ALTITUDE LIMITATIONS
Maximum pressure altitude for takeoff
and landing: : 15000 ft (4572 m)
Maximum operating pressure altitude: : 20000 ft (6096m)
AMBIENT AIR TEMPERATURE LIMITATIONS
The minimum ambient air temperature for operation is -25°C (-13°F).
The maximum sea level ambient air temperature for operation is +45°C (113°F)
and decreases with pressure altitude at the standard lapse rate of 2°C (3.6°F) every
1000 ft (305 m) up to 20000 ft (6096 m).
POWER PLANT LIMITATIONS
The helicopter is powered by two (2) Pratt & Whitney Canada Inc. PW206C
turboshaft engine.
GAS GENERATOR (N1) RPM
NOTE
100% N1 corresponds to 58000 RPM.
All engines operative (AEO)
Continuous operation : 50 to 97.4%
Maximum continuous : 97.4%
Takeoff range : 97.4% to 98.7%
Maximum : 98.7%
Transient (20 sec) : 103.4%
RFM A109E
E.A.S.A. Approved 1-9
Rev. 45
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