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9540-00-555-0815
Structural Beam
9540005550815 005550815 AMS-QQ-A-200/11 HT197 FS50104-2012-2 AND10136-2006 5779 AMS10136-2006 40176 QQ-A-200/11
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
May 2023
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// AMS-QQ-A - - AMS-QQ-A -200/11 - - -200/11 // AMS-QQ-A -200 - 11 // AMS-QQ-A -200/11 - / Beam9540005550815
/QQ-A-200/11-T6511 FS50104-2012-2AMS10136-2006QQ-A-200/11AMS-QQ-A-200/11 A structural // AMS-QQ-A
Structural Beam 9540005550815 005550815 Upgrade 9540-00-555-0815Structural Beam9540005550815 005550815
AMS-QQ-A-200/11 HT197 FS50104-2012-2 AND10136-2006 Structural Beam 9540012813896012813896 Upgrade your
// AMS-QQ-A -200/11 - /11 - AMS-QQ-A BEAM - - - BEAM AMS-QQ-A -200 /11 https - - AMS-QQ-A-200/11 BEAM
Beam 9540005550815 005550815 HT197 FS50104-2012-2AND10136-2006 5779 AMS10136-2006 40176 QQ-A-200/11
https//www.nsnlookup.com /fsg-59/fsc-5930/de 5930-12-146-0686 Rotary Switch 5930121460686121460686,HT197
Structural Beam 9540005550815 005550815,HT197 Upgrade for $1 a day Upgrade your Account Upgrade
Structural Beam 9540005550815 005550815 Upgrade your Account Upgrade 9540-00-555-0815Structural
Beam9540005550815 005550815 AMS-QQ-A-200/11 HT197 FS50104-2012-2AND10136-20065779 AMS10136-2006 40176
Restrictions 9540-00-555-0815
9540-00-555-0815 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 9540-00-555-0815
- US Air Force (FGGI)
- Effective Date:
- 1 Mar 2006
- Former MOE Rule:
- FGKZ
- Germany (ZG01)
- Effective Date:
- 1 Jan 2015
- Republic of Korea (ZH01)
- Effective Date:
- 1 Apr 1991
Approved Sources 9540-00-555-0815
- Part Number
- Manufacturer
- Status
- AMS-QQ-A-200/11
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- AMS10136-2006
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- HT197
- 10383 - Kaiser Aluminum And Chemical Corp (Active)
- Incomplete Reference
- Incomplete Reference
- FS50104-2012-2
- 89446 - Hiller Aircraft Corporation (Active)
- Incomplete Secondary Reference
- Incomplete Secondary Reference
- AND10136-2006
- 99237 - Airforce-Navy Aeronautical Design (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- 5779
- 01484 - Reynolds Metals Co (Obsolete)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS10136-2006
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- 40176
- 99267 - Bohn Aluminum And Brass Co Div Of (Obsolete)
- Canceled/Obsolete
- Canceled/Obsolete
- QQ-A-200/11
- 81348 - Federal Specifications Promulgated (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-200/11
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9540-00-555-0815
- 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]
- 0.125 Inches Nominal
- Fillet Radius Where Top Right Flange Joins Web Flange/Leg [BPXL]
- 0.125 Inches Nominal
- First Tip Radius [AJJB]
- 0.125 Inches Nominal
- First Tip Style [CMZY]
- Lower Radius
- 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]
- 1.000 Inches Nominal
- Left Side Top Flange Thickness [ADXR]
- 0.125 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 90.0 Degrees Nominal
- Leg Thickness [AJJP]
- 0.125 Inches Nominal
- Length [ABRY]
- 10.000 Feet Minimum And 12.000 Feet Maximum
- Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 1.000 Inches Nominal
- Right Side Top Flange Thickness [ADXS]
- 0.125 Inches Nominal
- Right Top Inside Angle [CRZC]
- 90.0 Degrees Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 1.250 Inches Nominal
- Top Flange Width [BQJG]
- 2.000 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.467 Pounds Per Linear Foot
- Third Tip Radius [CNBB]
- 0.062 Inches Nominal
- Third Tip Style [CNQM]
- Full Radius
- Third Tip Relationship To Preceding Tips [CNQL]
- Not Identical
DLA Procurement Analysis 9540-00-555-0815
Management Data 9540-00-555-0815
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Freight Information 9540-00-555-0815
9540-00-555-0815 has freight characteristics.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. 9540-00-555-0815 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. 9540-00-555-0815 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. 9540-00-555-0815 is not classified as a special type of cargo when transported by water. 9540-00-555-0815 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 9540-00-555-0815
- 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) 9540-00-555-0815 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: