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9540-01-430-5412
Structural Beam
9540014305412 014305412 AMS-QQ-A-200/15 CVC10030-12CJ QQ-A-200/15
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
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Related Documents 9540-01-430-5412 5+ Documents (More...)
-200/15 BEAM,STRUCTURAL 41 EA NS Request QQ-A-200 Quotation AMS-QQ-A-200/15 https/ 6 EA NS Request AMS-QQ-A
41 EA NS Request Quotation QQ-A-200/15 BEAM,STRUCTURAL 6 EA NS Request Quotation AMS-QQ-A-200/15 BEAM
41 EA NS Request QQ-A-200 Quotation AMS-QQ-A-200/15 https/ 6 EA NS Request Quotation AMS-QQ-A-200/15
AMS-QQ-A-200/15 https/ 6 EA NS Request AMS-QQ-A-200/15 BEAM,STRUCTURAL 41 41 EA NS Request QQ-A-200
Quotation AMS-QQ-A-200/15 BEAM,STRUCTURAL 41 EA NS Request QQ-A-200 Quotation AMS-QQ-A-200/15 https/
6 EA NS Request Quotation AMS-QQ-A-200/15 BEAM,STRUCTURAL 41 EA NS Request QQ-A-200 Quotation AMS-QQ-A
Request QQ-A-200 Quotation AMS-QQ-A-200/15 https/ 6 EA NS Request AMS-QQ-A-200/15 BEAM,STRUCTURAL 41
41 EA NS Request QQ-A-200 Quotation AMS-QQ-A-200/15 https/ 6 EA NS Request Quotation AMS-QQ-A-200/15
6 FT NS Request Quotation AMS-QQ-A-200/15 BEAM,STRUCTURAL QQ-A-200/15 BEAM,STRUCTURAL 6 EA NS Request
AMS-QQ-A-200/15 BEAM,STRUCTURAL 41 EA NS QQ-A-200/15 ANGLE,STRUCTURAL 6 FT NS Request Quotation AMS-QQ-A
Restrictions 9540-01-430-5412
9540-01-430-5412 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 9540-01-430-5412
- US Air Force (FNN5)
- Effective Date:
- 1 Jun 2003
- Former MOE Rule:
- FGKZ
Approved Sources 9540-01-430-5412
- Part Number
- Manufacturer
- Status
- AMS-QQ-A-200/15
- Manufacturer
- 0U583 - Sae International (Active)
- Incomplete Reference
- Incomplete Reference
- CVC10030-12CJ
- 80378 - Triumph Aerostructures, Llc (Active)
- Primary Buy
- Primary Buy
- QQ-A-200/15
- 81348 - Federal Specifications (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- AMS-QQ-A-200/15
- 81343 - Society Of Automotive Engineers Inc (Replaced)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 9540-01-430-5412
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- H Shape
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Bottom Left Flange Joins Web Flange/Leg [BPXK]
- 0.125 Inches Nominal
- Fillet Radius Where Bottom Right Flange Joins Web Flange/Leg [BPXM]
- 0.125 Inches Nominal
- 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 Inner Radius [CNBD]
- 0.020 Inches Nominal
- First Tip Outer Radius [CNBJ]
- 0.020 Inches Nominal
- First Tip Style [CMZY]
- Square W/ Inner And Outer Corner Radii
- Fourth Tip Relationship To Preceding Tips [CNQN]
- Identical W/First Tip
- Heat Treatment [HEAT]
- T-76511 Solution Heat Treated
- End Item Identification [AGAV]
- B-2 Bomber
- Material [MATT]
- Aluminum Alloy, Qq-A-200/15, Alloy 7075
- Nondefinitive Spec/Std Data [ZZZT]
- Alloy 7075 And Temper T76511
- Left Side Bottom Flange Distance To Center Of Both Flanges [BPXF]
- 0.992 Inches Nominal
- Left Side Flange Height [ADXJ]
- 2.000 Inches Nominal
- Left Bottom Inside Angle [CTBR]
- 90.0 Degrees Nominal
- Left Side Flange Thickness [ADXL]
- 0.125 Inches Nominal
- Left Side Top Flange Distance To Center Of Both Flanges [BPXD]
- 1.008 Inches Nominal
- Left Top Inside Angle [CSMZ]
- 90.0 Degrees Nominal
- Length [ABRY]
- 12.000 Feet Nominal
- Right Side Bottom Flange Distance To Center Of Both Flanges [BPXH]
- 1.122 Inches Nominal
- Right Side Flange Height [ADXK]
- 2.250 Inches Nominal
- Right Side Flange Thickness [ADXM]
- 0.125 Inches Nominal
- Right Side Top Flange Distance To Center Of Both Flanges [BPXG]
- 1.128 Inches Nominal
- Right Top Inside Angle [CRZC]
- 90.0 Degrees Nominal
- Right Bottom Inside Angle [CWKK]
- 90.0 Degrees Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Width [ABMK]
- 2.500 Inches Nominal
- Web Flange Thickness [BPXN]
- 0.125 Inches Nominal
- Third Tip Relationship To Preceding Tips [CNQL]
- Identical W/First Tip
Management Data 9540-01-430-5412
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Apr 2009
- Department of the Air Force (DF)
- FT
- Subscribe
- FT
Air Force
- Budget:
- S
- 57X3010 - Aircraft Replenishment Spares
- Aggregation Code:
- BQ
- B-2 TSSP, NORTHROP GRUMMAN
- Price Validation Code:
- E
- The current standard price is an estimated price.
Estimated Price challenges are allowed but follow procedures in para 60.b. (3) of section L of this manual.
This code will be changed to a P code upon notification of a contract price or this code will be changed to an updated code upon determination of a valid price.
- Expendability
Recoverability
Repairability: - N
- Expendable. Condemn at User. Stock Fund (except Munitions).
NATO Stock Numbers Related to 9540-01-430-5412
Freight Information 9540-01-430-5412
9540-01-430-5412 has freight characteristics.. 9540-01-430-5412 has a variance between NMFC and UFC when transported by rail and the description should be consulted.