SPECIFICATIONS:
HK36TTC
All specifications are subject to change without notice.
Powerplant
Bombardier Rotax 914-F3, turbo-charged, four-cylinder, horizontally
opposed, 115 hp
Hydraulic constant speed propeller with
hydro pneumatic feathered pitch
Also available with 80 or 100 hp normally
aspirated Rotax 912 engine.
| Recommended
TBO |
|
1,000 hr |
| Length |
|
23ft 6 in |
| Height |
|
5 ft 9 in |
| Wingspan |
|
54 ft 6 in |
| Wing
area |
|
165 sq ft |
| Wing
loading |
|
10.3 sq ft |
| Seats |
|
2 |
| Empty
weight, typical |
|
1,189 lb |
| Maximum
gross weight |
|
1,698 lb |
| Fuel
capacity, long range |
|
21.1 US gal (20.9 usable) |
| Oil
capacity |
|
3 qt |
| Maximum
tow weight |
|
1,653 lb |
| Performance |
|
|
| Takeoff
distance over 50-ft obstacle |
|
450 ft |
| Max
demonstrated crosswind component |
|
15 kt |
| Rate
of climb, sea level |
|
1,200 fpm |
| Cruise
speed @ 75% power |
|
121 ktas |
| Service
ceiling |
|
17,000 ft |
| Landing
distance, over 50 ft obstacle |
|
450 ft |
| Minimum
sink rate |
|
225 fpm |
| Glide
ratio |
|
1:27 |
|
|
|
| Limiting
and Recommended Airspeeds |
|
|
| Vne
(never exceed) |
|
141 kias |
| Vso
(stall, in landing configuration) |
|
42 kias |
|
