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Wright Aviation Services LLC Presents Piper Meridian Systems Training Program InstrumentationAvidyne Click Mouse to Advance Wright Aviation Services.

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Presentation on theme: "Wright Aviation Services LLC Presents Piper Meridian Systems Training Program InstrumentationAvidyne Click Mouse to Advance Wright Aviation Services."— Presentation transcript:

1 Wright Aviation Services LLC Presents Piper Meridian Systems Training Program InstrumentationAvidyne Click Mouse to Advance Wright Aviation Services

2 Meridian – PA46-500TP Instrumentation – Avidyne Flight Instruments Flight Instruments Click Mouse to Advance Wright Aviation Services

3 Meridian – PA46-500TP Instrumentation – Avidyne Flight Instruments Flight Instruments Auto Flight Auto Flight Click Mouse to Advance Wright Aviation Services

4 Meridian – PA46-500TP Instrumentation – Avidyne Flight Instruments Flight Instruments Auto Flight Auto Flight Navigation Navigation Click Mouse to Advance Wright Aviation Services

5 Meridian – PA46-500TP Instrumentation – Avidyne Flight Instruments Flight Instruments Auto Flight Auto Flight Navigation Navigation Communications Communications Click Mouse to Advance Wright Aviation Services

6 Meridian – PA46-500TP Instrumentation – Avidyne Flight Instruments Flight Instruments Auto Flight Auto Flight Navigation Navigation Communications Communications Flight Management Flight Management Click Mouse to Advance Wright Aviation Services

7 Meridian – PA46-500TP Instrumentation – Avidyne Flight Instruments Flight Instruments Auto Flight Auto Flight Navigation Navigation Communications Communications Flight Management Flight Management Information Management Information Management Click Mouse to Advance Wright Aviation Services

8 Meridian – PA46-500TP Instrumentation – Avidyne Flight Instruments Flight Management Click Mouse to Advance Wright Aviation Services

9 Meridian – PA46-500TP Instrumentation – Avidyne Auto Flight Navigation Information Management Communications Click Mouse to Advance Wright Aviation Services

10 Meridian – PA46-500TP Flight Instruments – Avidyne PFD Click Mouse to Advance Wright Aviation Services

11 Meridian – PA46-500TP Flight Instrumentation – Avidyne PFD Attitude Indicator Click Mouse to Advance Wright Aviation Services

12 Meridian – PA46-500TP Flight Instrumentation – Avidyne PFD Attitude Indicator Altimeter Tape Click Mouse to Advance Wright Aviation Services

13 Meridian – PA46-500TP Flight Instrumentation – Avidyne PFD Attitude Indicator Altimeter Tape Airspeed Tape Click Mouse to Advance Wright Aviation Services

14 Meridian – PA46-500TP Flight Instrumentation – Avidyne PFD Attitude Indicator Altimeter Tape Airspeed Tape Turn and Bank Indicator Click Mouse to Advance Wright Aviation Services

15 Meridian – PA46-500TP Flight Instrumentation – Avidyne PFD Attitude Indicator Altimeter Airspeed Indicator Turn and Bank Indicator Electronic HSI Click Mouse to Advance Wright Aviation Services

16 Meridian – PA46-500TP Flight Instrumentation – Avidyne PFD Attitude Indicator Altimeter Airspeed Indicator Turn and Bank Indicator HSI Vertical Speed Indicator Click Mouse to Advance Wright Aviation Services

17 Meridian – PA46-500TP Flight Instrumentation – Avidyne PFD Attitude Indicator Altimeter Airspeed Indicator Turn and Bank Indicator HSI Vertical Speed Indicator Flight Director Click Mouse to Advance Wright Aviation Services

18 Meridian – PA46-500TP Additional Information – Avidyne PFD Basics Click Mouse to Advance Wright Aviation Services

19 Meridian – PA46-500TP Additional Information – Avidyne Engine Information Torque ITT Temp Fuel Flow Fuel Remaining Click Mouse to Advance Wright Aviation Services

20 Meridian – PA46-500TP Additional Information – Avidyne Wind Vector Direction Speed Vector Arrow Click Mouse to Advance Wright Aviation Services

21 Meridian – PA46-500TP Additional Information – Avidyne Barometer setting Click Mouse to Advance Wright Aviation Services

22 Meridian – PA46-500TP Additional Information – Avidyne Altitude Settings Click Mouse to Advance Wright Aviation Services

23 Meridian – PA46-500TP Additional Information – Avidyne True Airspeed Ground Speed Outside Air Temp Click Mouse to Advance Wright Aviation Services

