MIL-HDBK 1028/6A
Table 1 (Continued)
Summary of Aircraft Utility Demands
NOTES:
(1)
For specific information on aircraft not listed, contact NAVAIR
8.0Y1G on DSN 664-1104.
(2)
Refer to MIL-HDBK-1004/5 for values.
(3)
Requirements per engine.
(4)
NAEC-GSED-86, Fixed Point Aircraft Utility Support System Report.
(5)
Nominal capacity at 45 degrees F supply air (hangar locations
only).
(6)
Analysis of Fixed Point Utility System - Supplement "86" Report.
(7)
ECS not available for A-4E aircraft.
(8)
For air start system demand calculations, assume F14s only start
one engine, and use cross bleed air to start second engine from
the first.
(9)
Manufacturer's information.
(10)
For demand calculations, prior to adjusting for diversity,
include only 20 percent of the F18 aircraft in the count for use
with Figure 2, the diversity curve, the remaining 80 percent will
use their on board auxiliary power units to provide electricity,
air start, and cooling capability.
(11)
Data to be provided by NAVAIR after testing is completed.
(12)
Values are theoretical not equipped for external air connections.
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