M24C_AUS
M24C FLIGHT MANUAL
ISSUE B
PAGE
December 2011
53
14. FREEDOM AND INTEGRITY OF CONTROL RODS (Fig. 6)
Closely examine the condition and security of the safety
points on the control rods (1), linkages, bearings
and fibrelock nuts. There should be insignificant play in the “Uniball” rod end bearings (2) and no
evidence of corrosion or damage.
The control rods (1) should be straight and undamaged.
The control rods (1) should be free to rotate slightly around their axis when gripped and given a light twist.
Any undue force needed or inability to twist the bearing may indicate a problem of the bearing and should
be further investigated
15. TRIM SYSTEM (Fig. 7)
Verify the correct fixing of the trim actuator (1) and the integrity of the control cable (2), springs (3) and
electrical connections.
16. CLOSURE THE RIGHT HAND SIDE FAIRING (Fig. 7)
Close the right hand side fairing engaging the locks by mean of a screwdriver with 1/4 turn. Verify the
correct closing and locking of the fairing and the integrity of the hinge
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 ...
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Page 45: ...M24C_AUS M24C FLIGHT MANUAL ISSUE B PAGE December 2011 45 SECTION FLIGHT PROCEDURE 4 ...
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Page 89: ...M24C_AUS M24C FLIGHT MANUAL ISSUE B PAGE December 2011 89 SECTION EMERGENCY PROCEDURES 5 ...
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Page 111: ...M24C_AUS M24C FLIGHT MANUAL ISSUE B PAGE December 2011 111 7 5 APPENDIX 5 PERFORMANCE DATA ...
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