Hawk Systems Study Guide 2023 with complete solution
Hawk Systems Study Guide 2023 with complete solution Total internal fuel 2920lbs (2.9) Length 12.5 (including pitot tube) Wingspan 9m (excluding wingtip launchers and fairings) Height 4m Basic weight Approx 9700lbs (Varies plane to plane) MTOW 20,062 lbs Normal landing weight 13,007 lbs Combined capacity of external tanks? 2080 lbs Total fuel capacity with tanks? Approx 5000 lbs Stall speed 115 Knots (Clean, 300lbs of fuel) 96 Knots (Landing config, 300lbs of fuel) Max range of M240B Approx 1100 Nm @ 39,000ft and M0.69 Approx 460 Nm @ SL and 300 KCAS Max endurance 6.8m/100lbs of fuel @ F200, 185KCAS, 5AoA, and 1500lbs of fuel What is the name of the engine Ardour MK 871-05 Thrust (SL) 5730 lbs BUOXY capacity? 200L Emerg Oxy Contents 70L Which flight controls have manual reversion? Rudder only if the HYD1 fails What parameters does the main generator provide (___V and ___V, ___ phase, ___ Hz AC/DC) 115V and 200V, three phase, 400Hz AC Is the APU Generator any different from the main Provides only 12 KVA compared to 25 kVA from the main What conditions does the aux gen supply power
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