Logo

SAE AS1974

Current Revision

Clamps, Support, Comparative Fatigue Strengths, Test Method

$74.00

$74.00

$133.20


Sub Total (1 Item(s))

$ 0.00

Estimated Shipping

$ 0.00

Total (Pre-Tax)

$ 0.00


Document Preview Not Available...

This SAE Aerospace Standard (AS) establishes vibration and transmissibility test procedures which compare the relative strengths of various loop and saddle type support clamps. This procedure is intended for conducting fatigue testing which is standard throughout the aerospace industry thereby establishing a clamp strength comparison that can be used in an evaluation process. The testing required by this document ensures that clamps will meet adequate fatigue requirements only. It does not infer qualification of the clamp installation techniques or its ability to meet in-service environments or operating conditions. Separate qualification testing should be performed to ensure satisfactory service of the installed clamp.

SDO SAE: SAE International
Document Number AS1974
Publication Date April 24, 2003
Language en - English
Page Count 7
Revision Level
Supercedes
Committee
Publish Date Document Id Type View
April 24, 2003 AS1974 Revision