Airplane Flight Manual XA42
AFM-XA42-0040-002-A.01
Page 3
EASA approved
Page date
Chapter 02
24.01.2011
2.5
PROPELLER
MT-Propeller MTV-9-B-C/C203-20d, 3-blade hydraulic constant speed
RPM limits
Max. takeoff:
Acrobatic
2700 rpm
Utility
2670 rpm
Max. continuous:
2500 rpm
2.6
WEIGHT LIMITS
Maximum empty weight
• Utility:
670 kg / 1477 lbs
• Acro:
670 kg / 1477 lbs
Maximum take-off weight
• Utility:
999 kg / 2200 lbs
• Acro:
850 kg / 1874 lbs
Maximum landing weight
• Utility:
999 kg / 2200 lbs
• Acro:
850 kg / 1874 lbs
2.7
WEIGHT AND CENTER OF GRAVITY ENVELOPE
Reference planes for CG calculations: • vertical:
firewall
• horizontal:
straight part of cockpit frame
2.7.1
UTILITY FLIGHT
Maximum takeoff
weight
Forward CG
Rear CG
999 kg / 2200 lbs
550 mm / 21,65 in / 25 %
700 mm / 27.55 in / 33 %
2.7.2
ACROBATIC FLIGHT
Maximum takeoff
weight
Forward CG
Rear CG
850 kg / 1874 lbs
550 mm / 21,65 in / 25 %
700 mm / 27.55 in / 33 %
2.8
BAGGAGE
Maximum allowable baggage is 10 kg / 22 lbs securely stowed
in the baggage compartment behind the pilot´s seat
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