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The Aircraft

XA42 (2-seater)

 

IMG 1814IMG 0372 
 

Performance

ENGINE Lycoming AEIO 580 B1A 315 hp (230 kw)
MAX. LEVEL SPEED IAS @ 3000 ft. Powersetting 100% 210 kts
Powersetting 75% 185 kts
ROLL RATE 450°/second
STALL SPEED 53 kts
RATE OF CLIMB 3200 ft/min
TAKE OFF OVER 50 ft OBSTACLE 260 m / 853 ft
LANDING OVER 50 ft OBSTACLE 400 m / 1312 ft
RANGE @ 75% Powersetting = 205kts TAS @ 10,000ft 800 NM

Dimensions

WING SPAN 7.50 m / 24.6 ft
WING AREA 11.25 m2 / 121.25 sq.ft
ASPECT RATIO 5
STABILIZER / ELEVATOR SPAN 3.20 m / 10.5 ft
STABILIZER / ELEVATOR AREA 2.98 m2 / 32.1 sq.ft
OVERALL LENGTH L 6.6 m / 21.6 ft
OVERALL HEIGHT, GROUND ATTITUDE 2.3 m / 7.5 ft

Weights

EMPTY WEIGHT 610 kg / 1344 lbs
MAX. TAKE OFF WEIGHT "Aerobatic" 850 kg / 1875 lbs
"Utility"  999 kg / 2200 lbs
WING LOADING "Aerobatic" 75.5 kg/m² / 15.4 lb/ft²
"Utility" 84.4 kg/m² / 17.3 lb/ft²

G Limits

"Aerobatic flight" +/-10G
"Utility" +4,4G / -2G

Design Speeds

VA 174 kts / 322 km/h
VC 185 kts / 345 km/h
VNE 225 kts / 416 km/h

RB-3sRB1s 

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