Aviation
AIRPLANE FLIGHT MANUAL
AQUILA AT01
Section 7
SYSTEM DESCRIPTION
Document No.: Issue: Supersedes Issue: Date: Page:
FM-AT01-1010-100E A.12 A.05 (30/09/2003) 17/09/2008 7 - 9
7.4 INSTRUMENT PANEL (Standard Equipment)
For minimum instrument requirements, refer to Section 2, Paragraph 2.12, of this manual.
No.
Description No.
Description No.
Description No.
Description No.
Description No.
Description
1
Cockpit Watch
9
Variometer
17
Voltmeter
25
Ventilation Nozzle
33
Instrument Light Switch
41
Reserved.
2
Airspeed Indicator
10
Manifold Press. Indicator
18
Ampèremeter
26
Ignition Switch
34
Cabin Light Switch
42
ELT-Rem. Contr. (opt.)
3
Turn Coordinator
11
RPM-Indicator (Prop.)
19
Engine Hour Meter
27
ALT/BAT-Switch
35
Flap Control Switch
43
Instr. Panel Light Switch
4
OAT-Indicator
12
Intercom PM 501 (opt.)
20
Cyl. Head Temp. Indicator
28
Electrical Fuel Pump
36
Trim Position Indicator
44
FLARM Display (opt.)
5
Attitude Gyro (ADI)
13
COM/NAV
21
Oil Temp. Indicator
29
Master Switch Avionics
37
Alternator Warning Light
6
Directional Gyro (HSI)
14
Transponder
22
Oil Pressure Indicator
30
NAV-Light Switch
38
Fuel Press. Warn. Light
7
Compass
15
Multifunctional Display
23
Engine Hour Meter
31
Anti-Collision-Light Sw.
39
12VDC-Receptacle
8
Altimeter
16
Fuel Level Indicator
24
Course Dev. Ind. (opt.)
32
Landing Light Switch
40
Circuit Breakers
15
34
32
31
30
27
26
25
24
40
39
25
Items 13, 14 and 15 may be arranged
interchanged among each other with
regard to their installation position.
The Engine Hour Meter is either installed
on position 23 as a circular instrument or
on position 19 as a rectangular
instrument. The respective other position
is then covered with a plate.
42
43
44
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