Teklam
FAA-APPROVED ALLOWABLE ALUMINUM PANELS
TEKLAM offers a large selection of panels with
FAA-approved 'A' and 'B' basis design allowables.

TEKLAM P/N

Click for Data Sheet and Inventory Status
Core Material
per AMS-C-7438
Top/Bottom Skin Alum per QQ-A-250
Part Thickness (inch)
Weight (lbs/sf)
AA209-33-250
5052-.0015-1/4-3.4
.020" 2024T3 CLAD
.250
.68
AA209-33-375
5052-.0015-1/4-3.4
.020" 2024T3 CLAD
.375
.73
AA209-33-500
5052-.0015-1/4-3.4
.020" 2024T3 CLAD
.500
.78
AA209-33-750
5052-.0015-1/4-3.4
.020" 2024T3 CLAD
.750
.87
AA209-33-1000
5052-.0015-1/4-3.4
.020" 2024T3 CLAD
1.000
.93
AA207-33-250
5052-.0020-3/16-5.7
.020" 2024T3 CLAD
.250
.75
AA207-33-375
5052-.0020-3/16-5.7
.020" 2024T3 CLAD
.375
.80
AA207-33-500
5052-.0020-3/16-5.7
.020" 2024T3 CLAD
.500
.85
AA207-33-750
5052-.0020-3/16-5.7
.020" 2024T3 CLAD
.750
.96
AA207-33-1000
5052-.0020-3/16-5.7
.020" 2024T3 CLAD
1.000
1.06
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