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 - 1
SECTION 7 - DESCRIPTION OF THE AIRCRAFT AND ITS
SYSTEMS
CONTENTS
Section
Page
7.1
General
7 - 3
7.3
Airframe
7 - 3
7.5
Flight controls
7 - 4
7.7
Instrument panel
7 - 6
7.11
Ground control
7 - 12
7.13
Wing flaps
7 - 12
7.15
Landing gear
7 - 13
7.17
Baggage compartment
7 - 13
7.19
Seats, seat belts and shoulder harnesses
7 - 13
7.21
Doors, windows and exits
7 - 15
7.23
Control locks
7 - 16
7.25
Engine
7 - 17
7.27
Propeller
7 - 22
7.29
Fuel system
7 - 23
7.33
Brake system
7 - 25
7.35
Power steering
7 - 26
7.37
Electrical system
7 - 26
7.39
Lighting system
7 - 30
7.43
Heating, ventilating, defrosting and air conditioning
7 - 32
7.49
Pitot pressure system
7 - 34
7.51
Static pressure system
7 - 34
7.57
Stall warning or angle of attack system
7 - 34
7.59
Icing equipment
7 - 36
7.61
Avionics
7 - 36
7.65
Cabin features
7 - 36