English
SA60L Light Sport Aircraft
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Maximum Cruise Speed
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Take-off run distance
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Landing run distance
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Avarage Fuel consumption
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SA60L
PRODUCT INTRODUCTION
The SA60L is a single-engine, two-seater aircraft with tricycle fixed landing gear light sport aircraft. It has obtained the type certificate (TC) and production license (PC) issued by the Civil Aviation Administration of China (CAAC).
The SA60L accounts for more than 70% of China's light sports aircraft market and has been exported to Australia and the United States.
The manufacturing raw material of most part of aircraft is carbon fiber composite material, and main structure is made by one-piece molding technology manufacturing.
The flight performance and safety reach the international advanced level. It has the characteristics of easy to operate, low use and maintenance costs, and excellent adaptability for takeoff and landing. It is suitable for private flights, flight training, flight experience, and it has been applied to fields such as flight performances, aerial photography and aerial survey etc.
The SA60L accounts for more than 70% of China's light sports aircraft market and has been exported to Australia and the United States.
The manufacturing raw material of most part of aircraft is carbon fiber composite material, and main structure is made by one-piece molding technology manufacturing.
The flight performance and safety reach the international advanced level. It has the characteristics of easy to operate, low use and maintenance costs, and excellent adaptability for takeoff and landing. It is suitable for private flights, flight training, flight experience, and it has been applied to fields such as flight performances, aerial photography and aerial survey etc.
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Seat 2 Length 22.6ft(6.89m) Wingspan 28.2ft(8.6m) Height 8.3in(2.53m) -
Empty weight 793.6lb(360kg) Maximum take-off weight 1322lb(600kg) Fuel Tank Capacity 60L*2(Include unusable fuel 3L*2) -
Maximum Cruise Speed 118 kts(220km/h) Never Exceed Speed 138kts(256km/h) Stall Speed 39kts(72km/h) Rate of Climb 984ft/min(5m/s) Take-off Run Distance 571ft(174m) Take off Distance 1096ft(334m) Landing Run Distance 476ft(145m) Landing Distance 1139ft(347m) Avarage Fuel Consumption 4.5gal/h(17L/h) Range 648nm(1200km) Max Operating Altitude 14763ft(4500m) -
Manufacturer Rotax 912ULS2 Horsepower 100HP Propeller 2 or 3 Blade Composite Propeller Fuel Mogas or 100LL Aviation Gasoline
PRODUCT PARAMETERS
It is made of carbon fiber composite materials and is integrally molded. The static pressure load test is +4G and -2G. The flight performance and safety standards have reached the international advanced level.
The aircraft has excellent controllability and can perform maneuvers such as circling on a steep slope, somersaults, rolling, and unpowered gliding.
Equipped with a Rotax 912ULS engine, it is simple and reliable.
The basic instrument configuration includes Garmin G5, Garmin Aera 660 GPS, radio, transponder (ADS-B out), engine instruments, backup instruments, etc.
The safety reminder function includes stall alarm, low fuel volume reminder, cabin door unlocked reminder, etc. It highly improve the flight safety.
The safety reminder function includes stall alarm, low fuel volume reminder, cabin door unlocked reminder, etc. It highly improve the flight safety.
Spacious cockpit layout, center stick control, and double linkage stick rudder are suitable for flight training, private flights, and flight operations.
We can customize the aircraft according to customer needs.
The aircraft has low operation and maintenance costs and can take off and land on flat grass and dirt roads.
The aircraft series has accumulated more than 110,000 flight hours.
OUR AIRCRAFT
Support
CONTACT
E-mail: shkj@starair.cn
Add: No.768, Zhixing Street, LuSong District, ZhuZhou, HuNan Province, China.
Add: No.768, Zhixing Street, LuSong District, ZhuZhou, HuNan Province, China.
