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9540-00-140-2399
Structural Angle
9540001402399 001402399 AMS-QQ-A-200/11 ALLOY 7075 TMPR- AND10134-0602 AMS10134A-0602 AMS-QQ-A-200A ASTM B221 AMS-STD-184 QQA200-11 LS10134-0602-5 AMS-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
Managed by United States
NSN Created on 27 Aug 1971
Data Last Changed
November 2023
November 2023
NATO Update Count
21
21
NATO Data Quality
Marketplace 9540-00-140-2399
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ASTM-B221 ANGLE,STRUCTURAL 151 FT NS
AMS-QQ-A-200/11 ANGLE,STRUCTURAL 3 FT NS
QQ-A-200/11 ANGLE,STRUCTURAL 4 FT NS
AMS-QQ-A200/11 ANGLE,STRUCTURAL 45 FT NS
ASTM-B-221 ANGLE,STRUCTURAL 2 FT NS
QQA200-11 ANGLE,STRUCTURAL 603 FT NS
QQ-A200/11 ANGLE,STRUCTURAL 16 FT NS
Updated Every Day 9540-00-140-2399 RQST NE
Updated Every Day 9540-00-140-2399 RQST
Updated Every Day 9540-00-140-2399 RQST NE
Related Documents 9540-00-140-2399 5+ Documents (More...)
Structural Angle 9540005126876005126876 - AND10134-0602 AMS10134A-0602 AMS-QQ-A-200A ASTM B221 https
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9540-00-140-2399Structural Angle9540001402399 001402399 AMS-QQ-A-200/11 ALLOY 7075 TMPR- AND10134-0602
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9540-00-140-2399Structural Angle9540001402399 001402399 AMS-QQ-A-200/11 ALLOY 7075 TMPR- AND10134-0602
AMS-QQ-A-225/9 AMS-QQ-A-200/11 ALLOY 7075 TMPR AMS-STD-184 QQ-A-200/11 QQ-A-225/9 ASTM B221 AMS-QQ-A
ALLOY 7075 TMPR AND10133-0701 AND10133-0701/ASTM B221-0 QQ-A-277 S97 AMS-STD-184 J219P108 QQ-A
-200/11 https//www.nsnlookup.com /fsg-95/fsc-9540/us 9540-00-140-2399 Structural Angle 9540001402399
ALLOY 7075 TMPR AND10133-0701 AND10133-0701/ASTM B221-0 QQ-A-277 S97 AMS-STD-184 J219P108 QQ-A
-200/11 https//www.nsnlookup.com /fsg-95/fsc-9540/us 9540-00-140-2399 Structural Angle 9540001402399
AND10134-1205QQ-A-200/11 A Quotation QQA200-11 BEAM,STRUCTURAL 603 EA NS Request Quotation AMS-QQ-A
/fsc-9540/us 9540-00-487-5678 Structural Angle 9540004875678 004875678 QQ-A-200/11 ASTM B221 AMS-QQ-A
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/fsc-9540/us 9540-00-487-5678 Structural Angle 9540004875678 004875678 QQ-A-200/11 ASTM B221 AMS-QQ-A
https//www.nsnlookup.com /fsg-95/fsc-9540/us 9540-00-140-2399 Structural Angle 9540001402399 001402399
AMS-QQ-A-200/11 ALLOY 7075 TMPR AMS-STD-184 38390 A structural shape fabricated from a ferrous
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$1 a day Upgrade your Account Upgrade 9540-00-140-2399Structural Angle9540001402399 001402399 AMS-QQ-A
AND10136-2403 LS10136-2403-5 QQA200-11 AMS-STD-184 AMS-QQ-A-200A A structural shape fabricated
QQ-A-200/11 BEAM,STRUCTURAL 4 FT NS Request Quotation AMS-QQ-A-200/11 BEAM,STRUCTURAL 3 FT NS Request
A structural shape fabricated AMS-QQ-A-200/11 BEAM,STRUCTURAL 3 https//www.nsnlookup.com /fsg-95
QQ-A-200/11 BEAM,STRUCTURAL 4 FT NS Request Quotation AMS-QQ-A-200/11 BEAM,STRUCTURAL 3 FT NS Request
A structural shape fabricated AMS-QQ-A-200/11 BEAM,STRUCTURAL 3 https//www.nsnlookup.com /fsg-95
Restrictions 9540-00-140-2399
9540-00-140-2399 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 has been confirmed as a Non-Critical Munitions List Item or a Non-Sensitive Commerce Control List Item and cannnot be in the possession of any party outside of the USA who is a not an authorized NATO Government. Any other possessor of this item should mutilate it now as possession violates international and local laws. This item is a confirmed Commerce Control List Item (CCLI). This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 9540-00-140-2399
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 9540-00-140-2399
- US Army (A920)
- Effective Date:
- 1 Mar 2006
- Former MOE Rule:
- A186
- 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:
- GTKE
- Spain (YB01)
- Effective Date:
- 1 Feb 1994
- New Zealand (ZE01)
- Effective Date:
- 1 Sep 1993
- Germany (ZG01)
- Effective Date:
- 1 Apr 1991
- Republic of Korea (ZH01)
- Effective Date:
- 1 Mar 1997
- Turkey (ZW01)
- Effective Date:
- 1 Nov 2005
Approved Sources 9540-00-140-2399
- Part Number
- Manufacturer
- Status
