Technical data

Page Date: 6. April 2010 2 - 3
Pilot´s Operating Handbook
EXTRA 300LT
Section 2
Limitations
2.1 GENERAL
This section includes operating limitations, instrument markings, and basic placards
necessary for the safe operation of the aircraft, its engine, standard systems, and standard
equipment. The limitations included in this section have been approved by the EASA.
Observance of these operating limitations is required by national aviation regulations.
N O T E
In case of an aircraft equipped with specific options additional information required
for safe operation will be contained in Section 9 "Supplements".
Instrument markings and placards are provided for the acrobatic category only; for normal
category refer to corresponding limitations. This aircraft is certified under Type Certification
Data Sheet (T.C.D.S. EASA.A.362).
Any exceedance of given limitations has to be reported by the pilot so that necessary
inspection or maintenance procedures according to the MAINTENANCE MANUAL EA 300LT
can be performed .
2.2 AIR SPEED (IAS)
Never Exceed Speed V
NE
221 knots (409 km/h)
Max. Structural Cruising Speed (Normal Cat.) V
NO
143 knots (265 km/h)
Max. Structural Cruising Speed (Acro Cat. I , II, III) V
NO
160 knots (296 km/h)
Maneuver Speed (Normal Cat.) V
A
143 knots (265 km/h)
Maneuver Speed (Acro Cat. I , II, III) V
A
160 knots (296 km/h)
2.3 CROSS-WIND COMPONENT
Max. demonstrated cross-wind component for take-off and landing is 15 knots (27 km/h).
2.4 ENGINE
Engine-type: Textron-Lycoming AEIO-580-B1A
Rated maximum power: 235 kW (315 HP) @ 2700 rpm.
2.4.1 FUEL
Minimum grade aviation gasoline: 100/100LL; for alternate fuelgrades see latest revision of
Lycoming S.I. No. 1070.
Total fuel capacity: 221 L (58.4 US.gal)
Usable fuel capacity: 209 L (55.2 US.gal)
Total fuel capacity for acrobatic in acro & center tank: 69 L (18.2 US.gal)
Usable fuel capacity for acrobatic in acro & center tank: 67 L (17.7 US.gal)
For acrobatic flight wing tanks must be empty.