% % % Figure 1: Interior Placards and Markings - Airplanes with the TAE 125 Diesel Engine Installed %
Page 2 Doc # 6.02.01 09 Jan 2003 Rev. 4
11-31-00
DA 40 Series
Placards and Markings
AMM AIRCRAFT
% 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 For
N 30 60 E 120 150
non-icing conditions. Provided that national operational requirements% are met and the appropriate equipment is installed, this airplane is ap-
Steer
proved for the following kinds of operation: day VFR and night VFR.
21S 15
All aerobatic maneuvers including spinning are prohibited. For
For
S 210 240 W 300 330
% further operational limitations refer to the Airplane Flight Manual.
N 30 60
E 120 150 Steer For
Steer
For S 210 240 W 300 330
No smoking
Steer
Date RADIOS ON
RADIOS ONDate
%
CAUTION
WARNING
WHITE WIRE
PWR/XMT5
START ALTERNATOR PITOT
OE-XXX
PILOT CO-PILOT
%
4
6
DOORS ECU A LOW FUEL
M ISO U ALL
LOW VOLTS ECU B TRIM FAIL T
OE-XXX
S N EU IO
CT OFF VOLUME SQUELCH VOLUME
ENGINE FUEL TRANS GLOW
SQUELCH GNS 430
GARMIN
INSTRUMENT
EMERG. TRANSFER
RNG
C
COS
WPT
PWR
KHPN
C
ON 136.975 RPM
VOL PUSH
KHPN
SQ
0
D MENU
118.000 DIS
%
9
1
V
n
VLOC 4.85
VOL PUSH
m CLR ENT
160
ID
V 117.95 TKE
OFF
40
NAV 000o
AIRSPEED 108.00
8
2
DEFAULT
ALT
GPSTO NAVCOM Oil Pressure Cooling Temp140 VLOC GSFLOOD
VLOC
TERM
IN.Hgmb
165 k
CALIBRATED tON 28.7
TO
PUSH PUSH CRSR Oil Temp Gearbox Temp
GPS NAV
20,000 FEET C/V
KNOTS
GPS120
73
60 CDI OBS MSG FPL PROC
%
100
OFF
ECU
80
64
5
OBSTO LOAD
SWAP ECU
D.C.
0
ELEC.
24
10 Water Level 15
9
%
1
5TEST
L Fuel Quantity R Fuel Quantity
UP VERTICAL SPEED
82
ALT
100 FEET PER MINUTE
L Fuel Temp (oC) R Fuel Temp (oC)
20
33
IN.Hg
15
mb
0
CALIBRATED
TO
28.7O.A.T. VOLTS
20
20,000 FEET
TURN COORDINATOR
Ampere Volt
73
DOWN
L
R
15
5 64
UT LT
%
2 MIN. Fuel Flow
5
6
10
FT ET NO PITCH PUSH
INFORMATION
SELECT CONTROL
DAVTRON
Ess. Bus not for normal operation. See AFM
T/O V = 108 ktsLDG V FE = 91 kts
FE
%
GTX 327
GARMIN
ON
IDENT
FUNC CRSR
PRESSURE ALT
1200
ALT ALTmax.
START
12300f
108 KIAS
tRVFR CLRSTOP
%
%
%
%
%
%
%
%
%
%
max.
91 KIAS
01234 567 89
5303070303 3 5 5 510510101025510155 5 3 3 105 325103 3 5155 3302
28 VDC ACCESSORY PWR GROUND OPS. ONLY 2A MAX
L D
P
ON
O C
A
C
E R
K
A F K
B I
R I
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本文鏈接地址：鉆石40飛機維護手冊 DA 40 SERIES AMM 1(78)
