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|  MIL-E-7016F
fully explained in notes. For example, calibration power
requirements might require closer voltage tolerance than
that required for normal operation.
c. Multiple power sources: When an equipment requires, orPOW
is served by multiple power sources at the same time, its
requirements shall be entered in the load analysis is of each
power source. such multiple entries shall not be com-
pounded in system power totals.
" Operating conditions" entries. All entries shall be accurate
3.4.4.5.2
within 5% maximum error.
Contents. The report shall consist of applicable items from the
3.5
following outline, with ac and dc analyses repeated as required for each electric
ppwer system in the aircraft:
Item
Title Page (see 3.5.1)
I
Table of Contents (see 3.5.2)
II
Introduction (see 3.5.3)
III
A. Statement of mission (optional see 3.5.3)
B. Operating Conditions (see 3.5.3.2)
C. Electric Bus Wiring Diagram (see 3.5.3.3)
D. Description of Electric System Operation
(see 3.5.3.4)
E. Generator Mounting and Drive Data (see 3.5.3.5)
F. Power Source Output Data (see 3.5.3.6)
AC Load Analyses (see 3.5.4)
IV
A. Connected Load Chart (see 3.5.4.1)
B. Load Analysis Chart (see 3.5.4.2)
C. Transient Analyses (see 3. 5.4.3)
D. Power Source Utilization Analysis Chart
(see 3.5.4.4)
E. Power Source Utilization Graph (see 3.5.4.5)
F. Adjusted Power Source Graph (see 3.5.4.6)
DC Analyses (see 3.5.4 and 3.5.5)
V
A. Connected Load Chart (see 3.5.4.1)
B. Load Analysis Chart (see 3. 5.4.2)
C. Transient Analyses (see 3.5.4.3)
D. Power Source Utilization Analysis Chart (see
3.5.4.4)
4
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