M24C_AUS
M24C FLIGHT MANUAL
.
PAGE
ISSUE B
32
December
2011
WARNING:
115% power can be used when necessary for takeoff operations, always
taking care not to exceed the engine’s maximum speed (5800 r.p.m.).
NOTE:
The maximum continuous power is limited to 100% of the available power.
The maximum available power (115%) can only be used for not more than 5 minutes. After 5
minutes, the red “DANGER” warning light is activated and the turbo’s management system
automatically reduces the delivered power until reaching maximum continuous power
(100%).
2.6.e ROTOR BRAKE LEVER (Fig. 11)
This lever is used to stop the rotation of the rotor after landing and during all taxiing, holding-point and
parking operations.
-
To engage the brake pull up the lever (1) to vertical position; when the rotor brake is engaged
the warning light (2) “BRAKE” comes on.
Summary of Contents for M-24C Orion
Page 9: ...M24C_AUS M24C FLIGHT MANUAL ISSUE B PAGE December 2011 9 SECTION INTRODUCTION 1 ...
Page 37: ...M24C_AUS M24C FLIGHT MANUAL ISSUE B PAGE December 2011 37 SECTION OPERATING LIMITS 3 ...
Page 39: ...M24C_AUS M24C FLIGHT MANUAL ISSUE B PAGE December 2011 39 ...
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Page 45: ...M24C_AUS M24C FLIGHT MANUAL ISSUE B PAGE December 2011 45 SECTION FLIGHT PROCEDURE 4 ...
Page 72: ...M24C_AUS M24C FLIGHT MANUAL PAGE ISSUE B 72 December 2011 ...
Page 89: ...M24C_AUS M24C FLIGHT MANUAL ISSUE B PAGE December 2011 89 SECTION EMERGENCY PROCEDURES 5 ...
Page 94: ...M24C_AUS M24C FLIGHT MANUAL PAGE ISSUE B 94 December 2011 ...
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Page 101: ...M24C_AUS M24C FLIGHT MANUAL ISSUE B PAGE December 2011 101 SECTION APPENDIX 7 ...
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Page 107: ...M24C_AUS M24C FLIGHT MANUAL ISSUE B PAGE December 2011 107 7 3 APPENDIX 3 ENGINE PARAMETERS ...
Page 108: ...M24C_AUS M24C FLIGHT MANUAL PAGE ISSUE B 108 December 2011 ...
Page 111: ...M24C_AUS M24C FLIGHT MANUAL ISSUE B PAGE December 2011 111 7 5 APPENDIX 5 PERFORMANCE DATA ...
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