Capy Machine Shop Inc. NSN Parts: 160D611607-16 - 1128CE40133-14
FSC 1560 Airframe Structural Components
| MFG SKU | NSN | Item Name | Details | CAGE Code | RFQ |
|---|---|---|---|---|---|
| 160D611607-16 160D61160716 | 1560-01-077-8107 | Fitting, Wing Splice, Right hand | III End Item Identification: A-10A acft General Characteristics Item Description: Located on upper, inboard aft of wing station 110.00; made from forging 160D611607F; penetrant inspect per MIL-I-6866 type 1, a or b, and MIL-I-25135 group V or higher after machining | 0BVP9 | |
| A51P20623-1 A51P206231 | 1560-00-148-9067 | Flange Assembly | 0BVP9 | ||
| A51B52556-11 A51B5255611 | 1560-00-762-9644 | Flap Hinge, Inboard | General Characteristics Item Description: Aluminum, 18.790 in. lg, 1.040 in. W, 1.000 in. H | 0BVP9 | |
| A51B52556-13 A51B5255613 | 1560-00-762-9650 | Flap Hinge, Inboard | III End Item Identification: Aircraft, tomcat F-14 General Characteristics Item Description: Aluminum, 48.965 in lg, 1.040 in W, 1.000 in H | 0BVP9 | |
| A51B52556-15 A51B5255615 | 1560-00-762-9656 | Flap, Hinged, Inboard | General Characteristics Item Description: Aluminum, 19.705 in. lg, 1.040 in. W, 1.000 in. H | 0BVP9 | |
| 1128AB40345-2 1128AB403452 | 1560-00-243-4662 | Footrest Assy, Cockp | 0BVP9 | ||
| 160D112005-25 160D11200525 | 1560-01-246-9037 | Former, Aircraft | Aircraft Mission Design Series: A-10A Material: Aluminum alloy 7075 Material Document and Classification: QQ-A-250/13-0 fed spec single material response | 0BVP9 | |
| 160D412026-49 160D41202649 | 1560-01-532-5455 | Former, Aircraft | Aircraft Mission Design Series: A-10A aircraft Special Features: Annealed cres sheet; U/O -13 Material: Steel comp 301 | 0BVP9 | |
| 160D414036-3 160D4140363 | 1560-01-049-0329 | Former, Aircraft | Aircraft Mission Design Series: A-10A End Item Identification: Aircraft, A-10A | 0BVP9 | |
| 160D611628-16 160D61162816 | 1560-01-189-1522 | Former, Aircraft | Aircraft Mission Design Series: Acft model A-10A Material: Aluminum alloy 2024 Aircraft Location: Lwr rear spar | 0BVP9 | |
| A51B20058-24 A51B2005824 | 1560-01-360-9589 | Former, Aircraft | Aircraft Mission Design Series: F-14 Material: Aluminum alloy 2024 Overall Width: 6.000 inches nominal | 0BVP9 | |
| A51B52112-42 A51B5211242 | 1560-01-272-9222 | Former, Aircraft | III End Item Identification: Aircraft tomcat F-14 Aircraft Mission Design Series: F-14 Material: Aluminum alloy 2024 | 0BVP9 | |
| A51B97123-17 A51B9712317 | 1560-01-218-0997 | Former, Rudder | 0BVP9 | ||
| A51B20660-4 A51B206604 | 1560-01-039-0802 | Frame Assembly, Fair | General Characteristics Item Description: Aluminum alloy type 2024-T6 GM20153 fscm 26512 | 0BVP9 | |
| A51B20660-3 A51B206603 | 1560-01-039-0800 | Frame Assembly, Fairing | General Characteristics Item Description: Aluminum alloy type 2024-T6 GM20153 fscm 26512 | 0BVP9 | |
| A51B47560-11 A51B4756011 | 1560-00-781-5319 | Frame, Access Hole | Material: Aluminum alloy 2024 overall Material Document and Classification: QQ-A-250/4 fed spec single material response overall Overall Length: 8.500 inches nominal | 0BVP9 | |
| A51B47561-11 A51B4756111 | 1560-00-781-5323 | Frame, Access Hole | Material: Aluminum alloy 2024 overall Material Document and Classification: QQ-A-250/4 fed spec single material response overall Overall Length: 8.500 inches nominal | 0BVP9 | |
| A51F11527-11 A51F1152711 | 1560-01-239-7215 | Frame, Access Hole | 0BVP9 | ||
| 1128CE40133-12 1128CE4013312 | 1560-00-482-4230 | Frame, Cockpit | 0BVP9 | ||
| 1128CE40133-14 1128CE4013314 | 1560-00-482-4232 | Frame, Cockpit | 0BVP9 |
