Wing Area
30.15 m2
(324.54 ft2)
5.70 m (16 ft 10 in.)

Height
3.20 m (10 ft 6 in.)
Length 10.90 m (35 ft 9 in.)
Wing Span 15.87 m (52 ft 1 in.)

3.00 m
(9 ft 10 in.)

WEIGHT AND BALANCE

BASIC EMPTY WEIGHT (STANDARD IFR) The basic empty weight is defined as the complete aircraft, empty of usable fuel and without optional equipment, but including engine oil, unusable fuel and items of equipment that are an integral part of the basic aircraft.  1,400 KG*  3,086 LB* 
MAXIMUM OPERATING WEIGHTS MAX. RAMP WEIGHT MAX. TAKE-OFF WEIGHT MAX. LANDING WEIGHT MAX. ZERO FUEL WEIGHT The above weights comply with CAR 3.  2,810 KG 2,800 KG 2,660 KG 2,400 KG  6,195 LB 6,173 LB 5,863 LB 5,291 LB 
CENTRE OF GRAVITY RANGE UP TO 1,450 KG (3,197 LB) AT 2,800 KG (6,173 LB) With linear variation between given points.  11% TO 38% MAC 32% TO 38% MAC 
SPEEDS 
Equivalent Air Speeds (EAS) at Max. Operating Weight DESIGN DIVING SPEED (VD) NEVER EXCEED SPEED (VNE) DESIGN CRUISING SPEED (VC) MAX. FLAP EXTENDED SPEED (VFE) STALL SPEED (IDLE POWER) WITH FLAPS UP (VS) STALL SPEED (IDLE POWER) WITH FLAPS DOWN (VSO) MAX. SPEED IN LEVEL FLIGHT WITH MAX. CONTINUOUS POWER (VH)  167 KNOTS 151 KNOTS 119 KNOTS 95 KNOTS 58 KNOTS 52 KNOTS 125 KNOTS 
RANGE 
MAX. RANGE AT OPTIMUM SPEED, NO RESERVES, AT 10,000 FT ENDURANCE AT OPTIMUM SPEED, NO RESERVES MAX RANGE WITH UNDERWING TANKS** ENDURANCE WITH UNDERWING TANKS** AVERAGE FUEL CONSUMPTION  500 NM 4 H 20 MIN 870 NM 7 H 35 MIN 148 LITRES/H (39 US GAL/H) 
* 1,250–1,400 kg (2,750–3,086 lb) depending on configuration. ** Two x 243.5 litres (64 US gal) usable capacity. 

PERFORMANCE

ALTITUDE LIMITS
MAX. OPERATING ALTITUDE  25,000 FT 
SERVICE CEILING (AT MAX. WEIGHT)  20,500 FT 
TEMPERATURE LIMITS 
MINIMUM  – 55° C 
MAXIMUM  + 55° C 
NORMAL LOAD FACTORS MAX. POSITIVE G  + 3.58 G 
MAX. NEGATIVE G  – 1.43 G 
MAX. POSITIVE G WITH FLAPS DOWN  + 2.00 G 
WING LOADING  92.87 KG/M2  19.02 LB/FT2 
CLIMB MAX. RATE OF CLIMB AT SEA LEVEL  1,010 FT/MIN 
MAX. RATE OF CLIMB AT 5,000 FT  935 FT/MIN 
TAKE-OFF AND LANDING PERFORMANCE NORMAL CONDITIONS 
TAKE-OFF GROUND ROLL AT SEA LEVEL  197 M  646 FT 
TAKE-OFF DISTANCE TO 15 M (50 FT)  475 M  1,558 FT 
LANDING GROUND ROLL AT SEA LEVEL*  127 M  417 FT 
LANDING DISTANCE FROM 15 M (50 FT)* * Reverse thrust selected on touchdown.  315 M  1,033 FT