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9540-00-145-4517
Structural Angle
9540001454517 001454517 AND10133-2403 QQA200-3
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
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ANGLE,STRUCTURAL 45 FT NS Request Quotation QQA200-11 ANGLE,STRUCTURAL 603 FT NS Request Quotation AND10133-2403
Structural Angle 9540001454517 001454517 $1 a day Upgrade your Account Upgrade 9540-00-145-4517Structural
AMS-QQA200-3 A structural shape fabricated from a ferrous or nonferrous material and resembling the
Structural Angle 9540001454517 001454517 AMS-QQA200-3 A structural shape fabricated from a ferrous
AMS-QQ-A-200/11 A structural shape fabricated https/ https//www.nsnlookup.com /fsg-95/fsc-9540/us 9540-00-145-4517
Structural Angle 9540001454517 001454517 AMS-QQA200-3 A structural shape fabricated from a ferrous
AMS-QQA200-3 A structural shape fabricated from a ferrous or nonferrous material and has a flange
www.nsnlookup.com /fsg-95/fsc-9540/us 9540-00-085-0558 Structural Angle 9540000850558 000850558 AMS-QQA200-3
LS10138-1004-2 AND10138-1004 QQA200-3 A structural shape fabricated from a ferrous or nonferrous material
Approved Sources 9540-00-008-2215 Part NumberManufacturerStatusAMS-QQA200-3 0U583 - Sae International
Restrictions 9540-00-145-4517
9540-00-145-4517 is a Structural Angle 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 9540-00-145-4517
- NASA (G190)
- Effective Date:
- 1 Apr 1991
- Brazil (YA01)
- Effective Date:
- 1 Aug 2000
Approved Sources 9540-00-145-4517
- Part Number
- Manufacturer
- Status
- AND10133-2403
- Manufacturer
- 99237 - Airforce-Navy Aeronautical Design (Active)
- Incomplete Standard
- Incomplete Standard
- QQA200-3
- 81348 - Federal Specifications (Active)
- Incomplete Standard
- Incomplete Standard
Datasheet 9540-00-145-4517
- Characteristic
- Specifications
- FIIG
- Specifications
- A13100
- Basic Shape Style [AGTA]
- Angle
- Base Flange Thickness [AJGP]
- 0.250 Inches Nominal
- Fabrication Method [AARN]
- Extruded
- Fillet Radius Where Left Flange Joins Base Flange [AJGL]
- 0.250 Inches Nominal
- First Tip Radius [AJJB]
- 0.250 Inches Nominal
- First Tip Style [CMZY]
- Right Quarter Radius
- Heat Treatment [HEAT]
- T-4 Solution Heat Treated
- Material Document And Classification [MDCL]
- Qq-A-200/3 Fed Spec 1St Material Response
- Material [MATT]
- Aluminum Alloy 2024
- Nondefinitive Spec/Std Data [ZZZT]
- T4 Temper
- 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 Radius [CMZZ]
- 0.250 Inches Nominal
- Second Tip Relationship To First Tip [CNQJ]
- Not Identical
- Second Tip Style [CNQK]
- Upper Radius
- Overall Height [ABKW]
- 2.500 Inches Nominal
- Overall Width [ABMK]
- 2.500 Inches Nominal
- Weight Per Unit Measure [BRFD]
- 1.409 Pounds Per Linear Foot
NATO Stock Numbers Related to 9540-00-145-4517
Freight Information 9540-00-145-4517
9540-00-145-4517 has freight characteristics.. 9540-00-145-4517 has a variance between NMFC and UFC when transported by rail and the description should be consulted.