MIL-PRF-21480 Revision B:2010
Current
The latest, up-to-date edition.
Generator System, Electric Power, 400 Hertz, Alternating Current, Aircraft; General Specification for
22-03-2010
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. VERIFICATION
5. PACKAGING
6. NOTES
Specifies the general requirements for three phase, four wire, wye-connected, 400 Hertz, alternating current (AC), constant input speed, electric power generator systems for use on aircraft.
| DevelopmentNote |
Supersedes MIL G 21480 (A). (03/2010) B NOTICE 1 - Notice of Validation. (12/2014)
|
| DocumentType |
Standard
|
| Pages |
86
|
| ProductNote |
NEW CHILD NOT 2 2019 IS ADDED
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| Supersedes |
This specification establishes the general requirements for three phase, four wire, wye-connected, 400 Hertz, alternating current (AC), constant input speed, electric power generator systems for use on aircraft.
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| MIL-PRF-21480-12 Revision F:2012 | GENERATOR SYSTEM, 40 KVA, 400 HZ AC INTEGRALLY EXCITED, BRUSHLESS TYPE |
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| MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
| MIL-STD-130 Revision N:2007 | IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
| SAE AMS 2175 : 2010 | CASTINGS, CLASSIFICATION AND INSPECTION OF |
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| MIL-PRF-7808 Revision L:1997 | LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE |
| DOD-PRF-85734 Revision A:2004 | LUBRICATING OIL, HELICOPTER TRANSMISSION SYSTEM, SYNTHETIC BASE |
| MIL-STD-889 Revision C:2016 | DISSIMILAR METALS |
| MIL-PRF-23699 Revision G:2014 | Lubricating Oil, Aircraft Turbine Engine, Synthetic Base, NATO Code Numbers: O-152, O-154, O-156, and O-167 |
| SAE AS 8879 : 2004 | SCREW THREADS - UNJ PROFILE, INCH CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER |
| MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
| MIL-STD-202 Revision H:2015 | ELECTRONIC AND ELECTRICAL COMPONENT PARTS |
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