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9540-01-071-8254
Structural Angle
9540010718254 010718254 AMS-QQ-A-200/3 K10A64T8511 AND10133-1202 10133-1202 MS14284E125 ASTM B221 QQ-A-200/3 9540PL0905372
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
November 2023
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- , ASTM AMS-QQ-A-200/3 - - , ASTM B221 QQ-A AMS-QQ-A -200 /3 https//www.nsnlookup.com /fsg-95/fsc-9540
AMS-QQ-A -200/3 https AMS-QQ-A -200 ,ASTM B221 ,ASTM B221 QQ-A - AMS-QQ-A -200/3 - ,ASTM B221 QQ-A-200
Quotation ASTM-B-221 ANGLE,STRUCTURAL 2 FT NS Request Quotation ASTM-B221 ANGLE,STRUCTURAL 151 FT NS
Request Quotation QQ-A-200/3 ANGLE,STRUCTURAL 1 FT NS Request Quotation Updated Every Day 9540-00-169
- ,ASTM B221 ANGLE,STRUCTURAL - ,ASTM AMS-QQ-A - 200/3 - - , ASTM B221 QQ-A AMS-QQ-A - ,ASTM B221
- ,ASTM B221 ANGLE,STRUCTURAL - ,ASTM AMS-QQ-A - 200/3 - - , ASTM B221 QQ-A AMS-QQ-A B221 - ,ASTM
-200/3 - QQ-A-200 AMS-QQ-A-200/3 https AMS-QQ-A -200/3 https AMS-QQ-A -200 ,ASTM B221 ,ASTM B221 QQ-A
- AMS-QQ-A -200/3 - ,ASTM B221 QQ-A-200 AMS-QQ-A AMS-QQ-A-200/3 https https//www.nsnlookup.com /fsg-95
- ,ASTM B221 QQ-A- 200 AMS-QQ-A-200/3 - ,ASTM B221 QQ-A - AMS-QQ-A - AMS-QQ-A AMS-QQ-A -200/3 - ,ASTM
AMS-QQ-A-200/3 - ,ASTM B221 QQ-A - AMS-QQ-A - AMS-QQ-A AMS-QQ-A -200/3 - ,ASTM ,ASTM B221 QQ-A- 200 AMS-QQ-A
Restrictions 9540-01-071-8254
9540-01-071-8254 is a Structural Angle that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. 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.
End Users 9540-01-071-8254
- US Air Force (FGGI)
- Effective Date:
- 1 Mar 2006
- Former MOE Rule:
- FGKZ
- US Navy (N9BZ)
- Effective Date:
- 1 Mar 2006
- Former MOE Rule:
- N9ZD
- Supplementary Collaborators:
- GTHD
- Poland (WP01)
- Effective Date:
- 1 Apr 2011
- Brazil (YA01)
- Effective Date:
- 1 Oct 2000
- Singapore (YJ01)
- Effective Date:
- 1 Apr 1991
- Italy (ZR01)
- Effective Date:
- 1 Dec 2007
- Denmark (ZS01)
- Effective Date:
- 1 Mar 2002
- Greece (ZU01)
- Effective Date:
- 1 Sep 2011
Approved Sources 9540-01-071-8254
- Part Number
- Manufacturer
- Status
- MS14284E125
- Manufacturer
- 96906 - Military Standards (Active)
- Definitive Standard
- Definitive Standard
- AMS-QQ-A-200/3
- 0U583 - Sae International (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- K10A64T8511
- 81755 - Lockheed Martin Corporation (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- AND10133-1202
- 99237 - Airforce-Navy Aeronautical Design (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- 10133-1202
- 29321 - Transtar Metals Corp (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- ASTM B221
- 81346 - American Society For Testing And (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-200/3
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- QQ-A-200/3
- 81348 - Federal Specifications Promulgated (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- 9540PL0905372
- 9009H - Jednolity Indeks Materialowy - (Active)
- NATO Reference
- NATO Reference
- 10133-1202
- 14304 - L3harris Technologies, Inc. (Active)
- Advisory Reference
- Advisory Reference
Datasheet 9540-01-071-8254
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Angle
- Base Flange Thickness [AJGP]
- 0.094 Inches Nominal
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Left Flange Joins Base Flange [AJGL]
- 0.188 Inches Nominal
- First Tip Radius [AJJB]
- 0.094 Inches Nominal
- First Tip Style [CMZY]
- Right Quarter Radius
- Heat Treatment [HEAT]
- T-8511 Solution Heat Treated
- Material [MATT]
- Aluminum Alloy Ams-Qq-A-200/3, Alloy 2024
- Nondefinitive Spec/Std Data [ZZZT]
- Alloy 2024, Temper T8511
- Left Side Flange Thickness [ADXL]
