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Standard

PAPER HONEYCOMB 60 lb (25 kg) Paper

1983-01-01
HISTORICAL
AMS3720A
This specification covers paper base honeycomb material having a cell size of 0.330 or 0.440 in. (8.38 or 11.18 mm). Unless otherwise ordered, size 0.440 in. (11.18 mm) be supplied.
Standard

Paper Honeycomb 125 lb (55 kg) Paper

2012-01-16
CURRENT
AMS3722B
This specification covers paper base honeycomb material having a cell size of 0.440 in. (11.18 mm). Unless otherwise ordered, size 0.440 in. (11.18 mm) will be supplied.
Standard

SHIMS, FILLED RESIN COMPOUND

1993-01-01
HISTORICAL
AMS3726B
This specification covers filled, resinous, thermosetting compounds capable of being applied and cured in place between the surfaces of mechanically fastened (joined) structures.
Standard

SHIMS, FILLED RESIN COMPOUND

1991-10-01
HISTORICAL
AMS3726A
This specification covers filled, resinous, thermosetting compounds capable of being applied and cured in place between the surfaces of mechanically fastened (joined) structures.
Standard

Shims, Filled Resin Compound

2010-08-18
HISTORICAL
AMS3726D
This specification covers filled, thermosetting resin compounds capable of being applied and cured in place between the surfaces of mechanically fastened (joined) structures.
Standard

Shims, Filled Resin Compound

2006-01-06
HISTORICAL
AMS3726C
This specification covers filled, thermosetting resin compounds capable of being applied and cured in place between the surfaces of mechanically fastened (joined) structures.
Standard

Shims, Filled Resin Compound

2011-08-25
CURRENT
AMS3726E
This specification covers filled, thermosetting resin compounds capable of being applied and cured in place between the surfaces of mechanically fastened (joined) structures.
Standard

SHIMS, FILLED RESIN COMPOUND

2011-08-25
HISTORICAL
AMS3726
This specification covers filled, resinous, thermosetting compounds capable of being applied and cured in place between the surfaces of mechanically fastened (joined) structures.
Standard

AUTOMATED MANUFACTURE OF CONTINUOUS MULTI-PLY GRAPHITE FIBER/EPOXY RESIN IMPREGNATED BROADGOODS

1980-10-01
HISTORICAL
ARP1674
This Aerospace Recommended Practice (ARP) describes a manufacturing method for processing unidirectional graphite fiber/epoxy resin impregnated sheet and tape into multi-ply broadgoods and tape produced on an automated cross-plying machine. Broadgoods or tape of two or more ply configurations may be processed, where ply orientations of 0°, 45°, 90°, and 135° (as examples) may be automatically layed in a programmed sequence. In all configurations, the 0° ply direction is parallel to the length of the broadgoods roll or sheet, or tape.
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