NSN 9540-01-428-9028

Structural Angle

FSC: 9540 NIIN: 014289028

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Product Characteristics

NSN:

9540014289028

Demilitarization:

INC:

37017

Shelf Life:

N/A

Fabrication Method:

Extruded

Overall Height:

1.170 inches

Overall Width:

3.000 inches

Length:

12.000 feet

Left Side Flange Thickness:

0.143 inches

End Application:

B-2 bomber

Basic Shape Style:

Angle

Fillet Radius Where Left Flange Joins Base Flange:

0.120 inches

Base Flange Thickness:

0.113 inches

First Tip Style:

Square w/ inner and outer corner radii

First Tip Inner Radius:

0.030 inches

First Tip Outer Radius:

0.030 inches

Second Tip Relationship To First Tip:

Identical

Left Inside Angle:

91.0 degrees

Heat Treatment:

O-annealed

Material:

Aluminum alloy, qq-a-200/11, alloy 7075

Material:

Aluminum alloy, qq-a-200/11, alloy 7075

Nondefinitive Specification/std Data:

Alloy 7075 and temper 0

Part Numbers

AMS-QQ-A-200/11
SOCIETY OF AUTOMOTIVE ENGINEERS INC
CVC10001-305CA
TRIUMPH AEROSTRUCTURES, LLC
QQ-A-200/11
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