Bell Cranks - Page 35 of 59
1465 part numbers
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flight safety critical aircraft part special features
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aluminum alloy material
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cadmium surface treatment
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2.541 inches bore length
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4.954 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
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steel material
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raised face pivot hole, clevis both ends style designator
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between 1.374 inches and 1.376 inches bore diameter
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4.140 inches bore length
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steel material
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cadmium surface treatment
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1.687 inches bore diameter
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steel material
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cadmium and zinc surface treatment
128L10034-6
NSN 1680-01-089-4042
Cross Reference:
128L10034-4
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fulcrum bore and fulcrum shaft features provided
1128L40501-5
NSN 1680-01-089-4044
Cross Reference:
1128L40501-1, 1128L40501-3, 1128L40501-5/-6
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fulcrum shaft features provided
1128L40501-6
NSN 1680-01-089-4046
Cross Reference:
1128L40501-2, 1128L40501-4
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fulcrum shaft features provided
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between 1.790 inches and 1.820 inches bore diameter
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4.190 inches bore length
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7.940 inches 1st end center to center distance between fulcrum and arm end hole/slot/ball
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cadmium surface treatment
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clevis ends twisted, other arm offset style designator
128L10034-5
NSN 1680-01-090-9311
Cross Reference:
128L10034-3
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fulcrum bore and fulcrum shaft features provided
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1.687 inches bore diameter
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steel material
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5.000 inches 2nd end center to center distance between fulcrum and arm end hole/slot/ball
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aluminum alloy material
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between 1.374 inches and 1.376 inches bore diameter
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4.140 inches bore length
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steel material
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cadmium surface treatment
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blackhawk uh-60 end application
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blackhawk uh-60 airframe end application
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uh-60 blackhawk airframe/aux power unit end application
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ch-47 airframe unit end application
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ch-47, rotary wing aircraft end application
414C1131
NSN 1680-01-105-8792
Cross Reference:
414C1131-1
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ch-47, rotary wing aircraft end application