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Prueba avion

Assessment

Presentation

Science

2nd Grade

Practice Problem

Hard

Created by

Santiago Luqué

Used 1+ times

FREE Resource

39 Slides • 0 Questions

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G1000

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WHAT IS PFD AND MFD?

PFD: is a modern aircraft instrument dedicated to flight information, primary flight displays are built around a Liquid-crystal
display or CRT display device. Representations of older six pack or "steam gauge" instruments are combined on one compact
display, simplifying pilot workflow and streamlining cockpit layouts.

MFD: presents information drawn from a variety of aircraft information systems, many installations allow overlay or
inclusion of systems indications in the primary flight display (PFD), so MFD prevents the need for a separate display for each
system.
As does the flight management system (FMS) or area navigation (RNAV) unit, the MFD allows you to select different pages
from different chapters that display information provided by various aircraft systems.

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G1000 IN ONE AIR – DA40

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G1000 IN ONE AIR – DA42

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G1000 IN ONE AIR – DA42 ALSIM
SIMMULATOR

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G1000 IN ONE AIR – G1000 SIMMULATOR

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G1000 IN ONE AIR – CIRRUS SR22 (G1000)

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G1000 IN ONE AIR – STUDENTS LOUNGE SIM

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SYSTEM DESCRIPTION

The G1000 system is an integrated flight control system that presents flight instrumentation, position, navigation,
communication, and identification information to the pilot through large-format displays.

The system consists of the following Line Replaceable Units (LRUs):

GDU 1040/1044B Primary Flight Display (PFD)
• GDU 1040/1044B Multi Function Display (MFD)
GIA 63/63W Integrated Avionics Unit (IAU)
GDC 74A Air Data Computer (ADC)
GEA 71 Engine/Airframe Unit
GRS 77 Attitude and Heading Reference System
(AHRS)
GMU 44 Magnetometer

GMA 1347 Audio System with Integrated Marker
Beacon Receiver
GTX 33 Mode S Transponder
GDL 69A Satellite Data Link Receiver
• GTS 800 Traffic Avoidance System (optional)
GDL 90 ADS-B/FIS-B Data Link Transceiver (optional)
GSA 81 AFCS Servos
• GSM 85 Servo Gearboxs

*This course is designed to provide an overview of the G1000 Integrated Flight Deck as installed in Cessna Nav
III aircraft

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LINE REPLACEABLE UNITS (LRU)

GDU 1040/1044B
PFD and MFD

GIA 63/63W
Integrated Avionics
Unit (IAU)

GDC 74A Air
Data Computer
(ADC)

GEA 71
Engine/Airframe
Unit

GRS 77 Attitude and
Heading Reference
System (AHRS)

GMU 44
Magnetometer

GMA 1347 Audio
System

GTX 33 Mode S
Transponder

GDL 69A Satellite
Data Link Receiver

GTS 800 Traffic
Avoidance System

GDL 90
ADS-B/FIS-B Data
Link Transceiver

GSA 81 AFCS
Servos AND GSM
85 Servo Gearboxs

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G1000 CONTROLS

1 NAV VOL/ID Knob – Controls the NAV audio level. Volume
level is shown in the field as a percentage.
2 NAV Frequency Transfer Key – Transfers the standby and
active NAV frequencies.
3 Dual NAV Knob – Tunes the MHz (large knob) and kHz (small
knob) standby frequencies for the NAV. Press to change
4 Heading Knob – Turn to manually select a heading on the
HSI. When pressed, it synchronizes the heading bug.
5 Joystick – Changes the map range when rotated. Activates
the map pointer when pressed.
6 CRS/BARO Knob – The large knob sets the altimeter
barometric pressure and the small knob adjusts the course.
Pressing this knob centers the CDI on the currently selected
VOR.

