Serving our customers with quality and safety first.
B-1B aircraft
dimensions inin. 2.565 long, 0.385 stem diameter, 7/16-20 thread per MS33649-4, 0.400 below 0.680 hex head; 0-rings per M25988/1-004, dielectric strengh 500 vac min., insulation resistance 1 megohb min.at 500 vdc, pressure 3000 psi max. operating, temerature -65 to +400 degree f
1EA
Schedule B number: 9027803500
nmfc 061700
Physical analysis instruments and apparatus, except using optical radiations
FSC 2995 ⁓ Miscellaneous engine accessories, aircraft
Note-items classified in this class must be specifically designed for use with aircraft or quided missile primemovers only.
Excluding exhaust system; (fsc 1560); jet engine hydraulic reservoirs (fsc 2840); jet engine oil tanks (fsc 2840); electrical starters (fsc 2925); cockpit mounted control quadrants (fsc 1680); aircraft engine covers (fsc 1730).
Used on b-1b aircraft. dimensions in" 2.565 long, 0.385 stem diameter, 7/16-20 thread per MS33649-4, 0.400 below 0.680 hex head; 0-rings per M25988/1-004, dielectric strengh 500 vac min., insulation resistance 1 megohb min.at 500 vdc, pressure 3000 psi max. operating, temerature -65 to +400 degree f
Nothing similar to this part number was found in our inventory
A sensing device designed to detect the presence of metallic foreign matter in fuel, hydraulic, or lubricating systems. detection completes an integral electrical circuit that actuates an external signal and/or actuate the engine to stop.