| Specifications: |
| Powerplant |
Lycoming
AEIO-360-H1B |
| Horse Power
@ RPM |
180 @ 2700
rpm |
| Recommended
Engine TBO |
1400 hours |
| Propeller,
Standard Constant Speed |
Hartzell
HC-C2YR-4CF/FC7666A-2 |
| Propeller
Diameter |
74 in. |
| Length |
22.9 ft. |
| Height |
7.7 ft. |
| Wingspan |
32 ft. |
| Wing Area |
169.1 sq.
ft. |
| Wing
Loading |
10.64 lb. /
sq. ft. |
| Power
Loading |
10 lb. / HP |
| Seats |
2, Tandem |
| Cabin
Length |
8 ft. 10
in. |
| Cabin Width |
2 ft. 6 in. |
| Cabin
Height |
3 ft. 11
in. |
| Empty
Weight (typical) |
1340 lbs. |
| Maximum
Gross Weight |
1800 lbs. |
| Useful Load |
460 lbs. |
| Payload
with Full Fuel |
226 lbs. |
| Fuel
Capacity, Standard |
40 gal. (39
gal. Usable) |
| Oil
Capacity |
10 quarts |
| Baggage
Capacity |
100 lbs.
(10.4 cubic feet) |
| Performance: |
| Acrobatic
Limit Loading |
+6,
-5 g's |
| Maximum
Inverted Time |
2 min. |
| Takeoff
Distance, Ground Roll |
495 ft. |
| Takeoff
Distance Over 50-ft Obstacle |
904 ft. |
| Maximum
Demonstrated Crosswind Component |
17 kts. |
| Rate of
Climb, Sea Level |
1280 fpm |
| Maximum
Level Speed, Sea Level |
155 mph |
| Cruise
Speed / Endurance with 45 Minute
Reserve @ 75% Power (Standard
Fuel Tanks) |
147 mph /
3.4 hours |
|
Fuel Consumption @ Altitude |
9.5 gph @
5000 ft. |
| Cruise
Speed / Endurance with 45 Minute
Reserve @ 55% Power (Standard
Fuel Tanks) |
128 mph /
4.4 hours |
|
Fuel Consumption @ Altitude |
7.6 gph @
5000 ft. |
| Service
Ceiling |
15800 ft. |
| Landing
Distance over 50-ft. Obstacle |
1051 ft. |
| Landing
Distance, Ground Roll |
425 ft. |
| Limited and
Recommended Airspeeds: |
| VX
(Best Angle) |
58 mph |
| VY
(Best Rate) |
80 mph |
| VA
(Design Maneuvering) |
132 mph |
| VNO
(Maximum Structural Cruising) |
160 mph |
| VNE
(Never Exceed) |
200 mph |
| VR
(Rotation) |
56 mph |
| VS1
(Stall, Clean) |
53 mph |
