Garmin Software Version 0764.20 Guide de l'utilisateur Page 126
- Page / 194
- Table des matières
- MARQUE LIVRES
Noté. / 5. Basé sur avis des utilisateurs
Cirrus Perspective
™
by Garmin – Cockpit Reference Guide for the SR20/SR22/SR22T
190-00821-10 Rev. A
110
Additional Features
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
AlertsAppendixIndex
Roll Engagement
Roll Limit Indicators are displayed on the roll scale at 45° right and left, indicating
where ESP
™
will engage. As roll attitude exceeds 45°, ESP
™
will engage and the on-side
Roll Limit Indicator will move to 30°. The Roll Limit Indicator is now showing where
ESP
™
will disengage as roll attitude decreases to within the desirable roll attitude range.
Once engaged, ESP
™
force will be applied between 30° and 75°. 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
™
will disengage at 30°.
ESP
™
is automatically disengaged if the aircraft reaches the autopilot roll engagement
attitude limit of 75°.
Pitch Engagement
ESP
™
engages at 17.5° nose-up and 15.5° nose-down. Once ESP
™
is engaged, it
will apply opposing force between 17.5° and 50° nose-up and between 15.5° and 50°
nose-down. Maximum opposing force is applied between 22.5° and 50° nose-up and
between 20.5° and 50° nose-down.
With ESP
™
engaged, and the aircraft in a nose-up condition, opposing force steadily
decreases from 17.5° nose-up to 12.5° nose-up as aircraft pitch moves toward zero
degrees. ESP
™
disengages at 12.5° nose-up. With ESP
™
engaged, and the aircraft in
a nose-down condition, opposing force steadily decreases from 15.5° nose-down to
10.5° nose-down as aircraft pitch moves toward zero degrees. ESP
™
disengages at
10.5° nose-down.
The opposing force increases or decreases depending on the pitch angle and the
direction of pitch travel. This force is intended to encourage movement in the pitch
axis in the direction of the normal pitch attitude range for the aircraft.
There are no indications marking the pitch ESP
™
engage and disengage limits in
these nose-up/nose-down conditions.
High Airspeed Protection
Exceeding Vne will result in ESP
™
applying force to raise the nose of the aircraft.
When the high airspeed condition is remedied, ESP
™
force is no longer applied.
- Cirrus SR20/SR22/SR22T 1
- 190-00821-10 Rev. A 10
- Record of Revisions 11
- 190-00821-10 Rev. A i 13
- Table of Contents 14
- FLIGHT INSTRUMENTS 17
- 190-00821-10 Rev. A 3 19
- ENGINE INDICATION SYSTEM 21
- Fuel Flow 22
- 190-00821-10 Rev. A 7 23
- 190-00821-10 Rev. A 9 25
- Full Fuel (SR20) 26
- Initial Usable Fuel Page 26
- Fuel to TABS (SR22) 26
- Full Fuel (SR22) 27
- 190-00821-10 Rev. A 13 29
- 190-00821-10 Rev. A 15 31
- ICS Isolation Modes 33
- All Intercom Mode 34
- ICS Keys Mode Operation 35
- Aircraft Audio 35
- 190-00821-10 Rev. A 21 37
- 190-00821-10 Rev. A 23 39
- Key is recorded. Audio is 40
- 190-00821-10 Rev. A 25 41
- Selected Altitude 42
- 190-00821-10 Rev. A 27 43
- GPS NAVIGATION 45
- Knob to activate the cursor 46
- 190-00821-10 Rev. A 31 47
- Subdued Text 49
- Large Text 49
- Small Text 49
- FLIGHT PLANNING 51
- 190-00821-10 Rev. A 37 53
- 190-00821-10 Rev. A 39 55
- 190-00821-10 Rev. A 41 57
- Creating a stored flight plan: 59
- 190-00821-10 Rev. A 45 61
- 190-00821-10 Rev. A 47 63
- Key to display the Page Menu 64
- Remove using the cursor: 64
- 190-00821-10 Rev. A 49 65
- Delete using the cursor: 66
- Knob to remove the 66
- PROCEDURES 69
- 190-00821-10 Rev. A 55 71
- Altitudes Displayed With 73
- Altitudes Displayed Without 73
- Temperature Compensation 73
- HAZARD AVOIDANCE 75
- 190-00821-10 Rev. A 61 77
- Wx Product 79
- Status Icons 79
- Description 79
- 190-00821-10 Rev. A 65 81
- 190-00821-10 Rev. A 67 83
- 190-00821-10 Rev. A 69 85
- 190-00821-10 Rev. A 71 87
- 190-00821-10 Rev. A 73 89
- Multi Function 91
- System Self Test: 92
- Symbol Description 93
- 190-00821-10 Rev. A 79 95
- Enable/Disable Aviation Data: 96
- Inhibit Terrain Alerting: 96
- Enable Terrain Alerting: 96
- Manual System Test: 97
- Inhibit TAWS: 98
- Enable TAWS: 99
- Blank Page 100
- ADDITIONAL FEATURES 101
- 190-00821-10 Rev. A 87 103
- 190-00821-10 Rev. A 89 105
- 190-00821-10 Rev. A 91 107
- 190-00821-10 Rev. A 93 109
- 190-00821-10 Rev. A 95 111
- Sending a Text Message: 113
- 190-00821-10 Rev. A 99 115
- 190-00821-10 Rev. A 101 117
- Editing a Saved Network: 119
- 190-00821-10 Rev. A 105 121
- 190-00821-10 Rev. A 107 123
- 190-00821-10 Rev. A 109 125
- Creating a profile: 127
- Selecting an active profile: 127
- Renaming a profile: 128
- Deleting a profile: 128
- Importing a profile: 128
- Exporting a profile: 129
- ABNORMAL OPERATION 131
- Position 133
- Extreme Pitch Indication 133
- Dead Reckoning Indications 135
- ANNUNCIATIONS & ALERTS 137
- 190-00821-10 Rev. A 123 139
- In air only / 140
- Garmin AFCS only / 140
- SR22T only 140
- Garmin AFCS only 141
- Garmin AFCS 142
- 190-00821-10 Rev. A 127 143
- 190-00821-10 Rev. A 129 145
- 190-00821-10 Rev. A 131 147
- Voice Alert Description 149
- 190-00821-10 Rev. A 135 151
- 190-00821-10 Rev. A 137 153
- 190-00821-10 Rev. A 139 155
- 190-00821-10 Rev. A 141 157
- 190-00821-10 Rev. A 143 159
- 190-00821-10 Rev. A 145 161
- 190-00821-10 Rev. A 147 163
- 190-00821-10 Rev. A 149 165
- 190-00821-10 Rev. A 151 167
- 190-00821-10 Rev. A 153 169
- 190-00821-10 Rev. A 155 171
- APPENDIX 173
- 190-00821-10 Rev. A 175
- Uploading Database to GRS 186
- Uploading Database to GRS2 187
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