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 5990-00-956-9130
NSN 5910-01-197-2690
NSN 5905-01-043-5021
NSN 6685-01-052-3118
NSN 5960-01-526-2323
NSN 5835-01-261-9878
NSN 5930-01-081-1341
NSN 5910-01-023-0078
NSN 6685-01-311-0385
NSN 6650-01-501-1825
NSN 6145-01-196-7895
NSN 5965-00-255-3889