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Angle - Equal Thickness - AND10134-2005


Extrusion Pricing for AND10134-2005

For extrusion pricing, delivery and availablility complete the information below:

AND10134-2005

AND10134-2005

Dimension For AND10134-2005

Dimension
A 2.000
B 1.250
A 50.800
B 31.750
Thickness
T 0.188
T 4.775
Radius
R 0.188
R1 0.188
R2 0.188
R3 0.010
R4 0.010
R5 0.010
R 4.775
R1 4.775
R2 4.775
R3 0.254
R4 0.254
R5 0.254
Degree
DE 90. 00

Cross-Ref for AND10134-2005

In addition to your part number AND10134-2005. You may also be interested to know that this part number has a cross reference to:

P/N:
AND10134-2005
Boeing Formed Shapes:
S-2348
Cessna:
S1205311
Deutsche Airbus:
9540-00-145-8455
Douglas:
K10-172
Douglas Formed Shapes:
GS180C84
General Dynamics:
LS-M10473-2005

Information about AND10134-2005

AND10134-2005 aircraft extrusion, also known as aerospace extrusion used in the manufacture and repair or commercial and military aircraft. AND10134-2005 is an - Angle - Equal Thickness. The weight per foot is 0.680 and has a circle size of 4 - 5 C/S and the factor is 9. AND10134-2005 is manufactured in aircraft grade aluminum and the part number is related to the shape of the part. AND10134-2005 Angle - Equal Thickness will also cross reference to AND10134-2005, Contact Us.

Chemical Analysis for AND10134-2005 | 7075-T6511 AMS-QQ-A-200/11

silicon
0.4
iron
0.5
copper
1.2 - 2.0
manganese
0.3
magnesium
2.1 - 2.9
chromium
0.18 - 0.28
zinc
5.1 - 6.1
titanium
0.2
aluminum
Remainder

Information

The shapes listed on our site are standard shapes, like angles channels and tee's. We have many complex shapes in stock including seat tracks that may not be viable on our website. Unless specified we generally stock and distribute in 12ft (3660mm) Lengths. We have capability to make up to 40ft length shapes. Stock items are shipped within 2 days and we also will accommodate AOG shipments.

Mechanical Analysis for AND10134-2005 | 7075-T6511 AMS-QQ-A-200/11

Thickness Min Tensile Ksi Max Tensile Ksi Min Yield Ksi Max Yield Ksi Elongation Percent
0.001 - 0.249 78 0 70 0 7
0.250 - 4.999 81 0 73 0 7
0.500 - 1.499 81 0 72 0 7
1.500 - 2.999 81 0 72 0 7
3.000 - 4.999 81 0 71 0 7
4.500 - 5.000 78 0 70 0 6