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H-Beam Un-Equal Thickness - TMS60-19892


Extrusion Pricing for TMS60-19892

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

TMS60-19892
Dimension
A 5.500
B 2.200
C 1.065
A 139.700
B 55.880
C 27.051
Thickness
T1 0.150
T2 0.070
T3 0.150
T1 3.810
T2 1.778
T3 3.810
Radius
R 0.120
R1 0.120
R2 0.031
R3 0.062
R4 0.062
R 3.048
R1 3.048
R2 0.787
R3 1.575
R4 1.575
Degree
DE 90. 00

Cross Reference

In addition to your part number TMS60-19892. You may also be interested to know that this part number has a cross reference to:

P/N:
TMS60-19892
Boeing:
BAC1518-615

Information about TMS60-19892

TMS60-19892 aircraft extrusion, also known as aerospace extrusion used in the manufacture and repair or commercial and military aircraft. TMS60-19892 is an - H-Beam Un-Equal Thickness. The weight per foot is 1.239 and has a circle size of 1 - 2 C/S and the factor is 16. TMS60-19892 is manufactured in aircraft grade aluminum and the part number is related to the shape of the part. TMS60-19892 H-Beam Un-Equal Thickness will also cross reference to TMS60-19892, Contact Us.

Chemical Analysis for TMS60-19892 | 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 TMS60-19892 | 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