24 Meridian – PA46-500TP Additional Information – Avidyne PFD Heading Information Present Heading Present Heading Click Mouse to Advance Wright Aviation Services

25 Meridian – PA46-500TP Additional Information – Avidyne PFD Heading Information Present Heading Present Heading Desired Heading Desired Heading Bug indicator Bug indicator Digital readout Digital readout Click Mouse to Advance Wright Aviation Services

26 Meridian – PA46-500TP Additional Information – Avidyne PFD Heading Information Present Heading Present Heading Desired Heading Desired Heading Bug indicator Bug indicator Digital readout Digital readout Selector key Selector key Click Mouse to Advance Wright Aviation Services

27 Meridian – PA46-500TP Additional Information – Avidyne PFD Heading Information Present Heading Present Heading Desired Heading Desired Heading Bug indicator Bug indicator Digital readout Digital readout Selector key Selector key Heading Knob Heading Knob Click Mouse to Advance Wright Aviation Services

28 Meridian – PA46-500TP Additional Information – Avidyne PFD HSI Course Information Course indicator & CDI Course indicator & CDI Bearing Pointer Bearing Pointer Active Segment Active Segment Non-Active Segments Non-Active Segments Click Mouse to Advance Wright Aviation Services

29 Meridian – PA46-500TP Additional Information – Avidyne PFD Source Selection Course Indicator & CDI Course Indicator & CDI GPS1 GPS2 VLOC1 Click Mouse to Advance Wright Aviation Services

30 Meridian – PA46-500TP Additional Information – Avidyne PFD Source Selection Course Indicator & CDI Course Indicator & CDI Bearing Pointer Bearing Pointer GPS1 GPS2 VLOC1 Click Mouse to Advance Wright Aviation Services

31 Meridian – PA46-500TP Additional Information – Avidyne PFD Source Selection Course Indicator & CDI Course Indicator & CDI Bearing Pointer Bearing Pointer Aux Text box Aux Text box GPS1 GPS2 VLOC1 Click Mouse to Advance Wright Aviation Services

32 Meridian – PA46-500TP Additional Information – Avidyne PFD Range: Controls the range of the map display within the HSI. Press the bezzle key and turn the knob to increase/decrease the moving map range. Click Mouse to Advance Wright Aviation Services

33 Meridian – PA46-500TP Additional Information – Avidyne PFD View: When Range/View is selected, pressing in on the knob cycles the EHSI through its four available views. 1 – Compass Rose w/moving map 2 – Compass Rose w/no map ° Arc with moving map 4 – 120° Arc w/no map Click Mouse to Advance Wright Aviation Services

34 Meridian – PA46-500TP Additional Information – Avidyne PFD Course/OBS selector knob In VLOC, select course to by turning the knob – it controls the course pointer and is used as OBS with VORs In GPS modes, the GPS computer controls the course selection. Click Mouse to Advance Wright Aviation Services

35 Meridian – PA46-500TP Flight Management – Avidyne/Garmin Components Information Information Airports Airports Nav Aids Nav Aids Waypoints Waypoints IFR Procedures IFR Procedures Nearest Nearest Flight Plan Flight Plan Active Active Stored Stored Displays Displays Maps Maps Information Information Tools Tools Click Mouse to Advance Wright Aviation Services

36 Meridian – PA46-500TP Flight Management – Avidyne/Garmin Information Available Airports Runways Runways Frequencies Frequencies Approaches Approaches Services Services Other published info Other published info Nav Aids & Waypoints VORs/NDBs VORs/NDBs ARTCC & FSS Services ARTCC & FSS Services User waypoints User waypoints IFR Procedures Approaches Approaches Arrival Procedures Arrival Procedures Departure Procedures Departure Procedures Click Mouse to Advance Wright Aviation Services

37 Meridian – PA46-500TP Flight Management – Avidyne/Garmin Flight Plans Active Plan Direct To Direct To Route of Flight Route of Flight Active Segment Active Segment Time, Distance, ETA Time, Distance, ETA Bearing & Distance Bearing & Distance Stored Plans 31 waypoint plans 31 waypoint plans 19 stored 19 stored Activate & Change Load Inverted Load Inverted Add delete bypass Add delete bypass Click Mouse to Advance Wright Aviation Services

38 Meridian – PA46-500TP Flight Management – Avidyne/Garmin Displays Information Windows Chapters & pages Chapters & pages Overlay info Overlay info Pop-up windows Pop-up windows Selectable info boxes Selectable info boxes Search tools Search tools Moving Map Scalable picture Scalable picture Information source Information source User waypoints User waypointsCalculators Real time info Real time info Flight & Fuel what ifs Flight & Fuel what ifs TAS/Winds/Density Alt TAS/Winds/Density Alt Click Mouse to Advance Wright Aviation Services

