Apollo Fox

EA-81 SUBARU

Engine Type                All-aluminum, 4-cylinder, 4-stroke, liquid-cooled
Displacement             1781 cc
Power Output              100 hp
Bore                              92 mm
Stroke                           67 mm
Fuel                               Unleaded (automotive)
Weight                          90 kg
Reduction Ratio         2.2 : 1
Prop Rotation             Clockwise
Reduction System     HTD belt (60 mm. wide)
Cooling                        Liquid (water-glycol mixture)
Ignition                         Electronic, single spark plugs
Alternator                     45 amp
Carburetion                 Dual Bing altitude-compensating carburetors
Fuel Consumption     0.24 kg./hp/hr @ 75% power
Starter                           Electric gear reduction

The Apollo Fox is built according to the "BCAR" Section S constuction norm.
The aircraft has welded steel alloy tube fuselage covered with "ceconite"
fabric. The wing are made of aluminium alloy both spars and ribs and then
covered with "ceconite". Wing can be folded backwards. One pilote can do it
within 10 minutes. The landing gear is aluminium plate sheet system, like
on all Cessna. Wheels are equipped with hidraulic disc or mechanic drum
brakes. Apollo Fox has very good rudder harmony and very easy to fly and
land.
Available tail or nose wheel configurations.
Engine: Rotax 582 UL Mod 99 (65Hp), 912UL (80 Hp), 912 ULS (100 Hp),
Jabiru 2200 (80Hp), Subaru EA 81 (100 Hp).
Propeller: 2 blades wooden or 3-4 blades plastic, fiberglass, carbon
ground or air adjustable propellers.