7 Dual COM Knob – Tunes the MHz (large knob) and kHz (small knob) standby frequencies for the COM transceiver.
8 COM Frequency Transfer Key – Transfers the standby and active COM frequencies. Pressing and holding this key for two
seconds automatically tunes the emergency frequency (121.5 MHz) in the active frequency field.
9 COM VOL/SQ Knob – Controls COM audio level. Audio volume level is shown in the field as a percentage.
17 Dual ALT Knob – Sets the selected altitude in the box located above the Altimeter. The large knob selects the thousands
(500m for metric), while the small knob selects the hundreds (50m for metric).

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10 Direct-to Key – Allows the user to enter a destination waypoint and establish a direct course to the
selected destination (specified by the identifier, chosen from the active route, or taken from the map
pointer position).
11 FPL Key – Displays the active Flight Plan Page for creating and editing the active flight plan, or for
accessing stored flight plans.
12 CLR Key (DFLT MAP) – Erases information, cancels an entry, or removes page menus. To display the
Navigation Map Page immediately, press and hold CLR (MFD only).

13 Dual FMS Knob – Press to turn the selection cursor ON/OFF.
Data Entry: With the cursor ON, turn to enter data in the highlighted field (large knob moves cursor location; small knob
selects character for highlighted cursor location).
Scrolling: When a list of information is too long for the window/box, a scroll bar appears, indicating more items to view.
With cursor ON, turn large knob to scroll through the list.
14 MENU Key – Displays a context-sensitive list of options. This list allows the user to access additional features, or to make
setting changes that relate to certain pages.
15 PROC Key – Selects approaches, departures and arrivals from the flight plan. If a flight plan is used, available procedures
for the departure and/or arrival airport are automatically suggested.
16 ENT Key – Accepts a menu selection or data entry. This key is used to approve an operation or complete data entry. It is
also used to confirm selections and information entries.

G1000 CONTROLS

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1 COM1 MIC 2 COM1 3 COM2 MIC 4 COM2 5, 6, 7, 8, 17 (disabled)
9 PA – Selects the Passenger Address system.
10 SPKR – Selects and deselects the cabin speaker.
11 MKR/MUTE – Mutes the currently received marker beacon receiver audio.
12 HI SENS – Press to increase marker beacon receiver sensitivity. Press again to return to normal.
13 DME – Pressing turns DME audio on or off.
14 NAV116 NAV2 – When selected, audio from the NAV receiver can be heard. (morse)
15 ADF – Pressing turns on or off the audio from the ADF receiver.
18 MAN SQ – Press to enable manual squelch for the intercom.
19 PLAY – Press once to play the last recorded audio. Pressing the PLAY Key during play begins
playing the previously recorded memory block.
20 PILOT – Pressing selects the pilot intercom isolation. Press again to deselect pilot isolation.
21 COPLT – Pressing selects the copilot intercom isolation. Press again to deselect copilot isolation.
22 PILOTKnob – Press to switch between volume and squelch control as indicated by the ‘VOL’ or
‘SQ’ being illuminated. 23 PASS Knob – Turn to adjust Copilot/Passenger intercom volume or
squelch.
24 Reversionary Mode Button – Pressing manually selects Reversionary Mode.

G1000 CONTROLS

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SECURE DIGITAL (SD) CARDS

The PFD and MFD data card slots use Secure Digital (SD) cards, SD cards are used for storing the various databases and
system software updates (Each display bezel is equipped with two SD card slots). The top slot is used for importing and
exporting flight plans, Flight Data Logging, and loading navigation database updates. The bottom slot of each display
contains a Garmin Supplemental Data Card which is used for storing the various databases.

Installing an SD card:
1) Insert the SD card in the SD card slot,
pushing the card in until the spring latch
engages. The front of the card should
remain flush with the face of the display
bezel.
2) To eject the card, gently press on the SD
card to release the spring latch.

