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9540-01-071-3509
Structural Angle
9540010713509 010713509 AMS10134-0501 MS14284E009 K10A5T3511 AMS-QQ-A-200/3 AND10134-0501/QQ-A-200/3-T3511 10134-0501 ASTM B221 AND10134-0501 QQ-A-200/3 9540PL0900354 9540PL1909964
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
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November 2023
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Related Documents 9540-01-071-3509 5+ Documents (More...)
T4 ASTM B221 10164 QQ-A -T4ASTM B221 QQ-A AMS-QQ-A -200/3 - ,ASTM B221 QQ-A - ,ASTM B221 QQ-A AMS-QQ-A
-200/3 - ,ASTM B221 AMS-QQ-A -200/3 - ,ASTM B221 014971115 ANGLE,STRUCTURAL - ,ASTM AMS-QQ-A-200/3 -
/3- T4 ASTM B22110164 QQ-A -T4ASTM B221 QQ-A AMS-QQ-A -200/3 - ,ASTM B221 QQ-A - ,ASTM B221 QQ-A AMS-QQ-A
- ,ASTM B221 QQ-A - ,ASTM B221 QQ-A AMS-QQ-A -200/3 - ,ASTM B221AMS-QQ-A https 10164 QQ-A -T4ASTM
ASTM B221 10164 QQ-A -T4ASTM B221 QQ-A AMS-QQ-A -200/3 - ,ASTM B221 QQ-A - ,ASTM B221 QQ-A AMS-QQ-A -
- ,ASTM B221 QQ-A - ,ASTM B221 QQ-A AMS-QQ-A -200/3 - ,ASTM B221AMS-QQ-A -200/3 - ,ASTM B221
- ,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
Restrictions 9540-01-071-3509
9540-01-071-3509 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.
End Users 9540-01-071-3509
- 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:
- GT
- Poland (WP01)
- Effective Date:
- 1 Apr 2011
- Brazil (YA01)
- Effective Date:
- 1 Oct 2000
- Spain (YB01)
- Effective Date:
- 1 Apr 1991
- Singapore (YJ01)
- Effective Date:
- 1 Apr 1991
- Germany (ZG01)
- Effective Date:
- 1 Apr 1991
- Italy (ZR01)
- Effective Date:
- 1 Dec 2007
- Greece (ZU01)
- Effective Date:
- 1 Jan 2007
Approved Sources 9540-01-071-3509
- Part Number
- Manufacturer
- Status
- AMS10134-0501
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- AMS10134-0501
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Original Design
- Original Design
- MS14284E009
- 96906 - Military Standards (Active)
- Incomplete Standard
- Incomplete Standard
- K10A5T3511
- 81755 - Lockheed Martin Corporation (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- AMS-QQ-A-200/3
- 0U583 - Sae International (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- AND10134-0501/QQ-A-200/3-T3511
- 14153 - Defense Logistics Agency (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- 10134-0501
- 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
- AND10134-0501
- 99237 - Airforce-Navy Aeronautical Design (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- QQ-A-200/3
- 81348 - Federal Specifications Promulgated (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- 9540PL0900354
- 9009H - Jednolity Indeks Materialowy - (Active)
- NATO Reference
- NATO Reference
- 9540PL1909964
- 9009H - Jednolity Indeks Materialowy - (Active)
- NATO Reference
- NATO Reference
Datasheet 9540-01-071-3509
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Angle
- Base Flange Thickness [AJGP]
- 0.050 Inches Nominal
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Left Flange Joins Base Flange [AJGL]
- 0.063 Inches Nominal
- First Tip Radius [AJJB]
- 0.050 Inches Nominal
- First Tip Style [CMZY]
- Right Quarter Radius
- Heat Treatment [HEAT]
- T-3511 Solution Heat Treated
- Material [MATT]
- Aluminum Alloy, Astm B221, Alloy 2024
- Nondefinitive Spec/Std Data [ZZZT]
- Alloy 2024 And Temper T3511
- Left Side Flange Thickness [ADXL]
- 0.050 Inches Nominal
- Left Inside Angle [CQHP]
- 90.0 Degrees Nominal
- Second Tip Radius [CMZZ]
- 0.050 Inches Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Not Identical
- Second Tip Style [CNQK]
- Upper Radius
- Overall Height [ABKW]
- 0.500 Inches Nominal
- Overall Width [ABMK]
- 0.625 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.064 Pounds Per Linear Foot
DLA Procurement Analysis 9540-01-071-3509
Management Data 9540-01-071-3509
Navy
- Cognizance:
- 9B
- Navy-owned stocks of DLA material
Naval Inventory Control Point, Mechanicsburg
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Freight Information 9540-01-071-3509
9540-01-071-3509 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. 9540-01-071-3509 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. 9540-01-071-3509 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. 9540-01-071-3509 is not classified as a special type of cargo when transported by water. 9540-01-071-3509 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 9540-01-071-3509
- 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) 9540-01-071-3509 October 2021
Criticality and Quality
- Critical Item Code:
- 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):
- N
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: