A32 Data
(at 600 kgs MTOW, ISA standard conditions)
| Take-off roll | under 100 m |
| Take-off to 50’ | 230 m |
| Crosswind limit (novice) | 14 kts |
| Typical cruise TAS | 40-115 kts |
| Best climb rate | 65 kts |
| Best climb angle | 54 kts |
| Vne (never exceed) | 125 kts |
| Stall TAS (landing configuration) | 27 kts |
| Flap limit speed | 81 kts |
| Vno (manouvering speed) | 81 kts |
| Best glide speed (no flap) | 59 kts |
| Approach speed, full flap | 49 kts |
| Landing roll | under 100 m |
| Landing from 50’ | 245 m |
| MTOW (land plane) | 600 kgs |
| Typical empty weight | 315-320 kgs |
| Fuel capacity | 95 lts usable |
| Carry including fuel | 280-285 kgs |
| Usable load after full fuel | 215-220 kgs |
| Cruise endurance (912ULS) | 4.5 hrs +res |
| Wing span | 9.45 m |
| Length | 6.27 m |
| Height | 2.22 m |
| Main gear track | 1.75 m |
| Cabin width at elbows | 1.29 m |
| Operational load limits | +4 -2 G |
| Tested at 650 kgs to | +6 -3 G |