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Page Title:
Reliability and Maintainability Demonstration Requirements |
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| MIL-D-23222A(AS)
(Cont)
3.16.3
Satisfactory operation of the camera control system
(2)
throughout the designed range of the camera con-
trol system, but within the design flight envelope
of the helicopter, and for the cameras being
installed.
Suitability and operability of the viewfinder,
(3)
oblique sights and/or other sighting equipment
for properly positioning photographic targets.
(4)
Adequacy of camera doors and windows to afford the
camera a view unobstructed by the airframe, dirt,
oil film, water condensation reflection or other
deleterious effects.
Suitability of camera compartment temperatures
(5)
pressurization and vacuum supply; accessibility
to and operability of doors, windows, cameras, and
associated equipment as applicable.
Usability of the photographs from all installed
(6)
cameras operated in accordance with paragraph (2)
above, including radar recording, and night
photography as applicable.
Adequacy of camera initiating, operating and indi-
(7)
cator mechanisms of the camera control system.
(8)
Adequacy of recording equipment, as applicable.
Suitability of the automatic pilot to maintain
(9)
photographic flight line requirements as appli-
cable.
3.17
RELIABILITY AND MAINTAINABILITY DEMONSTRATION RE-
QUIREMENTS
3.17.1
GENERAL. - The specified reliability and maintain-
ability tests shall be performed to show that the
helicopter can meet the reliability and maintainability guarantees.
These tests shall be performed in combination with or, if necessary, in
addition to aerodynamic, hydrodynamic, power plant, armaments equipment,
electrical, avionics, shipboard suitability and photographic demon-
stration tests. Any reliability and maintainability demonstration
92
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