NATO Stock Number
5340-00-153-1011
Sold in multiples of
10 EA
DEMIL
DEMIL/MLI
First Leg Length
1.307 inches
Second Leg Length
Between 1.769 inches and 1.779 inches
End Application
W/s: engine, aircraft, tf-33-p-7 (c-141a/b); engine, aircraft tf33-pw-102 (c-135e, ec-135h/k/p); engine, aircraft tf33-p-3/5/9 (c/ec-135, b-52h); engine, aircraft tf-30
First Leg Hole Diameter
Between 0.216 inches and 0.226 inches
Second Leg Hole Diameter
Between 0.276 inches and 0.286 inches
Second Leg Distance Between Hole Centers Along Width
1.173 inches
Second Leg Distance From Edge To Hole Center Along Width
0.250 inches
Second Leg Distance From Edge To Hole Center Along Length
Between 0.200 inches and 0.210 inches
First Leg Thickness
Between 0.056 inches and 0.062 inches
Second Leg Thickness
Between 0.056 inches and 0.062 inches
First Leg Distance From Edge To Hole Center Along Width
0.250 inches
First Leg Distance From Edge To Hole Center Along Length
0.250 inches
First Leg End Radius
0.250 inches
First Leg Style
End radius and tapered
First Leg Hole Arrangement Style
One hole
Second Leg Hole Arrangement Style
Two holes
First Leg Angle
90.0 degrees
Material
Steel comp 410
Material Specification
Ams 5504 assn standard single material response
Style Designator
Angle
