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9540-00-556-8823
Structural Beam
9540005568823 005568823 AMS-QQ-A-200/11 1MA160D01-10273 QQ-A-200/11 10164563
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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Related Documents 9540-00-556-8823 5+ Documents (More...)
ANGLE Quotation AMS-QQ-A-200/11 ANGLE,STRUCTURAL 3 EA NS Request Quotation QQA200-11 ANGLE,STRUCTURAL
ANGLE BEAM,STRUCTURAL 3 EA NS Request Quotation AMS-QQ-A-200/11 ANGLE,STRUCTURAL 3 EA NS Request
ANGLE,STRUCTURAL Quotation AMS-QQ-A-200/11 ANGLE,STRUCTURAL 3 EA NS Request Quotation QQA200-
ANGLE,STRUCTURAL 3 EA NS Request Quotation Quotation AMS-QQ-A-200/11 ANGLE,STRUCTURAL 3 EA NS
AMS-QQ-A-200/11 ANGLE,STRUCTURAL 3 EA NS Request Quotation AMS-QQ-A200/11 ANGLE,STRUCTURAL 45 EA NS
ANGLE,STRUCTURAL Quotation AMS-QQ-A-200/11 ANGLE,STRUCTURAL 3 EA NS Request Quotation QQA200-
AMS-QQ-A-200/11 HA18106-7075T6511 Managed by United States NSN Created on 3 Apr 1979 Data Last Changed
005056436 AMS-QQ-A-200/11 18106 A structural shape fabricated from a ferrous or nonferrous material
Quotation AMS-QQ-A-200/11 ANGLE,STRUCTURAL 3 EA NS Request Quotation QQA200-11 ANGLE,STRUCTURAL https
BEAM,STRUCTURAL 3 EA NS Request Quotation AMS-QQ-A-200/11 ANGLE,STRUCTURAL 3 EA NS Request Quotation
Restrictions 9540-00-556-8823
9540-00-556-8823 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. The precious metals content of this item is unknown.
End Users 9540-00-556-8823
- 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 9540-00-556-8823
- Part Number
- Manufacturer
- Status
- AMS-QQ-A-200/11
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- 1MA160D01-10273
- 76301 - The Boeing Company (Active)
- Incomplete Reference
- Incomplete Reference
- QQ-A-200/11
- 81348 - Federal Specifications (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-200/11
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
- 10164563
- A486G - Nimikkeistokeskus Ncb Finland (Active)
- NATO Reference
- NATO Reference
Datasheet 9540-00-556-8823
- 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 Document And Classification [MDCL]
- Qq-A-200/11 Fed Spec 1St Material Response
- Material [MATT]
- Aluminum Alloy 7075
- Nondefinitive Spec/Std Data [ZZZT]
- O Temper
- Left Side Top Flange Distance To Center Of Both Flanges [BPXD]
- 1.029 Inches Nominal
- Left Side Top Flange Thickness [ADXR]
- 0.063 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 90.0 Degrees Nominal
- Leg Thickness [AJJP]
- 0.063 Inches Nominal
- Length [ABRY]
- 10.000 Feet Minimum And 12.000 Feet Maximum
- Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 1.171 Inches Nominal
- Right Side Top Flange Thickness [ADXS]
- 0.063 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]
- 2.200 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 0.257 Pounds Per Linear Foot
- Third Tip Relationship To Preceding Tips [CNQL]
- Identical W/First Tip
Weapon Systems (WSDC) 9540-00-556-8823
DLA Procurement Analysis 9540-00-556-8823
Management Data 9540-00-556-8823
Navy
- Cognizance:
- 9B
- Navy-owned stocks of DLA material
Naval Inventory Control Point, Mechanicsburg
NATO Stock Numbers Related to 9540-00-556-8823
Freight Information 9540-00-556-8823
9540-00-556-8823 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. 9540-00-556-8823 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. 9540-00-556-8823 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. 9540-00-556-8823 is not classified as a special type of cargo when transported by water. 9540-00-556-8823 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 9540-00-556-8823
- 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) 9540-00-556-8823 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: