NSN 9540-00-596-3016

Structural Angle

FSC: 9540 NIIN: 005963016

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Product Characteristics

NSN:

9540005963016

Demilitarization:

INC:

37017

Shelf Life:

N/A

Fabrication Method:

Extruded

Overall Height:

0.875 inches

Overall Width:

0.875 inches

Left Side Flange Thickness:

0.062 inches

Basic Shape Style:

Angle

Fillet Radius Where Left Flange Joins Base Flange:

0.047 inches

Base Flange Thickness:

0.062 inches

Weight Per Unit Measure:

0.130 pounds per linear foot

First Tip Style:

Square end

Second Tip Relationship To First Tip:

Identical

Left Inside Angle:

90.0 degrees

Heat Treatment:

T-3511 solution heat treated

Material:

Aluminum alloy ams-qq-a-200/3, alloy 2024

Material:

Aluminum alloy ams-qq-a-200/3, alloy 2024

Nondefinitive Specification/std Data:

Alloy, 2024, temper t6511

Part Numbers

1E241
BOEING COMPANY, THE
23299
ALUMINUM CO OF AMERICA
AMS-QQ-A-200/3
SOCIETY OF AUTOMOTIVE ENGINEERS INC
ASTM B221
AMERICAN SOCIETY FOR TESTING AND
CVC2071
TRIUMPH AEROSTRUCTURES, LLC
QQ-A-200/3
FEDERAL SPECIFICATIONS
QQ-A-267
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

BOEING COMPANY, THE - 43999

ALUMINUM CO OF AMERICA - 01634

SOCIETY OF AUTOMOTIVE ENGINEERS INC - 81343

AMERICAN SOCIETY FOR TESTING AND - 81346

TRIUMPH AEROSTRUCTURES, LLC - 80378

FEDERAL SPECIFICATIONS - 81348