Garmin Software Version 0764.14 Podręcznik Użytkownika Strona 118
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Oceniono. / 5. Na podstawie oceny klientów
Cirrus Perspective
™
by Garmin – Cockpit Reference Guide for the SR20/SR22/SR22T
190-00821-08 Rev. A
102
Additional Features
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
AlertsAppendixIndex
As the aircraft reaches 12,500 feet the system sets the AFCS to Altitude Hold
mode. The AFCS will also remain in Automatic Descent Mode as indicated by ‘EDM’
continuing to be displayed as an AFCS Status Annunciation as well as the continuing
presence of the repeating chime. At this point, the AFCS must be disconnected to
cancel Automatic Descent Mode.
ELECTRONIC STABILITY AND PROTECTION (ESP
™
) (OPTIONAL)
The pilot can interrupt ESP
™
by pressing and holding the Autopilot Disconnect
(AP DISC) switch. Upon releasing the AP DISC switch, ESP
™
force will again be
applied, provided aircraft roll attitude is within engagement limits. ESP
™
can also be
overridden by overpowering the servo’s mechanical torque limit.
ESP
™
can be enabled or disabled on the AUX-SYSTEM SETUP2PageontheMFD.
To enable or disable ESP
™
:
1)
Turn the large FMS Knob to select the AUX Page Group.
2)
Turn the small FMS Knob to select the System Setup Page.
3)
If necessary, select the SETUP 2 Softkey to display the AUX-SYSTEM SETUP 2
Page. If the AUX-SYSTEM SETUP 2 is already displayed, proceed to step 4.
4)
Press the FMS Knob to activate the cursor.
5)
Turn the large FMS Knob to place the cursor in the STABILITY &
PROTECTION field.
6)
Turn the small FMS Knob to select ‘ENABLE’ or ‘DISABLE’.
7)
Press the FMS Knob to remove the cursor.
ESP
™
is automatically enabled on system power up.
Roll Engagement
RollLimitIndicatorsaredisplayedontherollscaleat45°rightandleft,indicating
where ESP
™
willengage.Asrollattitudeexceeds45°,ESP
™
will engage and the on-side
RollLimitIndicatorwillmoveto30°.TheRollLimitIndicatorisnowshowingwhere
ESP
™
will disengage as roll attitude decreases to within the desirable roll attitude range.
Once engaged, ESP
™
forcewillbeappliedbetween30°and75°. The force increases
as roll attitude increases and decreases as roll attitude decreases. The applied force is
intended to encourage pilot input that returns the airplane to a more normal roll
attitude. As roll attitude decreases, ESP
™
willdisengageat30°.
ESP
™
is automatically disengaged if the aircraft reaches the autopilot roll engagement
attitudelimitof75°.
- Cirrus SR20/SR22/SR22T 1
- 190-00821-08 Rev. A 10
- Record of Revisions 11
- 190-00821-08 Rev. A i 13
- Table of Contents 14
- FLIGHT INSTRUMENTS 17
- 190-00821-08 Rev. A 3 19
- ENGINE INDICATION SYSTEM 21
- Fuel Flow 22
- 190-00821-08 Rev. A 7 23
- 190-00821-08 Rev. A 9 25
- Full Fuel (SR20) 26
- Initial Usable Fuel Page 26
- Fuel to TABS (SR22) 26
- Full Fuel (SR22) 27
- 190-00821-08 Rev. A 13 29
- 190-00821-08 Rev. A 15 31
- ICS Isolation Modes 33
- All Intercom Mode 34
- ICS Keys Mode Operation 35
- Aircraft Audio 35
- 190-00821-08 Rev. A 21 37
- 190-00821-08 Rev. A 23 39
- Key is recorded. Audio is 40
- 190-00821-08 Rev. A 25 41
- Selected Altitude 42
- 190-00821-08 Rev. A 27 43
- GPS NAVIGATION 45
- Knob to activate the cursor 46
- 190-00821-08 Rev. A 31 47
- Subdued Text 49
- Large Text 49
- Small Text 49
- FLIGHT PLANNING 51
- 190-00821-08 Rev. A 37 53
- 190-00821-08 Rev. A 39 55
- 190-00821-08 Rev. A 41 57
- Creating a stored flight plan: 58
- 190-00821-08 Rev. A 45 61
- Key to display the Page Menu 62
- Remove using the cursor: 63
- Delete using the cursor: 64
- Knob to remove the 64
- (active flight plan only): 65
- PROCEDURES 67
- 190-00821-08 Rev. A 53 69
- HAZARD AVOIDANCE 71
- 190-00821-08 Rev. A 57 73
- Wx Product 75
- Status Icons 75
- Description 75
- 190-00821-08 Rev. A 61 77
- 190-00821-08 Rev. A 63 79
- 190-00821-08 Rev. A 65 81
- 190-00821-08 Rev. A 67 83
- 190-00821-08 Rev. A 69 85
- Multi Function 87
- Symbol Description 89
- 190-00821-08 Rev. A 75 91
- 190-00821-08 Rev. A 77 93
- 190-00821-08 Rev. A 79 95
- ADDITIONAL FEATURES 97
- The Perspective 98
- , ChartView, or FliteCharts 99
- , it may 99
- 190-00821-08 Rev. A 85 101
- 190-00821-08 Rev. A 87 103
- 190-00821-08 Rev. A 89 105
- 190-00821-08 Rev. A 91 107
- 190-00821-08 Rev. A 93 109
- 190-00821-08 Rev. A 95 111
- 190-00821-08 Rev. A 97 113
- 190-00821-08 Rev. A 99 115
- 190-00821-08 Rev. A 101 117
- 190-00821-08 Rev. A 103 119
- 190-00821-08 Rev. A 105 121
- ABNORMAL OPERATION 123
- Position 125
- Extreme Pitch Indication 125
- Dead Reckoning Indications 127
- Blank Page 128
- ANNUNCIATIONS & ALERTS 129
- In air only / 130
- GFC 700 only / 130
- SR22T only 130
- GFC 700 only 131
- 190-00821-08 Rev. A 117 133
- 190-00821-08 Rev. A 119 135
- 190-00821-08 Rev. A 121 137
- 190-00821-08 Rev. A 123 139
- Aural Alert Description 140
- 190-00821-08 Rev. A 125 141
- 190-00821-08 Rev. A 127 143
- 190-00821-08 Rev. A 129 145
- 190-00821-08 Rev. A 131 147
- 190-00821-08 Rev. A 133 149
- 190-00821-08 Rev. A 135 151
- 190-00821-08 Rev. A 137 153
- 190-00821-08 Rev. A 139 155
- 190-00821-08 Rev. A 141 157
- 190-00821-08 Rev. A 143 159
- 190-00821-08 Rev. A 145 161
- APPENDIX 163
- 190-00821-08 Rev. A 165
- Uploading Database to GRS 176
- Uploading Database to GRS2 177
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