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a
RESULTS
i
.
Go?
Ye
Waiter - The Raydist positioning system was unable to control
the aircraft after approximately H-10 min.
The "progress" and "azimuth"
needles on the pilot's indicator became erratic at that point.
Barley
(1)
Thermal - not measured
(2)
Gust - 43% design
2
at
limit in side fuselage bending
N—
The instrumentation eSSbres experienced were comprised of jamming
of the cockpit photo panel camera; malfunctioning nose boom pressure
transducer and losing the right wing outboard station bending moment
bridge.
4