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Apollo Fox


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 wings are made of aluminium alloy both spars and ribs and then covered with ceconite.
Wing can be folded backwards. One pilot can do it within 10 minutes. The landing gears are aluminium plate sheet as year suspension. Wheels are equipped with hidraulic disc or mechanical drum brakes.

Available tail or nose wheel configurations.

Engine opts:
Rotax 582 UL Mod 99 (65Hp)
Rotax 912UL (80 Hp)
Rotax 912 ULS (100 Hp)
Jabiru 2200 (80Hp)
Subaru EA 81 (100 Hp).

Stall: 35 kt / 40 mph / 64 kmh
Cruise: 81 kt / 93 mph / 150 kmh
VNE: 97 kt / 112 mph / 180 kmh
Empty Weight: 274 kg / 604 lbs
MTOW Weight: 450 kg / 992 lbs
Take-off distance (50ft obstacle): 460 ft / 140 m
Landing distance (50ft obstacle): 660 ft / 200 m


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