Airframe Structural Components: 10-20136-540, 102382-2, 10-2429-4
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 10-20136-540 1020136540 | 1560-00-778-5413 | Blanket Assembly, Duct | III End Item Identification: Aircraft model B52 General Characteristics Item Description: Fiberglass | The Boeing Company (81205) | |
| 102015-1 1020151 | 1560-00-113-7438 | Pipe, Exhaust | Special Features: Nickel-chromium-rion alloy, ams 5597 and ams 5664, 38.920 in. dia inlet end, 25.880 in. dia outlet end, 76.730 in. O/a lg, 52 holes 0.281 in. dia in inlet flange, 51 equally spaced on 38.420 in. bolt circle dia, and 1 hole offset Reference Number Differentiating Characteristics: Gas differentiated by source control dwg no. | Triumph Fabrications - SAN Diego (10234) | |
| 10-20205-502 1020205502 | 1560-00-676-0821 | Duct Assembly-Air Conditioning-H | III End Item Identification: B-52 Special Features: 2.500 in od | The Boeing Company (81205,82918) | |
| 10-205158-3R 102051583R | 1560-00-191-1418 | Fairing, Aircraft | III End Item Identification: T-33 Aircraft Location: Used on fillet assembly upper rear wing-fuselage Side FOR Which Designed: Right side | Lockheed Martin Corporation (98897) | |
| 10-205158-6L 102051586L | 1560-00-191-1417 | Fairing, Aircraft | III End Item Identification: T-33 Aircraft Location: Used on fillet assembly Aircraft Station Number: FS277.5 | Lockheed Martin Corporation (98897) | |
| 10-205158-6R 102051586R | 1560-00-191-1416 | Support, Structural Component, Air | Aircraft Mission Design Series: T-33 | Lockheed Martin Corporation (98897) | |
| 10-205756L 10205756L | 1560-00-191-1410 | Panel, Structural, Aircraft | Aircraft Mission Design Series: T-33 Special Features: U/a wing panel | Lockheed Martin Corporation (98897) | |
| 10-205756R 10205756R | 1560-00-191-1409 | Panel, Structural, Aircraft | Aircraft Mission Design Series: T-33 Special Features: U/a: wing panel | Lockheed Martin Corporation (98897) | |
| 1020716606 | 1560-01-168-4730 | Support, Aft Sensor | III End Item Identification: Acft model AV-8 General Characteristics Item Description: Aluminum alloy per MIL-A-21180, class 10, cond T61; 7.850 in. lg; 4.615 in. w; 2.490 in. H | PCC Structurals Groton (10207) | |
| 10210 | 1560-00-614-1060 | Clamp Assembly, Manifold | III End Item Identification: C131/T29 acft General Characteristics Item Description: C/O 1 ea spacer P/N 32115-23, 2 ea trunnion P/N 32115-24, 1 ea clamp assy P/N 32115-8 | Hamilton Sundstrand Corporation (55820) | |
| 1021054 | 1560-00-532-6635 | Support, Structural Component, Air | Special Features: Aluminum alloy | Cessna Aircraft Company (71379) Regal Air Inc. (4J976) | |
| 102111-1-16 102111116 | 1560-01-542-9390 | Hinge, Aircraft | III End Item Identification: F/A-18E/F pse: gsu test set Special Features: Nha test set electronic power; test point unit Material: Steel comp 304 | Testek Inc. (06659) | |
| 10-21P22-502 1021P22502 | 1560-01-074-5286 | Ramp Cockpit Floor | Aerospace Lighting Corp. (59579) | ||
| 10-21S22-502 1021S22502 | 1560-01-074-5287 | Ramp Cockpit Floor | Aerospace Lighting Corp. (59579) | ||
| 102205 | 1560-01-587-1799 | Support, Structural Component, Air | III End Item Identification: F-100 rear engine transportation trailer | Air Logistics Corporation (01413) | |
| 102382-1 1023821 | 1560-01-322-1727 | Strut, Aircraft | Specification/Standard Data: 54786-102382 manufacturers standard | BAE Systems Aerospace & Defense (54786) | |
| 102382-2 1023822 | 1560-01-322-1728 | Strut, Aircraft | Specification/Standard Data: 54786-102382 manufacturers standard | BAE Systems Aerospace & Defense (54786) | |
| 1023WM10040-511 1023WM10040511 | 1560-01-095-9096 | Fitting, Special | III End Item Identification: C-2A aircraft | Northrop Grumman Systems Corporation (61174) | |
| 10-2429-2 1024292 | 1560-00-628-0158 | Coupling, Flexible, Air Refueling | End Item Identification: Aircraft model C135 | The Boeing Company (81205) | |
| 10-2429-4 1024294 | 1560-00-923-1486 | Tube Coupling, Fuel | III End Item Identification: C-135 aircraft General Characteristics Item Description: Used on FLEX1BLE TUBE;C/O-TUBE-2, COLLAR-1, NAMEPLATE-1, DAMPER-2, BELLOWS-1, FLANGE-2;TUBE MATERIAL-0.025 thk cres 321 sh per ams 5510 | The Boeing Company (81205) |