Apollo FOX User Manual

16
WARNING
This engine is not certified for aircraft, and failure may occur at
any time! The pilot bears full responsibility for the consequences
of it’s failure.
Propeller manufacturer: ..................................... DM prop.
Propeller diameter .............................................. 1700 mm
Max. propeller speed .......................................... 2600 r.p.m.
Max. airspeed (V
NE
) ........................................... 200 km/h
Blade angle at 75% ........................................... 18 °
Max. out-of-balance ............. ……………….. 0.5 g/600 mm
Propeller purpose ............................................... tractor
2.6 Weights
Empty weight (standard version) ........................ ..275 kg
Max. take-off weight .................... .................... 450 kg
With – Emergency parachute.................................472,5
Max. landing weight ........................................... ..450 kg/ 472,5 Kg
Max. fuel weight ............................................. .... 48 kg
Max. baggage weight in baggage compartment ....10 kg
Maximum crew weight…………………………….. 180kg
Minimum crew weight ...................................... .. 55 kg
Maximum weight of baggage behind pilot’s seat….10 kg
2.7 Centre of Gravity Position
The weight and C.G. position found – empty weight :
Weight:
275
kg
C.G. Position:
+ 0,
37
metre
WARNING
The C.G.limits in flight position must be between :
+ 0,31metre and + 0,49 metre
2.7. a
Positions/distances from leading edge:
Pilots:+500 mm
Fuel tank: +400 mm
Baggage compartment: +920 mm

Apollo FOX Specifications

General

Manufacturer	Apollo Ultralight Aircraft
Type	Light Sport Aircraft
Seating capacity	2
Height	2.3 m
Engine	Rotax 912
Stall speed	65 km/h
Service Ceiling	3, 000 m