Turbine Engine Starting System Design Requirements
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Product Code: ARP949
Date Published: 1969-05-01 - A newer version of this standard is available.
Date Reaffirmed: September 1994
Issuing Committee:
Ae-6 Starting Systems And Auxiliary Power Committee
Scope
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.
Product Status: In Stock
File Size:
85K
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| Current & Historical versions of this standard |
|---|
| Standard |
Date published |
?Status |
| ARP949B |
1999-03-01 |
Revised |
| ARP949A |
1983-08-01 |
Reaffirmed |
| ARP949 |
1969-05-01 |
Reaffirmed |
|
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