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Dynon Avionics SkyView HDX, Дополнение к руководству по летной эксплуатации самолета

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SkyView

 

Airplane Flight Manual Supplement, Rev N,

 

10/23/2020

 

Page | 7-21

 

 

  

Figure 8: Airspeed Marking Examples 

 

 

Содержание SkyView HDX

Страница 1: ...SkyView Airplane Flight Manual Supplement Rev N 10 23 2020 Page i SkyView Airplane Flight Manual Supplement or Supplemental Airplane Flight Manual 103272 000...

Страница 2: ...eby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use provided that such...

Страница 3: ...Manual AFM or when no AFM exists used as a supplemental aircraft operating manual when the Dynon Avionics SkyView HDX System is installed in accordance with STC SA02594SE The information contained he...

Страница 4: ...improved clarity Added autopilot servo jam emergency procedure Clarified language on FAA approval signature page Formatted section 5 5 Autopilot Operation for improved clarity F 4 29 2019 ECO 327677 C...

Страница 5: ...lot Controls o 6 6 Vertical Guidance Source Loss o 6 9 Yaw Damper Updated the following sections of Section 7 Normal Operations for technical accuracy o 7 10 Course OBS Setting o 7 11 HDX Backup Power...

Страница 6: ...0 Reorganized document according to GAMA 1 guidelines Aircraft specific information moved to separate Appendices to aid technical reviews of document as more Autopilots are added to airplanes on the A...

Страница 7: ...ed old Section 3 1 2 Autopilot Yaw Damper Override to new Section 9 1 1 Subsequent Section 6 headings renumbered Updated language in new Section 3 1 3 Autopilot Yaw Damper Servo Jam Updated language i...

Страница 8: ...3 3 4 Normal Operations 4 1 4 1 General 4 1 4 2 SkyView HDX Backup Power Check 4 8 4 3 EFIS D10A Standby Display Backup Battery Condition Check 4 8 4 4 Autopilot Controls 4 8 4 5 Autopilot Operation C...

Страница 9: ...utopilot Limitations 10 1 10 2 Autopilot Servo Frangible Link Break Away Forces 10 1 11 Appendix 2 Beechcraft Bonanza P35 through V35B 11 1 11 1 Autopilot Limitations 11 1 11 2 Autopilot Servo Frangib...

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Страница 11: ...desired altitudes or exceeding engine parameter limits Airspeed altitude and attitude data is collected by the Air Data Attitude Heading Reference System ADAHRS Engine fuel and electrical system data...

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Страница 13: ...isibility For all airplanes equipped with EMS Configuring the screen layout of a SkyView HDX display unit so the primary engine instruments are not visible to the pilot is prohibited For twin engine a...

Страница 14: ...planes SkyView HDX Synthetic Vision is advisory in nature and must not be used as the sole means of terrain and obstacle avoidance 2 5 Map For all airplanes The SkyView HDX Map and Flight Planning fun...

Страница 15: ..._______________________________________ PRESS 2 Pitot Heat Switch _____________________________________________________ ON 3 Maneuver away from icing conditions 4 Choose one Airspeed reads 0 on all in...

Страница 16: ..._____________________________ PRESS 2 Flight Controls _________________________________ APPLY BREAK AWAY FORCE 3 Flight Controls _________________________________________________ OPERATE 4 AP Power Sw...

Страница 17: ...in Menu indicates STAY ON and POWER OFF 1 STAY ON Button ___________________________________________________ PRESS 2 Plan to land at nearest suitable airport The system is operating on the Backup Batt...

Страница 18: ...connect Autopilot 1 Disconnect Autopilot Press and release red AP Disconnect Button either yoke or panel mounted OR Press the AP Button on the Autopilot Control Panel OR Press the AP Button on the Aut...

Страница 19: ...and Buttons Knobs are located on the left and right sides of the display They can be rotated both directions and pushed The current knob function is indicated by the soft label above the knob Knob fun...

Страница 20: ...s allows the pilot to choose whether a display should show PFD Map or Engine information or some combination thereof See Figure 2 for details for the touchable screen areas of main flight functions Ad...

Страница 21: ...the Knob Function Menu then it does not have a touchable screen area and cannot be assigned to the left knob To add or remove bugs to from the Knob Function Menu go to MENU PFD TOOLS BUGS BARO Setting...

