34-CONTENTS Page 34 Aug 01/05
CES
CHAPTER 34
__________
NAVIGATION
TABLE OF CONTENTS
_________________
SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________ Control 40 ALL Reconfiguration Switching 43 ALL BITE Function 43 ALL Access to the VOR/MKR Sub-menu 45 001-049, 101-105 Functions 151-199, Activation of the Test Function 45 001-049, 101-105 151-199, Access to the VOR/MKR Sub-menu 45 051-099, 106-149 Functions 201-299, 301-399
401-499,
Activation of the Test Function 47 051-099, 106-149 201-299, 301-399 401-499,
BITE Test 47 ALL
CFDIU Interface 47 ALL
Power-up Tests Initialization 51 ALL
and Cockpit Repercussions
VOR/MARKER 34-55-00
ADJUSTMENT/TEST 501 ALL
BITE Test of the VOR/MKR 501 ALL
Operational Test of the VOR/MKR 509 ALL
Functional Test of the VOR/MKR 512 ALL
ANTENNA - VOR 34-55-11
REMOVAL/INSTALLATION 401 ALL
Removal of the VOR Antenna 4RS 401 ALL
Installation of the VOR Antenna 405 ALL
4RS
ANTENNA - MARKER 34-55-18
REMOVAL/INSTALLATION 401 ALL
Removal of the Marker Antenna 401 ALL
(1RS)
Installation of the Marker Antenna 405 ALL
(1RS)
RECEIVER - VOR/MARKER 34-55-31
REMOVAL/INSTALLATION 401 ALL
Removal of the VOR/MKR Receiver 401 ALL
(3RS1, 3RS2)
Installation of the VOR/MKR 404 ALL
Receiver (3RS1, 3RS2)
RMI - VOR/DME 34-57-22
REMOVAL/INSTALLATION 1 401 001-049, 051-099 101-105, 151-199 Removal of the VOR/DME RMI (11FN) 401 001-049, 051-099 101-105, 151-199
34-CONTENTS Page 35 Aug 01/05
CES
CHAPTER 34
__________
NAVIGATION
TABLE OF CONTENTS
_________________
SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________ Installation of the VOR/DME RMI 404 001-049, 051-099 (11FN) 101-105, 151-199 RMI - VOR/ADF/DME 34-57-22 REMOVAL/INSTALLATION 2 401 106-149, 201-299 301-399, 401-499 Removal of the VOR/ADF/DME RMI 401 106-149, 201-299 (21FN) 301-399, 401-499 Installation of the VOR/ADF/DME 404 106-149, 201-299 RMI (21FN) 301-399, 401-499
SATELLITE NAVIGATION 34-58-00 DESCRIPTION AND OPERATION 1 ALL General 1 ALL
34-CONTENTS Page 36 Aug 01/05
CES NAVIGATION - GENERAL - DESCRIPTION AND OPERATION
________________________________________________
1. General
_______
R (Ref. Fig. 001) The aircraft navigation systems provide the crew with the data required for flight within the most appropriate safety requirements. These data can be divided into four groups :
-Air Data/Inertial Reference System (ADIRS)
-Landing and taxing aids
-Independent position determining
-Dependent position determining.
2. System Description
__________________
A. ADIRS
This part of the navigation system comprises :
-three Air Data/Inertial Reference Units (ADIRU)
-standby systems.
Each ADIRU performs :
-
the air data function through its Air Data Reference (ADR) portion.
-
the attitude, heading and position function through its Inertial Reference (IR) portion.
(1) Air data function Air data are provided by four independent sources :
(a)
Three main systems Each of the three main systems includes static probes, pitot probes and their associated Air Data Modules (ADM), Total Air Temperature (TAT) sensors and Angle of Attack (AOA) sensors. They provide the ADR portion of the ADIRU with the necessary data for the generation of parameters which are transmitted to the Primary Flight Displays (PFD) and Navigation Displays (ND) and the Angle of Attack (AOA) indicator (optional) and to the various aircraft systems.
(b)
A standby system
1 The standby system includes a standby altimeter, a standby
_ airspeed indicator and a metric altimeter (optional) (Ref. 34-21) and the optional system ISIS (Ref. 34-22). They are provided with pressure by static probes and pitot probe linked to the ADIRU 3. More explanations are given in the ADIRU system (Ref. 34-13).
1EFF : ALL 1 34-00-00Page 1 1 1 May 01/02 1 1 1CES 1
R R Navigation - Systems Overvieww Figure 001
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