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US TA4CH
TIE DOWN
TIE DOWN
TIE DOWN
EMERGENCY
LOCATOR TRANSMITTER
INSTALLED HERE
ICI L'ELTHERE
EMPLACEMENT
DE LA RADIOBALISE
DO NOT PUSH ON SPINNER
STEP
BELOW
STEP
BELOW
GROUND
HERE
Fuel Drains Located Underneath.
Ground Aircraft before Refueling.
Note: The content of this placard
changes for different installed
equipment.
Placards and Markings
DA20-C1 AMM
Page 2
29 Apr 2004 11-20-00 Doc # DA201-C1
Rev. 9
MAINTENANCE
FUEL DRAINS
FUEL DRAINS
REFUELLING
GROUND
CAUTION
USE ONLY AVIATION
GRADE OIL !
OIL 6.0 US Qts.
5.68 L
SAE 20W-50
OR ACCORDING TO
FLIGHT MANUAL
TO OPEN CANOPY
(Inside Oil Filler Door)
(Below Fuselage)
(Below Fuselage)
1. OPEN WINDOW, UNLOCK HANDLE
2. UNLOCK OPPOSITE SIDE AND
LIFT UP CANOPY
Figure 2: General and Emergency Exterior Placards
DA20-C1 AMM
Placards and Markings
Doc # DA201-C1
Rev. 9 11-30-00 Page 1
29 Apr 2004
CHAPTER 11-30
INTERIOR PLACARDS AND MARKINGS
1. General
Figures 1 to 4 show the interior placards:
Figure 1: General Placards On The Instrument Panel
OFF
PRIME
EPU STROBE LANDING TAXI POSITION MAP INS
LIGHTS
BRIGHT
DIM
OFF
ON
Maneuvering speed V = 106kts A
Maneuvering speed V = 104kts
GPS limited for VFR only.
No smoking!
NOSE UP
NEUTRAL
NOSE DOWN
TRIM
ON
OFF
MASTER PUMP
AVIONIC FUEL GEN/BAT
Flaps
Usable
Usable
91 L/24 US gal.
MIC
This airplane is classified as a very light airplane
approved for VFR only, in non-icing conditions. All
aerobatic maneuvers, includingintentional spinning,
are prohibited. See Flight Manual for other limitations.
This airplane is classified as a very light airplane
approved for VFR only, in non-icing conditions.
All aerobatic maneuvers, except forintentional spinning
which is permitted with flaps UP only, are
prohibited. See Flight Manual for other limitations.
Note: The content
of this Placard changes
for different countries.
Refer to the Flight
Manual for the Airplane.
Note: The content of this Placard
changes for different installed equipment
CRUISE
T/O
LDG
PITOT
HEAT
L
ELEC.
D.C.
TURN COORDINATOR
INFORMATION NO PITCH 2 MI N. R
INSTRUMENT EPU TAXI STROBE PITOT LANDING POSITION MAP LIGHTS
BRIGHT DIM
OFF ON
GPS limited for VFR only.
No smoking!
S 15 21
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
0 0 0 0 0 OUTSIDE AIR TEMP.
FAHRENHEIT
A309F
+ 60 8
VDO
12 14
16 10
VOLT
GEN. GEN. CONTROL BATTERY ELECTRICAL
ADF DME AVIONICS MARKER HSI
240
Cylinder Head
100
460 600 °F
360 420
VDO
Temp.
VDO
FUEL/FLOW
US.GAL/HR
LITERS/HR
35
4
5
0
0
2
8
25
15
6
45
12
40
10
75 240
OIL
VDO
220
°F
170
Usable
74L/19.5 US gal.
VDO
0
1 1 2
1
4 3 14
FUEL
80 10
VDO
OIL
lbs./sq.inch
30 60
8
10
6
4
2
16
VDO
EGT
x100°F
14
2
2
2
5
1
2
10
10
2
1
50
3
3
3
5
5
25
50
ENGINE OIL PRESS OIL TEMP FUEL PRESS START
SLIP FUEL QTY. SYSTEM O.A.T.
TRIM FLAPS & FUEL PUMP PITOT HEAT TURN
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
C U S O T I N
20
20
15
UP 5 10
VERTICAL SPEED 100 FEET PER MINUTE
15
10 DOWN
5 0
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
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本文链接地址：
钻石20系列AMM 1(48)
