Model: X9241585-10

B-1b aircraft

Cres bar alloy ph13-8m0; per ams 5629; 2.250 in. Center to center distance between fulcrum and 1st end arm end hole; 0.375 in. 1st arm end radius; 2.745 in. Center to center distance between fulcrum and 2nd arm end hole; 0.440 in. 2nd arm end radius; 0.437 in. Min to 0.438 in. Max 1st arm end hole dia; 0.500 in. Min to 0.501 in. Max 2nd arm end hole dia; 4.976 in. 1st arm thickness; 0.500 in. 1st arm slot width; 0.666 in. 2nd arm horizontal slot width; 0.870 in. 1st arm end thickness; 1.042 in. 2nd end thickness; fulcrum bore provided; bore diameter 0.875 in.

Uplock assembly, nose landing gear

1680-01-364-4094

X9241585-10

Crank Assembly,bell