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 6130-01-361-1285
NSN 6650-01-523-7026
NSN 5895-01-010-3102
NSN 6135-01-222-0703
NSN 5835-00-174-7763
NSN 5835-01-426-6573
NSN 6620-01-106-3553
NSN 6685-01-029-3773
NSN 5930-01-334-8177
NSN 5945-00-283-4256
NSN 6645-01-556-5263
NSN 5990-00-043-4048