Aeroprakt A22LS Foxbat
The A22LS is the load carrier of the Foxbat family. Powered by the 4-stroke liquid-cooled Rotax 912ULS 100 hp engine, it is perfect for flying training, two-up touring and for the sport pilot who often flies with a friend. It comes standard with long range tanks, giving it a duration of over 6 hours with a reserve.
It has a legal carrying capacity of around 290 kilos, although the airframe is stressed to be safe to carry up to around 340 kilos. This weight includes the pilot, passenger/co-pilot, fuel and baggage.
Its empty weight is around 310 kilos, so with 100 hp to play with, there’s plenty of performance available. Take-off and landing distances are a little longer than the A22L but still typically under 75 metres at MTOW.
Dimensions
A22LS Foxbat
|
MTOW (certified legal) |
600 kgs |
|
MTOW (airframe design) |
650 kgs |
|
Typical empty |
310 kgs |
|
Usable |
290 kgs |
|
Max baggage (rear) |
20 kgs |
|
Wingspan |
9.55 m |
|
Length |
6.23 m |
|
Height (top of fin) |
2.40 m |
|
Main gear track |
1.76 m |
|
Wing area |
12.62 sq m |
|
Wing loading |
47.54 kg/sq m |
|
Aspect ratio |
7:1 |
|
Mean Aerodynamic Chord |
1.4 m |
|
Glide ratio |
11.0:1 |
|
Cockpit width |
128+ cms / 50+ inches at elbow & shoulder |
|
Standard engine |
Rotax 912ULS (100 bhp) |
|
Standard propeller |
3-blade carbon fibre, on-ground adjustable |
|
Max fuel capacity |
2 x 57 litre wing tanks, total 112 litres usable |
Performance at MTOW, nil wind, ISA Standard Day
A22LS Foxbat
|
Take off run |
under 75 m |
|
Landing run |
under 75 m |
|
Stall (full flap, idle) |
32 kts |
|
Max flap speed |
83 kts |
|
Max manoeuvre Va |
99 kts |
|
Max level TAS |
115 kts |
|
Never exceed Vne |
120 kts |
|
Normal cruise |
100 kts/> 18 lph |
|
Economy cruise |
90 kts/> 14 lph |
|
Crosswind max (no flap) |
17 kts |
|
Service ceiling |
16,500 ft |
|
Range |
615 nm |
|
Typical cruise duration |
6.25 hrs + reserve |
|
Best climb at MTOW |
900+ fpm |
|
Typical rate of climb, single person |
1,400+ fpm |
|
Tested load factors |
+6 -3 g |
|
Operational load factors |
+4 -2 g |




