\ 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