39 Meridian – PA46-500TP Auto Flight Avidyne PFD-Magic 1500-GNS430W Click Mouse to Advance Wright Aviation Services

40 Meridian – PA46-500TP Avidyne PFD-Magic 1500-GNS430W Coupled Heading Mode AP to HGD Bug AP to HGD Bug Climb / Descend Preselect Altitude Preselect Altitude Vertical Speed Vertical Speed Indicated Airspeed Indicated Airspeed Auto Navigation Course tracking Course tracking VOR or GPS VOR or GPS Leg Sequencing Leg Sequencing NAV NAV GPSS GPSS Click Mouse to Advance Wright Aviation Services

41 Meridian – PA46-500TP Avidyne PFD-Magic 1500-GNS430W Coupled Heading Operation Push HDG knob to Sync with present heading Press HDG on AP Turn knob to select desired heading AP limited to standard rate turns Can be used in conjunction with track intercept by NAV after HDG. Heading Bug Knob Click Mouse to Advance Wright Aviation Services

42 Meridian PA46-500TP Auto Flight Intelliflight 1500 Autopilot With AP turned ON and ENGAGED Pressing HDG button engage the Heading Mode of the AP. Pressing HDG button engage the Heading Mode of the AP. With AP OFF but FD ON, pressing HDG button will provide FD guidance ONLY. With AP OFF but FD ON, pressing HDG button will provide FD guidance ONLY. With AP engaged, HDG mode can be entered from any other directional control mode. With AP engaged, HDG mode can be entered from any other directional control mode. Click Mouse to Advance Wright Aviation Services

43 Meridian PA46-500TP Auto Flight Intelliflight 1500 Autopilot With AP turned ON and ENGAGED Pressing Nav button engage the directional control mode of the AP. Pressing Nav button engage the directional control mode of the AP. The course needle and CDI will control the AP. The course needle and CDI will control the AP. When CDI needle deflection is greater than 50% from center, the autopilot will establish the aircraft on a 45° intercept angle relative to the selected course. When CDI needle deflection is greater than 50% from center, the autopilot will establish the aircraft on a 45° intercept angle relative to the selected course. Even if CDI needle deflection is less than 50%, the autopilot may still establish an intercept angle of 45°, provided that the aircraft's closure rate to the selected course is sufficiently slow. Otherwise, the intercept angle will be less than 45°. Even if CDI needle deflection is less than 50%, the autopilot may still establish an intercept angle of 45°, provided that the aircraft's closure rate to the selected course is sufficiently slow. Otherwise, the intercept angle will be less than 45°. An exception to this occurs in the case of a pilot selectable intercept angle. Once the point has been reached at which the autopilot must begin to turn the aircraft onto the course, the course is captured. An exception to this occurs in the case of a pilot selectable intercept angle. Once the point has been reached at which the autopilot must begin to turn the aircraft onto the course, the course is captured. Click Mouse to Advance Wright Aviation Services

44 Meridian PA46-500TP Auto Flight Intelliflight 1500 Autopilot With AP turned ON and ENGAGED Program a valid waypoint or flight plan into the GPS Navigator, and press the NAV mode selector switch. The NAV GPSS annunciation will appear as shown. The autopilot will laterally steer the aircraft along the predefined course. During the GPSS mode of operation, the autopilot will not accept any course error input from the Course Pointer. Program a valid waypoint or flight plan into the GPS Navigator, and press the NAV mode selector switch. The NAV GPSS annunciation will appear as shown. The autopilot will laterally steer the aircraft along the predefined course. During the GPSS mode of operation, the autopilot will not accept any course error input from the Course Pointer. As with the NAV mode, the AP will set up a 45 degree intercept of the GPS course line TO the next waypoint or next active GPS leg. As with the NAV mode, the AP will set up a 45 degree intercept of the GPS course line TO the next waypoint or next active GPS leg. GPSS can be activated from any other AP directional control mode GPSS can be activated from any other AP directional control mode Click Mouse to Advance Wright Aviation Services

