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9540-01-421-1992

Structural Angle

9540014211992 014211992 AMS-QQ-A-200/11 CVC10001-337CJ QQ-A-200/11

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

9540-01-421-1992 ANGLE,STRUCTURAL 9540014211992 014211992

Managed by United States
NSN Created on 3 Nov 1995
Data Last Changed
January 2023
NATO Update Count
8
NATO Data Quality
AGTA Style E2 for 9540-01-421-1992 1/2
NSN 9540-01-421-1992 (Identification) 1/2
CMZY Style 7 for 9540-01-421-1992 2/2
NSN 9540-01-421-1992 (Identification) 2/2

9540-01-421-1992 Stock and Availability Marketplace 9540-01-421-1992

9540-01-421-1992 Related Documents Related Documents 9540-01-421-1992 5+ Documents (More...)

AMS-QQ-A-200/11 CVC10001-337CJ QQ-A-200/11 A structural shape fabricated from a ferrous or nonferrous
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BEAM 200 AMS-QQ-A-200/ 11 / https // AMS-QQ-A -200/ 11 // https//www.nsnlookup.com https AMS-QQ-A
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9540-01-421-1992 Demil Restrictions 9540-01-421-1992

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

9540-01-421-1992 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.

9540-01-421-1992 End Users End Users 9540-01-421-1992

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

9540-01-421-1992 Manufacturers Approved Sources 9540-01-421-1992

9540-01-421-1992 Technical Data Datasheet 9540-01-421-1992

Characteristic
Specifications
FIIG
A13100
Base Flange Thickness [AJGP]
0.100 Inches Nominal
Basic Shape Style [AGTA]
Angle
Fabrication Method [AARN]
Extruded
Fillet Radius Where Left Flange Joins Base Flange [AJGL]
0.125 Inches Nominal
First Tip Inner Radius [CNBD]
0.020 Inches Nominal
First Tip Outer Radius [CNBJ]
0.020 Inches Nominal
First Tip Style [CMZY]
Square W/ Inner And Outer Corner Radii
Heat Treatment [HEAT]
T-76511 Solution Heat Treated
Material [MATT]
Aluminum Alloy, Qq-A-200/11, 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]
0.100 Inches Nominal
Length [ABRY]
12.000 Feet Nominal
Second Tip Relationship To First Tip [CNQJ]
Identical
Overall Height [ABKW]
1.000 Inches Nominal
Overall Width [ABMK]
1.250 Inches Nominal

9540-01-421-1992 Management Data Management Data 9540-01-421-1992

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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9540-01-421-1992 Freight Data Freight Information 9540-01-421-1992

9540-01-421-1992 has freight characteristics.. 9540-01-421-1992 has a variance between NMFC and UFC when transported by rail and the description should be consulted.