Specification - Nut - Aircraft Self-Locking for 160,000 to 180,000 psi Tension Bolts
Document status: [ Not for New Design ]
TUBE ASSEMBLY, CONTROL, ALUMINUM ALLOY, WITH RIVETED THREADED ROD ENDS
Document status: [ Revised ]
Tube Assembly-Control Aluminum Alloy with Riveted Threaded Rod Ends
Document status: [ Revised ]
TUBE ASSEMBLY, CONTROL, ALUMINUM ALLOY, WITH RIVETED THREADED ROD ENDS
Document status: [ Revised ]