45 Meridian PA46-500TP Auto Flight Intelliflight 1500 Autopilot With AP turned ON and ENGAGED Press and hold the CWS Switch to engage the CWS mode. The CWS annunciation will appear as shown in Fig. 3-6, while an audible alert sounds. In addition, both the roll and pitch servos will disengage. Maneuver the aircraft as desired, and then release the CWS Switch to disengage the CWS mode. The CWS annunciation will extinguish, the audible alert will be squelched, and both servos will re-engage. Press and hold the CWS Switch to engage the CWS mode. The CWS annunciation will appear as shown in Fig. 3-6, while an audible alert sounds. In addition, both the roll and pitch servos will disengage. Maneuver the aircraft as desired, and then release the CWS Switch to disengage the CWS mode. The CWS annunciation will extinguish, the audible alert will be squelched, and both servos will re-engage. The autopilot will resume operation in the previous mode. If the HDG mode was engaged, the autopilot will hold the selected heading. If the NAV, GPSS, APR, or REV mode was engaged, the autopilot will track the selected course. If the IAS, VS, or ALT mode was engaged, the autopilot will hold the new indicated airspeed, vertical speed, or altitude, respectively. If the ROLL or PITCH mode was engaged, the autopilot will hold the new roll attitude or pitch attitude, respectively. The autopilot will resume operation in the previous mode. If the HDG mode was engaged, the autopilot will hold the selected heading. If the NAV, GPSS, APR, or REV mode was engaged, the autopilot will track the selected course. If the IAS, VS, or ALT mode was engaged, the autopilot will hold the new indicated airspeed, vertical speed, or altitude, respectively. If the ROLL or PITCH mode was engaged, the autopilot will hold the new roll attitude or pitch attitude, respectively. Click Mouse to Advance Wright Aviation Services

46 Meridian PA46-500TP Auto Flight Intelliflight 1500 Autopilot With AP turned OFF and FD ON With the AP READY annunciation displayed, pressing the FD mode selector switch will engage the FD mode, as indicated by an illuminated FD LED shown above. With the AP READY annunciation displayed, pressing the FD mode selector switch will engage the FD mode, as indicated by an illuminated FD LED shown above. Alternately, with the AP READY annunciation displayed, pressing the AP mode selector switch will engage the AP and FD modes. Under this circumstance, press the AP mode selector switch again to disengage the AP mode, thereby disengaging both the roll and pitch servos. Alternately, with the AP READY annunciation displayed, pressing the AP mode selector switch will engage the AP and FD modes. Under this circumstance, press the AP mode selector switch again to disengage the AP mode, thereby disengaging both the roll and pitch servos. With the FD mode engaged and the AP mode disengaged, the pilot must steer the aircraft toward the Command Bars, until the Aircraft Symbol is tucked into them, for any roll axis or pitch axis mode of operation. The flight director provides a visual indication of how accurately the pilot is tracking the autopilot's roll and pitch commands but the AP is NOT ENGAGED. With the FD mode engaged and the AP mode disengaged, the pilot must steer the aircraft toward the Command Bars, until the Aircraft Symbol is tucked into them, for any roll axis or pitch axis mode of operation. The flight director provides a visual indication of how accurately the pilot is tracking the autopilot's roll and pitch commands but the AP is NOT ENGAGED. Click Mouse to Advance Wright Aviation Services

47 Meridian PA46-500TP Auto Flight Intelliflight 1500 Autopilot With AP turned ON and ENGAGED From the AP READY, ALT HOLD, IAD and GS modes, the pitch attitude mode can be engaged. The PITCH annunciation will appear as shown. The autopilot will hold the aircraft at its current (captured) pitch attitude. From the AP READY, ALT HOLD, IAD and GS modes, the pitch attitude mode can be engaged. The PITCH annunciation will appear as shown. The autopilot will hold the aircraft at its current (captured) pitch attitude. Actions to take based on the existing mode: Actions to take based on the existing mode: AP Ready – press AP or FS; from IAS mode – press IAS key; from ALT mode – press ALT key; from GS mode – press GA (go-around) to activate PITCH mode to capture and hold the current pitch. AP Ready – press AP or FS; from IAS mode – press IAS key; from ALT mode – press ALT key; from GS mode – press GA (go-around) to activate PITCH mode to capture and hold the current pitch. The captured pitch attitude may be increased or decreased by pressing the UP or DN Modifier Switch, respectively. A single press of the switch will change the pitch attitude 0.25°. However, pressing and holding the switch will cause the pitch attitude to change at a rate of 1°-per-second. The captured pitch attitude may be increased or decreased by pressing the UP or DN Modifier Switch, respectively. A single press of the switch will change the pitch attitude 0.25°. However, pressing and holding the switch will cause the pitch attitude to change at a rate of 1°-per-second. Click Mouse to Advance Wright Aviation Services

