NATO Stock Number
5340-00-390-1631
Sold in multiples of
1 EA
DEMIL
DEMIL/MLI
Fabrication Method (non-core)
Machined
First Leg Length
0.975 inches
Second Leg Length
2.092 inches
End Application
W/s: engine, aircraft, f100-pw-200 (f-16a/b/c/d); support equipment, c-5 aircraft; aircraft, eagle f-15; engine, aircraft, f100-pw-100 (f-15a/b/c/d); aircraft, f-16; engine, aircraft, f100 pw220 (f-15c/d/e)
Second Leg Width
1.882 inches
First Leg Hole Diameter
Between 0.276 inches and 0.286 inches
Second Leg Hole Diameter
Between 0.216 inches and 0.226 inches
Second Leg Distance From Edge To Hole Center Along Width
0.250 inches
Second Leg Distance From Edge To Hole Center Along Length
0.250 inches
First Leg Thickness
Between 0.045 inches and 0.055 inches
Second Leg Thickness
Between 0.045 inches and 0.055 inches
First Leg Width
1.882 inches
First Leg Corner Radius
0.250 inches
First Leg Distance Between Hole Centers Along Width
1.382 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
Second Leg End Radius
0.250 inches
First Leg Style
Corner radius
First Leg Hole Arrangement Style
Two holes
Second Leg Style
End radius and tapered
Second Leg Hole Arrangement Style
One hole
Second Leg Relationship To First Leg
Not identical
First Leg Angle
90.0 degrees
Material
Titanium alloy
Material Specification
Ams 4911 assn standard single material response
Style Designator
Angle