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 |