48 Meridian PA46-500TP Auto Flight Intelliflight 1500 Autopilot From any active condition, the corresponding subsequent event will engage the altitude hold mode. The ALT HOLD annunciation will appear as shown above. From any active condition, the corresponding subsequent event will engage the altitude hold mode. The ALT HOLD annunciation will appear as shown above. Rotating either concentric ALT SEL Rotary Knob a single detent will cause the current (captured) baro-corrected altitude to also appear, as a number in units of FT (i.e., for example, FT). The autopilot will hold the aircraft at the captured altitude. Rotating either concentric ALT SEL Rotary Knob a single detent will cause the current (captured) baro-corrected altitude to also appear, as a number in units of FT (i.e., for example, FT). The autopilot will hold the aircraft at the captured altitude. The captured altitude may be increased or decreased by pressing the UP or DN Modifier Switch, respectively. A single press of the switch will change the altitude by 20 FT, and the range is ±500 FT from the original captured altitude. However, pressing and holding the switch will cause the altitude to change at a rate of 40 FT-per-second. The captured altitude may be increased or decreased by pressing the UP or DN Modifier Switch, respectively. A single press of the switch will change the altitude by 20 FT, and the range is ±500 FT from the original captured altitude. However, pressing and holding the switch will cause the altitude to change at a rate of 40 FT-per-second. Click Mouse to Advance Wright Aviation Services

49 Meridian PA46-500TP Auto Flight Intelliflight 1500 Autopilot With AP turned ON and ENGAGED From altitude hold, preselecting a new altitude is accomplished by rotating the ALT SEL knob (clockwise to increase altitude, counterclockwise to reduce). From altitude hold, preselecting a new altitude is accomplished by rotating the ALT SEL knob (clockwise to increase altitude, counterclockwise to reduce). When ready to change altitude, select method – either by VS or by IAS. When ready to change altitude, select method – either by VS or by IAS. Once climb or descent is initiated, it will continue until the pre-selected altitude is achieved, at which point it will return to ALT HOLD mode. Once climb or descent is initiated, it will continue until the pre-selected altitude is achieved, at which point it will return to ALT HOLD mode. During climb or descent, pressing ALT will cause the AP to capture the altitude at the moment ALT is pressed. During climb or descent, pressing ALT will cause the AP to capture the altitude at the moment ALT is pressed. Click Mouse to Advance Wright Aviation Services

50 Meridian PA46-500TP Auto Flight Intelliflight 1500 Autopilot With AP turned ON and ENGAGED From any active condition shown in above, the corresponding subsequent event will engage the vertical speed mode. The VS annunciation will appear as above, along with the current (captured) vertical speed. The latter appears as a number in units of FPM, prefixed by either an UP arrow to indicate a climb, or a DOWN arrow to indicate a descent (i.e., for example, 500 indicates 500 FPM climbing). The autopilot will hold the aircraft at the captured vertical speed. From any active condition shown in above, the corresponding subsequent event will engage the vertical speed mode. The VS annunciation will appear as above, along with the current (captured) vertical speed. The latter appears as a number in units of FPM, prefixed by either an UP arrow to indicate a climb, or a DOWN arrow to indicate a descent (i.e., for example, 500 indicates 500 FPM climbing). The autopilot will hold the aircraft at the captured vertical speed. The captured vertical speed may be increased or decreased by pressing the UP or DN Modifier Switch, respectively. A single press of the switch will change the vertical speed by 100 FPM. However, pressing and holding the switch will cause the vertical speed to change at a rate of 400 FPM-per-second. The captured vertical speed may be increased or decreased by pressing the UP or DN Modifier Switch, respectively. A single press of the switch will change the vertical speed by 100 FPM. However, pressing and holding the switch will cause the vertical speed to change at a rate of 400 FPM-per-second. During a climb, should the commanded vertical speed exceed the actual vertical speed by 300 FPM for a period of 10 seconds, the VS annunciation will flash as an alert to the potential for an impending stall condition. In this event, immediately increase the aircraft's thrust if possible, reduce the commanded vertical speed using the DN Modifier Switch, or both, until the VS annunciation stops flashing. During a climb, should the commanded vertical speed exceed the actual vertical speed by 300 FPM for a period of 10 seconds, the VS annunciation will flash as an alert to the potential for an impending stall condition. In this event, immediately increase the aircraft's thrust if possible, reduce the commanded vertical speed using the DN Modifier Switch, or both, until the VS annunciation stops flashing. Click Mouse to Advance Wright Aviation Services

