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 6620-00-586-6460
NSN 5915-01-148-1891
NSN 5905-01-223-1010
NSN 4140-00-274-3333
NSN 4140-00-257-5215
NSN 5990-00-495-2859
NSN 5945-01-352-0663
NSN 6220-01-005-8038
NSN 5950-00-529-0599
NSN 6240-01-182-3002
NSN 6645-01-335-9183
NSN 6220-01-197-0486