| Maximum Take Off Weight | 1057kg |
| Basic Empty Weight | Refer to individual aircraft flight manual |
| Minimum Payload | MTOW - BEW |
| Fuel Capacity | 48 US gal, or 181 litres, usable |
Percentage of power, fuel flow and RPM for given altitudes (mixture leaned to best power setting)
|
| Power |
Litres/hour |
Height and RPM |
| 2000' |
4000' |
6000' |
| 55% |
|
|
|
|
| 65% |
|
|
|
|
| 75% |
|
|
|
|
|
| Oil | 8 US quarts max (normally operate at 6 US quarts) |
| Airspeeds | KIAS |
| VNE (never exceed) | 160 |
| VNO (normal operating) | 126 |
| VA (manoeuvring at MTOW) | 111 |
| VS0 (stall with full flap at MTOW) | 44 |
| VS1 (stall with no flap at MTOW) | 50 |
| VX (best angle of climb) | 66 |
| VY (best rate of climb) | 76 |
| Cruise climb | 85 |
| VFE (maximum flap operating speed) | 103 |
| Best glide speed (MTOW) | 76 |
| Takeoff safety speed | see POH |
| Minimum approach speed (Full flap at MTOW) | 63 |
| Minimum approach speed (No flap at MTOW) | 65 |
| Turbulence penetration speed (keeping the speed down minimises risk of structural damage) | 111 |
| Maximum crosswind | 17 |