SAE ARP949A
Turbine Engine Starting System Design Requirements.
This recommended practice is intended to define and establish, where applicable, a standard presentation of the engine characteristics required for the determination of a satisfactory starting system for aircraft gas turbine engines.
History:Standard | Published | Revision | Status |
---|---|---|---|
ARP949B | 1999-03-01 | Latest | |
ARP949A | 1983-08-01 | Historical | |
ARP949 | 1969-05-01 | Historical |