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9540-00-250-1055
Structural Angle
9540002501055 002501055 734J SAE-AMS-QQ-A-200/8 ASTM B221 AMS-QQ-A-200/8 QQ-A-200/8
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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Related Documents 9540-00-250-1055 5+ Documents (More...)
Quotation ASTM-B221 -95/fsc-9540/us 9540-00-250-1055 https//www.nsnlookup.com /fsg SAE-AMS-QQ-A
-1055 Structural Angle 9540002501055 002501055,734J SAE-AMS-QQ-A -200 /8 Quotation ASTM-B221 -95/fsc-
A SAE-AMS-QQ-A-200 https//www.nsnlookup.com /fsg-95 Quotation ASTM-B221 ASTM-B221 https 95 SAE-AMS-QQ-A
SAE-AMS-QQ-A -200/8 Quotation https SAE-AMS-QQ-A -200/8 Quotation https//www.nsnlookup.com /fsg-95/fsc
SAE-AMS-QQ-A https ASTM-B221 https SAE-AMS-QQ-A SAE-AMS-QQ-A -200/8 Quotation ASTM-B221 -95/fsc- 9540
Angle 9540002776272002776272 https SAE-AMS-QQ-A SAE-AMS-QQ-A SAE-AMS-QQ-A -200/8 Quotation ASTM-B221
Structural Angle 9540002501055 002501055,734J SAE-AMS-QQ-A -200/8 Quotation ASTM-B221 Quotation
ASTM-B221 https ASTM-B221 https SAE-AMS-QQ-A https https ASTM-B221 https SAE-AMS-QQ-A SAE-AMS-QQ-A -
-01-260-7834 Structural Angle 9540012607834012607834 //www.nsnlookup.com /fsg-95/fsc-9540 A SAE-AMS-QQ-A-200/8
AMS-QQ-A 012607834 A SAE-AMS-QQ-A-200/8 https//www.nsnlookup.com /fsg-95/fsc-9540/us 9540-01-260
Restrictions 9540-00-250-1055
9540-00-250-1055 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.
Import and Export 9540-00-250-1055
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 9540-00-250-1055
- US Air Force (FGGI)
- Effective Date:
- 1 Mar 2006
- Former MOE Rule:
- FGKZ
- US Navy (N9BZ)
- Effective Date:
- 1 Mar 2006
Approved Sources 9540-00-250-1055
- Part Number
- Manufacturer
- Status
- 734J
- Manufacturer
- 01634 - Aluminum Co Of America (Active)
- Incomplete Reference
- Incomplete Reference
- SAE-AMS-QQ-A-200/8
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- ASTM B221
- 81346 - American Society For Testing And (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-200/8
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-200/8
- 0U583 - Sae International (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- QQ-A-200/8
- 81348 - Federal Specifications Promulgated (Active)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9540-00-250-1055
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Angle
- Base Flange Thickness [AJGP]
- 0.250 Inches Nominal
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Left Flange Joins Base Flange [AJGL]
- 0.312 Inches Nominal
- First Tip Radius [AJJB]
- 0.250 Inches Nominal
- First Tip Style [CMZY]
- Right Quarter Radius
- Heat Treatment [HEAT]
- T-6 Solution Heat Treated
- Material [MATT]
- Aluminum Alloy Ams-Qq-A-200/8, Alloy 6061
- Nondefinitive Spec/Std Data [ZZZT]
- Alloy 6061, Temper T6
- Left Side Flange Thickness [ADXL]
- 0.250 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]
- 0.250 Inches Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Not Identical
- Second Tip Style [CNQK]
- Upper Radius
- Overall Height [ABKW]
- 2.500 Inches Nominal
- Overall Width [ABMK]
- 3.000 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 1.570 Pounds Per Linear Foot
DLA Procurement Analysis 9540-00-250-1055
- Last Stock Position:
- 50 In Stock
- DLA Administrative Lead Time:
- Subscribe
- DLA Production Lead Time:
- Subscribe
Management Data 9540-00-250-1055
Air Force
- Fund:
- SF
- Stock fund applicable to items managed for the Air Force by the respective Inventory Control Point
- Budget:
- 9
- 57X4921.070 - General Support DIV - Air Force decentralized managed expense items (ERRC XB3, XF3) with a unit cost of less than $250,000 that are requisitioned/procured at base (retail) level from DLA, GSA, Army, Navy, Depot Maintenance Service, Air Force Industrial Fund (AFMC), local manufacture and commercial vendors
- Price Validation Code:
- N
- The current standard price in Catalog Management Data (CMD) has not analyzed or coded for LP/LM.
The price has not been analyzed or reviewed for accuracy.
ZOP or Standard price challenges are permissible but must be supported with adequate justification. However, if coded for Local Purchase (LP) or Fabrication/Manufacture as indicated with an (LM) Acquisition Advice Code of āLā or āFā, then it must be evaluated locally where purchased or fabricated.
- Expendability
Recoverability
Repairability: - N
- Expendable. Condemn at User. Stock Fund (except Munitions).
Navy
- Cognizance:
- 9B
- Navy-owned stocks of DLA material
Naval Inventory Control Point, Mechanicsburg
NATO Stock Numbers Related to 9540-00-250-1055
Freight Information 9540-00-250-1055
9540-00-250-1055 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 013140. A Sub NMFC of X. It has a NMFC Description of ALUMINUM ANGLES. 9540-00-250-1055 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. 9540-00-250-1055 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. 9540-00-250-1055 is not classified as a special type of cargo when transported by water. 9540-00-250-1055 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 9540-00-250-1055
- 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
- Special requirements
- --
Intermediate Pack Level
- Quantity of Unit Packs
- Container
- --
- No Requirement
Contracting Technical Data File (CTDF) 9540-00-250-1055 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: