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20 Sep 2007
Section 11-30
Interior Placards and Markings - Lycoming Engine
1. General
Figure 1 shows the interior placards and markings.
Figures 2 and 3 show the instrument panel placards.
% Figures 4 and the following show additional or alternate placards required by design changes.
AIRCRAFT
Placards and Markings DA 40 Series
AMM
Page 2
20 Sep 2007 11-30-00 Doc # 6.02.01
Rev. 5
Figure 1: Interior Placards and Markings
AIRCRAFT
DA 40 Series
AMM
Placards and Markings
Doc # 6.02.01
Rev. 5 11-30-00 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
For
For
Steer
Steer
Date RADIOS ON
N
S
30 60 E 120 150
210 240 W 300 330
ON
OFF
CABIN
LOCK
RELEASE
DEFROST
PARKIN
G
BRAKE
HEAT
FLOOR
Fuel Selector
LEFT RIGHT
20 US gal.
76 l
20 US gal.
76 l
OFF
MAX
PWR
HIGH
RPM
T
HR
OTTL
E
PR
OPELLER
RICH
MIXTURE
LEA
IDLE LOW N
RPM
ON
OFF
CABIN
L
OCK
REL
EASE
DEF
R
OST
PA
RKIN
G
B
RAKE
HEAT
FL
OOR
Fuel Selector
LEFT RIGHT
20 US gal.
76 l
20 US gal.
7 6 l
OFF
MAX
PWR
HIGH
RPM
T
HR
OTTL
E
P
R
OPELL
E
R
RICH
MIXT
URE
L
EA
I DLE N
LOW
RPM
A LT ERNAT E AIR
A LT ERNAT E AIR
ON
max. indica te d f ue l quantit y: 15 US gal
left and right tank max. 10 US gal difference
For use of max. tank capacity see AFM
ALTERNATE AIR
UP
T/O
LDG
max
max A
View A
ENGINE
AVIONICS
LIGHTING
SYSTEMS
ELECTRICAL
FAN/OAT ANNUN.
PITOT
HEAT
FUEL
PUMP DG T & B FLAPS HORIZON
MASTER
CONTROL
ALT. ALT.
PROT. CONT. ALT. BATT.
ESSENTIAL 28 VDC
TIE ACC. PWR.
OPS.
GROUND
ONLY
2A MAX
INST. STROBE POSITION TAXI/MAP LANDING FLOOD
AVIONIC
BUS
ESSENTIAL
AVIONIC
AUTO
PILOT
START IGNITION INST. 1
NAV/COM 1 GPS
NAV/COM 2
XPDR
AUDIO ADF DME
EGT/CHT EGT/CHT AUTOTRACK FUEL/COMP FLIGHT
GRAPH DIGITAL ON/OFF MODE DATA
Ess. Bus NOT for normal operation. See AFM.
Ess. Bus NOT for normal o per ation . See AFM.
ON
OFF
EM ERG ENCY
NAV2
NAV1
PROT.
ALT.
CON T.
ALT.
PUMP
FUE L
TIE
MAIN
TI E
ESSENTIAL
HEAT
PI TOT
PILOT
AUTO
IN ST. 1
2AMAX
ONLY
OPS.
GROUN D
ACC. PWR.
28 VDC
FLOOD
ANNUN.
DME
XPDR
ADF
START
ENG INE
IGNITION
GPS
NAV/COM2 AUDIO
NAV/COM1
A VI ON IC S
LANDING
FLA PS
TAXI /MAP
LIGHT ING
DG T & B
S YS TEMS
ALT. BATT.
ELECTRICAL
INST. S TROBE
FAN/OAT
POSITION
HORIZON
INST RUM E NT
FLO OD
OFF
OFF
ON
ON
MODE DATA
FUEL/COMP
DIGITAL
EGT/CHT
ON/OFF
AUTOTRACK
GRAPH
EGT/CHT FLIGHT
IN .
HG
PSI
°F
US
gal /
hour
MAN
Fuel/
Oi l
Al l
Temp
Fuel
Flow
CONTROL
MASTER
AVIONIC
ESSENTIAL
BU S
AVIONIC
only when Essential Bus
is installed
No smoking.
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
further operational limitations refer to the Airplane Flight Manual.
NAV1
NAV2
MAN
Fuel/
Oil
All
Temp
Fuel
Flow
IN.
HG
PSI
°F
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钻石40系列AMM 1(63)