- 0.094 Inches Nominal
- Left Inside Angle [CQHP]
- 90.0 Degrees Nominal
- Length [ABRY]
- 10.000 Feet Minimum And 12.000 Feet Maximum
- Second Tip Radius [CMZZ]
- 0.094 Inches Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Not Identical
- Second Tip Style [CNQK]
- Upper Radius
- Overall Height [ABKW]
- 1.250 Inches Nominal
- Overall Width [ABMK]
- 1.250 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.276 Pounds Per Linear Foot
Weapon Systems (WSDC) 9540-01-071-8254
DLA Procurement Analysis 9540-01-071-8254
- Last Stock Position:
- 223 In Stock
- DLA Administrative Lead Time:
- Subscribe
- DLA Production Lead Time:
- Subscribe
Management Data 9540-01-071-8254
Navy
- Cognizance:
- 9B
- Navy-owned stocks of DLA material
Naval Inventory Control Point, Mechanicsburg
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Freight Information 9540-01-071-8254
9540-01-071-8254 has freight characteristics managed by the Southwestern Power Administration.It has a National Motor Freight Classification (NMFC) of 013140. A Sub NMFC of X. It has a NMFC Description of ALUMINUM ANGLES. 9540-01-071-8254 is rated as class 60 when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 05390 which rates the freight between FCL and LCL. 9540-01-071-8254 has a variance between NMFC and UFC when transported by rail and the description should be consulted. It has a Water Commodity Code (WCC) of 576 for ocean manifesting and military sealift. 9540-01-071-8254 is not classified as a special type of cargo when transported by water. 9540-01-071-8254 is not a consolidation and does not exceed 84" in any dimension. It should be compatible with a standard 72" Aircraft Cargo Door when transported by air.
Packaging Data 9540-01-071-8254
- Responsible Activity
- Packaging Data Source
- Primary Inventory Control Activity (PICA)
- --
Item Pack Level (Unpackaged)
- Item Size
- Item Weight
- Characteristics
- Weight/Dimensions Category
- Fragility
- Item Preservation
- Item Weight
- --
- --
- Plated/Coated Item
- Over 10lb
- Less than 85G
- Special Requirement
- --
Unit Pack Level (Packaged)
- Quantity per Pack
- Unit Size
- Unit Weight
- Unit Cube
- Preservation Method
- Cleaning/Drying
- Unit Size
- 1
- --
- --
- --
- --
- --
- --
- Preservation Material
- Wrapping Material
- Cushioning/Dunnage
- Cushioning Thickness
- Container
- Special Marking
- Wrapping Material
- --
- --
- --
- --
- No Requirement
- No special marking
- --
Intermediate Pack Level
- Quantity of Unit Packs
- Container
- --
- No Requirement
Contracting Technical Data File (CTDF) 9540-01-071-8254 October 2021
Criticality and Quality
- Critical Item Code:
- X
- Flight Safety:
- Life Support:
- Certified Samples:
- Serialization:
- First Article Test (FAT):
- Certificate of Quality Compliance:
- Production Lot Testing:
- Special Testing:
- Qualified Products List (QPL):
Commercial Properties
- Government Furnished Material:
- Government Furnished Tooling:
- Government Furnished Property:
- Price Evaluation Code:
- Diminshing Manufacturing Sources:
- Warranty:
- Commerical Off The Shelf (COTS):
- End Item Application:
- Auctioning Candidate:
- Source of Procurement:
- Contract Option:
Restrictions
- Boeing Rights Guard:
- Export Controlled:
- Controlled Technical Data Package (TDP):
- Restricted Technical Data Package (TDP):
- Contains Classified Material
- Weapons System Indicator Code (WSIC):
- F
Packaging Requirements
- Packaging Determination Table:
- Packaging Review Code:
- N
- Special Packaging Instruction Number (SPIN):
- Special Packaging Instruction Number Revision:
- Special Packaging Instruction Number Date:
- Pallet Reference Number Required: