Airframe Structural Components: 175542-2, 175543-1, 175619R
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 175542-2 1755422 | 1560-01-574-7071 | Panel Assembly, Airc | Northrop Grumman Systems Corporation (26512) | ||
| 175543-1 1755431 | 1560-01-574-1609 | Panel Assembly, Airc | Northrop Grumman Systems Corporation (26512) | ||
| 175543-2 1755432 | 1560-01-574-1607 | Panel Assembly, Airc | Northrop Grumman Systems Corporation (26512) | ||
| 175550 | 1560-00-088-2206 | Release Assembly, Manual | III End Item Identification: Aircraft model F111 | Curtiss-Wright Controls Inc. (71791) | |
| 175550-2 1755502 | 1560-00-696-1315 | Connector, Stick Ass | III End Item Identification: T-33 | Lockheed Martin Corporation (98897) | |
| 175557 | 1560-00-574-0827 | Driver, Manual Release | General Characteristics Item Description: Steel, ams 5643, 0.860 in. lg, 0.622 in. min, 0.624 in. max od, 0.389 in. min, 0.396 in. max dia internal drive W/0.376 in. nom sq drive adaption, 0.375 in. min, 0.377 in. max dia through center holes at 90.0 deg to drive hole 0.504 in. from end, 1 ea 0.094 in. dia through center hole 0.112 in. from end, 1 ea 0.010 in. min, 0.015 in. max deep index line on end centered on lesser dia hole | Curtiss-Wright Controls Inc. (71791) | |
| 175558 | 1560-00-575-9110 | Adapter, Ground Lock | Curtiss-Wright Controls Inc. (71791) | ||
| 175581 | 1560-00-123-4627 | Coupling, Manual Release | III End Item Identification: Aircraft model F111 General Characteristics Item Description: Steel, 1.080 in. lg, 0.830 od | Curtiss-Wright Controls Inc. (71791) | |
| 175585 | 1560-00-122-6780 | Fitting, Structural Component, Air | Aircraft Mission Design Series: T-33 | Lockheed Martin Corporation (98897) | |
| 175593 | 1560-00-692-1319 | Retainer, Aileron to | Lockheed Martin Corporation (98897) | ||
| 175605-2L 1756052L | 1560-01-160-1362 | Socket eng Trun Spt | III End Item Identification: T-33 | Lockheed Martin Corporation (98897) | |
| 175605L | 1560-00-122-6774 | Socket Assembly, Engine Trunnion | General Characteristics Item Description: Assembly consists of three bushings and an aluminum alloy rough forging | Lockheed Martin Corporation (98897) | |
| 175605R | 1560-00-122-6775 | Socket Assembly, Engine Trunnion | General Characteristics Item Description: Assembly consists of three bushings and an aluminum alloy rough forging | Lockheed Martin Corporation (98897) | |
| 175608 | 1560-00-122-6536 | Cap, Engine Trunnion | III End Item Identification: Aircraft model T33 General Characteristics Item Description: Aluminum alloy, QQ-A-225/6 | Lockheed Martin Corporation (98897) | |
| 175608-2 1756082 | 1560-01-159-7281 | Support, Structural Component, Air | Aircraft Mission Design Series: T-33 | Lockheed Martin Corporation (98897) | |
| 17561-103B 17561103B | 1560-01-566-7727 | Duct Assembly, Bleed Air | III End Item Identification: C-5A mod Special Features: Nha 4A59100; max 6.37 lbs;make from titanium MIL-T-9046 type I comp b or ams 4941;LOCATED owfb sta 80.93 THRU149.02;USED on outer wing bleed air manifold duct assembly | Arrowhead Products Corporation (70628) | |
| 175612 | 1560-00-122-6537 | Ball Assembly, Engine | III End Item Identification: Aircraft model T33 | Lockheed Martin Corporation (98897) | |
| 175615 | 1560-00-047-3899 | Brace Assembly | III End Item Identification: T-33 aircraft General Characteristics Item Description: Used for forward engine mount;c/O-tube, FITTING-2, 175610 terminal, nut, washer;tube made from 1.0 od X .065 8630 steel tube per MIL-T-6732, type 1, cond n;total LENGTH-33.25 in | Lockheed Martin Corporation (98897) | |
| 175618 | 1560-00-437-2462 | Socket Assembly | III End Item Identification: T-33 | Lockheed Martin Corporation (98897) | |
| 175619R | 1560-00-121-2021 | Support, Structural Component, Air | Aircraft Mission Design Series: T-33A | Lockheed Martin Corporation (98897) |