VFR Module 1. G1000 Transition VFR Module 1

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Transcription:

VFR Module 1

Course Content G1000 Proficiency Module 1 G1000 (VFR) Module 2 Autopilot (VFR)

Objectives for Module 1 Develop knowledge and skills for successful VFR transition to G1000. Elements: Flight management skills PFD organization Use of nav/com radios MFD organization Malfunctions Systems

G1000 Flight Management Skills Information Management Personal preference (e.g., PFD/MFD configuration) Operation at hand (e.g., navigation, weather) Situational awareness Know what is know-able (and how to find it) Automation Management Autopilot Nav source CDI sensitivity Risk Management Limitations of the aircraft & the glass cockpit technology Limitations of the pilot s knowledge, experience, proficiency

G1000 Components Primary Flight Display (PFD) Multi-Function Display (MFD) Attitude Heading & Reference System (AHRS) Air Data Computer (ADC) Engine Interface Unit Moving Map + other displays Magnetometer Mode S Transponder

G1000 Components Note: This slide is intended for general illustration purposes. Please refer to the documentation for the specific airplane(s) in your unit. Some may be equipped with the GFC700 autopilot (vice KAP140).

System Start-up At system start, the engine and system instruments are displayed on the left side of the PFD in order to provide information necessary for the start-up sequence.

System Start-up Follow checklist carefully! Check standby battery per checklist. Master Switches ON PFD should come on and red Xs clear in about 15 seconds. AHRS should align after 45 seconds and Reversionary mode screen is displayed. Items powered by Avionics Bus 2 (such as NAV 2 and COM 2 will have red Xs until that bus is turned on.

System Start-up Annunciators should illuminate Low Volts will not illuminate if battery has more than adequate charge

MFD Engine Instruments Manifold pressure (MP) RPM (prop) Fuel flow Oil pressure, oil temp, CHT, and EGT Fuel quantity Electrical system

PFD Instrument Display Ball replaced by trapezoid Altitude bug is pilot memory aid Altitude tape range is 600 feet Airspeed tape range is 60 knots Rate of turn trend marks replace turn coordinator and indicate amount of turn in six seconds

PFD Instrument Display Standby Active Waypoint Status Bar Active Standby Comm Frequencies Navigation Frequencies Transponder Outside Air Temperature Clock

Controls for PFD and MFD Pilot can make all inputs with right hand in the central tuning area. NOTE: CAP aircraft have a second audio panel to the right of the MFD.

Controls for PFD and MFD Baro (altimeter setting) Course (triangle) Selects OBS course* 3-second display window Push to center CDI Volume & Squelch Com toggle & emergency key Com frequency selector* Large knob tunes megahertz Small knob tunes kilohertz Push to select b/w Com 1 / Com 2 Range & Joystick Turn to select map range Push to use as joystick *Note: OBS course selection will not work in GPS mode unless the OBS soft key is pressed to disable auto-sequencing.

Controls for PFD and MFD Direct To Key Flight Plan Key Clear Key Remove item Back up a step Press/ hold for default display on MFD Menu Key Procedures Key Enter Key Accept item Confirm selection

Controls for PFD and MFD Flight Management System (FMS) Push small inner knob to activate cursor Large outer knob moves cursor between fields or items Small inner knob enters data or brings up selection list Either knob will move through list

Controls for PFD and MFD Volume & NAV ID Nav flipflop toggle Nav frequency selector* Large knob tunes megahertz Small knob tunes kilohertz Push to select b/w Nav 1 / Nav 2 Heading selector (push to sync with direction of flight) Altitude selector (bug & ref window)

Softkeys Along the bottom of display is a row of softkeys (software enabled keys). The function of each softkey is show by the label above it. INSET key displays 2 x2 moving map on PFD.

