L E A N
IFR. All aerobatic maneuvers including spinning are prohibited. For further operational limitations refer to the Airplane Flight Manual.
No smoking.
location shown for IFR models located below COM/NAV in VFR models
LP O
ON
D A CC E R KA F KB R II O NN S G
T
H E A T
OFF
F L O O R B R A K E
R E L E A S E
20 US gal. 20 US gal.
76 l 76 l
OFF
% Figure 2: Instrument Panel Placards for Larger Instrument Panels
Doc # 6.02.01 Page 3
Rev. 4 09 Jan 2003
11-30-00
DA 40 Series
Placards and Markings
AMM
AIRCRAFT
EGT/CHT EGT/CHT AUTOTRACK FUEL/COMP FLIGHT
only when GPS,
N 30
60
E 120 150
IFR For
GRAPH DIGITAL ON/OFF MODE DATA
limited to VFR use,
%
H OFF models Steer
O is installed
R only
For
S 210
240 W
300
330
Z
% GPS limited to VFR use only.
ON ON Steer
RADIOS ON
%
Date
EMERGENCY
only when autopilot is installed
I
% Limitations for KAP 140 Autopilot System:
or (see Chapter 28):
Do not use AP if "Alternate Static" is open. N
D U I N C I
% Autopilot OFF during take-off and landing.
IFR NAV1 A
T
Maximum speed for autopilot operation is 165 KIAS. T
S
Minimum speed for autopilot operation is 70 KIAS. models I
O
% Minimum altitude for autopilot operation:
N
Cruise, Climb, Descent and Maneuvering: 800 feet AGL only
NAV2
IN.
or (for longe range tanks, see Ch. 28):
Approach: 200 feet AGL MA N
HG
%
Fu el/
PSI % only when O il
GRND COM2
ON
°F
Te mp
Ground COM2 A ll
21 S 15
% switch is inst'd
US
For N 30 60 E 120 150
Fuel
Steer
gal/
% OFF
For S 210 240 W 300 330
(O.M 40-121)
Flow h our
Steer
Date RADIOS ON
GPS limited to VFR use only.
% GRND COM2
ON
OFF
%
Limitations for KA P 140 Autopilot S ystem:
D o notuse AP i f"AlternateStatic " isopen.
A utopilot OFFd uring take -off andlanding.
M axim um speed forautopilot operationis165 KIAS.
M inim um speed for autopilot op erationis70 K IAS.
M inim um altitud efor autopiloto peration:
C ruise, Climb,D escentand Ma neuvering:800 feet AGL
A pproach: 200 feet AGL
%
% EGT/CHT EG T/CHT AUTOTR ACK FUEL/COMP FLIGHT
GRAPH D IGITAL ON/OF F MODE DATA
max. indicated fuel quantity: 15 US gal
left and right tank max. 10 US gal difference For use of max. tank capacity see AFM
%
Maneuvering speed: v = 108 KIAS (above 980 up to 1150 kg / above 2161 up to 2535 lb) v = 94 KIAS (780 to 980 kg / 1720 to 2161 lb)
A
A
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, night VFR and
IFR. All aerobatic maneuvers including spinning are prohibited. For
Ess. Bus NOT for normal operation. See AFM.
further operational limitations refer to the Airplane Flight Manual.
No smoking.
%
%
3 33 5 555105525 7.55 37.55 3 25533310552527070 55
28 VDC ACCESSORY PWR
%
GROUND OPS. ONLY 2A MAX
LP OON D A CC
E FK R KA
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本文鏈接地址：鉆石40飛機維護手冊 DA 40 SERIES AMM 1(76)