Страница 22: ...itude After the BARO is synchronized a GPSALT message will appear in the altimeter box on the PFD In the Air Adjusts the altimeter based on the METAR of the flight plan s destination airport if within...

Страница 23: ...IN 3 Push knob to close menu menu will also close automatically after 5 seconds This assigns MIN to knob and MIN is shown above knob The Minimum Altimeter area on the PFD is also outlined to show that...

Страница 24: ...rce is re selected Knob Control Panel The Knob Control Panel see Figure 3 is an optional panel mounted module for SkyView This control panel has three knobs dedicated to the most common SkyView bug fu...

Страница 25: ...ess the knob to select an airport 3 TWR ATIS GND and ATC will now select appropriate frequencies for the selected airport 4 Press the knob to toggle the selected active and standby frequencies 5 Press...

Страница 26: ...t failed or the battery is not connected IFR flight with a yellow or red back up battery status indicator displayed is prohibited 4 3 EFIS D10A Standby Display Backup Battery Condition Check The batte...

Страница 27: ...for low light visibility but do not indicate autopilot operation status Use the autopilot mode display and or the autopilot menu to determine autopilot operation status Figure 5 SV AP PANEL Horizonta...

Страница 28: ...ven if Autopilot is disconnected The level function cannot guarantee recovery below VNE in all starting attitudes due to G limiting and servo effort limiting Recoveries have only been demonstrated fro...

Страница 29: ...ce and is tracking a vertical deviation i e status bar shows VNAV or GS as the active mode To engage the Go Around function press the NOSE UP button on the AP Control panel Pressing Go Around NOSE UP...

Страница 30: ...u to arm the NAV mode b Press the VNAV button in the Pitch Menu to arm VNAV mode NAV and VNAV modes arm and activate independently from each other There is no limitation upon the order the modes can b...

Страница 31: ...controls in the centered position when operating the autopilot on the ground to offset this effect 2 Align HDG TRK bug with current heading 3 Select ALT and HDG 4 Engage Autopilot 5 Set Vertical Speed...

Страница 32: ...AUTOPILOT DISCONECT aural should be heard Turn the AP Servo Power switch to OFF and ensure the autopilot disconnects AUTOPILOT DISCONECT aural should be heard Press the AP button on the Autopilot Con...

Страница 33: ...rplane Flight Manual Supplement Rev N 10 23 2020 Page 5 1 5 Performance No change to airplane performance Refer to the airplane s Pilot s Operating Handbook and associated Aircraft Flight Manual and s...

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Страница 35: ...Flight Manual and supplements Installation of a SkyView HDX system impacts the airplane s level weight and balance once during initial installation Certified installers must add new empty weight and b...

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Страница 37: ...yView HDX equipped airplanes always include a Standby Display that provides a display screen and an ADAHRS in a single component with a back up battery to present attitude altitude and airspeed inform...

Страница 38: ...ents connected to the SkyView HDX Network as appropriate 7 8 Flight Crew Alerting System The Flight Crew Alerting System is a central feature of the SkyView HDX system This system provides the pilot a...

Страница 39: ...PILOT DISCONNECT Figure 6 Warning Notification Indication Pressing the WARNING CAUTION or MESSAGE button i e Button 8 opens the Alert Notification Window This window displays text associated with each...

Страница 40: ...dio Alert System has failed AoA system will not operate if installed Do not fly Use visual alerts to monitor status BACKUP BATTERY LOW WARNING The Backup Battery connected to the SkyView display unit...

Страница 41: ...ystem ADAHRS INTERNAL ERROR WARNING System sensor tests performed on ADAHRS failed Do not fly Monitor Standby Display System ADAHRS FAIL WARNING SkyView HDX has detected a problem with the ADAHRS modu...

Страница 42: ...t Manual RPM LOW ENGINE SPEED Tachometer indicator has entered configured Red Low range Refer to Airplane Flight Manual Refer to Airplane Flight Manual EGT X HIGH EXHAUST GAS TEMPERATURE EGT indicator...

Страница 43: ...ered configured Red High range Refer to Airplane Flight Manual Refer to Airplane Flight Manual OIL PRES LOW OIL PRESSURE Oil Pressure indicator has entered configured Red Low range Refer to Airplane F...

