Page Date: 20. April 2002
2 - 5
Pilot´s Operating Handbook
EXTRA 300L
Section 2
Limitations
f) Cylinder head temperature
-Max
260°C
500°F
2.5
PROPELLER
MT-Propeller Entwicklung GmbH, Federal Republic of Germany
a) Type MTV-14-B-C/C190-17
-Maximum Take-Off and Maximum Continuous
2700 rpm
b) Type MTV-9-B-C/C200-15
-Maximum Take-Off (5 min)
2700 rpm
-Maximum Continuous
2400 rpm*
N O T E*
RPM limitation due to compliance with applicable noise protection requirements
(FAR 36). However for non-US registered airplanes an enhanced rotational speed
limitation of 2700 RPM may be permissable when registered in the Acrobatic
Category only as ICAO Annex 16 grants an exception for airplanes specially
designed for acrobatic purposes.
2.6
WEIGHT LIMITS
Max allowed empty weight:
-Normal category
745 kg (1643lbs)
-Acrobatic category ( 1 seat)
701 kg (1546lbs)
( 2 seats)
665 kg (1466lbs)
Max allowed T/O weight:
-Normal category
950 kg (2095 lbs)
-Acrobatic category ( 1 seat)
820 kg (1808 lbs)
( 2 seats)
870 kg (1918 lbs)
Max allowed landing weight:
950 kg (2095 lbs)
2.7
WEIGHT AND C.G. ENVELOPE
Vertical reference = fire-wall.
Horizontal reference = upper longerons in cockpit.
2.7.1
NORMAL FLIGHT
Max T/O Weight:
forward C.G.
rear C.G.
950 kg (2095 lbs)
67.1 cm (26.4")
84.1 cm (33.1")
(and below)
2.7.2
ACROBATIC FLIGHT (1 SEAT)
Max T/O Weight:
forward C.G.
rear C.G.
820 kg (1808 lbs)
67.1 cm (26.4")
84.1 cm (33.1")
(and below)
Page Date: 5. December 2008
Page Date: 8. October 2009
Summary of Contents for 300L
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