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9540-01-185-3755
Structural Beam
9540011853755 011853755 1MA160D01-10297 60-5537 AMS-QQ-A-200/11 QQ-A-200/11 10164625
A structural shape fabricated from a ferrous or nonferrous material and resembles the following cross-sectional forms: For the letter H, both flanges of the H section are equal or longer than the width measured along the axis of the web; for the letter I, a 16 2/3 percent slope on the inside face of the ferrous type flange, either one or both of the nonferrous type flanges are shorter than the length measured along the axis of the web; for the letters T and Z, on nonferrous type, the web is usually at right angles to the flanges. Letter H section may have a maximum of 5 percent slope on the inside face of the flanges. View more Structural Beam
November 2023
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Updated Every Day Related Documents 9540-01-185-3755 5+ Documents (More...)
Quotation AMS-QQ-A-200/11 ANGLE,STRUCTURAL 3 EA NS Request https//www.nsnlookup.com /fsg-95/fsc
-9540 Request Quotation QQ-A200/11 ANGLE,STRUCTURAL 16 EA NS Quotation AMS-QQ-A-200/11 ANGLE,STRUCTURAL
BEAM,STRUCTURAL 3 EA NS Request Quotation AMS-QQ-A-200/11 ANGLE,STRUCTURAL 3 EA NS Request Quotation
STRUCTURAL ALLOY 7075 TMPR 120078 AMS-STD-184 AMS-QQ-A-200/11 PA12597 QQ-A-200/11 A structural
AMS-QQ-A-200/11 ANGLE,STRUCTURAL 3 EA NS Request Quotation QQA200-11 ANGLE,STRUCTURAL 603 EA NS Request
structural shape fabricated from a ferrous or nonferrous ANGLE,STRUCTURAL 16 EA NS Quotation AMS-QQ-A-200/11
ANGLE,STRUCTURAL 3 EA NS Request Quotation Quotation AMS-QQ-A-200/11 ANGLE,STRUCTURAL 3 EA NS
ANGLE,STRUCTURAL Quotation AMS-QQ-A-200/11 ANGLE,STRUCTURAL 3 EA NS Request Quotation QQA200-
AMS-QQ-A200/11 BAR,METAL 45 EA NS Request Quotation QQ-A-200/11 BAR,METAL 4 EA NS Request Quotation AMS-QQ-A
ANGLE,STRUCTURAL 4 EA NS Request Quotation QQ-A200/11 ANGLE,STRUCTURAL 16 AMS-QQ-A-200/11 ANGLE,STRUCTURAL
Restrictions 9540-01-185-3755
9540-01-185-3755 is a Structural Beam 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 9540-01-185-3755
- US Navy (N9BZ)
- Effective Date:
- 1 Mar 2006
- Former MOE Rule:
- N9ZD
- Supplementary Collaborators:
- KE
- Finland (WF01)
- Effective Date:
- 1 Jul 2009
- Spain (YB01)
- Effective Date:
- 1 Apr 1991
- Canada (ZC01)
- Effective Date:
- 1 Apr 1991
Approved Sources 9540-01-185-3755
- Part Number
- Manufacturer
- Status
- AMS-QQ-A-200/11
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- 1MA160D01-10297
- 76301 - The Boeing Company (Active)
- Incomplete Reference
- Incomplete Reference
- 60-5537
- 29321 - Transtar Metals Corp (Active)
- Incomplete Reference
- Incomplete Reference
- AMS-QQ-A-200/11
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- QQ-A-200/11
- 81348 - Federal Specifications Promulgated (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- 10164625
- A486G - Nimikkeistokeskus Ncb Finland (Active)
- NATO Reference
- NATO Reference
Datasheet 9540-01-185-3755
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- T Shape
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Top Left Flange Joins Web Flange/Leg [BPXJ]
- 0.090 Inches Nominal
- Fillet Radius Where Top Right Flange Joins Web Flange/Leg [BPXL]
- 0.090 Inches Nominal
- First Tip Style [CMZY]
- Square End
- Heat Treatment [HEAT]
- O-Annealed
- Material [MATT]
- Aluminum Alloy Ams-Qq-A-200/11, Alloy 7075
- Nondefinitive Spec/Std Data [ZZZT]
- O Temper
- Left Side Top Flange Distance To Center Of Both Flanges [BPXD]
- 1.240 Inches Nominal
- Left Side Top Flange Thickness [ADXR]
- 0.080 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 89.0 Degrees Nominal
- Leg Thickness [AJJP]
- 0.080 Inches Nominal
- Length [ABRY]
- 10.000 Feet Minimum And 12.000 Feet Maximum
- Right Top Inside Angle [CRZC]
- 91.0 Degrees Nominal
- Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 1.290 Inches Nominal
- Right Side Top Flange Thickness [ADXS]
- 0.080 Inches Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 1.630 Inches Nominal
- Top Flange Width [BQJG]
- 2.530 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.396 Pounds Per Linear Foot
- Third Tip Relationship To Preceding Tips [CNQL]
- Identical W/First Tip
Weapon Systems (WSDC) 9540-01-185-3755
DLA Procurement Analysis 9540-01-185-3755
- Last Stock Position:
- 12 In Stock
- DLA Administrative Lead Time:
- Subscribe
- DLA Production Lead Time:
- Subscribe
Management Data 9540-01-185-3755
Navy
- Cognizance:
- 9B
- Navy-owned stocks of DLA material
Naval Inventory Control Point, Mechanicsburg
NATO Stock Numbers Related to 9540-01-185-3755
Freight Information 9540-01-185-3755
9540-01-185-3755 has freight characteristics managed by the Southwestern Power Administration.It has a National Motor Freight Classification (NMFC) of 104420. A Sub NMFC of X. It has a NMFC Description of BEAMS NOI I/S. 9540-01-185-3755 is rated as class 50 when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 53800 which rates the freight between FCL and LCL. 9540-01-185-3755 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. 9540-01-185-3755 is not classified as a special type of cargo when transported by water. 9540-01-185-3755 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 9540-01-185-3755
- 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
Procurement History 9540-01-185-3755 2 Records
Contracting Technical Data File (CTDF) 9540-01-185-3755 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):
- T
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: