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