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MAP SYMBOLS

Common symbols on MDF map and PDF INSET map

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Traffic Advisories (TA) alert the crew to
intruding aircraft. When traffic meets the
advisory criteria for the TA, a solid yellow circle
symbol is generated. A TA which is detected
but is outside the range of the map on which
traffic is displayed are indicated with a message
in the lower left corner of the map.

MAP SYMBOLS – TRAFFIC ADVISORIES

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The altitude difference between the requesting aircraft and other intruder aircraft is displayed above/below the traffic
symbol in hundreds of feet. If the other aircraft is above the requesting aircraft, the altitude separation appears above the
traffic symbol; if below, the altitude separation appears below. Altitude trend is displayed as an up/down arrow (for speeds
greater than 500 fpm in either direction) to the right of the target symbol.

TIS also provides a vector line
showing the direction in which
the traffic is moving, to the
nearest 45°. Traffic information
for which TIS is unable to
determine the bearing
(non-bearing traffic) is displayed
in the center of the Traffic Map
Page

MAP SYMBOLS – TRAFFIC ADVISORIES

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MAP SYMBOLS

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MAP SYMBOLS – TERRAIN PROXIMITY,
TAWS

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MAP SYMBOLS

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MAP SYMBOLS

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NORMAL DISPLAY OPERATION (PFD)

In normal operating mode, the PFD presents graphical flight instrumentation replacing the traditional flight instrument
cluster. The MFD normally displays a full-color moving map with navigation information while the left portion of the MFD is
dedicated to the Engine Indication System.

Reversionary mode: In the event of a display failure, the G1000 System automatically switches
to reversionary (backup) mode. In reversionary mode, all important flight information is
presented on the remaining display in the same format as in normal operating mode.

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INSTRUMENTS

1 NAV Frequency Box
2 Airspeed Indicator
3 True Airspeed
4 Current Heading
5 Turn Rate Indicator
6 Heading Bug
7 Outside Air Temperature (OAT)
8 Softkeys
9 System Time
10 Transponder Data Box
11 Horizontal Situation Indicator (HSI)

12 Barometric Altimeter Setting
13 Vertical Speed Indicator (VSI)
14 Reference Altitude Bug
15 Altimeter
16 Reference Altitude
17 COM Frequency Box
18 Navigation Status Box
19 Slip/Skid Indicator
20 Attitude Indicator

*Supplemental data: Trend vector, Airspeed awareness
ranges, Course deviation indicator (CDI), Timer, Vertical
Deviation, Glideslope, Glidepath Indicators

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INSTRUMENTS

1 Traffic Annunciation
2 Vspeed Reference
3 Selected Heading
4 Wind Data
5 Inset Map
6 DME Information Window
7 Bearing Information Windows
8 Minimum Descent Altitude/Decision
Height
9 Flight Plan Window
10 Annunciation Window
11 Selected Course
12 Current Vertical Speed
13 Glideslope Indicator
14 Marker Beacon Annunciation
15 Terrain Annunciation
16 AFCS Status Annunciation

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INSTRUMENTS

ALTIMETER

AIRSPEED INDICATOR

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INSTRUMENTS

ARTIFICIAL HORIZON
AND TURN INDICATOR
1 Roll Pointer
2 Roll Scale
3 Horizon Line
4 Aircraft Symbol
5 Land Representation
6 Pitch Scale
7 Slip/Skid Indicator
8 Sky Representation
9 Roll Scale Zero

Slip/Skid
indication

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INSTRUMENTS

HORIZONTAL SITUATION

INDICATOR (HSI)

1 Turn Rate Indicator
2 Selected Heading
3 Current Track Indicator
4 Lateral Deviation Scale
5 Navigation Source
6 Aircraft Symbol
7 Course Deviation Indicator (CDI)
8 Rotating Compass Card
9 OBS Mode Active
10 To/From Indicator
11 Heading Bug
12 Course Pointer
13 Flight Phase
14 Selected Course
15 Turn Rate and Heading Trend Vector
16 Current Heading
17 Lubber Line

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PFD ANNUNCIATIONS AND ALERTING

The Annunciation Window appears to the right of the Vertical
Speed Indicator and displays abbreviated annunciation text for
aircraft alerts. Warnings appear in red, cautions in yellow,
advisory alerts in white, and safe operating annunciations in
green. New alerts are displayed at the top of the Annunciation
Window, regardless of priority.

