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9540-01-445-7866

Structural Angle

9540014457866 014457866 MIL-T-81556 CVC10002-96GA

A structural shape fabricated from a ferrous or nonferrous material and resembling the letter L in cross-sectional form. The edges may have a bulb, be rounded, and the inside corner may have a fillet. View more Structural Angle

9540-01-445-7866 ANGLE,STRUCTURAL 9540014457866 014457866

Managed by United States
NSN Created on 12 Jun 1997
Data Last Changed
January 2023
NATO Update Count
4
NATO Data Quality
AGTA Style E2 for 9540-01-445-7866 1/2
NSN 9540-01-445-7866 (Identification) 1/2
CMZY Style 1 for 9540-01-445-7866 2/2
NSN 9540-01-445-7866 (Identification) 2/2

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MIL-T-81556 CVC10002-96GA A structural shape fabricated from a ferrous or nonferrous material and resembling
(Identification) 1/2 NSN 9540-01-445-7866 (Identification) 2/2 - - 1.
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81556CVC10060-1012GACVC10060-1012GAX144 A specially shaped fabrication of ferrous or nonferrous MIL-T-81556
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9540-01-445-7866 Demil Restrictions 9540-01-445-7866

DEMIL: A | DEMILI: | CRITICALITY: X | HMIC: N | PMIC: A | EDC: | ADPEC: 0

9540-01-445-7866 is a Structural Angle that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.

9540-01-445-7866 End Users End Users 9540-01-445-7866

US Air Force (FNN5)
Effective Date:
1 Jun 2003
Former MOE Rule:
FGKZ

9540-01-445-7866 Manufacturers Approved Sources 9540-01-445-7866

9540-01-445-7866 Technical Data Datasheet 9540-01-445-7866

Characteristic
Specifications
FIIG
A13100
Base Flange Thickness [AJGP]
0.200 Inches Nominal
Basic Shape Style [AGTA]
Angle
Fabrication Method [AARN]
Extruded
Fillet Radius Where Left Flange Joins Base Flange [AJGL]
0.250 Inches Nominal
First Tip Style [CMZY]
Square End
Heat Treatment [HEAT]
Annealed
Material [MATT]
Titanium Alloy, Mil-T-81556, Comp Ab-1
Nondefinitive Spec/Std Data [ZZZT]
Composition Ab-1 (6Al-4V) And Condition Annealed
Left Inside Angle [CQHP]
76.0 Degrees Nominal
Left Side Flange Thickness [ADXL]
0.090 Inches Nominal
Length [ABRY]
12.000 Feet Nominal
Second Tip Relationship To First Tip [CNQJ]
Identical
Overall Height [ABKW]
1.500 Inches Nominal
Overall Width [ABMK]
1.900 Inches Nominal

9540-01-445-7866 Management Data Management Data 9540-01-445-7866

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
May 2009
Department of the Air Force (DF)
FT
Subscribe

Air Force Air Force

Budget:
S
57X3010 - Aircraft Replenishment Spares
Aggregation Code:
BQ
B-2 TSSP, NORTHROP GRUMMAN
Price Validation Code:
E
The current standard price is an estimated price.
Estimated Price challenges are allowed but follow procedures in para 60.b. (3) of section L of this manual.
This code will be changed to a P code upon notification of a contract price or this code will be changed to an updated code upon determination of a valid price.
Expendability
Recoverability
Repairability:
N
Expendable. Condemn at User. Stock Fund (except Munitions).

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9540-01-445-7866 Freight Data Freight Information 9540-01-445-7866

9540-01-445-7866 has freight characteristics managed by the Southwestern Power Administration.. 9540-01-445-7866 has a variance between NMFC and UFC when transported by rail and the description should be consulted.