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Limitations for KAP 140 Autopilot System:
Maximum speed for autopilot operation is 165 KIAS.
Minimum speed for autopilot operation is 70 KIAS.
Do not use AP if "Alternate Static" is open.
Approach:
Autopilot OFF during take-off and landing.
Minimum altitude for autopilot operation:
Cruise, Climb, Descent and Maneuvering:800 feet AGL
200 feet AGL
Limitations for KAP 140 Autopilot System:
M ax im um sp e ed f o r a uto pi l ot op era ti o n i s 16 5 K IA S.
M in im um s pe ed fo r au to p il ot op e ra t io n i s 70 K IA S.
Do no t u se AP i f " A l te rna te S tatic " is o pe n .
Ap pro ac h:
Au top il ot OF F d ur i ng ta ke -of f an d l an di ng .
M in im um a lti t ud e for a utop i lo t o pe ration :
Cru is e, Cl imb , De sc en t a nd Ma ne uv eri ng :8 00 f e et AGL
2 00 f e et AGL
only when autopilot is installed
GPS limited to VFR use only.
only when GPS,
limited to VFR use,
is installed
G PS limi ted to VFR us e onl y.
m ax . in d i c ate d fue l qu a n ti ty: 1 5 U S g a l
l eft a nd ri ght ta nk ma x. 10 U S g al d iffere nce
F or use o f ma x. ta nk ca pa city se e AFM
or (see Chapter 28):
or (for longe range tanks, see Ch. 28):
MO D E D A T A
F UE L/C OM P
D IG IT A L
EG T /C HT
ON /OF F
A UT OT R A CK
GR AP H
E GT /C HT F L IG H T
25 5 3 3 3 10 5 5 25 2 70 70 5 5
28 VDC ACCESSORY PWR
GROUND OPS. ONLY 2A MAX
28 VDC ACCESSORY PWR
GROUND OPS. ONLY 2A MAX
3 3 3 5 5 5 5 10 5 5 25 7.5 5 3 7.5 5 3
GRND COM2
ON
OFF
GRND COM2
ON
OFF
Figure 3: Instrument Panel Placards for Smaller Instrument Panels
AIRCRAFT
DA 40 Series
AMM
Placards and Markings
Doc # 6.02.01
Rev. 5 11-30-00 Page 5
20 Sep 2007
Figure 4: Additional Instrument Panel Placards for Long Range Tank
(optional, see OÄM 40-071)
%
%
%
%
%
%
%
%
%
%
%
%
%
%
%
Figure 5: Fuel Selector Placard for Long Range Tank
(optional, see OÄM 40-071)
AIRCRAFT
Placards and Markings DA 40 Series
AMM
Page 6
20 Sep 2007 11-30-00 Doc # 6.02.01
Rev. 5
Maneuvering Speed:
% vA = 111 KIAS (above 1036 up to 1200 kg, above 2284 up to 2646 lb)
vA % = 94 KIAS (780 to 1036 kg, 1720 to 2284 lb)
The airplane may only be operated in accordance with the Airplane Flight Manual. It
can be operated in the „Normal“ and the „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 further operational limitations refer to the Airplane Flight Manual.
% No smoking.
% Figure 6: Alternate limitations placard for 1200 kg MTOM (if MÄM 40-227 is carried out)
AIRCRAFT
DA 40 Series
AMM
Placards and Markings
Doc # 6.02.01
Rev. 5 11-31-00 Page 1
20 Sep 2007
Section 11-31
Interior Placards and Markings - TAE 125 Diesel Engine
1. General
Figure 1 shows the interior placards and markings for airplanes with the TAE 125 Diesel engine
installed.
Figure 2 shows the instrument panel placards.
% In case of Diesel Fuel operation (MÄM 40-129) the fuel temp limitation placard (D4D-1131-20-29) is
% located beside the AED.
% Diesel Fuel or Unknown Fuel Blend:
% Yellow blinking: No engine start permitted
% Yellow steady on
% (LH fuel tank): No take-off permitted
AIRCRAFT
Placards and Markings DA 40 Series
AMM
Page 2
20 Sep 2007 11-31-00 Doc # 6.02.01
Rev. 5
Figure 1: Interior Placards and Markings - Airplanes with the TAE 125 Diesel Engine Installed
AIRCRAFT
DA 40 Series
AMM
Placards and Markings
Doc # 6.02.01
Rev. 5 11-31-00 Page 3
20 Sep 2007
21 S 15
For
For
Steer
Steer
Date RADIOS ON
N
S
30 60 E 120 150
210 240 W 300 330
5 30 30 70 30 3 3 5 5 5 10 5 10 10 10 25 5 10 15 5 5 3 3 10 5 3 25 10 3 3 5 15 5 3 30 2
KNOTS
160
120
140
AIRSPEED
100
80
60
40
PULL
CAGETO
20
20
10
10
10
10
20
20
0
I N . Hg
CA L IBRA T E D
TO
2 0,0 0 0 F EE T
m b
28. 7
28.8
975 28.6 970
100
FEET
　
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