Traffic is displayed symbolically on the PFD Inset Map, the MFD
Navigation Map Page, and various other MFD page maps.

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PFD ANNUNCIATIONS AND ALERTING

Traffic and

TAWS

Altitude alerting

Marker beacon annunciations

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NORMAL DISPLAY OPERATION (MFD) /
ENGINE INDICATION SYSTEM (EIS)

The Engine Indication System (EIS) displays critical engine, electrical, fuel, and other system parameters on the left side of
the Multi Function Display (MFD) during normal operations . In reversionary mode, the displays are re-configured to present
Primary Flight Display (PFD) symbology together with the EIS

Normal mode

Reversionary mode

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ENGINE DISPLAY

1 Engine Manifold Pressure Gauge (MAN IN) - Displays engine power in inches of mercury (in Hg).
2 Tachometer (RPM) - Displays propeller speeds in revolutions per minute (rpm).
3 Fuel Flow Indicator (FFLOW GPH) - Displays the current fuel flow in gallons per hour (gph).
4 Oil Pressure Indicator (OIL PRES) - Displays pressure of the oil supplied to the engine in pounds per
square inch (psi)
5 Oil Temperature Indicator (OIL TEMP) - Displays the engine oil temperature in degrees Fahrenheit (°F)
6 Cylinder Head Temperature Indicator (CHT) - Displays the head temperature of the hottest cylinder
(number shown in triangular pointer) in °F
7 Exhaust Gas Temperature Indicator (EGT) - Displays the exhaust gas temperature of the hottest
cylinder (number shown in triangular pointer) in °F
10 Fuel Quantity Indicator (FUEL QTY GAL) - Displays the quantity of fuel in gallons (gal) in each tank
(left–L and right–R) from zero to full (F)
12 Voltmeter (M, E BUS VOLTS) - Displays the main and essential bus voltages
13 Ammeter (M, S BATT AMPS) - Displays the main and standby battery load in amperes

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LEAN DISPLAY

1 Engine Manifold Pressure Gauge (MAN IN) - Displays engine power in inches of mercury (in Hg)
2 Tachometer (RPM) - Displays propeller speeds in revolutions per minute (rpm).
3 Fuel Flow (FFLOW GPH) - Displays the current fuel flow in gallons per hour (gph).
5 Exhaust Gas Temperature Bar Graph (EGT °F) - Displays the exhaust gas temperature of all
cylinders in °F; a readout for the selected cylinder (by default, the hottest cylinder) is shown below
the bar graph. The selected cylinder is indicated in light blue. Cylinders whose EGTs are in the
normal range appear in white. The EGT deviation from peak (DPEAK) for the selected cylinder is
displayed below the indicator when the ASSIST Softkey is pressed.
6 Cylinder Head Temperature Bar Graph (CHT) – Same than before but with cylinder head
temperature. Cylinder whose CHTs are in the normal range appear in white. Cylinders whose CHTs
enter the warning range appear in red.
7 Fuel Quantity Indicator (FUEL QTY GAL) - Displays the quantity of fuel in gallons (gal) in each tank
(left–L and right–R)

