
MIL-S-26547 Revision C:1985
Current
The latest, up-to-date edition.

Starter-Generator Engine STU-6A
07-26-1985
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PACKAGING
6. NOTES
Describes the aircraft gas turbine engine driven starter generators for use in 28-volts (V) direct current (dc) systems.
DevelopmentNote |
C NOTICE 1 - Notice of Inactivation for new design. (07/2005) C NOTICE 2 - Notice of Validation but remains Inactive for New Design. (11/2008)
|
DocumentType |
Standard
|
Pages |
30
|
ProductNote |
NEW CHILD NOT 3 2019 IS NOW ADDED.
|
PublisherName |
US Military Specs/Standards/Handbooks
|
Status |
Current
|
This specification covers aircraft gas turbine engine driven starter generators for use in 28-volts (V) direct current (dc) systems.
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