Airframe Structural Components: 3F676-02805-1, 3G10215-102, 3G11557-101
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 3F676-02805-1 3F676028051 | 1560-00-866-7705 | Flange, Attachment, Molded Tank | Hole Diameter: 0.271 inches minimum and 0.291 inches maximum Active Face Design: Raised Basic Material: Aluminum alloy | American Fuel Cell and Coated (05476) | |
| 3F676-02813-1 3F676028131 | 1560-00-866-7687 | Fitting Assembly | III End Item Identification: Aircraft model T38 | American Fuel Cell and Coated (05476) | |
| 3F676-02815-1 3F676028151 | 1560-00-866-7689 | Fitting Assy | American Fuel Cell and Coated (05476) | ||
| 3F676-02816-1 3F676028161 | 1560-00-866-7690 | Flange, Attachment, Molded Tank | Hole Diameter: 0.271 inches minimum and 0.291 inches maximum Active Face Design: Raised Basic Material: Aluminum alloy | American Fuel Cell and Coated (05476) | |
| 3F90000-105 3F90000105 | 1560-00-656-3572 | Fitting, Quick Disconnect, Restrai | III End Item Identification: Aircraft model C141 General Characteristics Item Description: Steel, 2.497 in. O/a lg, 2.200 in. min, 2.215 in. max O/a od | Lockheed Martin Corporation (98897) | |
| 3F975-00941 3F97500941 | 1560-00-866-7704 | Flange, Attachment, Molded Tank | Hole Diameter: 0.271 inches minimum and 0.291 inches maximum Active Face Design: Raised Basic Material: Aluminum alloy | American Fuel Cell and Coated (05476) | |
| 3F975-00944 3F97500944 | 1560-00-866-7717 | Fitting Assembly | III End Item Identification: Aircraft model T38 | American Fuel Cell and Coated (05476) | |
| 3F975-01032 3F97501032 | 1560-00-866-7686 | Fitting Assy | American Fuel Cell and Coated (05476) | ||
| 3G10214-105 3G10214105 | 1560-00-911-2009 | Cover, Access | Material: Aluminum alloy 2024 Material Document AND Classification: QQ-A-250/5 fed spec single material response Hole Diameter: 0.218 inches minimum and 0.224 inches maximum | Lockheed Martin Corporation (98897) | |
| 3G10214-106 3G10214106 | 1560-00-911-2010 | Cover, Access | Material: Aluminum alloy 2024 Material Document AND Classification: QQ-A-250/5 fed spec single material response Hole Diameter: 0.218 inches minimum and 0.224 inches maximum | Lockheed Martin Corporation (98897) | |
| 3G10215-101 3G10215101 | 1560-00-927-5014 | Uplock Assembly, Main Landing Gea | General Characteristics Item Description: Appl C141 acft | Lockheed Martin Corporation (98897) | |
| 3G10215-102 3G10215102 | 1560-00-927-5015 | Uplock Assembly, Main Landing Gea | General Characteristics Item Description: Appl C141 acft | Lockheed Martin Corporation (98897) | |
| 3G11133-101 3G11133101 | 1560-00-202-5408 | Stop, Spring, Actuator | General Characteristics Item Description: Aluminum alloy 7075-T6, QQ-A-282, 2.562 in. O-a lg, 1.410 in. O-a diaof head, 2.312 in. shank lg | Lockheed Martin Corporation (98897) | |
| 3G11511-101 3G11511101 | 1560-00-019-5746 | Bracket Assembly, Door | III End Item Identification: Aircraft model C141 General Characteristics Item Description: Aluminum alloy, 5.300 in. O/a lg, 3.140 in. O/a W, 2.800 in. O/a H | Lockheed Martin Corporation (98897) | |
| 3G11525-109 3G11525109 | 1560-00-408-3744 | Torque Tube, Landing Gear Door | III End Item Identification: Aircraft model C141 | Lockheed Martin Corporation (98897) | |
| 3G11546-101 3G11546101 | 1560-00-019-5749 | Trunnion Pin, Bellc | General Characteristics Item Description: Steel, 4330, MIL-S-8699, hard chrome plate finish, 3.500 in. l, 2.4988 in. min, 2.4998 in. max dia, drilled thru 1.750 in. dia, counter-bored 1.700 in. deep, 2.000 in. dia, 0.2610 in. min, 0.2620 in. max dia thru hole at right angles to longitudinal center line 2.300 in. from end, applicable to C141 acft | Lockheed Martin Corporation (98897) | |
| 3G11546-103 3G11546103 | 1560-00-019-5750 | Trunnion Pin, Bellc | General Characteristics Item Description: Steel, 4330, MIL-S-8699, hard chrome plate finish, 4.200 in. l, 2.4988 in. min, 2.4998 in. max dia, drilled thru 1.750 in. dia, counter-bored 2.300 in. deep, 2.000 in. dia, 0.2610 in. min, 0.2620 in. max dia thru hole at right angles to longitudianl center line 2.400 in. from end, applicable to C141 acft | Beta Corp. (06671) Lockheed Martin Corporation (98897) P/M Engineering Co. Inc. (34374) | |
| 3G11547-103 3G11547103 | 1560-00-204-3700 | Link, Threaded, Ball Joint | General Characteristics Item Description: Steel 4140, MIL-S-5626, 8.590 in. min, 8.600 in. max lg, 1.625 in. od, 1-1/8-12 UNF-3B thd 2.200 in. lg both ends, 1.250 in. id center area | Lockheed Martin Corporation (98897) | |
| 3G11551-101 3G11551101 | 1560-00-868-5307 | Stop, Bogey Position | General Characteristics Item Description: Cres MIL-S-25043 annealed, stock size 0.090 by 1 by 2 in. | Lockheed Martin Corporation (98897) | |
| 3G11557-101 3G11557101 | 1560-00-868-5308 | Block, Radius, Door Bracket | General Characteristics Item Description: Aluminum alloy, QQ-A-282, 2.880 in. lg, 3.000 in. dia | Lockheed Martin Corporation (98897) |