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Page Title:
Anti-Foging and Rain Removal Systems |
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| MIL-D-23222A(AS)
3.12.12
(Cont)
(a)
Stature
(b)
Weight
(c)
Sitting Height
(d)
Eye Height Sitting
(e)
Bideltoid Diameter
(f)
Functional Reach
(g)
Forearm Hand Length
(h)
Elbow Rest Height
(i)
Buttock-Knee Length
(j)
Waist Circumference
(k)
Buttock Circumference
(l)
Shoulder Circumference
(m)
Chest Depth
(n)
Knee Height Sitting
(o)
Hip Breadth Sitting
(p)
Head Height
(2) The contractor shall demonstrated, or shall have de-
monstrated, that the aircraft meets the following re-
quirements as applicable to the particulary aircrft:
All crew station seat arrangement, seat ad-
justment, plugs and connections shall be compat-
ible with all services personnel flight equipment
(including parachutes, anti-exposure suit, survi-
val vest, floatation garment, body armor, etc.)
planned for van in the aircraft when in actual
service.
Aircrew station displays, dimensions, geometry,
and location actumtion, and and accuracy of
operating all controls essential to flight oper-
ations shall be is accordance with MIL-STD-250
and MS335575.
External visibility from the design are position
shall conform to MIL-STD-850.
Emergency
Escape. (See paragraphy 3.12.11).
3.12.13
ANTI-FOGGING AND RAIN REMOVAL SYSTEMS.- The systems
shall be demonstrated to show satisfactory operation in
accordance with contract requirements and to show compliance with Spec MIL-T-
5842.
AUTOMATIC BLADE FOLDING. - The contractor shall demonstrate
3.12.14
that it is possible to fold as well as unfold the blades in
winds up to 45 knots, from any direction, in less than 30 seconds without
supplimentary assistance.
83
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