51 Meridian PA46-500TP Auto Flight Intelliflight 1500 Autopilot Click Mouse to Advance Wright Aviation Services

52 Meridian PA46-500TP Auto Flight Intelliflight 1500 Autopilot With AP turned ON and ENGAGED To climb or descend with a constant airspeed, press the IAS button. This will capture the existing KIAS. The captured indicated airspeed may be increased or decreased by pressing the UP or DN Modifier Switch, respectively. A single press of the switch will change the indicated airspeed by 1 KT. However, pressing and holding the switch will cause the indicated airspeed to change at a rate of 20 KTS-per second. To climb or descend with a constant airspeed, press the IAS button. This will capture the existing KIAS. The captured indicated airspeed may be increased or decreased by pressing the UP or DN Modifier Switch, respectively. A single press of the switch will change the indicated airspeed by 1 KT. However, pressing and holding the switch will cause the indicated airspeed to change at a rate of 20 KTS-per second. Once KIAS is set, power changes can be used to either climb or descend. Conversely, leaving the power unchanged and either increasing or decreasing the desired IAS can be used to either climb or descend. Once KIAS is set, power changes can be used to either climb or descend. Conversely, leaving the power unchanged and either increasing or decreasing the desired IAS can be used to either climb or descend. Click Mouse to Advance Wright Aviation Services

53 Meridian PA46-500TP Auto Flight Intelliflight 1500 Autopilot Click Mouse to Advance Wright Aviation Services

54 Meridian – PA46-500TP Navigation Click Mouse to Advance Wright Aviation Services

55 Meridian – PA46-500TP Navigation Click here to go to a GNS430 Presentation if desired Garmin GNS430W System Click Mouse to Advance Wright Aviation Services

56 Meridian – PA46-500TP Communication Internal Communications Garmin GMA 347 Audio Panel Garmin GMA 347 Audio Panel External Communications Dual Garmin GNS 430Ws Dual Garmin GNS 430Ws Dual Garmin 330 Mode S Xpndrs Dual Garmin 330 Mode S Xpndrs Click Mouse to Advance Wright Aviation Services

57 Meridian – PA46-500TP Flight & Information Management Dual GNS 430W Com/Navs Nav Data Base Terrain Data Base Obstacles Data Base Traffic & Weather Interface Avidyne FlightMax Entegra Moving Map NexRad realtime weather information Traffic Awareness & Avoidance System Jeppesen CMax IFR Charts Click Mouse to Advance Wright Aviation Services

58 Meridian – PA46-500TP Flight & Information Management Dual GNS 430W Com/Navs Nav Data Base Terrain Data Base Obstacles Data Base Traffic & Weather Interface Avidyne FlightMax Entegra Radar and WX500 Stormscope Trip Information interfaced with WX Nearest Information Engine and Systems Performance Click Mouse to Advance Wright Aviation Services

59 Meridian – PA46-500TP Summary and Review Avidyne Meridian Cockpit Dual PFDs Dual PFDs Click Mouse to Advance Wright Aviation Services

60 Meridian – PA46-500TP Summary and Review Avidyne Meridian Cockpit S-Tec Intelliflite 1500 Autopilot S-Tec Intelliflite 1500 Autopilot Click Mouse to Advance Wright Aviation Services

61 Meridian – PA46-500TP Summary and Review Avidyne Meridian Cockpit S-Tec Intelliflite 1500 Autopilot S-Tec Intelliflite 1500 Autopilot Click Mouse to Advance Wright Aviation Services

62 Meridian – PA46-500TP Summary and Review Dual Garmin GNS430W Com/Nav/GPS Units Avidyne Meridian Cockpit Click Mouse to Advance Wright Aviation Services

63 Meridian – PA46-500TP Summary and Review Avidyne Meridian Cockpit Dual Garmin GTX330 Mode-S Transponders Click Mouse to Advance Wright Aviation Services

64 Meridian – PA46-500TP Summary and Review Avidyne Meridian Cockpit Garmin GMS 347 Audio Panel Garmin GMS 347 Audio Panel Click Mouse to Advance Wright Aviation Services

65 Meridian – PA46-500TP Summary and Review Avidyne Meridian Cockpit Garmin GMS 347 Audio Panel Garmin GMS 347 Audio Panel Click Mouse to Advance Wright Aviation Services

66 Meridian – PA46-500TP Summary and Review Click Mouse to Advance Wright Aviation Services Avidyne Meridian Cockpit Center Mounted Entegra Multi Function Display unit Center Mounted Entegra Multi Function Display unit

67 Meridian – PA46-500TP Summary and Review Avidyne Meridian Cockpit Center Mounted Entegra Multi Function Display unit Center Mounted Entegra Multi Function Display unit Click Mouse to Advance Wright Aviation Services

68 Meridian – PA46-500TP Summary and Review Engine DATA BOXs Engine DATA BOXs Trip DATA BOX Trip DATA BOX Avidyne Meridian Cockpit MFD Displays Click Mouse to Advance Wright Aviation Services

