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MESSAGES

82005-PG-D

SANDEL SN3500 EHSI PILOT’S GUIDE

PAGE

10-7

is usually the source of Fluxgate power.

Note 3:

Loss of the auxiliary 400HZ inverter will only cause the
ADF to become invalid if installed.

MESSAGES

82005-PG-D

SANDEL SN3500 EHSI PILOT’S GUIDE

PAGE

10-8

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Содержание sn3500 ehsi

Страница 1: ...82005 PG D SANDEL SN3500 EHSI PILOT S GUIDE SN3500 EHSI Navigation Display Pilot s Guide 82005 PG D SANDEL SN3500 EHSI PILOT S GUIDE PAGE II This page intentionally left blank...

Страница 2: ...legal and operational limitations of the equipment supplying data to it Always refer to your approved Aircraft Flight Manual Supplement for operation and limitations on the use of installed equipment...

Страница 3: ...4 4 GPS Mode Selection 4 4 Auto Slew Function 4 4 Course Pointer Display Function 4 4 82005 PG D SANDEL SN3500 EHSI PILOT S GUIDE PAGE VI CHAPTER 5 BEARING POINTERS 5 4 Bearing Pointers 5 4 BRG Menu...

Страница 4: ...p operation 6 4 Figure 6 2 Map setup menu 6 4 Figure 6 3 Select AIRSPC 6 4 Figure 6 4 Select ON 6 4 Figure 6 5 Storing settings 6 4 Figure 6 6 Removing map memory 6 4 Figure 6 7 Restoring default sett...

Страница 5: ...from GPS FMS to ILS Page 3 7 Revised display brightness operation Chapter 7 expanded to include FIS B datalink weather description Page 8 4 Eliminated NM icon for normal mode operation Page 9 1 Remove...

Страница 6: ...acon and GPS annunciator displays the SN3500 becomes the virtual equivalent of an EFIS NAV display sized and priced for general aviation cockpits The SN3500 EHSI uses Sandel s patented rear projection...

Страница 7: ...e also presented within the primary display area DISPLAY OVERVIEW 82005 PG D SANDEL SN3500 EHSI PILOT S GUIDE PAGE 2 2 Figure 2 2 Display areas The upper display area presents data from the selected c...

Страница 8: ...pointer 2 BRG2 is represented by the open tip arrowhead symbol Depending on the user selected settings these pointers may show the bearing to a VOR ADF or GPS waypoint The numeric information from the...

Страница 9: ...c heading and button labels Non active legs and waypoints of flight plan To From indicator Inner marker indicator Heading bug and associated data Traffic targets New Stormscope data DISPLAY OVERVIEW 8...

Страница 10: ...e versions Figure 3 1 Introduction screen After a few seconds this display will be removed and the compass card will be shown as below BASIC OPERATION 82005 PG D SANDEL SN3500 EHSI PILOT S GUIDE PAGE...

Страница 11: ...ea if available BASIC OPERATION 82005 PG D SANDEL SN3500 EHSI PILOT S GUIDE PAGE 3 4 In some installations the ILS Lockout function may be enabled on the SN3500 This function forces the selection of t...

Страница 12: ...when flying a complex flight plan as it eliminates the burden of manually setting the course pointer for each leg of the flight plan When auto slew is activated and a GPS FMS is selected as the NAV s...

Страница 13: ...y settings COPY MEM will be displayed momentarily to confirm this action Display and Button Brightness Both the display and button backlight brightness can be controlled through the menu The display b...

Страница 14: ...rce NAV OPERATION 82005 PG D SANDEL SN3500 EHSI PILOT S GUIDE PAGE 4 2 Options are AUTO and OFF When set to auto the course pointer cannot be set manually if the GPS FMS is navigating on a flight plan...

Страница 15: ...left knob until CRS PTR is highlighted in the far left column Rotate the heading bug knob to select the desired option Press M to exit the menu and return to normal operation NAV OPERATION 82005 PG D...

