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1.092in. and 1.105in.
1.188in.
F119-PW-100 engine on F-22
RING-Retaining, spiral
048-.052 thick
iron alloy, ams 5525, comp 660
iron alloy 660
ams 5525, comp 660 assn std single material response
1EA
Iron alloy 660
1.188 inches
1.092 inches minimum and 1.105 inches maximum
Schedule B number: 9606100000
Press-fasteners, snap-fasteners & press-studs & parts therefor
FSC 5325 ⁓ Fastening devices
Used on f119-pw-100 engine on f-22. 048-.052 thick ring-retaining, spiral 1.188" outside diameter 1.092" inside diameter
Nothing similar to this part number was found in our inventory
A resilient metal item, circular or nearly circular, which is designed to be inserted into an internal or external groove and retained by its own spring action, or it may have external prongs or projections designed to be inserted into a hole and retained by spring action of the prongs which grip by imbedding into the material. for items having internal prongs which perform the same function, see push on nut. it is used to keep and/or lock a part(s) in position, as a ball bearing on a shaft or in a housing. see also clip, retaining and pin, lock. excludes ring, connecting, round.