NATO Stock Number
5340-00-914-3751
Sold in multiples of
1 EA
DEMIL
NO
First Leg Length
Between 1.125 inches and 1.155 inches
Second Leg Length
Between 1.325 inches and 1.357 inches
End Application
Engine, aircraft j-52
Second Leg Width
Between 1.240 inches and 1.260 inches
Second Leg Corner Radius
Between 0.109 inches and 0.141 inches
First Leg Hole Diameter
Between 0.276 inches and 0.286 inches
Second Leg Distance From Edge To Hole Center Along Width
Between 0.620 inches and 0.630 inches
Second Leg Distance From Edge To Hole Center Along Length
Between 0.272 inches and 0.287 inches
Second Leg Slot Length
Between 0.340 inches and 0.350 inches
Second Leg Slot Width
Between 0.276 inches and 0.286 inches
First Leg Thickness
Between 0.071 inches and 0.085 inches
Second Leg Thickness
Between 0.071 inches and 0.085 inches
First Leg Width
Between 1.240 inches and 1.260 inches
First Leg Distance From Edge To Hole Center Along Width
Between 0.234 inches and 0.266 inches
First Leg Distance From Edge To Hole Center Along Length
Between 0.234 inches and 0.266 inches
First Leg End Radius
Between 0.234 inches and 0.266 inches
First Leg Style
End radius and tapered
First Leg Hole Arrangement Style
One hole
Second Leg Style
Corner radius
Second Leg Hole Arrangement Style
One slot
Second Leg Relationship To First Leg
Not identical
First Leg Angle
78.5 degrees
Material
Steel comp 410
Material Specification
Ams 5504 assn standard single material response
Style Designator
Angle
