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the press-to-test function of the GEN, CANOPY and START warnings.
The main bus provides power to the GEN and CANOPY warnings through the FUEL PRESS/OIL
PRESS circuit-breaker. The GEN and CANOPY warnings operate when the related system
provides a ground for the warning lamp.
The starter side of the starter relay supplies power for the START warning. An in-line fuse protects
the circuit. The external power bus supplies the EPU warning.
Refer to the related Chapters for data about the systems. Refer to Chapter 92 for wiring diagrams.
Indicating Systems
DA20-C1 AMM
Page 2
29 Apr 2004 31-50-00 Doc # DA201-C1
Rev. 9
CANOPY
Warning
START
Warning
GEN
Warning
EPU
Warning
(Optional)
Circuit-Breakers
L
ELEC.
D.C.
TURN COORDINATOR
INFORMATION
NO PITCH
2 MIN.
R
EPU PITOT STROBE LANDING TAXI POSITION MAP INSTRUMENT
LIGHTS
BRIGHT
DIM
OFF
ON
Maneuvering speed V = 104kts GPS limited for VFR only.
No smoking!
21 S 15
NOSE UP
NEUTRAL
NOSE DOWN
TRIM
INDENT
BENDIX/KING
TST
ALT
OFF
SBY
ON 0 1
KT 76A TSO
2 3
VDO
AMPS
60
-
0
HOURS 1/10
VDO
00 0 0 0
OUTSIDE AIR TEMP.
FAHRENHEIT
A309F
+
60 8
VDO
12 14
16
10
VOLT
MSG D CLR ENT
BENDIX / KING
NRST
ON
PUSH
APT VORNDB SUP ACT NAV FPL CAL SET OTH
KLN 35A
GPS
SCAN
PULL
240
Cylinder Head
100
460
600
°F
360420
VDO
Temp.
VDO
FUEL/FLOW
US.GAL/HR
LITERS/HR
35
4
5
0
0
2
8
15 25
6
45
12
40
10
75 240
OIL
VDO
220
°F
170
Usable
80.5L/21.3 US gal.
VDO
0 11
12
14 34
FUEL
10 80
VDO
OIL
lbs./sq.inch
30 60
8
10
6
4
2
16
VDO
EGT
x100°F
14
MIC
Flaps
ON
OFF
MASTER PUMP
AVIONIC FUEL GEN/BAT
Push-On
Volume ALL
ISO
PM 501
Squelch
100
80
KNOTS
60
AIRSPEED
160
40
140
120
12:45
CONTROL
DAVTRON
SELECT
GMT LT ET
CHRONOMETER
M800
4
5
6
SUCTION
20
20
15
UP
5
10
VERTICAL SPEED
100 FEET PER MINUTE
15
10
DOWN
5
0
4
IN.Hg
1
7
6 5
20.000 FEET
ALT
mb CALIBRATED
8
TO
9
0
3
28.7
2
5 0
3
10
15
1 10 30
0 0 0
HOURS
35
0
1
HUNDREDS
25
20
RPM
OBS
N
E
W
S
B S
PULL
TEST
TSO
OFF
KX 125
BENDIX/KING
COMM
PULL
25K MODE OBS
PULL
PULL
IDENT
NAV
SB
Y OBS
S
FLAG TO
FR
SB
B
Y
N
33
30
W
24
21
S
15
12
E
6
3
PUSH
This airplane is classified as a very light airplane
approved for VFR only, in non-icing conditions.
All aerobatic maneuvers, except for intentional
spinning which is permitted with flaps UP only, are
prohibited. See Flight Manual for other limitations.
ST
A
RT
GE
N
CA
N
OPY
EP
U
BATTERY GEN. COGNETNR.OL
ELECTRICAL
DME ADF
AVIONICS
MARKER HSI
2
2
2
5
1
2
10
10
2
1
50
3
3
3
5
5
25
50
ENGINE
OIL PRESS OIL TEMP
START FUEL PRESS
SLIP
FUEL QTY.
SYSTEM
FLAPS TRIM O.A.T. &
FUEL
PUMP
PITOT
HEAT
TURN
EGT
LANDING TAXI/MAP
LIGHTS
STROBE INST. POSITION PULSE LIGHT
3 3 3
5 5
AVIONICS
CONTROL
MASTER MASTER ICS ATC NAV/COM
1 GPS
OFF
PRIME
Figure 1: Warning And Caution Locations
DA20-C1 AMM
Indicating Systems
Doc # DA201-C1
Rev. 0 31-50-00 Page 101
19 Dec 1997
TROUBLE-SHOOTING
1. General
Use the data below to trouble-shoot the warning systems.
Complaint Possible Cause Remedy
　
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