025-00-16C M16C FLIGHT MANUAL, Issue G
02 March 2016
Page 17
2.4 GENERAL CONFIGURATION
2.4.1 DESCRIPTION OF MAIN
COMPONENTS
1 - Rotor
2 - Rotor blade hub-bar
3 - Rotor head
4 - Rotor brake
5 - Bendix gear
6 - Rotor control rods
7 - Trim control unit
8 - Trim actuator
9 - Fork unit
10
– Pre-rotation flexible shaft
11
– Pre-rotation unit
12 - Ground adjustable pitch
three bladed pusher propeller
13 - ROTAX piston engine
14 - Fuel tank cap
15 - Fuel tank
16 - Oil tank
17 - Radiator
18 - Battery
19 - Exhaust manifold
20 - Structure
21 - Main undercarriage
22 - Wheel
23 - Front steering wheel
24 - Stabilizer
25 - Winglet
26 - Rudder
27 - Trim tab
28 - Pilot/passenger cockpit
29 - Landing light
30 - Dynamic intake
31 - Pilot windscreen
32 - Pilot seat
33 - Passenger windscreen
34 - Passenger seat
35 - Instrument panel
36 - Control stick
37 - Rudder pedals
38 - Mast upper part
39 - Fin
40 - Heat exchanger
Содержание M-16 C
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