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Page Title:
Electric Load and Power Source Capacity, Aircraft Analysis |
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|  MIL-E-7016F
20 July 1976
SUPERSEDING
MIL-E-007016E(AS)
8 May 1972
MIL-E-7016D(ASG)
15 April 1965
MILITARY SPECIFICATION
ELECTRIC LOAD AND POWER SOURCE CAPACITY,
AIRCRAFT, ANALYSIS OF
This specification is approved for use by all Departments
and Agencies of the Department of Defense.
1.
SCOPE
Scope. This specification covers the methods and requirements
1.1
for preparing alternating current (at) and direct current (dc) electric load and power
source capacity analyses for aircraft.
2.
APPLICABLE
DOCUMENTS
Issues of documents. The following documents, of the issue in
2.1
effect on date of invitation for bids or request for proposal, form a part of this
specification to the extent specified herein:
SPECIFICATIONS
MILITARY
- Wiring, Aerospace Vehicle
MIL-W-5O88
Beneficial comments (recommedations, additions, deletions) and any
pertinent data which may be of use in improving this document should
be addressed to: Engineering Specifications and Standards Department
(Code 93), Naval Air Engineering Center, Lakehurst NJ 08733, by
using the self-addressed Standardization Document Improvement Pro-
posal (DD Form 1426) appearing at the end of this document or by
letter.
FSC MISC
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