PFD Softkeys Inset Pressing INSET softkey also displays the inset map menu options shown below. DCLTR declutter Press repeatedly to cycle through levels of detail on map BACK -- returns to previous level (defaults to upper level in 45 sec)

PFD Softkeys PFD PFD softkey allows configuration of PFD Metric DFLTS ( defaults ) removes metric; selects 360 HSI 360 / 120 arc view Std Baro selects 29.92

PFD Softkeys PFD (cont d) Bearing (Nav1) Bearing (Nav2)

PFD Softkeys OBS In GPS mode, OBS suspends auto sequencing and allows selection of a specified course

PFD Softkeys CDI CDI cycles through GPS, NAV1, NAV 2

Other PFD Softkeys XPDR Squawk code entry; mode selection (SBY ALT, ON), VFR, IDENT) Note GND in this mode, transponder will switch to ALT (Mode C) when the airplane accelerates to approximately 35 knots. IDENT Displays IDENT in XPDR status bar for 18 seconds and sends ID pulse

Other PFD Softkeys TMR/REF Key reference speeds and timer for approaches Note: DO NOT change the reference airspeeds!!

Other PFD Softkeys NRST Scrollable list of 25 nearest airports with basic information & frequencies ALERTS Use this key to acknowledge alerts and close window

PFD Color Coding Cyan Pilot adjustable items (e.g., freq. boxes) Green Active items (e.g, com/nav freqs & VHF.) Magenta GPS related Yellow Caution items (e.g., low vacuum) Red White Warning items (e.g., low oil pressure) Advisory or alert (e.g., airspace ahead)

Audio Unit Operation Powered on with Avionics Master Annunciators illuminate in self-test Returns to previous selections If GMA 1347 fails, built-in relay switches pilot s headset and MIC to Com 1 LED annunciators and backlighting controlled by G1000 CDU

Audio Unit Operation Transceivers Special Functions Marker Beacon Nav and Aux Radios Manual Squelch & Playback ICS Isolation Volume/Squelch Reversionary Mode

Audio Unit Operation Pilot may select ONE transmitter: Com1/MIC or Com2/MIC or Com3/MIC Corresponding receiver is automatically selected Additional receivers (right side) may be selected for monitoring Selection of MIC (left side) highlights selected frequency in GREEN on PFD and MFD

Audio Panel & PFD/MFD Keys Press double-arrow flipflop switch to move frequency from standby tuning box to active position. 133.100 Press appropriate key on audio panel to select COM1 or COM2. In this example: The COM1/MIC key on the left transmits. Press COM knob to move tuning box between COM1 and COM2 Active frequency displays in green; standby frequency displays in white and is bounded by the cyan tuning box. The COM 2 key on the right is selected for monitoring.

Audio Unit Operation - CAP CAP G1000 installations have two GMA 1347 audio panels. Only the TEL button is interconnected. May need manual squelch on right panel for good MIC opening. It is possible to transmit on two VHF radios simultaneously but critical communication may be blocked. Simultaneous transmission on VHF and FM is OK. Both panels may require manual squelch to break properly.

Audio Unit Operation - CAP disabled CAP FM Radio NOTE: CAP aircraft have two audio panels that are independent of each other. Becker Red button allows manual selection of Reversionary Mode; displays primary flight instruments and engine/airframe data on both displays CAP anomaly: red button on right audio panel does not work disabled Press no buttons to let everyone hear everything... Press PILOT or COPILOT to isolate one or the other Press both PILOT and COPILOT isolation buttons to isolate the crew

Other CAP Anomalies Seat Button selects who has the active PTT for second audio panel. Co-Pilot is Seat 2, Scanner behind Pilot is Seat 3. FM/UHF switch must be in FM - no UHF installed.

MFD - Organization Waypoint status bar (unlike PFD, pilot can configure MFD fields as desired) Engine and electrical system instruments Main MFD display area; info shown determined by selected chapter and page. Displays selected chapter (MAP) and page (Navigation Map) Use FMS knob to see and select the chapter and page to be displayed on the MFD.

