MIL-HDBK-704-1 Base Document:2004
Current
The latest, up-to-date edition.
Guidance for Test Procedures for Demonstration of Utilization Equipment Compliance to Aircraft Electrical Power Characteristics (Part 1 of 8 Parts)
09-04-2004
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FOREWORD
1. SCOPE
1.1 Scope
2. APPLICABLE DOCUMENTS
2.1 General
2.2 Government documents
2.2.1 Specifications, standards and handbooks
3. DEFINITIONS
3.1 Acronyms and definitions
4. GENERAL INFORMATION
4.1 Utilization equipment compliance testing
4.2 Compliance tests
4.3 Utilization equipment power groups
4.4 Aircraft electrical operating conditions
4.5 Utilization equipment performance specifications
4.5.1 Examples of utilization equipment performance
requirements
4.6 Dual source utilization equipment
4.7 Transformer rectifiers units
4.8 Inverters
4.9 Compliance to aircraft electrical power characteristics
demonstration test methods of MIL-HDBK-704-2 through -8
4.10 Stimulation and monitoring equipment
4.10.1 Stimulation equipment
4.10.2 Monitoring equipment
5. NOTES
5.1 Intended use
5.2 Single phase test numbers
5.3 Subject term (keyword) listing
TABLE
CONCLUDING MATERIAL
Provides guidance on test procedures for demonstration of utilization equipment to determine compliance with the aircraft electrical power characteristics of MIL-STD-704.
| DevelopmentNote |
NOTICE 1 - Notice of Validation. (02/2009) NOTICE 2 - Notice of Validation. (12/2013)
|
| DocumentType |
Standard
|
| Pages |
24
|
| ProductNote |
NEW CHILD NOT 3 2018 IS NOW ADDED
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
This handbook provides guidance on test procedures for demonstration of utilization equipment to determine compliance with the aircraft electrical power characteristics of MIL-STD-704. This handbook is for guidance only and cannot be cited as a requirement.
| MIL-PRF-29595 Revision A:2011 | BATTERIES AND CELLS, LITHIUM, RECHARGEABLE, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
| MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
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