Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Indonesian Aerospace N-219 Short Take-Off and Landing (STOL) / Light Utility Aircraft.
2 x Pratt & Whitney Canada PT6A-42 turboprop engines developing 850 horsepower and driving four-bladed propeller units.
Propulsion
249 mph
400 kph | 216 kts
Max Speed
9,843 ft
3,000 m | 2 miles
Service Ceiling
966 miles
1,555 km | 840 nm
Operational Range
2,000 ft/min
610 m/min
Rate-of-Climb