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1-5
Document No.:
EV97SLNOEN
Date of Issue:
02/2008
Revision:
-
1.4 Contents
1.
GENERAL ..................................................................................................................................1-1
1.1
I
NFORMATION SOURCE
................................................................................................................1-2
1.2
R
ECORD OF REVISIONS
................................................................................................................1-3
1.3
L
IST OF
E
FFECTIVE
P
AGES
...........................................................................................................1-4
1.4
C
ONTENTS
.................................................................................................................................1-5
2.
TECHNICAL DESCRIPTION......................................................................................................2-1
2.1
B
ASIC AND GENERAL INFORMATION
...............................................................................................2-2
2.1.1
Designation ..............................................................................................................................2-2
2.2
B
ASIC TECHNICAL DATA
...............................................................................................................2-3
2.2.1
Airplane views ..........................................................................................................................2-3
2.2.2
Three-view drawing ..................................................................................................................2-4
2.2.3
Basic dimensions......................................................................................................................2-5
2.2.4
Weight......................................................................................................................................2-6
2.2.5
Center of gravity.......................................................................................................................2-6
2.2.6
Operating limitations.................................................................................................................2-6
2.3
T
ECHNICAL DESCRIPTION OF THE AIRPLANE
....................................................................................2-7
2.3.1
General ....................................................................................................................................2-7
2.3.2
Fuselage ..................................................................................................................................2-7
2.3.3
Wing.........................................................................................................................................2-7
2.3.4
Horizontal tail unit .....................................................................................................................2-8
2.3.5
Vertical tail unit.........................................................................................................................2-8
2.3.6
Landing gear ............................................................................................................................2-9
2.3.7
Cockpit...................................................................................................................................2-16
2.3.8
Equipment..............................................................................................................................2-19
2.3.9
Avionics..................................................................................................................................2-21
2.3.10
Additional equipment...........................................................................................................2-22
2.3.11
Control system....................................................................................................................2-25
2.3.12
Powerplant..........................................................................................................................2-35
2.3.13
Fuel system ........................................................................................................................2-43
2.3.14
Engine lubrication system scheme ......................................................................................2-45
2.3.15
Cooling system description..................................................................................................2-46
2.3.16
Heating ...............................................................................................................................2-47
2.3.17
Ventilation...........................................................................................................................2-48
2.3.18
Wiring .................................................................................................................................2-49
2.3.19
Pitot-static system...............................................................................................................2-50
2.3.20
Placards..............................................................................................................................2-51
3.
OPERATION ..............................................................................................................................3-1
3.1
O
PERATION OUTLINES
.................................................................................................................3-2
3.2
A
IRPLANE ASSEMBLY
...................................................................................................................3-3
3.2.1
Wing.........................................................................................................................................3-3
3.2.2
Horizontal tail unit ...................................................................................................................3-10
3.2.3
Vertical tail unit.......................................................................................................................3-11
3.2.4
Landing gear ..........................................................................................................................3-12
3.2.5
Cockpit canopy.......................................................................................................................3-15
3.2.6
Installation and reinstallation of instruments............................................................................3-15
3.3
L
EVELING
.................................................................................................................................3-16
3.4
M
EASUREMENT OF CONTROL SURFACES DEFLECTIONS
..................................................................3-17
3.4.1
Required deflections...............................................................................................................3-17
3.4.2
Aileron deflection measurement..............................................................................................3-18
3.4.3
Flap deflection measurement..................................................................................................3-18
3.4.4
Elevator deflections measurement..........................................................................................3-19
3.4.5
Rudder deflection measurement .............................................................................................3-19