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 5935-01-371-3005
NSN 7035-00-834-2090
NSN 6145-01-192-6416
NSN 6130-01-176-4400
NSN 6150-01-065-0481
NSN 5965-01-089-8579
NSN 5905-01-462-1214
NSN 7035-00-360-2008
NSN 5910-00-006-3942
NSN 6145-01-439-8041
NSN 6105-00-485-5939
NSN 6610-01-624-1188