Страница 44: ...lot minimum airspeed Visual annunciation appears immediately Aural warning after 10 seconds No action Take command to manually increase airplane s speed Autopilot Bar changes color and temporarily fla...

Страница 45: ...res nose up trim Visual annunciation appears immediately Aural warning after 10 seconds No action Apply Nose Up Trim until the message stops TRIM RUNAWAY shown shown on PFD TRIM RUNAWAY SkyView has de...

Страница 46: ...FLIGHT ACTION IN FLIGHT ACTION BACKUP BATTERY IN USE CAUTION The SkyView display unit presenting the alert has switched to Backup Battery power Do not fly Choose one 1 Alert appears on all displays an...

Страница 47: ...play unit knob controls Use SkyView display unit knob controls NO HI RES TERRAIN CAUTION No high resolution terrain database is installed for airplane s current position Install high resolution databa...

Страница 48: ...rations in Instrument Meteorological Conditions IMC NEED USER AOA CAL CAUTION Angle of Attack AoA calibration for ADAHRS not performed Do not fly if flight requires Instrument Flight Rules IFR Avoid o...

Страница 49: ...IFR Use magnetic compass and GPS track for directional reference Avoid operations in Instrument Meteorological Conditions IMC MAG FACT CAL CORRUPT CAUTION The Remote Magnetometer s factory calibration...

Страница 50: ...tion XPNDR HEX CODE NOT SET CAUTION Transponder hex code is not entered in SkyView display units If Transponder is required do not fly Enter Transponder hex code in SETUP MENU TRANSPONDER SETUP Advise...

Страница 51: ...y and may have specific voice aural annunciations Messages are dependent upon installed systems and components See Table 4 for a full listing of Messages ordered by 1 Core System 2 Component and 3 Fun...

Страница 52: ...escended below set MINIMUM altitude No action Pilot awarness only SYSTEM EVENT X SEE SETUP MESSAGE SkyView has logged a system event for the Dynon Diagnostic file The airplane can be flown Contact Dyn...

Страница 53: ...w from the external flight plan source Pilot awarness only Pilot awarness only None LEAVING ALTITUDE The airplane is leaving the configured altitude No action Pilot awarness only None TRAFFIC A new tr...

Страница 54: ...ilot Bar flashes momentarily AUTOPILOT MODE An Autopilot mode has changed either manually or automaticly since it was engaged Pilot awarness only Pilot awarness only EXT LEVEL BUTTON STUCK MESSAGE The...

Страница 55: ...pilot for remainder of flight Slip Skid Indicator Ball turns Green with letters YD YAW DAMPER The Autopilot Yaw Damper has been engaged Pilot awareness only Pilot awareness only Slip Skid Indicator Ba...

Страница 56: ...Indicates minimum control speed VMC twin engine airplanes YELLOW BAND Indicates the range of speeds below the never exceed speed VNE and above the maximum normal operations speed VNO GREEN BAND Indica...

Страница 57: ...SkyView Airplane Flight Manual Supplement Rev N 10 23 2020 Page 7 21 Figure 8 Airspeed Marking Examples...

Страница 58: ...Operating range For twin engine airplanes SkyView HDX is configured to provide EMS information as follows During takeoffs and landings a secondary non PFD display unit must always present EMS informa...

Страница 59: ...creen On Single engine airplanes the 100 page see Figure 9 is used only when a display unit has been dedicated to EMS or when operating the engine on the ground for maintenance reasons On Twin engine...

Страница 60: ...Page 7 24 SkyView Airplane Flight Manual Supplement Rev N 10 23 2020 Figure 10 Example 100 Display Page for Twin engine Airplanes...

Страница 61: ...e engine airplanes the 50 page see Figure 11 is used to provide additional information beyond what is needed for engine operations such as timers and counters On Twin engine airplanes the 50 page see...

Страница 62: ...Page 7 26 SkyView Airplane Flight Manual Supplement Rev N 10 23 2020 Figure 12 Example 50 Page for Twin engine Airplanes...

Страница 63: ...y On Twin engine airplanes the Bottom Band see Figure 13 can be used to show the required information if the dedicated EMS display unit fails Figure 13 Example Bottom Band for Twin engine Airplanes Th...

