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rectangular
1.687in.
not casehardened
1.935in.
0.090in.
90 degree parallel
straight gap
helicopter, united technologies corp sikorsky aircraft division
internal
navy special project
gap opening 0.031 in. 0.281 in.
aluminum alloy, QQ-A-200/8, alloy 6061, T6 or aluminum alloy, QQ-A-200/8, 6061, T6 or aluminum alloy, QQ-A-225/8, alloy 6061, T6
aluminum alloy 6061 or aluminum alloy 6061 or aluminum alloy 6061
QQ-A-200/8, alloy 6061, T6 fed spec 1st material response and QQ-A-200/8, 6061, T6 fed spec 2nd material response and QQ-A-225/8, alloy 6061, T6 fed spec 3rd material response
anodize
anodized, MIL-A-8625, type 2, class 1
1EA
Aluminum alloy 6061 or aluminum alloy 6061 or aluminum alloy 6061
Straight gap
0.090 inches
1.935 inches
1.687 inches
Schedule B number: 9606100000
nmfc 095190
Press-fasteners, snap-fasteners & press-studs & parts therefor
FSC 5325 ⁓ Fastening devices
Used on helicopter,united technologies corp sikorsky aircraft division. anodize surface treated gap opening 0.031 in. 0.281 in. navy special project straight gap ring style 0.090" major thickness 1.935" outside diameter 1.687" inside diameter
1. | M1214-150BZ | Cage 08118 |
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.