MIL-A-23622 Base Document:1963
Current
The latest, up-to-date edition.
ACTUATOR, AIRCRAFT, ELECTRO-MECHANICAL, LINEAR, DIRECT CURRENT
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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.
| Committee |
FSC 1680
|
| 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
|
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| MIL-E-7080 Revision B:1962 | ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF |
| MS33547 Revision C:1957 | PIN, SPRING, FUNCTIONAL LIMITATIONS OF (ASG) |
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