MFD Engine Instruments Manifold pressure (MP) RPM (prop) Fuel flow Oil pressure, oil temp, CHT, and EGT Fuel quantity Electrical system

MFD - Organization Chapter (large knob) MAP Chapter WPT Chapter AUX Chapter NRST Chapter Page (small knob) 1 Navigation Airports Trip Planning Airports 2 Traffic Intersections Utility Intersections 3 Stormscope NDB GPS Status NDB 4 Weather VOR System Setup VOR 5 Terrain User XM User 6 -- -- System Status Frequency 7 -- -- -- Airspace

MFD Organization The FPL (flight plan) soft key functions like a separate chapter with pages. FPL chapter pages include: Active flight plan Catalog Vertical nav Use FPL pages to create, load, save, modify, or activate flight plans. FPL pages allow loading of stored flight plans This function is not available on the PFD.

MFD Map Setup Use the MENU key to select how to display: Aviation & land Map pointer & zoom Wind speed/direction Map orientation Course & track Topography scale Fuel range ring Lat/Long

MFD MAP Setup Lat/Lon (1) To display lat/lon on navigation map: Step 1: Press Menu for Map Setup options: Small FMS knob for choices ENT to confirm Large FMS knob for fields Small knob for choices

MFD Map Setup Lat/Lon (2) To display lat/lon on navigation map: Step 2: Use large FMS knob to select lat/lon from fields and press ENT Small knob for choices Large knob for fields ENT to confirm CLR to return to main menu

MFD Map Setup Lat/Lon (3) To display lat/lon on navigation map: Step 3: Verify! IMPORTANT: Range on MFD Moving Map must be the range specified in Map Setup menu. Lat/Long will not appear at ranges beyond that specified in the setup process.

MFD Map Setup User Waypoints (1) Creating a User Waypoint Lat/Lon box will appear in upper right corner below frequencies 2a 2b A flashing arrow will appear next to the symbol for your position Press PAN to freeze and display lat/long 2 MAP chapter Nav Page 1

MFD Map Setup User Waypoints (2) Creating a User Waypoint When the lat/lon box appears, press ENT to create a new user defined waypoint Use the FMS knobs to name the waypoint Position is defined automatically by lat/lon & reference to a nearby fix Press ENT to save the new User Defined Waypoint

MFD Map Interpretation Obstacle Proximity Obtacles are shown on the MAP chapter s NAVIGATION MAP page. The colors indicate proximity to the obstacle. Note: CAP does not subscribe to obstacle database updates.

MFD Map Interpretation - TIS Traffic Information Service TIS is a page in the MAP chapter. Uploads data through Mode S Transponder Data is delayed Must be within 55 nautical miles of a TRACON equipped to provide data Reports limited targets Within 7 nm of your position From 3500 above To 3000 Below ADVISORY ONLY! Keep your eyes outside!

MFD Map Interpretation Stormscope Stormscope is a page in the MAP chapter. Shows electrical discharges (lightning) Symbols become smaller with time passage. May be used in cell or strike mode NOT for STORM PENETRATION

MFD Map Interpretation Weather Datalink Weather is a page in the MAP chapter. It can display: NEXRAD Age of Wx Data

MFD Map Interpretation Weather Datalink For textual weather data, use softkeys along the bottom of the bezel while you are in the WPT chapter s Weather Information page.

MFD MAP Interpretation Terrain Proximity The MAP chapter s terrain proximity page uses color coding to display proximity to terrain. Red indicates terrain within 100 or above aircraft Yellow indicate terrains within 1000 of aircraft s altitude Terrain database is updated ANNUALLY AWARENESS ONLY

MFD AUX Setup/Interpretation Use FMS knobs to navigate to the GPS Status page of the AUX chapter in order to check the functionality of each GPS. Hollow=Hunting Filled=Found Aux p. 3 allows dual GPS function verification Etched=Excluded NOTE: Use soft keys to check operation of each GPS!

MFD NRST Interpretation Nearest (NRST) chapter pages include: Nearest Airports Nearest Intersections Nearest NDB Nearest VOR Nearest User WPT Nearest Frequencies Nearest Airspace Use NRST pages to find nearby waypoints. White line shows waypoint location in relation to your position NOTE: NRST keys on PFD and MFD are independent. You cannot use the NRST key on the PFD to access the NRST chapter on the MFD, nor can you use the NRST key on the MFD to access NRST functions on the PFD.

