SAE AMS3688B
Adhesive, Foaming, Honeycomb Core Splice, Structural, -55 to +82°C (-65 to +180°F).
Standard:
AKA:
- AMS3688
- Revision: B
- 2005-05-31
- 1988-10-01
- Ams P17 Composite Materials Committee
This specification covers a foaming-type, heat-curing, resin-base adhesive in the form of paste or sheet. Primarily for use in splicing aluminum alloy or nonmetallic honeycomb core and for providing a shear tie between core edges and inserts or edge members in honeycomb assemblies for use over the range -55 to +82C (-65 to +180F). It is useful for filling gaps between core faces which are inserted into channels or similar areas where bonding pressure cannot be obtained.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS3688B | 1988-10-01 | Latest | |
| AMS3688A | 1981-10-01 | Historical | |
| AMS3688 | 1974-03-01 | Historical |
- SAE AMS 3688
- Aerospace
- Adhesives and Sealants
- Composite materials
- Fabrics
- Fibers
- Glass
- Lightweight materials
- Resins
- Materials properties