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|  MIL-E-7016F
Introduction.
3.5.3
Statement of aircraft mission. The statement of aircraft mis-
3.5.3.1
sion shall consist of a brief statement of the mission, with general explanations
which will serve to clarify the function of the electric system with respect to the
mission (Optional).
Operating conditions. A list of the operating conditions repre-
3.5.3.2
sented by the G numbers shall be given, similar to the following:
G1
Ground maintenance
G2
Calibration
G3
Loading and preparation
G4
Start and warm up
G5
Taxi
G6
Take off & climb
G7
Cruise
G8
Cruise combat
G9
Landing
Gl0
Emergency
3.5.3.3
Bus wiring diagram. The bus wiring diagram shall consist of
a functional single-line diagram of the bus arrangement, with buses, power sources
and interconnections identified as illustrated in Figure 1.
3.5.3.4
Electric system operation. Power distribution from the source
output terminals to the buses shall be described briefly for both normal and abnormal
operation.
3.5.3.5
Generator Mounting and Drive Data. For a sample of Generator
Mounting and Drive Data, see Figure 2.
3.5.3.6
Power Source Output Data.
For a sample of Power Source Out-
put Data, see Figure 3.
3.5.4
AC and DC analyses.
3.5.4.1
Connected load chart. The connected load chart is a listing of
equipment for each bus grouped by its functional category (see 3.5.4.1.1), along
with power requirements per unit, applicable notes, and number of units. Entries
on this chart are used to identify entries on all succeeding sheets of the analysis of
a given source. If equipment requires multiple power sources, this fact should be
stated in the notes. Typical connected load charts are shown on Figures 4 and 10.
3.5.4.1.1
Functional category - column A. Each item of equipment shall
be assigned a functional category code letter identifying the function of the equipment
6
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