2010 Remos GX AvÄ±ator II

Tuesday, July 06, 2010 at 12:00 AM ET

Verified

Edited By: Omar Filipović

Key Takeaways:

The article presents the detailed specifications for the 2010 REMOS GX AVIATOR II aircraft.
It is powered by a 100 HP Rotax 912 UL-S engine, has a max takeoff weight of 1320 lbs, and a useful load of 518 lbs with full fuel.
Key performance figures include a maximum cruise speed of 112 knots, a range of 745 nautical miles, and a best rate of climb of 1050 fpm.
The aircraft demonstrates impressive short-field capability, requiring a takeoff roll of 510 ft and a landing roll of 270 ft.

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2010 Remos GX Aviator II

2010 REMOS GX AVIATOR II

Engine make/model:

Rotax 912 UL-S

Horsepower

100

Max takeoff weight (lbs.):

1320

Empty weight (lbs.):

670

Useful load, full fuel (lbs.):

518

Fuel capacity (gals.):

22

Wingspan:

30 ft. 6 in.

Wing area (sq. ft.):

118

G-load factor:

+4/-2

Cabin width (in.):

46.8

PERFORMANCE

Max. cruise speed (kts.):

112

V_s (kts.):

44

V_so (kts.):

38

Best rate of climb (fpm):

1050

Range (nm):

745

Takeoff roll (ft.):

510

Landing roll (ft.):

270

Takeoff over 50 ft. obstacle (ft.):

730

Landing over 50 ft. obstacle (ft.):

760

Source: Remos Aircraft Inc.

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