Anodized per p3101, surface treat thds per p3210, 8.765 in. Bsc lg, 4.180 in. Bsc w, 0.305 min 0.314 max in. Diameter of 5 holes, 0.253 in. Diameter 9 holes, 0.223 in. Diameter 4 holes
A housing designed to inclose, support, and position bearings, shafts, gears, and other components required to drive various turbine engine driven accessories.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 6150-01-318-5770
NSN 6135-00-412-1687
NSN 6130-00-279-5066
NSN 6240-00-221-0859
NSN 6620-00-234-8918
NSN 6240-00-553-8891
NSN 6645-01-491-1815
NSN 5935-01-112-0075
NSN 6685-00-276-1308
NSN 6110-00-058-2792
NSN 6320-00-115-0883
NSN 6130-01-279-1098