69 Meridian – PA46-500TP Summary and Review Radar ON/OFF control Radar ON/OFF control Avidyne Meridian Cockpit MFD Displays Click Mouse to Advance Wright Aviation Services

70 Meridian – PA46-500TP Summary and Review WX Report selection toggle WX Report selection toggle Avidyne Meridian Cockpit MFD Displays Click Mouse to Advance Wright Aviation Services

71 Meridian – PA46-500TP Summary and Review Stormscope selection toggle Stormscope selection toggle WX500 Strike – clear screen WX500 Strike – clear screen Avidyne Meridian Cockpit MFD Displays Click Mouse to Advance Wright Aviation Services

72 Meridian – PA46-500TP Summary and Review Traffic Display toggle Traffic Display toggle Above Above Normal Normal Below Below Unlimited Unlimited Avidyne Meridian Cockpit MFD Displays Click Mouse to Advance Wright Aviation Services

73 Meridian – PA46-500TP Summary and Review View Selection toggle View Selection toggle North up North up Track up Track up Forward Forward Circle Circle Avidyne Meridian Cockpit MFD Displays Click Mouse to Advance Wright Aviation Services

74 Meridian – PA46-500TP Summary and Review Declutter toggle Declutter toggle Cycles through from most to least cluttered and back. Cycles through from most to least cluttered and back. Avidyne Meridian Cockpit MFD Displays Click Mouse to Advance Wright Aviation Services

75 Meridian – PA46-500TP Summary and Review Base Map toggle Base Map toggle Terrain Terrain Base map Base map None None Avidyne Meridian Cockpit MFD Displays Click Mouse to Advance Wright Aviation Services

76 Meridian – PA46-500TP Summary and Review Weather Overlay Weather Overlay Data Link Radar Data Link Radar US RDR or CAN RDR US RDR or CAN RDR US RDR + US RDR + TWX CELL TWX CELL Avidyne Meridian Cockpit MFD Displays Click Mouse to Advance Wright Aviation Services

77 Meridian – PA46-500TP Summary and Review Radar Display & Controls Avidyne Meridian Cockpit MFD Displays Click Mouse to Advance Wright Aviation Services

78 Meridian – PA46-500TP Summary and Review Terrain Awareness System Avidyne Meridian Cockpit MFD Displays Click Mouse to Advance Wright Aviation Services

79 Meridian – PA46-500TP Summary and Review Jeppview Charts Avidyne Meridian Cockpit MFD Displays Click Mouse to Advance Wright Aviation Services

80 Meridian – PA46-500TP Summary and Review Trip (flight plan display) Pages Avidyne Meridian Cockpit MFD Displays Click Mouse to Advance Wright Aviation Services

81 Meridian – PA46-500TP Summary and Review Nearest Display Pages Avidyne Meridian Cockpit MFD Displays Click Mouse to Advance Wright Aviation Services

82 Meridian – PA46-500TP Summary and Review Aux or setup control pages Avidyne Meridian Cockpit MFD Displays Click Mouse to Advance Wright Aviation Services

83 Meridian – PA46-500TP Summary and Review Engine & Electrical System Page Avidyne Meridian Cockpit MFD Displays Click Mouse to Advance Wright Aviation Services

84 Meridian – PA46-500TP Summary and Review Flight Instruments Dual PFD w/EFIS and EHSI Dual PFD w/EFIS and EHSI Standby Attitude, Airspeed and Altitude Indicators Standby Attitude, Airspeed and Altitude Indicators Click Mouse to Advance Wright Aviation Services

85 Meridian – PA46-500TP Summary and Review Flight Instruments Dual PFD w/EFIS and EHSI Dual PFD w/EFIS and EHSI Standby Attitude, Airspeed and Altitude Indicators Standby Attitude, Airspeed and Altitude Indicators Auto Flight Auto Flight S-Tec 1500 autopilot with ALT/VS preselect & VS/IAS S-Tec 1500 autopilot with ALT/VS preselect & VS/IAS Click Mouse to Advance Wright Aviation Services

86 Meridian – PA46-500TP Summary and Review Flight Instruments Dual PFD w/EFIS and EHSI Dual PFD w/EFIS and EHSI Standby Attitude, Airspeed and Altitude Indicators Standby Attitude, Airspeed and Altitude Indicators Auto Flight Auto Flight S-Tec 1500 autopilot with ALT/VS preselect & VS/IAS S-Tec 1500 autopilot with ALT/VS preselect & VS/IAS Navigation Navigation GNS430W 1 or 2 GPS and radio navigation (VOR/LOC) GNS430W 1 or 2 GPS and radio navigation (VOR/LOC) Click Mouse to Advance Wright Aviation Services

