1640-17-116-5624

Aviation Rod End Clevis

1640171165624 171165624 S521F3221201

An aircraft control cable system item with a forked part, having transverse hole(s) in each arm (prong) to accommodate a bolt, pin, or the like, and having a connection facility opposite the fork. It is designed to be attached to a shaft, rod, turnbuckle or the like by welding, threading, and/or pinning. May include provisions for locking. View more Aviation Rod End Clevis

1640-17-116-5624 CLEVIS,ROD END,AVIATION 1640171165624 171165624

Managed by Netherlands
NSN Created on 15 Apr 2004
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
1640-17-116-5624 CLEVIS,ROD END,AVIATION 1640171165624 171165624 1/1
NSN 1640-17-116-5624 (Generic Image) 1/1

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S521F3221201 An aircraft control cable system item with a forked part, having transverse hole(s) in
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2004 1640-17-116-9699 Aviation Rod End Clevis S521F3267201RNCC: 3 | RNVC: 2 | DAC: 2 6 Oct 2004 1640-17-116-5624

1640-17-116-5624 Demil Restrictions 1640-17-116-5624

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

1640-17-116-5624 is a Aviation Rod End Clevis

1640-17-116-5624 End Users End Users 1640-17-116-5624

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