series: C-141 | Lockheed Martin Corporation (98897) |