Pilot´s Operating Handbook
EXTRA 200
2.5
PROPELLER
MT-Propeller Entwicklung GmbH, Federal Republic of Germany
Type: MTV-12-B-C/C183-17e
Max. Takeoff RPM:
Max. Continuous RPM:
2.6
WEIGHT LIMITS
Max. allowed empty weight:
-Normal category
-Acrobatic category ( 1 seat)
Max. allowed T/O weight:
-Normal category
-Acrobatic category ( 1 seat)
Max. allowed landing weight:
2.7
WEIGHT AND C.G. ENVELOPE
Vertical reference = firewall.
Horizontal reference = upper longerons in cockpit.
2.7.1
NORMAL FLIGHT
Max T/O Weight:
840 kg (1858 lbs)
(and below)
2.7.2
ACROBATIC FLIGHT (1 SEAT)
Max T/O Weight:
700 kg (1549 lbs)
(and below)
2.7.3
ACROBATIC FLIGHT (2 SEATS)
Max T/O Weight:
800 kg (1770 lbs)
(and below)
Page Date: 28. February 2006
Page Date: 20. April 2002
2700
2500
( 2 seats)
( 2 seats)
forward C.G.
73,2 cm (28,8")
forward C.G.
73,2 cm (28,8")
forward C.G.
73,2 cm (28,8")
646 kg (1424lbs)
591 kg (1302lbs)
606 kg (1335lbs)
840 kg (1858 lbs)
700 kg (1549 lbs)
800 kg (1770 lbs)
840 kg (1858 lbs)
rear C.G.
89.1 cm (35.0")
rear C.G.
89.1 cm (35.0")
rear C.G.
89.1 cm (35.0")
Section 2
Limitations
2 - 5
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