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Angle - Equal Thickness - AND10134-1406


Extrusion Pricing for AND10134-1406

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

AND10134-1406

AND10134-1406

Dimension Result For AND10134-1406

Dimension
A 1.500
B 1.250
A 38.100
B 31.750
Thickness
T 0.094
T 2.388
Radius
R 0.156
R1 0.094
R2 0.094
R3 0.010
R4 0.010
R5 0.010
R 3.962
R1 2.388
R2 2.388
R3 0.254
R4 0.254
R5 0.254
Degree
DE 90. 00

Cross Reference for AND10134-1406

In addition to your part number AND10134-1406. You may also be interested to know that this part number has a cross reference to:

P/N:
AND10134-1406
Boeing Formed Shapes:
S-2288
Canadair:
S-293
Cessna:
S1243327
Deutsche Airbus:
9540-00-186-6333
Douglas:
K10-70

Information about AND10134-1406

AND10134-1406 aircraft extrusion, also known as aerospace extrusion used in the manufacture and repair or commercial and military aircraft. AND10134-1406 is an - Angle - Equal Thickness. The weight per foot is 0.301 and has a circle size of 1 - 2 C/S and the factor is 18. AND10134-1406 is manufactured in aircraft grade aluminum and the part number is related to the shape of the part. AND10134-1406 Angle - Equal Thickness will also cross reference to AND10134-1406, Contact Us.

Chemical Analysis for AND10134-1406 | 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 AND10134-1406 | 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