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1
2
3
4
5
6
7
8
9
ALT
0
10
UP
DOWN
10
5
VERTICAL SPEED
100 FEET PER MINUTE
5
15
15
20
20
2 MIN.
D.C.
ELEC.
TURN COORDINATOR
NO PITCH
INFORMATION
L R
24
27
30
33
21
18
15
12
9
6
3
0
PUSH
24
27
30
33
21
1 8
15
12
9
6
3
0
OBS
NAV
VLOC
GPS
TO
ON
ON
OFF
OFF
INSTRUMENT
FLOOD
ECU
ECU
TEST
SWAP
UT
FT
LT
S E L E C T
O .A .T . VO LTS
CO NT RO L
DAV TRON
ET
S
4
5
6
U
C T I O
N
CAUTION
WARNING WHI TE WI RE
START
DOOR S
LOW VOLTS
ENGINE FUEL TRANS GLOW
ECU A
ECU B TRIM FAI L
LOW FUEL
ALTERNATOR PITOT
ISO
MUT
E
OFF
VOLUME SQUELCH VOLUME SQUELCH
PILOT CO-PILOT
PWR/XMT
ALL
T/O V = 108 kts F E
108 KIAS
91 KIAS
LDG V = 91 kts FE
max.
max.
GARMIN
P WR
PU SH
PU SH
VOL
VOL
SQ
ID
C
C
V
V
D
RNG
CLR
DE FA ULT
NA V
ENT
GPS
GNS 4 30
MENU
PUSH
C/V
PUSH
CRSR
COM
VLOC
COS
136.975
VLOC
117.95
TERM
GPS
KHPN
KHPN
NAV
CDI OBS MSG FPL PROC
WPT
DIS
TKE
GS
4.85
000º
165
118.000
108.00
n
m
kt
GTX 327
IDEN T FUNC
ON
STBY
OFF
ALT
VFR START
STOP
CRSR
CLR
0
GARM IN
1 2 3 4 5 6 7 8 9
ALT
R
PRESSURE ALT 1200 12300ft
RPM
LOAD
Oil Pressure Cooling Temp
Oil Temp Gearbox Temp
L Fuel Quantity R Fuel Quantity
Water Level
L Fuel Temp ( ºC) R Fuel Temp (ºC)
Ampere
Fuel Flow
Volt
0
I N. Hg
CA L IB RAT E D
T O
2 0,0 0 0 F EE T
m b
28.7
28.8
97528.6
970
100
FEET
1
2
3
4
5
6
7
8
9
ALT
28 VDC ACCESSORY PWR
GROUND OPS . O NLY 2A MAX
28 VDC ACCESSORY PWR
GROUND OPS. ONLY 2A MAX
For
For
Steer
Steer
Date RADIOS ON
N
S
30 60 E 120 150
210 240 W 300 330
ON
OFF
CABIN
LO
CK
RELEASE
DE
FR
OS
T
PA
R
KIN
G
B
R
AKE
HEAT
FLOO
R
ON
OFF
CABIN
LOCK
RE
L
EASE
D
EF
R
O
ST
PA
RKIN
G
B
RAKE
HEAT
FLOOR
A LT ERNAT E AIR
A LT ERNAT E AIR
ON
ALTERNATE AIR
UP
T/O
LDG
max
max
View A
A
Maneuvering speed
VA = 108 KIAS above 980 up to 1150 kg / above 2161 up to 2535 lb)
VA = 94 KIAS (780 to 980 kg / 1720 to 2161 lp)
This airplane may only be operated in accordance with the Airplane Flight
Manual. It can be operated in the "Normal" and "Utility" categories in
non-icing conditions. Provided that national operational requirements
are met and the appropriate equipment is installed, this airplane is approved
for the following kinds of operation: day VFR and night VFR.
All aerobatic maneuvers including spinning are prohibited. For
further operational limitations refer to the Airplane Flight Manual.
No smoking
Emergency Fuel Valve
NORMAL
OFF
EMERG. TRANSFER
CAUTION intermit tent use onl y
(see AFM)
100%
IDLE
Emergency Fuel Valve
NORMAL
OFF
EMERG. TRANSFER
CAUTION intermittent use only
(s ee AFM)
LO
HI
FRICTION
OE-XXX OE-XXX
Ess. Bus not for normal operation. See AFM
Ess. Bus not for normal operation. See AFM
Figure 2: Instrument Panel Placards and Markings -
Airplanes with the TAE 125 Diesel Engine Installed
AIRCRAFT
Placards and Markings DA 40 Series
AMM
Page 4
20 Sep 2007 11-31-00 Doc # 6.02.01
Rev. 5
Intentionally left blank
AIRCRAFT
DA 40 Series
AMM
Servicing
Doc # 6.02.01
Rev. 5 12-TITLE Page 1
20 Sep 2007
CHAPTER 12
　
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本文鏈接地址：鉆石40系列AMM 1(66)