Garmin Software Version 0321.23 Handbuch Seite 262
- Seite / 266
- Inhaltsverzeichnis
- FEHLERBEHEBUNG
- LESEZEICHEN
Bewertet. / 5. Basierend auf Kundenbewertungen
Page 8-10 G1000 System Maintenance Manual – Diamond DA40/40F
Revision G 190-00545-01
8.3 GFC 700 Ground Checkout
The following procedures verify the proper operation of the GFC 700 AFCS, after maintenance has been
performed. The technician performing these checks should be thoroughly familiar with the G1000 and
GFC 700 by studying the following references:
• G1000/DA40 Cockpit Reference Guide, Garmin P/N 190-00324-11
• Airplane Flight Manual Supplement: G1000 Integrated Avionics System with GFC 700
Automatic Flight Control System – Diamond Model DA40 & DA40F,
Garmin P/N 190-00492-10
8.3.1 Pre-Flight Test
1. Power down the G1000 system using the Avionics Master, then the BAT-side aircraft master
switch. If a ground power unit is being used, it too must be powered off. Wait 30 seconds then
restore power to the system. The GFC 700 will begin an automatic pre-flight test after AHRS and
ADC parameters become valid.
2. Verify that a white ‘PFT’ annunciation is displayed on the PFD, as shown in Figure 8-4.
Figure 8-4. Pre-Flight Test
NOTE
A red AFCS (
) annunciation may be displayed momentarily before PFT starts.
This indicates that the Autopilot and Manual Electric Trim are not available (due to
AHRS initialization, GFC 700 system failure, power loss, or because PFT has not been
performed)
3. Upon successful completion of the test, an aural alert will sound and the annunciation will clear.
For even-interval system power-up, the aural alert is generated by GIA 63 #1, whereas odd-
interval system power-ups are generated GIA 63 #2.
4. Repeat Step 1 to test the PFT aural alert for the opposite GIA 63.
5. Continue to Section 8.3.2. (If the ‘PFT’ annunciation turns red, the test has failed).
6. If the aural alert is not heard, but pre-flight testing passed, engage the Autopilot by pressing the
AP key and disengage the Autopilot by pressing the AP key again. Visual and aural disconnect
alerting should occur. If no alert is heard, the audio interface between the GIA and audio panel
should be checked.
- Diamond DA 40 & DA 40 F 1
- PARAGRAPH PAGE 4
- FIGURE PAGE 6
- TABLE PAGE 9
- 1 INTRODUCTION 11
- 1.2 Organization 19
- 1.3.1 Units of Measure 21
- 1.4 Publications 22
- 1.5 Distribution 24
- (Where Applicable) 25
- 2 SYSTEM DESCRIPTION 27
- 2.2 Equipment Descriptions 28
- 2.2.2 GMA 1347 Audio Panel 28
- 2.3.1 KAP 140 AFCS 31
- • Flight Director 34
- • Autopilot 34
- • Manual Electric Trim 34
- • Pitch 37
- • Pitch Trim 37
- • Roll 37
- 2.8 Shield Block Grounds 43
- 2.9 Sensor Installations 43
- 2.10 Block Diagrams 43
- 2.10.1 G1000 & KAP140 43
- 2.10.2 G1000 & GFC700 44
- 3.1.1 AFCS Controls 45
- 3.1.2 GMA 1347 Controls 46
- 3.1.3 FMS Knob 46
- 3.1.4 Softkeys 47
- 3.2 G1000 Operation Modes 47
- 3.2.1 Normal Mode 47
- 3.2.2 Reversionary Mode 48
- Configuration Mismatch 51
- SET>ACTV Softkey 51
- Configuration Correct 51
- 3.3.2 Configuration Prompts 52
- 3.4.2 Software Files 59
- 3.4.3 Configuration Files 60
- GRS Internal Memory 66
- GDC Internal Memory 66
- GDU 104X Software Load 67
- G1000 System Upload Selection 67
- 3.5.1 System Power Up 68
- 3.5.8 Software Check 77
- 3.5.9 TAWS Reactivation 80
- 3.5.11 ESP Reactivation 82
- SYSTEM ID Number Location 85
- 4.2 Servicing Information 94
- 4.2.2 Recommended Tools 95
- 4.3 Maintenance Intervals 96
- G1000 Equipment 96
- 4.4 Visual Inspection 100
- 190-00545-01 Revision G 101
- 4.5 Electrical Bonding Test 103
- 4.5.1 Requirements 103
- 4.5.2 Test Equipment 103
- 4.5.3 Procedure 103
- 4.6.2 Calibration Setup 108
- 4.6.3 Empty Calibration 109
- 4.6.4 5 Gallon Calibration 111
- message 118
- Figure 4-14) 124
