Garmin Software Version 0321.23 Instrukcja Obsługi Strona 80
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Page 3-36 G1000 System Maintenance Manual – Diamond DA40/40F
Revision G 190-00545-01
3.5.9 TAWS Reactivation
If the TAWS option was previously enabled and the G1000 was reconfigured (default GROUP
configuration file was loaded), it is necessary to reactivate TAWS. Perform this procedure to reactivate
TAWS.
NOTE
When the TAWS option is enabled for the first time (normally at Diamond factory), the
G1000 writes its unique system ID to the physical card and locks the files to this unique
ID. This prevents the unlock card from ever being used to activate TAWS in another
G1000 system. This unlock card is tied to the specific aircraft in which it was used for
the first time. For situations where TAWS must be re-activated, this card must be used.
Reference section 1.6 and the applicable General Arrangement Drawing for Unlock card
details.
1. Remove power from the PFD and MFD by opening the PFD and MFD circuit breakers.
2. A special TAWS Unlock card is required to enable TAWS. Refer to the appropriate General
Arrangement drawing for the correct part number. Insert this card in the upper slot of the PFD.
3. While holding the ENT key on the PFD and MFD, restore power to the displays.
4. When the words
appear in the upper left corner of both displays,
release the ENT keys.
5. On the PFD, go to the System Upload page using the FMS knob.
6. Activate the cursor. Use the small FMS knob to select OPTIONS in the GROUP field and press
the ENT key.
7. Highlight the ITEM field. Use the small FMS knob to select the ‘Enable TAWS’ option and
press the ENT key. Once the option is selected, the configuration files in the SECTION field will
be displayed. All files should be checked. If not, press the CHK ALL softkey.
8. Press the LOAD softkey.
9. Monitor the status of the upload. When the upload is finished, press the ENT key to acknowledge
the upload complete confirmation.
10. View the SUMMARY field and ensure that the item is ‘COMPLETE’.
11. De-activate the cursor.
12. Power down the system and remove the TAWS Enable card from the PFD.
- 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
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