Страница 64: ...Page 7 28 SkyView Airplane Flight Manual Supplement Rev N 10 23 2020 Figure 14 Example Partial Bottom Band Display Figure 15 Example Full Bottom Band Display...

Страница 65: ...isual indicators see Figure 17 and aural annunciations CHECK GEAR and GEAR OVERSPEED to alert the pilot to landing gear conditions Figure 17 Example Landing Gear Position Indicator The landing gear s...

Страница 66: ...tions are optional and are configured to function during initial system setup Visual indicators and aural annunciations function independently and are configured separately Temperature Indicators Cyli...

Страница 67: ...nchroscope is used to match the engine RPM to be the same The Synchroscope is located between the RPM indicators on all the engine displays When the Synchroscope is rotating clockwise the right engine...

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Страница 69: ...airplane Refer to the aircraft s Pilot s Operating Handbook and associated Aircraft Flight Manual and supplements Maintain and service SkyView HDX in accordance with the SkyView HDX General Maintenanc...

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Страница 71: ...t modes are annunciated visually on the PFD in a space reserved specifically for this purpose called the Autopilot Information Bar see Figure 22 Visual and voice aural alerts are provided when the Aut...

Страница 72: ...al axis modes 4 TAKE OFF PROTECTION Autopilot disengages if engaged when airspeed comes alive 20 kts to prevent the airplane from taking off with the autopilot engaged This allows the autopilot to be...

Страница 73: ...the condition of a flight control becoming jammed by an Autopilot servo malfunction The pilot must overcome the servo break away force if a flight control fails to move as expected and is jammed by th...

Страница 74: ...n the Autopilot is active and what lateral and or vertical control modes are active and which are armed The AP Info bar resides in the upper left of the PFD see Figure 22 and Figure 23 Touching the AP...

Страница 75: ...SkyView Airplane Flight Manual Supplement Rev N 10 23 2020 Page 9 5 Figure 22 Autopilot Information Bar Figure 23 Autopilot Information Bar shown with AP Engaged...

Страница 76: ...slip alerts will display in the PFD whenever a servo is unable to move the controls in the direction commanded by the Autopilot See Figure 24 for examples of these alerts and where they are located o...

Страница 77: ...rs a Slip Trim Alert for the affected axis When the alert persists the aircraft is likely severely out of trim In this situation disconnect the Autopilot trim the aircraft appropriately and then re en...

Страница 78: ...o the selected mode The servos will remain armed in the selected mode until the AP button is pushed Pushing the AP button will engage the servos into the armed mode currently displayed on the Autopilo...

Страница 79: ...t to the current indicated altitude VS Maintains the selected vertical speed as airplane performance allows until approaching the altitude bug then transitions to ALT mode NOTE If VS mode is selected...

Страница 80: ...e Autopilot Info Bar Go Around The Go Around function is available when the Autopilot is engaged in vertical guidance and is tracking a vertical deviation To engage the Go Around function press the NO...

Страница 81: ...uvers The Yaw Damper is engaged independently from the Autopilot and can be engaged when the autopilot is not engaged The Yaw Damper control appears only on the Autopilot Control Menu see Figure 28 To...

Страница 82: ...Engaged Indication Table 7 Yaw Damper Disconnect Methods DISCONNECT METHOD AP ENGAGED RESULT Press YD button on AP Control Menu YES or NO Yaw Damper servo disengages autopilot is not affected AP Disco...

Страница 83: ...p Setting Use of the Autopilot with flaps extended beyond 10 degrees is prohibited Minimum Altitude Use of the Autopilot below 250 feet AGL is prohibited Servo Frangible Link Use of the Autopilot when...

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Страница 85: ...ing Use of the Autopilot with flaps extended beyond 15 degrees is prohibited Minimum Altitude Use of the Autopilot below 425 feet AGL is prohibited Servo Frangible Link Use of the Autopilot when any s...

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Страница 87: ...Setting Use of the Autopilot with flaps extended beyond 10 degrees is prohibited Minimum Altitude Use of the Autopilot below 200 feet AGL is prohibited Maximum Climb Descend Rate Use of the Autopilot...

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