ENGINE
AVIONIC
ESSENTIAL BUS
I START IGNITION INST. 1 AVIONIC
N D U
I N
only when autopilot is installed
I T S
IFR NAV1 AC
LIGHTING
Limitations for KAP 140 Autopilot System: models TI
Do not use AP if "Alternate Static" is open. N
INST. STROBE POSITION TAXI/MAP LANDING FLOOD
only O
NAV2
IN.
Autopilot OFF during take-off and landing. MAN
HG
Maximum speed for autopilot operation is 165 KIAS.
Minimum speed for autopilot operation is 70 KIAS.
Fuel/
SYSTEMS
Minimum altitude for autopilot operation:
PSI
FUEL PITOT
PUMP FAN/OAT DG T & B HEAT FLAPS HORIZON ANNUN.
Oil
Cruise, Climb, Descent and Maneuvering: 800 feet AGL
All °F
Approach: 200 feet AGL
Temp
21S 15
US
For N 30 60 E 120 150
ELECTRICAL
Steer
Fuel gal/
ALT. ALT.
ESSENTIAL MASTER 28 VDC
For S 210 240 W 300 330
Flow
PROT. CONT.
Steer
ALT. BATT. TIE CONTROL ACC. PWR.
hour
Date RADIOS ON
GROUND
OPS.
ONLY
2A MAX
GPS limited to VFR use only.
EGT/CHT EGT/CHT AUTOTRACK FUEL/COMP FLIGHT
A VI O NICS
NAV /COM1 GP S XPD R
GRAPH DIGITAL ON/OFF MODE DATA
IN.
MAN HG
Fuel/ PSI
AUT O
Oi l
NAV/COM2 AUDIO ADF DME
PIL OT
Al l °F Temp
US gal /
ENG INE
Fuel
Flow
I NS T RUM E NT AVIONIC ESSENTIAL STA RT IGNIT ION INST. 1
hour
BU S AVIO NIC ON
OFF NAV1 LIGH TING
INST. STROBE POSITION TAXI/MAP LANDI NG FLOOD FLO OD E GT/ CHT E GT /CHT A UTOTRACK FUEL/COM P FLIGHT
GRAP H DIGIT AL ON/OFF MODE DA TA ON NAV2 S YS T E MS OFF FUEL PITOT
FAN/OAT DG T& B FLAPS HORIZON ANNUN.
PUMP HEAT
OFF
E LE CT RI CAL ESSENTIAL MASTER 28VDC
or (see Chapter 28):
A LT. AL T. MA IN AL T. BATT.
PROT. CONT. TIE TIE CONTR OL ACC. PWR.
%
GROUND ON OPS.
max. indicated fuel quantity: 15 US gal
ONLY EM ERGENC Y
left and right tank max. 10 US gal difference For use of max. tank capacity see AFM
2A MAX
Ess. Bus NOT for normal operation. See AFM.
%
or (for longe range tanks, see Ch. 28):
%
LP
ON O
D A CC
E F R KA K
%
B I R I O S N N G
Ess. Bus NOT for normal operation. See AFM.
ALTERNATE AIR T
H E RF B EL R LA O A ET O
%
A S E K
only when Essential Bus
R
OFFALTERNATE AIR
E
is installed ON
R
MAX HIGH I C
Maneuvering speed:
PWR RPM H
ALTERNATE AIR
vA = 108 KIAS (above 980 up to 1150 kg / above 2161 up to 2535 lb)
PT R M H O IR P
vA = 94 KIAS (780 to 980 kg / 1720 to 2161 lb)
XO E TT L UT L RL E
R E
This airplane may only be operated in accordance with the Airplane Flight
E
A max
Manual. It can be operated in the “Normal” and “Utility” categories in
L
E
A
N LOW
IDLE RPM
non-icing conditions. Provided that national operational requirements
R
are met and the appropriate equipment is installed, this airplane is
MAX HIGH
I
max
RPMPWR
approved for the following kinds of operation: day VFR, night VFR and
C
20 US gal. 20 US gal.76 l 76 l
FF
UP
O
PT RH O
T/O
R PO E
LDG
T LT LL EE
View A
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