Operation Manual
Table Of Contents
- 1 SYSTEM DESCRIPTION
- 1.1 System Overview
- 1.2 Abbreviations
- 2 Technical specifications
- 2.1 Signal Minimum Performance GP
- 2.2 Environmental characteristics
- 2.3 EMC characteristics
- 2.4 Mechanical characteristics
- 2.5 Power supply
- 3 Main cabinet
- 3.1 Power on/off
- 3.2 Local Control Operation
- 3.3 Local Keyboard/Display Operation
- 3.3.1 The menu structure.
- 3.3.2 Handling the different menuscreens.
- 3.3.2.1 The menu screen
- 3.3.2.2 The readout screen
- 3.3.2.3 The toggle screens
- 3.3.2.4 Input/Store screen
- 3.3.2.5 The quick read screens
- 3.3.3 The access levels.
- 3.3.3.1 Level 2
- 3.3.3.2 Level 3
- 3.3.3.3 Leaving the access levels
- 3.3.4 Function listing
- 3.3.4.1 Level 1
- 3.3.4.2 Level 2
- 3.3.4.3 Level 3
- 3.3.5 The menu tree
- 4 Tower Equipment
- 4.1 Remote Control Operation
- 4.2 Remote Slave Operation
- 4.3 Interlock Switch Operation
- 5 Remote Maintenance and Monitoring Software
- 5.1 Introduction
- 5.2 User interface components
- 5.3 Shortcuts
- 5.4 Configuring the RMM system
- 5.5 Setting up ILS stations
- 5.6 Connecting to an ILS station
- 5.7 Monitor measurements and status
- 5.8 Monitor settings
- 5.9 TX settings
- 5.10 Power scaling
- 5.11 Front panel operation
- 5.12 Get historical data
- 5.13 Continuous data logging
- 5.14 Events
- 5.15 Test DDM
- 5.16 Set ILS date/time
- 5.17 User administration
- 5.18 ILS Modem settings
- 5.19 Upload configuration to ILS
- 5.20 Write configuration to file
- 5.21 Lamp mappings
- 5.22 Medium storage sample interval
- 5.23 Displaying stored measurements
- 5.24 DIAGNOSTICS
- 5.25 Exporting data
- 5.26 Printing reports
- 5.27 Print screen
- 5.28 Technical note - Leased line SETUP (USRobotics)
- 5.29 Technical note - Dial up connection SETUP (USRobotics)
- 5.30 Technical note - Leased line SETUP (WESTERMO)
- 5.31 Technical note - dial up SETUP (WESTERMO)
- 6 Periodic maintenance CAT I and II
- 6.1 Weekly inspections
- 6.2 Monthly inspections
- 6.3 Quarterly inspections
- 6.4 Annual inspections
- 6.4.1 RF Frequency check.
- 6.4.1.1 Course Transmitter Frequency
- 6.4.1.2 Clearance Transmitter Frequency
- 6.4.2 LF Frequency check.
- 6.4.3 Transmitter waveforms checks.
- 6.4.3.1 PHASE CORR. check.
- 6.4.3.2 SBO waveform checks.
- 6.4.3.3 RF Phase
- 6.4.3.4 CSB waveform check. LF phase
- 6.4.3.5 DDM and SDM check.
- 6.4.3.6 Not in use
- 6.4.4 (Not in use)CSB output power.
- 6.4.5 Monitor Alarm Limit checks.
