ZLIN AIRCRAFT a.s.
Chapter 7
Z 242 L Flight Manual
Description of the aircraft and its systems
REVISION No. 3
25.2.2017
EASA Approved
7 - 7
1 -
Control stick
19 -
Instrument lighting dimmers
2 -
-
20 -
Main spar flange nitrogen pressure
3 -
Transmitter pushbutton (VHF)
indicator
4 -
Canopy arrestment in open position
21 -
Wing flap lever
5 -
Lever for canopy emergency jettisoning 22 -
Longitudinal trim
6 -
Outside air thermometer
23 -
Directional trim
7 -
Adjustable pedals set handle
24 -
Headphone connection socket
8 -
Magnetic compass I
25 -
Fuel selector valve
9 -
Towing gear control
26 -
Control stick lock
10 -
Ventilation and heating control
27 -
Switches
11 -
Ignition switch
28 -
Fuses
12 -
Master switch
29 -
Ventilation windows
13 -
Throttle control
30 -
Portable fire extinguisher
14 -
Annunciator lights
31 -
Seat position adjustment lever
15 -
Signalisation check pushbutton
32 -
Brake pedal
16 -
Propeller control
33 -
COM/NAV 1, COM/NAV 2 switches
17 -
Mixture control
34 -
Alternative static pressure source
18 -
Parking brake control
(ASPS) regulation screw
35 -
Alternative static pressure source
(ASPS) switch-valve
Fig. 7-
3B Typical arrangement of pilot’s compartment from S/N 0792 incl.