Remote Control Levers - Page 26 of 32
798 part numbers
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5 spline quantity
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t-38 aircraft end application
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splined bore type
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2.600 inches center to center distance between link and shaft holes
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1.055 inches link end thickness
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f-18 fighter aircraft end application
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c-17 globemaster aircraft end application
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steel material
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aisi 4130 assn standard single material response material specification
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0.375 inches bore diameter
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c-17 globemaster aircraft end application
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plain straight bore type
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plastic material
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c-17 globemaster aircraft end application
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plain straight bore type
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plastic material
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c-17 globemaster aircraft end application
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plastic material
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f-15 aircraft end application
49334
NSN 1680-01-391-1748
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b-2 aircraft end application
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dwg name - tube assembly, aa door special features
49301
NSN 1680-01-391-2987
49337
NSN 1680-01-391-4736
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b-2a aircraft; valve, brake meter end application
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aluminum alloy material
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anodize surface treatment
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clevis link end, securing hol (s) shaft end style designator
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b-2 bomber end application
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plain straight bore type
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handle-external jettison special features
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steel material
9475795-20
NSN 1680-01-393-7650
Cross Reference:
160D521120-24
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a-10a aircraft end application
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ah-64 apache helicopter end application
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aluminum alloy material
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one hole flat link end, clamp type shaft end style designator
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a10 aircraft end application
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harrier av-8 end application
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b-1b aircraft end application
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c-17 globemaster aircraft end application
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lever, adjustment-windshield wiper system special features
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steel material
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aircraft f/a 18 end application
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lever remote control special features
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ejection seat end application
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beechcraft bonanza acft end application
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aircraft, model s76 end application
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aircraft, model s76 end application
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used on f-18 aircraft end application