Garmin Software Version 1308.10 User's Guide Page 112
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Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240
190-01264-02 Rev. A
96
Additional Features
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSFMS Nav
Flight
PlanningProcedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
AlertsAppendixIndex
ELECTRONIC STABILITY AND PROTECTION
The Garmin ESP
™
Electronic Stability and Protection system is designed to provide
automatic control inputs to discourage aircraft operation outside the normal flight
envelope. ESP works to maintain the desired pitch and roll operating envelope by
automatically engaging one or more servos when the aircraft is near a defined pitch
and/or roll operating limit. While ESP uses the same sensors, processors, and actuators
as the GFC 700 autopilot, it is a separate function. When the GFC 700 autopilot is
engaged and/or the aircraft is at or below 200 feet AGL, the ESP system will not
operate.
ESP engages when the aircraft exceeds one or more conditions (pitch, roll, and/or
Vne) beyond the normal flight parameters. Enhanced stability for each condition is
provided by applying a force to the appropriate control surface to return the aircraft
to the normal flight envelope. This is perceived by the pilot as resistance to control
movement in the undesired direction when the aircraft approaches a steep attitude, high
airspeed, or when a stall is imminent.
As the aircraft deviates further from the normal attitude or airspeed continues to
increase, the force increases (up to an established maximum) to encourage control
movement in the direction necessary to return to the normal attitude and/or airspeed
range. Except in the case of high airspeed, when maximum force is reached, force remains
constant up to the maximum engagement limit. Above the maximum engagement
limit, forces are no longer applied. There is no maximum engagement related to a high
airspeed condition.
When ESP has been engaged for more than ten seconds (cumulative; not necessarily
consecutive seconds) of a 20-second interval, the autopilot is automatically engaged
with the flight director in Level Mode, bringing the aircraft into level flight. An aural
“Engaging Autopilot” alert is played and the flight director mode annunciation will
indicate ‘LVL’ for vertical and lateral modes.
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 pitch and roll attitudes are within engagement limits. ESP can also be
overridden by overpowering the servo’s mechanical torque limit.
ESP can be enabled or disabled on the Avionics Settings Screen on the Touchscreen
Controller.
- Integrated Flight Deck 1
- 190-01264-02 Rev. A 10
- Record of Revisions 11
- Table of Contents 13
- FLIGHT INSTRUMENTS 17
- Flight Instruments 18
- CHANGE NAVIGATION SOURCES 18
- 190-01264-02 Rev. A 3 19
- 190-01264-02 Rev. A 5 21
- ENGINE INDICATION SYSTEM 23
- Engine Indication System 24
- ENGINE/SYSTEM DISPLAY 24
- FUEL CALCULATIONS 26
- ENGINE LEAN ASSIST MODE 27
- Nav/Com/XPDR/Audio Panel 29
- SELECTING A COM RADIO 29
- COM FREQUENCY TUNING 30
- NAV RADIO TUNING 33
- ADF TUNING (OPTIONAL) 34
- DME TUNING (OPTIONAL) 35
- TRANSPONDER OPERATION 36
- Enter a Transponder Code 36
- Selecting a Transponder Mode: 36
- INTERCOM 38
- All Intercom Mode 38
- Pilot-Copilot Intercom Mode 39
- Pilot-Passenger Intercom Mode 40
- All Isolate Mode 40
- DIGITAL CLEARANCE PLAYER 43
- ENTERTAINMENT INPUTS 43
- FLIGHT DIRECTOR ACTIVATION 45
- VERTICAL MODES 46
- LATERAL MODES 47
- FMS NAVIGATION 49
- FMS Navigation 50
- ACTIVATE A STORED FLIGHT PLAN 50
- ACTIVATE A FLIGHT PLAN LEG 50
- STOP NAVIGATING A FLIGHT PLAN 51
- VERTICAL NAVIGATION (VNAV) 51
- FLIGHT PLANNING 57
- Flight Planning 58
- TRIP PLANNING 58
- CREATE A USER WAYPOINT 61
- CREATE A FLIGHT PLAN 62
- Creating a stored flight plan: 63
- ACTIVATING PARALLEL TRACK 66
- USER-DEFINED HOLDING PATTERNS 66
- INVERT AN ACTIVE FLIGHT PLAN 68
- STORE A FLIGHT PLAN 68
- 190-01264-02 Rev. A 55 71
- 190-01264-02 Rev. A 57 73
- PROCEDURES 75
- Procedures 76
- LOAD AN ARRIVAL PROCEDURE 76
- Controller: 76
- ( ) icon 81
- HAZARD AVOIDANCE 83
- Altitude Range 84
- SIRIUSXM WEATHER (OPTIONAL) 87
- GARMIN CONNEXT 89
- WEATHER (OPTIONAL) 89
- TRAFFIC ADVISORY SYSTEM 94
- Changing the altitude range: 96
- TERRAIN-SVT 96
- Hazard Avoidance 100
- ADDITIONAL FEATURES 101
- Additional Features 102
- FliteCharts 103
- (Optional) 103
- 190-01264-02 Rev. A 89 105
- Adjusting the volume: 106
- Mute settings: 106
- Adjusting Volume 106
- Reply to a Text Message 107
- Managing Text Messages 109
- Marking all messages as read: 110
- Delete all messages: 110
- SCHEDULED MESSAGES 110
- Entering a scheduled message: 110
- Edit a scheduled message: 111
- Deleting a scheduled message: 111
- To enable or disable ESP: 113
- Roll Engagement 113
- Pitch Engagement 113
- High Airspeed Protection 113
- Installed Documents 114
- User Documents 114
- Supported PDF Features 114
- Viewing Electronic Documents 115
- To select a document: 115
- To browse the document: 116
- Using document bookmarks: 116
- 190-01264-02 Rev. A 101 117
- Deleting a crew profile: 119
- Viewing Checklists: 120
- Resetting All Checklists: 121
- ABNORMAL OPERATION 123
- Abnormal Operation 124
- UNUSUAL ATTITUDES 125
- DEAD RECKONING 125
- OVERPOWERING AUTOPILOT SERVOS 128
- ANNUNCIATIONS & ALERTS 129
- Annunciations & Alerts 130
- COMPARATOR ALERTS 131
- REVERSIONARY SENSOR ALERTS 132
- MESSAGE ADVISORY 132
- AFCS ALERTS 133
- TERRAIN-SVT ALERTS 134
- TAWS ALERTS 136
- VOICE ALERTS 139
- DATABASE SYSTEM MESSAGES 141
- GSR 56 MESSAGE ADVISORIES 148
- MISCELLANEOUS SYSTEM MESSAGES 153
- APPENDIX 161
- Appendix 162
- GTC SCREENS 167
- Home Screen 167
- Weather Selection Screen 169
- Aircraft Systems Screen 170
- Services Screen 172
- Utilities Screen 173
- Setup Screen 175
- Waypoint Info Screen 176
- Nearest Screen 177
- DATABASE MANAGEMENT 179
- Jeppesen Databases 179
- Features): 180
- To view database status: 184
- Updating Garmin Databases 187
- CLEANING THE TOUCHSCREEN 190
- Blank Page 194
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