T.O. 2j-f110-14; fan fram assembly; no. 3 bearing; 2nd end dia. 7.400-7.401
A rigid metallic item, generally circular. It may be formed of segmented arcs. It is designed to prevent leakage of air in an engine, gas turbine, aircraft. It may be of various cross-sectional shapes. It may have mounting facilities. It may act as a spacer but its primary function is as an air seal.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 4140-00-100-4563
NSN 5945-01-143-3575
NSN 6610-01-642-9557
NSN 5855-01-232-9440
NSN 6650-01-336-5859
NSN 5930-01-040-9845
NSN 6645-00-070-0896
NSN 6105-00-280-2808
NSN 7035-01-191-2822
NSN 6150-01-447-2940
NSN 5999-00-647-1141
NSN 6320-01-021-6633