Model #L5200119-001

Flight control pull rod (NSN 1680-01-162-6438)

End Application
B-1b aircraft
General Description
Consists of -011 subassembly; 1 bushing; 1 clevis; 1 bolt; 1 collar; the deviation from straightness shall not exceed one degree from axis of the pull rod and .060 inch in any 12.00 inch length when the -011 subassembly positioned and supported so that its own weight minimizes axial distortion and thereis no tension applied
Fsc Application Data
Aircraft accessory equipment
Description
Pull Rod,flight Control
Cage Code
43999

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Updated: 05/29/2024