- 6.4.5.1 CL DDM ALARM
- 6.4.5.2 CL SDM ALARM
- 6.4.5.3 CL RF ALARM
- 6.4.5.4 DS DDM ALARM
- 6.4.5.5 NF DDM ALARM
- 6.4.5.6 CLR DDM ALARM
- 6.4.5.7 CLR SDM ALARM
- 6.4.5.8 CLR RF ALARM
- 6.4.6 Near Field Monitor delay
- 6.4.7 20 seconds inhibit
- 6.4.8 Battery maintenance
- 6.4.9 Final check GP
- 7 Corrective maintenance
- 7.1 Overview
- 7.2 Diagnostic functions
- 7.3 LRU change procedures
- 7.4 Detailed description of the automatic diagnostic algorithms
- 7.4.1 Overview
- 7.4.2 Possible diagnostic solutions
- 7.4.3 Current data diagnostics
- 7.4.3.1 I2C read error on any board implies a failure on that board
- 7.4.3.2 Maintenance parameter warnings
- 7.4.3.2.1 External power supply tests
- 7.4.3.2.2 Power supply 1 and 2 tests
- 7.4.3.2.3 Maintenance warnings without follow-errors
- 7.4.3.2.4 Power amplifier tests
- 7.4.3.2.5 Monitor 1 and 2 frontend tests
- 7.4.3.2.6 Remote control tests
- 7.4.3.2.7 Transmitter control tests
- 7.4.3.2.8 Standby monitor tests
- 7.4.3.2.9 Standby monitor frontend tests
- 7.4.3.2.10 User defined parameters
- A Monitor and Maintenance Parameters
- A.1 Monitor Alarm Parameters
- A.2 Maintenance Parameters
- B Factory default configuration settings
- B.1 Cat I monitor LIMIT configuration
- B.1.1 Description of the FFM EXE AL limits
- B.1.2 Description of the CL IDENT and CLR IDENT limits
- B.2 Cat II monitor LIMIT configuration
- B.3 Cat III monitor LIMIT configuration
- B.4 Executive Monitor delay configuration
- B.5 Maintenance parameter configuration
- B.6 Oscillator 1 and 2 (OS 1221)
- B.6.1 LF generator 1 and 2 (LF 1223)
- B.6.2 TX 1 and 2, Course and Clearance
- B.6.3 RF frontends for monitor 1, 2 and standby monitor (MF 1211/1219)
- B.6.4 Monitor 1, 2 and standby (MO 1212)
- B.6.5 Transmitter control board (TCA 1216)
- B.6.6 Remote monitoring board (RMA 1215)
- B.6.7 Power supply 1 and 2 (PS 1227)
- B.6.8 External power
- B.6.9 User defined inputs
- B.7 Maintenance delay configuration
- B.8 Morse code configuration
- B.9 Typical TX Adjustments values
- B.10 User administration configuration
- B.11 Frequency configuration strap settings
- B.11.1 OS1221B strap settings for 2-frequency GP
- C Maintenance Procedures
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the transmitter SBO attenuator value and record in Table “CEGS Monitor Reference Data”.
Compare the values to the reference values. If found outside the tolerance ivestigation should
be carried out.
(b) Decrease the sideband power (increase the SBO attenuator value) until the monitor is in
alarm. Confirm that this attenuator value is not greater than the flight checked reference value.
Record this SBO attenuator value. If the alarm value has been exceeded, corrective action
should be taken.
(c) Measure and record the width monitor DDM on Navia Aviation Form "CEGS Monitor Ref-
erence Data". The width DDM is availible in the PMDT Monitor 1 window
.
Note that no toler-
ance exists on this entry. It is used to detect trends.
(d) Increase the sideband power (decrease the SBO attenuator value) until the monitor is in
alarm. Confirm that this attenuator value is not less than the flight checked reference value.
Record this SBO attenuator value. If the alarm value has been exceeded, corrective action
should be taken.
(e) Measure and record the width monitor DDM on Navia Aviation Form “CEGS Monitor Refer-
ence Data”. The width DDM is availible in the PMDT Monitor 1 window
.
Note that no tolerance
exists on this entry. It is used to detect trends.
(g) Return the sideband power to normal.
3. Path angle alarms (integral).
(a) Connect the PIR to measure DDM in the carrier feedline (Facility CSB test connector).
(b) Using the PMDT, open Test DDM window, click on TX1 dominance Off button to activate 90
Hz predominance (assuming transmitter 1 is active to the antennas). If necessary adjust Inc or
Dec until the monitor course position channel has just passed the threshold of alarm. Measure
and record the carrier feedline DDM value on Navia Aviation Form “CEGS Monitor Reference
Data”. Confirm that the carrier feedline DDM is not more than established reference value. If
not within tolerance, corrective action is required.
(c) Measure and record the course monitor DDM on Navia Aviation Form “CEGS Monitor
Reference Data”. The course monitor DDM can be observed in the currently active Test DDM
window as parameter MON1 CL DDM Nom. Note that no tolerance is established for this
entry. It is used only to detect trends.
(d) Repeat the procedure in steps (b) and (c) with the TX1 dominance button activated to 150
Hz.
(e) Restore the TX1 dominance button to off.
4. SBO dephasing alarms.
(a) Insert a N type elbow in the CSB carrier feedline. (CSB phase retarded)
(b) Confirm that the phase change is within the operating tolerance in chapter 3.
(c) Repeat the procedure in step (b) with the SBO phase retarded.