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 5935-01-452-5184
NSN 5975-01-487-4379
NSN 6145-01-408-6103
NSN 5905-01-191-3941
NSN 6685-01-053-4337
NSN 6135-01-124-2376
NSN 5950-01-634-0677
NSN 6320-01-247-0898
NSN 6610-01-424-3213
NSN 5996-01-463-1685
NSN 2925-01-144-7106
NSN 6135-00-209-6918