FSC 1560 Airframe Structural Components: 1560-00-193-3560, 1560-00-193-3850, 1560-00-193-4114
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 1560-00-193-3560 1560001933560 | 12P12010-807 | Spike, Air Inlet, Aircraft | Aircraft Mission Design Series: F-111 | Lockheed Martin Corporation (81755) | |
| 1560-00-193-3561 1560001933561 | 12P12010-808 | Spike, Air Inlet, Aircraft | Aircraft Mission Design Series: F-111 | Lockheed Martin Corporation (81755) | |
| 1560-00-193-3748 1560001933748 | 1209906 | Shaft, Carburetor Air Valve | III End Item Identification: C-47/C-117 aircraft General Characteristics Item Description: Made from bar C.m. steel 4130 per QQ-S-684;DIMENSIONS-1.343 in. total length, SHAFT-1.218 in. l., THREAD-1/4-28 NF-3, 0.239 in. l. | Boeing Company, The (88277, 18355) | |
| 1560-00-193-3773 1560001933773 | 368387-25 | Door, Aircraft | III End Item Identification: C-130 Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5 T3 fed spec single material response | Lockheed Martin Corporation (98897) | |
| 1560-00-193-3846 1560001933846 | 5115205 | Flap, Wing Landing | III End Item Identification: Acft model C-47 | Boeing Company, The (18355, 88277) | |
| 1560-00-193-3847 1560001933847 | 5115205-1 | Flap, Wing Landing | III End Item Identification: Acft model C-47 | Boeing Company, The (18355, 88277) | |
| 1560-00-193-3848 1560001933848 | 5115205-18 | Hinge, Aircraft | Aircraft Mission Design Series: C-47 Aircraft Location: Flap, wing | Boeing Company, The (18355, 88277) | |
| 1560-00-193-3850 1560001933850 | 511521023N 5115210-23 5115210-23N | Support, Structural Component, Air | III End Item Identification: Aircraft model C-47 | Boeing Company, The (88277, 18355) | |
| 1560-00-193-3852 1560001933852 | 88-13088 | Plate, Wing Center s | Boeing Company, The (43999) | ||
| 1560-00-193-3924 1560001933924 | 205426-2 | Crank, Canopy Torque | Lockheed Martin Corporation (98897) | ||
| 1560-00-193-3925 1560001933925 | 205426-3 | Crank Assembly, Cano | Lockheed Martin Corporation (98897) | ||
| 1560-00-193-3927 1560001933927 | 205443 | Plate, Structural, Aircraft | Aircraft Mission Design Series: T-33 Overall Length: 3.000 inches nominal Overall Width: 0.880 inches nominal | Lockheed Martin Corporation (98897) | |
| 1560-00-193-3930 1560001933930 | 140-43050 | Shaft, Engine Control | III End Item Identification: Acft model F-86 | Boeing Company, The (43999) | |
| 1560-00-193-3957 1560001933957 | 205002L | Link, Forward Post | III End Item Identification: Acft model T-33 General Characteristics Item Description: Steel, 8630, MIL-S-6050 and MIL-S-18728 | Lockheed Martin Corporation (98897) | |
| 1560-00-193-3958 1560001933958 | 205002R | Link, Forward Post | III End Item Identification: Acft model T-33 General Characteristics Item Description: Steel, 8630, MIL-S-6050 and MIL-S-18728 | Lockheed Martin Corporation (98897) | |
| 1560-00-193-3959 1560001933959 | 204788 | Boot Assembly, Seal | III End Item Identification: Aircraft model T33 General Characteristics Item Description: Cloth, fiber glass, vinyl coated, 4.300 in. lg, 4.300 in. W, 2.300 in. D, 4 mounting holes 0.195 in. dia | Lockheed Martin Corporation (98897) | |
| 1560-00-193-3960 1560001933960 | 204787-2 | Support Assembly, La | Lockheed Martin Corporation (98897) | ||
| 1560-00-193-4026 1560001934026 | 1119758 | Plug, Wing Flap Indicator | General Characteristics Item Description: Steel, 1.000 in. lg, 0.265 in. dia | Boeing Company, The (18355, 88277) | |
| 1560-00-193-4105 1560001934105 | 178250 | Balance Weight, Aileron | Special Features: Lead per QQ-L-171, 5.000 in lg, 2.300 in wd, 0.750 in thk;used T-33 | Lockheed Martin Corporation (98897) | |
| 1560-00-193-4114 1560001934114 | 178377 | Plate, Defroster Air | General Characteristics Item Description: Aluminum alloy, QQ-A-200/3, 0.250 in. thk, 1.000 in. W, 1.000 in. LG0.170 in. dia mounting holes 4 places 0.73/ in. apart, 0.188 in. min, 0.189MAX dia hole drilled thru center | Lockheed Martin Corporation (98897) |