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9540-01-431-5255

Structural Angle

9540014315255 014315255 CVC10000-505CJ CVC10000-505CJX144 QQ-A-200/15 AMS-QQ-A-200/15

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

9540-01-431-5255 ANGLE,STRUCTURAL 9540014315255 014315255

Managed by United States
NSN Created on 14 May 1996
Data Last Changed
January 2023
NATO Update Count
8
NATO Data Quality
AGTA Style E2 for 9540-01-431-5255 1/3
NSN 9540-01-431-5255 (Identification) 1/3
CMZY Style 2 for 9540-01-431-5255 2/3
NSN 9540-01-431-5255 (Identification) 2/3
CNQK Style 4 for 9540-01-431-5255 3/3
NSN 9540-01-431-5255 (Identification) 3/3

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https/ 6 EA NS Request Quotation AMS-QQ-A-200/15 AMS-QQ-A-200/15 https/ 6 EA NS Request AMS-QQ-A-200
Structural Angle 9540014315255 014315255 ANGLE,STRUCTURAL 6 EA NS Request Quotation AMS-QQ-A-200
https/ 6 EA NS Request Quotation AMS-QQ-A-200/15 AMS-QQ-A-200/15 https/ 6 EA NS Request AMS-QQ-A-200
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9540-01-431-5255 Demil Restrictions 9540-01-431-5255

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

9540-01-431-5255 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.

9540-01-431-5255 End Users End Users 9540-01-431-5255

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

9540-01-431-5255 Manufacturers Approved Sources 9540-01-431-5255

9540-01-431-5255 Technical Data Datasheet 9540-01-431-5255

Characteristic
Specifications
FIIG
A13100
Base Flange Thickness [AJGP]
0.094 Inches Nominal
Basic Shape Style [AGTA]
Angle
Fabrication Method [AARN]
Extruded
Fillet Radius Where Left Flange Joins Base Flange [AJGL]
0.094 Inches Nominal
First Tip Radius [AJJB]
0.094 Inches Nominal
First Tip Style [CMZY]
Right Quarter Radius
Heat Treatment [HEAT]
T-76511 Solution Heat Treated
Material [MATT]
Aluminum Alloy, Qq-A-200/15, Alloy 7075
Nondefinitive Spec/Std Data [ZZZT]
Alloy 7075 And Temper T76511
Left Inside Angle [CQHP]
90.0 Degrees Nominal
Left Side Flange Thickness [ADXL]
0.094 Inches Nominal
Length [ABRY]
12.000 Feet Nominal
Second Tip Relationship To First Tip [CNQJ]
Not Identical
Second Tip Radius [CMZZ]
0.094 Inches Nominal
Second Tip Style [CNQK]
Upper Radius
Overall Height [ABKW]
0.750 Inches Nominal
Overall Width [ABMK]
0.750 Inches Nominal

9540-01-431-5255 Management Data Management Data 9540-01-431-5255

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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9540-01-431-5255 Freight Data Freight Information 9540-01-431-5255

9540-01-431-5255 has freight characteristics.. 9540-01-431-5255 has a variance between NMFC and UFC when transported by rail and the description should be consulted.