- AMS-QQ-A-200/11 ALLOY 7075 TMPR-
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- AND10134-0602
- 99237 - Airforce-Navy Aeronautical Design (Active)
- Incomplete Standard
- Incomplete Standard
- AMS10134A-0602
- 0U583 - Sae International (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- AMS-QQ-A-200A
- 0U583 - Sae International (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- AMS-STD-184
- 0U583 - Sae International (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- ASTM B221
- 81346 - American Society For Testing And (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-STD-184
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- QQA200-11
- 81348 - Federal Specifications (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- LS10134-0602-5
- 98897 - Lockheed Martin Corp (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-200/11
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-200A
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS10134A-0602
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9540-00-140-2399
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Angle
- Base Flange Thickness [AJGP]
- 0.063 Inches Nominal
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Left Flange Joins Base Flange [AJGL]
- 0.063 Inches Nominal
- First Tip Radius [AJJB]
- 0.063 Inches Nominal
- First Tip Style [CMZY]
- Right Quarter Radius
- Heat Treatment [HEAT]
- T-6511 Solution Heat Treated
- Material [MATT]
- Aluminum Alloy Ams-Qq-A-200/11, Alloy 7075
- Nondefinitive Spec/Std Data [ZZZT]
- Alloy 7075 And Temper T6511
- Left Inside Angle [CQHP]
- 90.0 Degrees Nominal
- Left Side Flange Thickness [ADXL]
- 0.063 Inches Nominal
- Length [ABRY]
- 12.000 Feet Nominal
- Reference Number Differentiating Characteristics [ZZZY]
- As Differentiated By Extra Long Reference Number
- Second Tip Radius [CMZZ]
- 0.063 Inches Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Not Identical
- Second Tip Style [CNQK]
- Upper Radius
- Overall Height [ABKW]
- 0.625 Inches Nominal
- Overall Width [ABMK]
- 0.750 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.100 Pounds Per Linear Foot
Weapon Systems (WSDC) 9540-00-140-2399
DLA Procurement Analysis 9540-00-140-2399
- Last Stock Position:
- 98 In Stock
- DLA Administrative Lead Time:
- Subscribe
- DLA Production Lead Time:
- Subscribe
Management Data 9540-00-140-2399
Army
- Materiel Category and Inventory Manager:
- J
- Ground Forces Support Materiel (DLA/GSA Items)
- Appropriation and Budget Activity:
- 2
- Stock Fund Secondary Items
- Management Inventory Segment:
- 2
- Non-Repairable Items(Exclusive of Insurance and Provisioning Items)
This code will be used to identify items, which are not reparable.
- Weapons System / End Item / Homogeneous Group:
- 00
- DLA/GSA Material
DLA/GSA-Managed Items that cannot be identified to a specific Army Weapons Systems/End Item
- Accounting Requirements:
- X
- Expendable item.An item of Army property coded with an ARC of X in the AMDF. Expendable items require no formal accountability after issue from a stock record account.Commercial and fabricated items similar to items coded X in the AMDF are considered expendable items.
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 9540-00-140-2399
9520-14-571-1226 9540-12-353-3582 9540-99-001-6833 9520-25-151-6205 9520-27-004-4658 9520-27-000-2311 9520-27-000-2309 9520-27-000-2380 9520-27-000-2331 9520-27-000-2223 9520-13-101-0988 9520-21-859-2545 9520-27-000-2343 9520-14-556-7789 9540-17-027-3361 9520-21-663-2057 9540-12-328-6559 9540-12-135-1694
Freight Information 9540-00-140-2399
9540-00-140-2399 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. 9540-00-140-2399 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. 9540-00-140-2399 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. 9540-00-140-2399 is not classified as a special type of cargo when transported by water. 9540-00-140-2399 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 9540-00-140-2399
- 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) 9540-00-140-2399 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):
- 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: