MIL-A-23622 Base Document:1963
Current
The latest, up-to-date edition.
Actuator, Aircraft, Electro-Mechanical, Linear, Direct Current
15-04-1963
1 SCOPE
2 APPLICABLE DOCUMENTS
3 REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PREPARATION FOR DELIVERY
6 NOTES
Describe the requirements for the design and testing of linear electro-mechanical actuators that are electrically reversible and mechanically irreversible with adjustable limit switches, operable from a 28 volt direct current system.
| DevelopmentNote |
Notice 1 - Notice of Inactivation for New Design Notice 2 - Notice of Inactivation for New Design (08/2001)
|
| DocumentType |
Standard
|
| Pages |
24
|
| ProductNote |
NEW CHILD NOT 3 2019 IS NOW ADDED
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
This specification defines the requirements for the design and testing of linear electro-mechanical actuators which are electrically reversible and mechanically irreversible with adjustable limit switches, operable from a 20 volt direct current system.
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