- Figure 4-15) 125
- Revision G 190-00545-01 128
- INLET AND 129
- DUCT (REF) 129
- 5 TROUBLESHOOTING 133
- Annunciation Window 134
- Alerts Window 134
- Alerts Softkey Annunciation 134
- System Annunciations 134
- Alert Name Purpose 136
- 5.2 System Annunciations 137
- Calibration): 139
- 5.2.3 ADF/DME Failure 143
- *KAP140 aircraft only 144
- Message Advisory Solution 145
- 5.4 TAWS Troubleshooting 146
- Condition Resolution 149
- 5.5.2 GFC Status Page 150
- SERVO DATA 151
- SLIP CLUTCH TEST RESULTS 151
- 5.5.5.1 Monitor Processor 156
- 5.5.5.2 Control Processor 157
- 5.6.1 Overview 159
- Primary Data Path 160
- Secondary Data Path 160
- Third Data Path 162
- Fourth Data Path 162
- Channel LRU Indicator Status 165
- 5.8 GDU 104X Alerts 175
- 5.8.2 Database Alerts 176
- 5.8.3 Cooling Alerts 177
- 5.8.4 Datacard Alerts 178
- 5.8.5 Key Alerts 178
- 5.8.6 Miscellaneous Alerts 179
- 5.8.7 GMA Common Problems 181
- 5.8.8 GMA Alerts 181
- 5.9 GIA 63 Troubleshooting 182
- 5.9.1 COM 182
- 5.9.2 NAV 182
- 5.9.3 G/S 182
- 5.9.4 GPS 182
- 5.10 GIA Alert Messages 183
- 5.10.1 COM Alerts 183
- 5.10.2 NAV Alerts 184
- 5.10.3 Glideslope Alerts 185
- 5.10.4 GPS Alerts 185
- 5.10.5 GIA Cooling Alerts 186
- 5.11 GEA Troubleshooting 187
- 5.11.1 GEA Common Problems 187
- 5.11.2 GEA Alerts 187
- 5.12 GTX Troubleshooting 187
- 5.12.1 GTX Alerts 187
- 5.13.1 AHRS Common Problems 188
- 5.13.2 GRS Alerts 188
- 5.13.3 GMU Alerts 189
- 5.14.2 GDC Alerts 189
- 5.15.2 GDL 69A Alerts 191
- 5.16 GDL 59 Troubleshooting 191
- 5.16.1 GDL 59 Alerts 191
- 5.17 GSR 56 Troubleshooting 192
- 5.17.1 GSR 56 Alerts 192
- Symptom Recommended Action 193
- Table 5-58 193
- 5.19 ESP Troubleshooting 194
- ___________ 196
- 6.1 GDU 104X MFD & PFD 198
- 6.2 GMA 1347 Audio Panel 198
- 6.5 GTX 33 Transponder 199
- 6.6 GTP 59 OAT Probe 200
- 6.7 GRS 77 AHRS 200
- 6.8 GMU 44 Magnetometer 201
- 6.9 GDL 69A 201
- Replacement: 202
- 3 Screw 1 211-60234-08 205
- 6.14 GA35 GPS/WAAS Antennas 206
- 7.1 GDU 104X MFD & PFD 211
- 7.1.2 GDU Software Loading 213
- 7.1.3 PFD/MFD Testing 213
- 7.2 GMA 1347 Audio Panel 215
- 7.2.2 GMA 1347 Testing 216
- 7.3.2 GIA 63 Testing 220
- • 131.250 MHz 221
- • 131.275 MHz 221
- • 131.300 MHz 221
- • 121.175 MHz 221
- • 121.200 MHz 221
- • 121.190 MHz 222
- • 130.285 MHz 222
- • 131.290 Mhz 222
- 7.4.2 GEA 71 Testing 225
- 7.5 GTX 33 Transponder 227
- 7.5.3 GTX 33 Testing 228
- 7.6.2 GDC 74A Testing 230
- 7.6.3 Airspeed Test 231
- 7.6.5 OAT Probe Check 232
- Procedure B: 234
- ROVIDED) 235
- 7.7.3 GRS/GMU Testing 243
- 7.8 GDL 69 XM Data Link 244
- 7.8.2 GDL 69 Testing 245
- 7.9 GDL 59 Datalink 245
- 7.9.2 GDL 59 Test 246
- 7.10 GSR 56 247
- 7.10.1 GSR 56 Testing 248
- GSR 56 Standalone Option 249
- GSA 81 Servo 250
- 7.11.2 GSA 81 Testing 251
- 8.1 Software Verification 253
- 8.2.1 GPS Failure Test 255
- 8.2.2 GIA Failure Test 256
- 8.2.3 Display Failure Test 258
- 8.3 GFC 700 Ground Checkout 262
- 8.3.1 Pre-Flight Test 262
- 8.3.2 AFCS Switch Checks 263
- 8.4 Maintenance Records 265
Verwandte Produkte und Handbücher für Navigatoren Garmin Software Version 0321.23
Navigatoren Garmin GPS 12CX Bedienungsanleitung
(67 Seiten)
(67 Seiten)
Navigatoren Garmin GPSMAP 496 Bedienungsanleitung
(196 Seiten)
(196 Seiten)
Navigatoren Garmin Pilatus PC_6 Betriebsanweisung
(404 Seiten)
(404 Seiten)
Navigatoren Garmin GPS Kit Bedienungsanleitung
(54 Seiten)
(54 Seiten)
Navigatoren Garmin Appliance Data Betriebsanweisung
(148 Seiten)
(148 Seiten)
Navigatoren Garmin GMR 18/24 Bedienungsanleitung
(12 Seiten)
(12 Seiten)
© 2020, manymanuals.de. Alle Rechte vorbehalten. | 0.038 s |
Manymanuals.com
Manymanuals.de
Manymanuals.fr
Manymanuals.it
Manymanuals.pl
Manymanuals.cz
Manymanuals.es
Manymanuals-pt.com
Kommentare zu diesen Handbüchern