Instruction Manual

System Components
System Components
Chapter 1
1-0
N
S
E
W
TO
FR
33
30
24
21
15
12
6
3
OBS
GS
N
A
V
ı
GS
ı
N
3
3
3
0
W
2
4
2
1
S
1
5
1
2
E
6
3
HDGNAV
GS
AIRCRAFT
POWER
ALTITUDE
11-33V
GRAY CODE
WPT ALERT
MESSAGE
MOVING MAP
DISPLAYS
KA 92 GPS ANTENNA
HSI
CDI
AUTOPILOT
REMOTE
ANNUNCIATORS
RS-232
OUTPUT
KLN 89(B) SYSTEM
REQUIRED FOR ALL INSTALLATIONS OPTIONAL
OR
KI 525A KI 206
COMPATIBLE
FUEL
MANAGEMENT
SYSTEM
REQUIRED FOR IFR APPROACH INSTALLATIONS (OF KLN 89B)
RS-232
INPUT
RS-232
INPUT
HEADING
RS-232
INPUT
GPS
APR
REMOTE SWITCH/
ANNUNCIATOR
ı
N
S
E
W
33
30
2
4
2
1
15
1
2
6
3
A
D
F
KI 229
N
33
30
W
24
21
S
15
12
E
6
3
A D
F
A D
F
NAV NAV
KNI 582
OR
COMPATIBLE
AIR
DATA
COMPUTER
LEFT/RIGHT
D-BAR
SELECTED
COURSE
GPS
ON
OFF
APT VOR NDB INT USR ACT NAV FPL CAL SET OTH
G
KLN 89 TSO
CRSR
PULL SCAN
ëî.ïnm|∞VOR 25R KLAX
ëî.ïnm|∞VOR 25R KLAX
ELMOOi|≥ 3 ELMOOi 15
ELMOOi|≥ 3 ELMOOi 15
>Leg| 4 LAX18 22
>Leg| 4 LAX18 22
FPL 0 | 9:KLAX 66
FPL 0 | 9:KLAX 66
ENT
>
CLRD
OBSNRSTALTMSG
RMI
ALT HDG NAV APR APGS
ALT HDG NAV APR BC
AP
ENG
TEST
KC 193
YD
RN RC PC
BC
ı
DN
UP