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SYSTEM DISPLAY

1 Engine Manifold Pressure Gauge (MAN IN) - Displays engine power in inches of mercury (in Hg).
2 Tachometer (RPM) - Displays propeller speeds in revolutions per minute (rpm).
3 Oil Pressure (OIL PSI) - Displays pressure of the oil supplied to the engine in pounds per square inch
(psi)
4 Oil Temperature (OIL °F) - Displays the engine oil temperature in degrees Fahrenheit (°F)
5 Engine Hours (Tach) (ENG HRS) - Displays a numeric readout for the time in hours (hrs) the engine has
been in service
6 Vacuum Pressure Indicator (VAC) - Displays vacuum pump pressure for the standby instruments
7 Fuel Flow (FFLOW GPH) - Displays the current fuel flow in gallons per hour (gph)
8 Calculated Fuel Used (GAL USED) - Displays quantity of fuel used in gallons (gal) based on fuel flow
since last reset
9 Set Fuel Remaining (GAL REM) - Displays current fuel remaining in gal as set by the pilot and adjusted
for fuel burn since last set
10 Fuel Quantity Indicator (FUEL QTY GAL) - Displays the quantity of fuel in gallons (gal) in each tank
(left–L and right–R) from zero to full (F)
11 Voltmeter (M, E BUS VOLTS) - Displays the main and essential bus voltages
12 Ammeter (M, S BATT AMPS) - Displays the main and standby battery load in amperes

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AIR DATA IMPUT FAILURE

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AUTO PILOT FUNCTIONS

18 AP Key – Engages/disengages the autopilot and flight director. Pressing the AP Key activates the flight
director and engages the autopilot in the default pitch axis and roll axis modes. Pressing the AP Key
again disengages the autopilot and deactivates the flight director.
19 HDG Key – Selects/deselects Heading Select Mode.
20 NAV Key – Selects/deselects Navigation Mode.
21 APR Key – Selects/deselects Approach Mode.
22 VS Key – Selects/deselects Vertical Speed Mode.
23 FLC Key – Selects/deselects Flight Level Change Mode.
24 FD Key – Activates/deactivates the flight director only. Pressing the FD Key turns on the flight director
in the default pitch axis and roll axis modes. Pressing the FD Key again deactivates the flight director and
removes the command bars, unless the autopilot is engaged. If the autopilot is engaged, the FD Key is
disabled.
25 ALT Key – Selects/deselects Altitude Hold Mode.
26 VNV Key – Selects/deselects Vertical Navigation Mode.
27 BC Key – Selects/deselects Back Course Mode.
28 29 NOSE UP/NOSE DN Keys – Controls the active pitch reference for the Pitch Hold, Vertical Speed,
and Flight Level Change modes.

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https://www.sportys.com/pilotshop/garminapp

GOOGLE: G1000 TRAINER V13

EXPLORE G1000

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WHAT IS “WX LGND”?

WX LGND displays icon and age on the Inset Map for the selected weather products (it is an optional function)

Steps to manage WX LGND options:

Displaying/removing the weather product information box on the PDF Inset Map:
1.

On the PFD, press the INSET softkey

2.

Press WX LGND softkey

3.

To remove the weather product information, press WX LGND

Viewing legends for displayed weather products (on the Weather Data Link (XM) Page):
1.

Select Weather Data Link (XM) Page

2.

Press LEGEND softkey to display the legends for the displayed weather products. OR:
a)

Press MENU key

b)

Select “Weather Legend” and press ENT key

3.

Turn the FMS knob to scroll through the legends

4.

To remove the legend window, press LEGEND softkey, the ENT or the CLR key, or press the FMS knob

Each active weather product has an associated legend which can be displayed on the Weather Data Link Page. A weather
product legend can also be displayed on the Navigation Map Page for active weather products displayed on that page.

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WHAT IS “NEXRAD”?

WSR-88D, or NEXRAD (NEXt-generation RADar), is a network of 158 high-resolution Doppler radar systems that are operated
by the National Weather Service (NWS). NEXRAD data provides centralized meteorological information for the continental
United States and selected overseas locations. NEXRAD network provides important information about severe weather and
air traffic safety, it detects precipitation and atmospheric movement or wind. It returns data which when processed can be
displayed in a mosaic map which shows patterns of precipitation and its movement.

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