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heat exchanger; nsn 2935010852864; fscm 12536; p/n 12117-000, e/i F16A/b aircraft
4.500 in. nom installed lg; .710 in. max dia, valve remain seated for all fuel pressures below 60 psid, temp range minus 65 deg f to plus 225 deg f, fluids JP-4 and JP-5 to MIL-T-5624, housing, guide and collar; aluminum 6061-T6 ams 4117 or 2024-T4 ams 4120; piston, piston cap, valve plug and spring retainer type 303 stainless steel ams 5640; SPRING-302 stainless steel ams 5688; spring P1N-420 stainless steel; SLEEVE-Viton; top washer and WASHER-Polytetrafluoroethylene ams 365; seal WASHER-Fluorosilicone elastomer MIL-R-25988, type 2, class 3 housing, guide collar; clear anodize MIL-A-8625, type ii, class 1 or 2, no dichromate seal; piston, piston cap, valve plug and spring RETAINER-Passivate MIL-S-5002, spring and spring PIN-Passivate MIL-STD-171
engine cooling system components, aircraft
1EA
Schedule B number: 8481809050
nmfc 051080
Other taps, cocks, valves, etc.
FSC 2935 ⁓ Engine system cooling components, aircraft prime moving
Note-this class includes only cooling system components for aircraft and/or guided missile prime movers only.
Excluding cooling system components not specifically designed for use with aircraft engines.
Used on heat exchanger; nsn 2935010852864; fscm 12536; p/n 12117-000,e/i f16a/b aircraft. 4.500 in. nom installed lg; .710 in. max dia, valve remain seated for all fuel pressures below 60 psid, temp range minus 65 deg f to plus 225 deg f, fluids jp-4
1. | 11-283 | Cage 27195 |