NATO Stock Number
5340-00-449-1906
Sold in multiples of
25 EA
DEMIL
NO
Fabrication Method (non-core)
Stamped
Mounting Hole Type
Plain
First Leg Length
Between 0.741 inches and 0.783 inches
Second Leg Length
Between 0.997 inches and 1.027 inches
First Leg Hole Diameter
Between 0.200 inches and 0.210 inches
First Leg Thickness
Between 0.056 inches and 0.058 inches
Second Leg Thickness
Between 0.056 inches and 0.058 inches
Center Section Height
Between 0.410 inches and 0.430 inches
Center Section Width
Between 0.490 inches and 0.510 inches
Center Section Thickness
Between 0.056 inches and 0.068 inches
First Leg Width
Between 0.490 inches and 0.510 inches
First Leg Distance From Edge To Hole Center Along Width
0.250 inches
First Leg Distance From Edge To Hole Center Along Length
Between 0.195 inches and 0.205 inches
First Leg End Radius
Between 0.469 inches and 0.531 inches
First Leg Style
End radius
First Leg Hole Arrangement Style
One hole
Second Leg Relationship To First Leg
Identical
First Leg Angle
90.0 degrees
Second Leg Angle
90.0 degrees
Material
Steel comp 321
Material Specification
Ams 5510 assn standard single material response
Style Designator
Double angle
Fsc Application Data
Jet engine, aircraft