Valve Pressure Relief Fuel NSN Part Sourcing

ASAP Part Services, owned and operated by ASAP Semiconductor, has over 6 billion parts inventoried. This includes new, old, used, and obsolete parts, such as 559A6D40, C491. As an ISO 9001:2015 certified and FAA AC 00-56B accredited company, we go to great lengths to ensure we are delivering quality parts. We partner exclusively with reliable manufacturers such as Circor Aerospace Inc. Our team provides superior quality assurance testing for III End Item Identification: F111 aircraft engine fuel system General Characteristics Item Description: Aluminum alloy W/anodized finish, 2 gpm at 55 psid rated flow, pressures, operating 60 psi, proof 120 psi, burst 180 psi, 30 psi min reset pressure, 45 psi max cracking pressure, 0.810 in. O/a lg, 0.650 in. dia top end, 0.810 in. dia hex, end fitting inlet per MS33656E6, thd and 0.350 in. lg, III End Item Identification: F111 aircraft engine fuel system General Characteristics Item Description: Aluminum alloy W/anodized finish, 2 gpm at 55 psid rated flow, pressures, operating 60 psi, proof 120 psi, burst 180 psi, 30 psi min reset pressure, 45 psi max cracking pressure, 0.810 in. O/a lg, 0.650 in. dia top end, 0.810 in. dia hex, end fitting inlet per MS33656E6, thd and 0.350 in. lg and more. So if you are in need of Valve Pressure Relief Fuel or any other NSN parts, submit an Instant RFQ and receive a quote in as little as 15 minutes.

Manufacturers for Valve Pressure Relief Fuel
circor aerospace inc

Valve Pressure Relief Fuel Part Numbers List

Part Number NSN Details QTY RFQ
559A6D40 2915-00-949-1948 iii end item identification: f111 aircraft engine fuel system general characteristics item description: aluminum alloy w/anodized finish, 2 gpm at 55 psid rated flow, pressures, operating 60 psi, proof 120 psi, burst 180 psi, 30 psi min reset pressure, 45 psi max cracking pressure, 0.810 in. o/a lg, 0.650 in. dia top end, 0.810 in. dia hex, end fitting inlet per ms33656e6, thd and 0.350 in. lg Avl RFQ
C491 2915-00-949-1948 iii end item identification: f111 aircraft engine fuel system general characteristics item description: aluminum alloy w/anodized finish, 2 gpm at 55 psid rated flow, pressures, operating 60 psi, proof 120 psi, burst 180 psi, 30 psi min reset pressure, 45 psi max cracking pressure, 0.810 in. o/a lg, 0.650 in. dia top end, 0.810 in. dia hex, end fitting inlet per ms33656e6, thd and 0.350 in. lg Avl RFQ


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