GENERAL INFORMATION / SUMMARY OF PERFORMANCE SPECIFICATIONS 1-3
CHANGE A1 ICON A5-B / PILOT’S OPERATING HANDBOOK
CHAPTER 1
1.3 SUMMARY OF PERFORMANCE SPECIFICATIONS
Parameter Value
Gross Weight
1510 lb
f
Top Speed at SL, V
H
(MCP, 5500 RPM)
95 KTAS
Cruise Speed, 5000 RPM, 8000 ft 84 KTAS
Range (5000 RPM, 8000 ft, including
takeoff and climb from SL)
427 nm (with 45 min reserve)
Best Angle of Climb Speed, V
X
(Flaps 0°)
54 KIAS
Best Angle of Climb Speed, V
X
(Flaps
15°/30°)
50 KIAS
Best Rate of Climb Speed, V
Y
58 KIAS
Rate of Climb at V
X
(SL)
616 ft/min
Rate of Climb at V
Y
(SL)
629 ft/min
Stall Speed, V
S
(Flaps and landing gear
up)
45 KIAS
Stall Speed, V
S0
(Flaps and landing gear
down)
39 KIAS
Total Fuel Capacity 20.1 US gallons
Total Usable Fuel 20 US gallons
Approved Types of Fuel
Unleaded automotive fuel with up to 10%
maximum ethanol content meeting ASTM
D4814 with minimum RON 95 (minimum
Anti-Knock Index 91)
Grade 100LL aviation gasoline (AVGAS)
meeting ASTM D910
Max Engine Power at SL 100 hp at 5800 RPM (5 min max)
Max Demonstrated Direct Crosswind
Component—Land and Water (not a
limitation)
12 knots
Service Ceiling at Gross Weight (100
ft/min Climb Rate)
15,000 ft