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9540-00-140-2401
Structural Angle
9540001402401 001402401 AMS-QQ-A-200/9 AND10134-2001 AND10134-2001/QQ-A-200/9-T5 QQ-A-200/9 ASTM B221
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
May 2023
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Related Documents 9540-00-140-2401 5+ Documents (More...)
/fsg-95/fsc-9540/us 9540-00-548-7197 Structural Channel 9540005487197 005487197 ASTM B221 AMS-QQ-A-200
ANGLE,STRUCTURAL 29 EA NS Request AMS-QQ-A -200/9 TUBE,METALLIC -T5 QQ-A-200/9 ASTM B221 A structural
ASTM B221 QQ-A-200/9 AND10134 ANGLE,STRUCTURAL 151 EA NS Request Quotation ASTM-B-221 ANGLE,STRUCTURAL
2 EA NS Request Quotation AND10134 /www.nsnlookup.com /fsg-95/fsc-9540/us 9540-00-140-2401 Structural
95/fsc-9540/us 9540-00-140-2401 Structural Angle 9540001402401 001402401 AND10134-2001 AND10134-2001/
ANGLE,STRUCTURAL 29 EA NS Request AMS-QQ-A -200/9 TUBE,METALLIC -2001/QQ-A-200/9-T5 QQ-A-200/9ASTM
8 EA NS Request Quotation AMS-QQ-A-200/9 ANGLE,STRUCTURAL 29 EA NS Request AMS-QQ-A -200/9 TUBE,METALLIC
/fsg-95/fsc-9540/us 9540-00-140-2401 Structural Angle 9540001402401 001402401 AND10134-2001 AND10134
Angle 9540001404978 001404978 -T5 QQ-A-200/9 ASTM B221 AMS-QQ-A- ANGLE,STRUCTURAL 29 EA NS Request AMS-QQ-A
ASTM B221 AMS-QQ-A-200/9 A structural shape fabricated from a ferrous or nonferrous ANGLE,STRUCTURAL
Restrictions 9540-00-140-2401
9540-00-140-2401 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 9540-00-140-2401
- 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
- Brazil (YA01)
- Effective Date:
- 1 Aug 2000
- Germany (ZG01)
- Effective Date:
- 1 Apr 1991
- United Kingdom (ZK01)
- Effective Date:
- 1 Apr 1991
Approved Sources 9540-00-140-2401
- Part Number
- Manufacturer
- Status
- AMS-QQ-A-200/9
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- AND10134-2001
- 99237 - Airforce-Navy Aeronautical Design (Active)
- Incomplete Standard
- Incomplete Standard
- AND10134-2001/QQ-A-200/9-T5
- 14153 - Defense Logistics Agency (Active)
- Secondary Buy
- Secondary Buy
- QQ-A-200/9
- 81348 - Federal Specifications (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- ASTM B221
- 81346 - American Society For Testing And (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-200/9
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9540-00-140-2401
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Angle
- Base Flange Thickness [AJGP]
- 0.125 Inches Nominal
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Left Flange Joins Base Flange [AJGL]
- 0.156 Inches Nominal
- First Tip Radius [AJJB]
- 0.125 Inches Nominal
- First Tip Style [CMZY]
- Right Quarter Radius
- Heat Treatment [HEAT]
- T-5 Solution Heat Treated
- Material [MATT]
- Aluminum Alloy Ams-Qq-A-200/9, Alloy 6063
- Nondefinitive Spec/Std Data [ZZZT]
- Alloy 6063 And Temper T5
- Left Inside Angle [CQHP]
- 90.0 Degrees Nominal
- Left Side Flange Thickness [ADXL]
- 0.125 Inches Nominal
- Length [ABRY]
- 20.000 Feet Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Not Identical
- Second Tip Radius [CMZZ]
- 0.125 Inches Nominal
- Second Tip Style [CNQK]
- Upper Radius
- Overall Height [ABKW]
- 1.000 Inches Nominal
- Overall Width [ABMK]
- 2.000 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.430 Pounds Per Linear Foot
DLA Procurement Analysis 9540-00-140-2401
Management Data 9540-00-140-2401
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:
- V
- The current standard price has been validated.
The item has been analyzed in conjunction with the Zero Overpricing Program and is in the accepted price range.
The item was procured under open competition and under the competitive arena the price is considered fair and reasonable.
ZOP or Standard price challenges are permissible but must be supported by adequate justification.
- 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 9540-00-140-2401
Freight Information 9540-00-140-2401
9540-00-140-2401 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. 9540-00-140-2401 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. 9540-00-140-2401 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. 9540-00-140-2401 is not classified as a special type of cargo when transported by water. 9540-00-140-2401 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 9540-00-140-2401
- 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) 9540-00-140-2401 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:
- Special Packaging Instruction Number (SPIN):
- Special Packaging Instruction Number Revision:
- Special Packaging Instruction Number Date:
- Pallet Reference Number Required: