1680-01-364-4094
Find complete technical information, availability, and procurement data for: 1680-01-364-4094
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includes 1 bushing; heat treat to cond h1000; per mil-h-6875 special features, b-1b aircraft end item identification, cres bar alloy ph13-8m0; per ams 5629; 2.250 in. center to center distance between fulcrum and 1st end arm end hole; 0.375 in. 1st arm end radius; 2.745 in. center to center distance between fulcrum and 2nd arm end hole; 0.440 in. 2nd arm end radius; 0.437 in. min to 0.438 in. max 1st arm end hole dia; 0.500 in. min to 0.501 in. max 2nd arm end hole dia; 4.976 in. 1st arm thickness; 0.500 in. 1st arm slot width; 0.666 in. 2nd arm horizontal slot width; 0.870 in. 1st arm end thickness; 1.042 in. 2nd end thickness; fulcrum bore provided; bore dia 0.875 in. general characteristics item description, uplock assy,nose landing gear fsc application data
Product Characteristics
Below you’ll find the complete technical specifications and performance data for this part, including material details and compliance information.
- End Item Identification
- b-1b aircraft
- Special Features
- includes 1 bushing; heat treat to cond h1000; per mil-h-6875
- General Characteristics Item Description
- cres bar alloy ph13-8m0; per ams 5629; 2.250 in. center to center distance between fulcrum and 1st end arm end hole; 0.375 in. 1st arm end radius; 2.745 in. center to center distance between fulcrum and 2nd arm end hole; 0.440 in. 2nd arm end radius; 0.437 in. min to 0.438 in. max 1st arm end hole dia; 0.500 in. min to 0.501 in. max 2nd arm end hole dia; 4.976 in. 1st arm thickness; 0.500 in. 1st arm slot width; 0.666 in. 2nd arm horizontal slot width; 0.870 in. 1st arm end thickness; 1.042 in. 2nd end thickness; fulcrum bore provided; bore dia 0.875 in.
- Fsc Application Data
- uplock assy,nose landing gear
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|---|---|
| X9241585-10 | Bell Crank Assembly |
FAQs
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When the NSN 1680-01-364-4094 was assigned to the Federal Catalog?
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