System Annunciations ALERT Messages Advisory no audio Caution one chime abnormal condition may require pilot attention Warning repeated warning tone abnormal condition requiring immediate attention System Annunciators Component Failures

System Annunciations OIL PRESSURE LOW VOLTS PITCH TRIM LOW VACUUM LOW FUEL L LOW FUEL R STBY BAT Oil Pressure - <20 PSI Low Volts - <24 Volts Pitch Trim Test Mode, Runaway Low Vacuum - <3 in. Hg Low Fuel Left - <8 gals. Low Fuel Right - <8 gals. Standby Battery Drawing >0.5 amps

System Annunciations Main Bus reaches 24 Volts Low Voltage Refer to appropriate checklist Be sure Standby Battery switch is in ARMED position before cycling the alternator control unit If indication persists, begin load shedding and look for a place to land as soon as practical

System Annunciations STBY BAT Standby battery is discharging at greater than.5 amp per minute Standby battery should NOT discharge during normal flight

System Annunciations Low Vacuum Vacuum Pump failure Low vacuum affects only the standby attitude indicator

System Annunciations Failure of Line Replaceable Units (LRU) AHRS Attitude and Heading Reference System (GRS 77) Loss of: Attitude indicator ehsi

System Annunciations Failure of Line Replaceable Units (LRU) Magnetometer Failure Loss of Heading Information Only (GMU 44)

System Annunciations Failure of Line Replaceable Units (LRU) ADC Failure Loss of airspeed, Altitude, and vertical speed and OAT (GDC 74A)

System Annunciations Failure of Line Replaceable Units (LRU) Integrated Avionics Unit failure(s) Loss of com 1 and/or com 2 Loss of nav 1 and/or nav 2 Loss of transponder (GIA 63)

System Annunciations Failure of Line Replaceable Units (LRU) Engine and Airframe computer failure Loss of engine instrumentation (GEA 71)

System Annunciations Do NOT pull circuit breakers to demonstrate or test the pilot on LRU failures More in the instructor s course on simulating failures

Avionics Bus 2 Bus 2 Electrical Distribution Box Crossfeed Bus Essential Bus Bus 1 Avionics Bus 1 Electrical System ALT BAT Standby Battery

Fuel System Actual fuel flow is measured by a turbine type transducer mounted on the centerline of the engine between the fuel/air control unit and the fuel distribution unit Fuel flow is displayed in GPH on EIS GAL USED is provided as a totalizer function on the EIS System page After refueling, go to the system EIS page and select RST USED and input fuel quantity.

Fuel System Indicators show quantity of fuel up to limit of fuel sensor float travel (approx. 36 gallons) More fuel may be added to completely fill the tank, but no increase will be indicated on the EIS fuel indicator Visual check of each tank is required Bottom of filler neck is approx. 32 gallons Line of holes in side of filler neck is approximately 37 gallons

Fuel System With fuel indication of 8 gallons or less (for more than 60 seconds), a tone will sound and: PFD will show Low Fuel L or Low Fuel R in the alert section The MFD fuel indicator label will change from white to steady amber

Fuel System When fuel quantity reaches calibrated unusable fuel empty level, label changes to: flashing red It may get very quiet.

Vacuum System To check vacuum: Press Engine softkey Then press System softkey Only one vacuum instrument Attitude Indicator Back-up only Required for IFR (KOEL) Autopilot does not use this system

Limitations Advisory* Information Only: Navigation MAP Traffic MAP Terrain Awareness MAP Weather MAP *NOTE: Garmin documentation clearly states that the system provides this information for enhanced situational awareness. It does not substitute for pilot observation and pilot vigilance.

Dispatch - KOEL Kinds of Operations Equipment List The Kinds of Operations Equipment List table (POH pages 2-9 through 2-13) identifies the equipment required to be operational for airworthiness Cessna 182T Nav III airplane is approved for day and night, VFR and IFR operations Flight into known icing is prohibited

Questions?

VFR Part 1