Vhf Navigation - BOMBARDIER Challenger 601-3A CL-600-2B16 Pilot Training Manual

VHF NAVIGATION

The VHF NAV systems No. 1 and No. 2 receive
and process the following ground-based VHF-
tuned navaids to provide short-range naviga-
tion:
• VHF omnirange (VOR)
• Localizer (LOC)
• Glide-slope (GS)
• Marker beacon signals (MKR)
Each VHF NAV system consists of an antenna
and a control unit (Figure 16-12). The VHF
FULL GSPD
MAP WX
ARC TTG
FMS 1
ADF 1
TEST
OFF
OFF
VOR 1
OFF
ADI DH HSI
BRG
DIM TST DIM
DISPLAY CONTROLLER
Collins
A
C XFR
T
MEM
MEM RMT HLD
NAV
ON
HLD
STO
OFF
V
TEST
ACT
VHF NAV 1
16-12 CL 601-3A/R
VOR/LOC DISPLAYS
ET V/L FMS
FMS 2
ADF 2
VOR 2
OFF
WX
BRG
DIM
Collins
A
C XFR
T
MEM
MEM
ADF
ADF
TONE
STO
ANT
OFF
V
TEST
ACT
ADF 1
Figure 16-11. Navigation System Cockpit Controls
FOR TRAINING PURPOSES ONLY
FlightSafety Canada
CL-600-2B16 PILOT TRAINING MANUAL
NAV system provides VOR, LOC, and GS de-
viation; VOR, LOC, and MKR audio; VOR
bearing, VOR TO/FROM data, and MKR
annunciation.
The VHF NAV system supplies VOR infor-
mation for use and display for the following:
• EFIS
• FMS
• MFD
• Audio integrating system
• Autopilot
MKR BEACON
VOR/LOC DISPLAYS
Collins
A
C
T
MEM
ADF
ANT
OFF
V
FULL GSPD
MAP WX ET
ARC TTG
FMS 1
ADF 1
TEST
OFF
VOR 1 OFF
OFF
ADI DH HSI WX
BRG DIM TST DIM DIM
DISPLAY CONTROLLER
Collins
A
XFR C
T
MEM
MEM RMT
ADF
ON
TONE HLD
STO STO
OFF
V
TEST TEST
ACT
ADF 2 VHF NAV 2
L t é e
L t d .
V/L FMS
FMS 2
ADF 2
VOR 2
OFF
BRG
XFR
MEM
HLD
NAV
ACT