TUCANO R - CIVILIAN TRAINER
Specifications
Aircraft Dimension
Aircraft length 23,29 ft
Wing Span 27.59 ft
Wing Area 111 Sq. ft
Cabin Height 3,12 ft
Cabin Width 2,36 ft
Max Seating capacity 2
Fuel Tank capacity 2×15,85 US gal
Aircraft Dimension
Maximum take off Weight (LSA rules)
Empty weight
1320 lb
930 lb
Useful Load
390 lb
Baggage allowance with 1 pilot
Baggage allowance with 2 pilot
154 lb
75lb
Design Weight
1433lb with a load factor of +6-3 G
Design Weight
1653 with a loaf factor of +4 -2 G
Power Plant & Performance (1433 lb – 650kg)
Power Unit
Rate of Climb
Max Cruise Speed (85%)
Stall
L.C.
Average Consumption
65% power
Range
NM
VNE
kts
Rotax 912 (100 hp)
1000 ft/min
120 kts
40 kts
4,7 US gal/hr
648
178
Rotax 912 IS
(100 hp)
1000 ft/min
up to 8000 ft
120 kts
40 kts
4,5 US gal/hr
670
178
Rotax 914 (115hp)
1200 ft/min
125 kts
40 kts
5,8 US gal/hr
620
178
Rotax 915 IS
(140 hp)
1300 ft/min up to 10000 ft
150 kts (TAS) alt. 6000 ft
50 kts
7,5 US gal/hr
610
178
*Rotax 912 with a Two-blade Fixed Propeller
CRUISE Performance 915is -141 hp – (1653 lb – 750 kg)
Altitude
% Power
climb
80 kts
KTAS
Average Consumption
6000 ft
65%
85% Eco
85% Pow
1000 ft/min
130
143
148
6.6 US gal/hr
9 US gal/hr
10.1 US gal/hr
9000 ft
65%
85% Eco
85% Pow
950 ft/min
130
145
150
6.9 US gal/hr
8.5 US gal/hr
10.3 US gal/hr
12000 ft
65%
85% Eco
85% Pow
900 ft/min
142
149
160
6.9 US gal/hr
8.7 US gal/hr
10.9 US gal/hr
15000 ft
65%
85% Eco
85% Pow
850 ft/min
147
155
164
6.9 US gal/hr
8.7 US gal/hr
11 US gal/hr
Cruise Performance with MTOW 650 kg (1433 lbs) are 7 knots more for every range
