Premium Information is available for this item - Upgrade for $1 a day
9540-01-475-1087
Structural Angle
9540014751087 014751087 CVC10000-532CA
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
![]()
January 2023
4


Marketplace 9540-01-475-1087
Request a Quotation from participating marketplace vendors
Related Documents 9540-01-475-1087 1+ Documents (More...)
9540-01-475-1087 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-95/fsc-9540/us 9540-01-475-1087
Day 9540-01-475-1087 RQST NE Related Documents 9540-01-475-1087 1+ Documents ( More... ) https//www.nsnlookup.com
Restrictions 9540-01-475-1087
9540-01-475-1087 is a Structural Angle that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. 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 9540-01-475-1087
- US Air Force (FNN5)
- Effective Date:
- 1 Jun 2003
- Former MOE Rule:
- FGKZ
Approved Sources 9540-01-475-1087
- Part Number
- Manufacturer
- Status
- CVC10000-532CA
- Manufacturer
- 80378 - Triumph Aerostructures, Llc (Active)
- Primary Buy
- Primary Buy
Datasheet 9540-01-475-1087
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Base Flange Thickness [AJGP]
- 0.250 Inches Nominal
- Basic Shape Style [AGTA]
- Angle
- Fabrication Method [AARN]
- Extruded
- First Tip Radius [AJJB]
- 0.250 Inches Nominal
- First Tip Style [CMZY]
- Right Quarter Radius
- End Item Identification [AGAV]
- Intermediate; Aircraft, B-2 Bomber (Atb)
- Material Document And Classification [MDCL]
- Qq-A-430, Alloy 7075 Fed Spec 1St Material Response
- Material [MATT]
- Aluminum Alloy 7075
- Left Inside Angle [CQHP]
- 90.0 Degrees Nominal
- Left Side Flange Thickness [ADXL]
- 0.250 Inches Nominal
- Length [ABRY]
- 10.000 Feet Minimum And 12.000 Feet Maximum
- Second Tip Relationship To First Tip [CNQJ]
- Identical
- Overall Height [ABKW]
- 3.000 Inches Nominal
- Overall Width [ABMK]
- 3.000 Inches Nominal
Management Data 9540-01-475-1087
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- May 2009
- Department of the Air Force (DF)
- FT
- Subscribe
- FT
Similar Supply Items to 9540-01-475-1087


















Freight Information 9540-01-475-1087
9540-01-475-1087 has freight characteristics.. 9540-01-475-1087 has a variance between NMFC and UFC when transported by rail and the description should be consulted.