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SAE AIR1296 Rev A

Concurrent Design of Engines and Specifications of Starting Systems for Helicopters
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SAE AIR1296 Rev A

Concurrent Design of Engines and Specifications of Starting Systems for Helicopters

PUBLISH DATE 2026
SAE AIR1296 Rev A
It is recommended that all helicopter engine development programs include an evaluation of engine starting requirements. The evaluation should include starting requirement effects on helicopter weight, cost, and mission effectiveness. The evaluation should be appropriate to the engine stage of development.
SDO SAE: SAE International
Document Number AIR1296
Publication Date April 25, 2026
Language en - English
Page Count 2
Revision Level A
Supercedes
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