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TB20 MAINTENANCE MANUAL 34 导航 TB20飞机维护手册 2(10)

时间:2011-11-09 16:09来源:蓝天飞行翻译 作者:航空
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VHF NAV / COMM transceiver 1 251C / 34-50-00
Course deviation indicator 1 251 R or
251L / 34-52-00
Circuit breaker :
- "COM / NAV 2" 1 230 232L WM

3. OPERATION NOTE : For equipment operation and maintenance, refer to the supplier's Maintenance Manual.
AFAF
Validity : KX 165 without EFIS 34-52 00Page 1
(BQ) NOV 01
 
ANTENNE
VOR
VOR
ANTENNA
NAV 2 installation - Electrical schematic
Figure 1 - Without glideslope
 
ANTENNE
GS
GS
ANTENNA
ANTENNE
VOR
VOR
ANTENNA
 

 
SEPARATEUR
DE SIGNAUX
GS
GS SIGNAL
SEPARATOR
 
SEPARATEUR
DE SIGNAUX
VOR
VOR SIGNAL
SEPARATOR
 
CANAL DME
DME CHANNEL
 
INSTALLATION DME
DME INSTALLATION
( 34 - 55 - 00 )
 

 
VERS NAV 1 TO NAV -I
VERS NAV 1
TO NAV 1
 

 
EMETTEUR /
RECEPTEUR VHF - NAV / COMM VHF - NAV / COMM TRANSCEIVER
 
DONNEES VOR / LOC
VOR / LOC DATA
("DEV / TO - FROM / FLAG")
"OBS RESOLVER"
DONNEES GS
GS DATA ("DEV / FLAG")
 
INDICATEUR
ECART DE
ROUTE
COURSE DEVIATION INDICATOR
 
BOITE DE
COMMANDE AUDIO
AUDIO CONTROL BOX
 
 [(
HAUT PARLEUR
LOUDSPEAKER ( LS )
 
(c) CASQUE HEADSET
 

 
NAV 2 installation - Electrical schematic
Figure 1A - With glideslooe
 
AFAF
Validity : KX 165 without EFIS 34 52-00(BQ) Page 4
FEB 00
 
NAV 2 INSTALLATION
DESCRIPTION AND OPERATION
1. GENERAL
The VOR is a short- and middle-range navigation aid. It enables the pilot to locate the position of his aircraft with regard to a half-line (radial) crossing the VOR station or also to determine the particular radial crossing the aircraft position.
In ILS operation (landing aid), the system allows a continuous guidance in azimuth (LOC) and in elevation (GLIDE slope approach plane).
The optional NAV 2 installation consists of :
- the A77 COMM./VOR-ILS/GPS transceiver GNS 430
- the M74 course deviation indicator GI 106A
The system uses the VOR/LOC antenna, the GS antenna and the VOR and GS signal separators. All these elements can be found in NAV 1 installation — refer to 34-51-00.
The NAV 2 installation transmits navigation information to radio magnetic indication system (Option RMI - KNI 582) - refer to 34-25-00.
For the description of communication function of the A77 COMM.NOR-ILS/GPS transceiver - refer to 23-13-00.
 
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