Airframe Structural Components: 3P21721-103, 3P21770-101, 3P21773-109
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 3P21721-103 3P21721103 | 1560-01-269-3573 | Plate, Structural, Aircraft | III End Item Identification: C-141 Aircraft Location: Doubler | Lockheed Martin Corporation (98897) | |
| 3P21725-103 3P21725103 | 1560-01-345-2645 | Scupper, Oil, Forward Cowl | III End Item Identification: C-141 acft General Characteristics Item Description: Al alloy 2024-0 clad per QQ-A-362, T6 | Lockheed Martin Corporation (98897) | |
| 3P21726-101 3P21726101 | 1560-01-244-1871 | Scupper | III End Item Identification: C-141 acft General Characteristics Item Description: Aluminum alloy 2024-0; O/a dim. 14.000 by 22.000IN.; P/O cowl door assy;power plant | Lockheed Martin Corporation (98897) | |
| 3P21729-103 3P21729103 | 1560-00-204-6734 | Fitting, Cowl | III End Item Identification: Aircraft model C141 General Characteristics Item Description: Aluminum alloy, AMS4260 comp 356 cond T6, 2.860 in. O/a lg, 0.750 in. O/a W, 0.265 in. O/a thk, 2 mtg holes 0.218 in. min, 0.224 in. max dia | Lockheed Martin Corporation (98897) Rohr Inc. (51563) Space AGE Mfg Corp. (32483) | |
| 3P21736-101 3P21736101 | 1560-00-868-5321 | Stop Assembly, Door Access | General Characteristics Item Description: Consists of two /2/ tees, part no, s. 3P21736-103 and 3P21736-105, TWO/2/ washers, part no. AN960D10, one /1/ nut, part no. MS21042-3, one /1/SCREW, part no. NAS623-3-4, 1.500 in. lg, 2.280 in. W | Lockheed Martin Corporation (98897) | |
| 3P21737-101 3P21737101 | 1560-00-868-5322 | Stop Assembly, Door Access | General Characteristics Item Description: One /1/ angle 0.080 in. by 1.000 in. by 4.000 in. O/a dim, part NO.3P21737-103, one /1/ angle 0.080 in. by 2.000 in. by 5.000 in. O/a dim, part no. 3P21737-105, one /1/ nut, part no. MS21042-3, one /1/ screw, part no. NAS623-3-4, two /2/ washers, part no. AN960D10 | Lockheed Martin Corporation (98897) | |
| 3P21744-101 3P21744101 | 1560-00-424-9169 | Fitting, rod Support, Forward Cowl | General Characteristics Item Description: Aluminum alloy, QQ-A-268, temper T351, 2.600 in. lg | Lockheed Martin Corporation (98897) | |
| 3P21747-101 3P21747101 | 1560-00-110-3096 | Swivel Assembly, Cowl | General Characteristics Item Description: 1 swivel P/N 3P21748-103, 1 tee P/N 3P21747-105, 1 gusset P-N 3P21747-105 | Lockheed Martin Corporation (98897) | |
| 3P21751-101 3P21751101 | 1560-01-072-2659 | Fitting, Cowl Door | III End Item Identification: Acft C-141 | Inspirnetics Inc. (2X974) Lockheed Martin Corporation (98897) | |
| 3P21752-103 3P21752103 | 1560-00-572-2609 | Rod Assembly, Support, Forward Cow | III End Item Identification: Aircraft model C141 | Lockheed Martin Corporation (98897) | |
| 3P21753-104 3P21753104 | 1560-01-345-3900 | Frame, Aircraft | Aircraft Mission Design Series: C-141 Material: Aluminum alloy 2024 Aircraft Location: Aft cowl, lower | Lockheed Martin Corporation (98897) | |
| 3P21754-103 3P21754103 | 1560-01-268-2092 | Former, Aircraft | III End Item Identification: C-141 | Lockheed Martin Corporation (98897) | |
| 3P21754-104 3P21754104 | 1560-01-345-5051 | Frame, Aircraft | Aircraft Mission Design Series: C-141 Material: Aluminum alloy 2024 Aircraft Location: Aft cowl, lower | Lockheed Martin Corporation (98897) | |
| 3P21756-101 3P21756101 | 1560-01-345-9670 | Intercostal, Aircraft | Aircraft Mission Design Series: C-141 Material: Aluminum alloy 2024 Aircraft Location: Cowl door panel, lower, aft | Lockheed Martin Corporation (98897) | |
| 3P21769-101 3P21769101 | 1560-01-279-0082 | Plate, Structural, Aircraft | III End Item Identification: C-141 Aircraft Location: Stiffener, aft cowl | Lockheed Martin Corporation (98897) | |
| 3P21769-102 3P21769102 | 1560-01-020-8542 | Strip, Cowl | III End Item Identification: C141 a/C aircraft | Lockheed Martin Corporation (98897) | |
| 3P21770-101 3P21770101 | 1560-01-017-4362 | Stiffener, Aircraft | Aircraft Mission Design Series: C-141AA | Lockheed Martin Corporation (98897) | |
| 3P21770-102 3P21770102 | 1560-00-424-9167 | Stiffener, Engine Cowl | General Characteristics Item Description: Aluminum alloy, QQ-A-362, temper 0, 31 deg bend, 0.020 in. thk | Lockheed Martin Corporation (98897) Precision Metal-FAB Inc. (1CC84) Rohr Inc. (51563) | |
| 3P21771-102 3P21771102 | 1560-00-534-3927 | Stiffener, Aircraft | Aircraft Mission Design Series: C-141 | Lockheed Martin Corporation (98897) | |
| 3P21773-109 3P21773109 | 1560-01-345-5057 | Skin, Aircraft | Aircraft Mission Design Series: C-141 Material: Aluminum alloy 2024 Aircraft Location: Segment, duct, R-H, aft cowl | Lockheed Martin Corporation (98897) |