NSN 9540-01-468-0130

Structural Angle

FSC: 9540 NIIN: 014680130

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Product Characteristics

NSN:

9540014680130

Demilitarization:

INC:

37017

Shelf Life:

N/A

Fabrication Method:

Extruded

Overall Height:

2.000 inches

Overall Width:

2.500 inches

Length:

12.000 inches

Left Side Flange Thickness:

0.320 inches

End Application:

B-2 aircraft

Basic Shape Style:

Angle

Fillet Radius Where Left Flange Joins Base Flange:

0.125 inches

Base Flange Thickness:

0.320 inches

First Tip Radius:

0.032 inches

First Tip Style:

Right quarter radius

Second Tip Radius:

0.032 inches

Second Tip Relationship To First Tip:

Not identical

Second Tip Style:

Upper radius

Left Inside Angle:

90.0 degrees

Part Name Assigned By Controlling Agency:

Angle, unequal legs and thicknesses

Heat Treatment:

T76511 solution heat treated

Material:

Aluminum alloy, ams-qq-a-200/15, alloy 7075

Material:

Aluminum alloy, ams-qq-a-200/15, alloy 7075

Part Numbers

AMS-QQ-A-200/15
SOCIETY OF AUTOMOTIVE ENGINEERS INC
CVC10001-331CJ
TRIUMPH AEROSTRUCTURES, LLC
QQ-A-200/15
FEDERAL SPECIFICATIONS

Shipping & Handling

HMIRS:

No MSDS. No hazardous material.

ESD:

No known electrostatic discharge.

Professional Distribution

ITAR Registered
DDTC Registered
HAZMAT Certified
AS9120 Quality Standards
100% Quality Inspections

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Cage Codes

SOCIETY OF AUTOMOTIVE ENGINEERS INC - 81343

TRIUMPH AEROSTRUCTURES, LLC - 80378

FEDERAL SPECIFICATIONS - 81348