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-8
-7
-9
-5
ALTITUDE
(FEET)
RANGE
SCALE
(NM)
LINE OF
SIGHT
(NM)
10 25 50 100 200
(TILT LIMITED
REGION)
(LINE OF SIGHT LIMITED REGION)
GX_16_042
For Training Purposes Only
Sept 04
16-33
P I LOT T R A I N I N G GU I D E
NAVIGATION
LIGHTNING SENSOR SYSTEM (LSS) (IF INSTALLED)
The lightning sensor system is used to detect lightning. The LSS rotary knob is used to
select the following functions:
- OFF. Turns off the LSS (if installed)
- SBY. Selects the LSS in standby mode. The data is inhibited, but LSS accumulates
data.
- LX. LSS is fully operational and displays data on the MFD. As it is a passive
listening device, lighting display is available on ground.
- CLR/TST. LSS accumulated data is cleared from memory. After 3 seconds the test
mode is initiated.
LSS TILT
CLR
TST
OFF
SBY LX
PULL
ACT
+
–
GX_16_038
SAT
GSPD
-56
TAT
TAS
-40
234
345
TOC KLM
DEF GHJ
4000 4000
FL180
Annunciation
TGT
LX OFF
T5.0
GMAP
LSS TILT
CLR
TST
OFF
SBY LX
PULL
ACT
+
–
GX_16_039
SAT
GSPD
-56
TAT
TAS
-40
234
345
TOC KLM
DEF GHJ
4000 4000
FL180
Annunciation
TGT
STBY
T5.0
GMAP
LSS TILT
CLR
TST
OFF
SBY LX
PULL
ACT
+
–
GX_16_040
SAT
GSPD
-56
TAT
TAS
-40
234
345
TOC KLM
DEF GHJ
4000 4000
FL180
Annunciation
TGT
LX
T5.0
GMAP
50 50
3
6
33
30
N
Rate 1:
Rate 2:
Rate 3:
ALERT:
Lightning rate of 2-15
strokes in the last 2 minutes.
Lightning rate of 16-31
strokes in the last 2 minutes.
Lightning rate of >32
strokes in the last 2 minutes.
Range is indeterminate but
bearing accurately determined.
Azimuth should be closely monitored.
LSS TILT
CLR
TST
OFF
SBY LX
PULL
ACT
+
–
GX_16_041
SAT
GSPD
-56
TAT
TAS
-40
234
345
TOC KLM
DEF GHJ
4000 4000
FL180
Annunciation
TGT
LX/T
T5.0
GMAP
P I LOT T R A I N I N G GU I D E
NAVIGATION
16-34 For Training Purposes Only
Sept 04
WEATHER RADAR SCHEMATIC
WX
SAT
GSPD
-56
TAT
TAS
-40
234
345
LX
0 . 05L
HDG
315
ETE 1+36
NM
360 FMS1
N
5 5
3
6
33
30
KLM
KKLM
TOC
TOC
GHJ
KGHJ
DEF
KDEF
4000 4000
FL180
RADAR LSS TILT
TST
FP
GMAP
CLR
TST
SBY OFF
WX RCT SBY LX
PULL
ACT
+
–
GAIN
MIN MAX
PULL
VAR
TRB STAB TGT SECT
OFF
RADAR TILT
TST
FP
SBY GMAP
WX RCT
PULL
ACT
+
–
GAIN
MIN MAX
PULL
VAR
TRB STAB TGT SECT
OFF
GX_16_043
IAC 3
IAC 2
IAC 1
IAC 3
IAC 2
IAC 1
MFD
Controller
1
MFD
Controller
2
WOW
WOW WOW
IRU 1 IRU 2
CAIMS
DU 5
WX RECEIVER/
TRANSMITTER/
ANTENNA
PILOT’S WX CONTROLLER COPILOT’S WX CONTROLLER
WX
SAT
GSPD
-56
TAT
TAS
-40
234
345
LX
0 . 05L
HDG
315
ETE 1+36
NM
360 FMS1
N
5 5
3
6
33
30
KLM
KKLM
TOC
TOC
GHJ
KGHJ
DEF
KDEF
4000 4000
FL180
DU 2
For Training Purposes Only
Sept 04
16-35
P I LOT T R A I N I N G GU I D E
NAVIGATION
TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS)
The TCAS is an airborne system that interrogates ATC transponders in nearby
airplanes to identify and display potential and predicted collision threats, within 700
feet of closest point of approach. TCAS monitors a radius of up to 120 nautical miles
(optional above 40 miles) about the airplane, computes range, bearing and closure rate
of up to 12 other transponder equipped airplanes relative to the “own” airplane. TCAS
　
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