87 Meridian – PA46-500TP Summary and Review Flight Instruments Dual PFD w/EFIS and EHSI Dual PFD w/EFIS and EHSI Standby Attitude, Airspeed and Altitude Indicators Standby Attitude, Airspeed and Altitude Indicators Auto Flight Auto Flight S-Tec 1500 autopilot with ALT/VS preselect & VS/IAS S-Tec 1500 autopilot with ALT/VS preselect & VS/IAS Navigation Navigation GNS430W 1 or 2 GPS and radio navigation (VOR/LOC) GNS430W 1 or 2 GPS and radio navigation (VOR/LOC) Communications Communications GNS430W 1 or 2 COM w/stored airport & ATC COM frequencies GNS430W 1 or 2 COM w/stored airport & ATC COM frequencies Click Mouse to Advance Wright Aviation Services

88 Meridian – PA46-500TP Summary and Review Flight Instruments Dual PFD w/EFIS and EHSI Dual PFD w/EFIS and EHSI Standby Attitude, Airspeed and Altitude Indicators Standby Attitude, Airspeed and Altitude Indicators Auto Flight Auto Flight S-Tec 1500 autopilot with ALT/VS preselect & VS/IAS S-Tec 1500 autopilot with ALT/VS preselect & VS/IAS Navigation Navigation GNS430W 1 or 2 GPS and radio navigation (VOR/LOC) GNS430W 1 or 2 GPS and radio navigation (VOR/LOC) Communications Communications GNS430W 1 or 2 COM w/stored airport & ATC COM frequencies GNS430W 1 or 2 COM w/stored airport & ATC COM frequencies Flight Management Flight Management GNS430W 1 or 2 flight plans – 1 active & 19 saved GNS430W 1 or 2 flight plans – 1 active & 19 saved Click Mouse to Advance Wright Aviation Services

89 Meridian – PA46-500TP Summary and Review Flight Instruments Dual PFD w/EFIS and EHSI Dual PFD w/EFIS and EHSI Standby Attitude, Airspeed and Altitude Indicators Standby Attitude, Airspeed and Altitude Indicators Auto Flight Auto Flight S-Tec 1500 autopilot with ALT/VS preselect & VS/IAS S-Tec 1500 autopilot with ALT/VS preselect & VS/IAS Navigation Navigation GNS430W 1 or 2 GPS and radio navigation (VOR/LOC) GNS430W 1 or 2 GPS and radio navigation (VOR/LOC) Communications Communications GNS430W 1 or 2 COM w/stored airport & ATC COM frequencies GNS430W 1 or 2 COM w/stored airport & ATC COM frequencies Flight Management Flight Management GNS430W 1 or 2 flight plans – 1 active & 19 saved GNS430W 1 or 2 flight plans – 1 active & 19 saved Information Management Information Management GNS430W 1 or 2 GNS430W 1 or 2 Avidyne MFD Avidyne MFD Click Mouse to Advance Wright Aviation Services

90 Meridian – PA46-500TP Summary and Review Flight Instruments Dual PFD w/EFIS and EHSI Dual PFD w/EFIS and EHSI Standby Attitude, Airspeed and Altitude Indicators Standby Attitude, Airspeed and Altitude Indicators Auto Flight Auto Flight S-Tec 1500 autopilot with ALT/VS preselect & VS/IAS S-Tec 1500 autopilot with ALT/VS preselect & VS/IAS Navigation Navigation GNS430W 1 or 2 GPS and radio navigation (VOR/LOC) GNS430W 1 or 2 GPS and radio navigation (VOR/LOC) Communications Communications GNS430W 1 or 2 COM w/stored airport & ATC COM frequencies GNS430W 1 or 2 COM w/stored airport & ATC COM frequencies Flight Management Flight Management GNS430W 1 or 2 flight plans – 1 active & 19 saved GNS430W 1 or 2 flight plans – 1 active & 19 saved Information Management Information Management GNS430W 1 or 2 GNS430W 1 or 2 Avidyne MFD Avidyne MFD Nav data includes Airports, Nav Aids, ATC & FSS info and IFR procedures Click Mouse to Advance Wright Aviation Services

91 Meridian – PA46-500TP Avidyne Cockpit Created by Wright Aviation Services LLC Scottsdale/Phoenix Arizona Copyright Wright Aviation Service THE END Contact Information Phone: Website: Click Mouse to Advance Wright Aviation Services


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