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Page Title:
Avionics Systems Demonstration Data Reports (Cont) |
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| MIL-D-2322A (AS)
3.19.2.8
(cont)
(14)
A discussion of the flight performance of all
electronic system during any of the simulated
missions specified for the helicopter including
a qualitative analysis of the overall system
integration with details of any peculiarities
that may exist which might affect the designed
mission of the helicopter.
The recommended maintenance and test procedures
(15)
using standard or special contractor-furnished
equipments. This shall include test setup, pro-
cedures, special handling equipment, bench check
and line maintenance procedures as analyzed in
a mm-hour maintenance time study. Any informa-
tion regarding reliability or failure of components
should also be reported. This report shall also
include utilization and efficiency of any special
test or auxiliary equipment to be supplied by
the contractor.
The instrumentaion used by the contractor and
(16)
installed in the airframe during the electronics
demonstration. These reports shall include a
complete, detail description of the airborne
electronic systems, terminal equipments, test
conditions, and terrain over which tests were
made. Reference shall be made to sections of the
applicable specifications which governed the
evaluations. The report shall contain compre-
hensive discussion of the results obtained and
emphasize any operational limitations imposed by
hardware design. Any contractor request for
a waiver of the applicable specification or
portions there of skill reference and be supported
by the discussions contained in these reports.
The discussion and data shall be sufficient to
judge the validity of the conclusions reached by
the contractor.
The results of flight tests performed to confirm
(17)
model measurements on antennas shall be reported
and field-intensity measurements shall be referred
to isotropic antenna signal level. The isotropic
antenna signal level shall include a factor to
108
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