Страница 16: ...NAV1 Yellow NAV2 The cross side color of the bearing pointer and its associated numeric display is yellow when NAV1 is selected and green when NAV2 is selected The digital numeric bearing to the navi...

Страница 17: ...the GPS FMS flight plan waypoints come from the internal database of the SN3500 and are color coded cyan Controlled and Special Use Airspace also comes from the SN3500 s internal database and are col...

Страница 18: ...on screen changes are made to S but can be copied to memories 1 4 as desired The purpose of having a separate scratchpad is to allow you to quickly add or delete items from your map display to attend...

Страница 19: ...e GPS FMS flight plan on the display The active leg and waypoint will be shown in magenta and the other waypoints and course lines will be shown in white Use the or buttons to adjust the map range Set...

Страница 20: ...he map menu rotate the left knob to highlight an item in the left column and rotate the right knob to select the available options in the right column The middle column will display the current select...

Страница 21: ...previously Rotate the left knob to highlight MENU SEL Rotate the right knob until MEMORY in the right column is highlighted MAP OPERATIONS 82005 PG D SANDEL SN3500 EHSI PILOT S GUIDE PAGE 6 10 Rotate...

Страница 22: ...scratchpad memory The scratchpad can now be further modified or press M to exit the menu and return to normal operation Automatic Decluttering Occasionally the SN3500 map display may become too clutt...

Страница 23: ...on the SN3500 in white for 30 seconds after which they are shown in green Cell strikes older than 3 minutes are removed from the display Figure 7 1 WX 500 Stormscope display WX Menu The WX menu can on...

Страница 24: ...are installed Figure 7 5 LTNG SRC mode menu WX500 Display only strikes from WX 500 WSI Display only strikes from WSI BOTH Display strikes from WX 500 WSI WEATHER DISPLAY INTERFACE 82005 PG D SANDEL S...

Страница 25: ...s to provide weather and other non control flight advisory information to pilots in a manner that will enhance their awareness of the flight conditions and enable better strategic route planning The i...

Страница 26: ...this information has been processed it is then up linked to satellites for retransmission to aircraft receivers This process can take up to 3 minutes depending on the amount of information to be uplin...

Страница 27: ...ERFACE 82005 PG D SANDEL SN3500 EHSI PILOT S GUIDE PAGE 7 10 Figures 7 12 and 7 13 illustrate two other situations where observed flight conditions will not correlate to the display in figure 7 10 Fig...

Страница 28: ...PLAY INTERFACE 82005 PG D SANDEL SN3500 EHSI PILOT S GUIDE PAGE 7 11 Figure 7 13 Between layers WEATHER DISPLAY INTERFACE 82005 PG D SANDEL SN3500 EHSI PILOT S GUIDE PAGE 7 12 This page intentionally...

Страница 29: ...ance information is NOT shown on the Altitude Mode Traffic Display Mode Traffic Targets 2m Range Ring TRAFFIC DISPLAY INTERFACE 82005 PG D SANDEL SN3500 EHSI PILOT S GUIDE PAGE 8 2 SN3500 display Traf...

Страница 30: ...suppress the display of non alerting traffic i e traffic other than RAs or TAs This can be useful in busy terminal areas where the display of all traffic may cause the screen to become too cluttered T...

Страница 31: ...mode is set to ON Figure 8 3 ON AUTO menu ALT RANGE Ryan 9900BX TAS Only Selects the desired altitude mode display When interfaced with a traffic processor other than the Ryan 9900BX the altitude mod...

Страница 32: ...played Numeric information display shows NAV flag Note CDI pointer will be visible under the red X for two minutes after power up to allow testing for certain GPS receivers FLAGS AND ABNORMAL CONDITIO...

Страница 33: ...during fast slave correction Heading has not stabilized Map flag Redlined map icons indicates that the map cannot be displayed because of loss of LNAV Stormscope flag Redlined WX indicates loss of dat...

Страница 34: ...SN3500 EHSI PILOT S GUIDE PAGE 10 2 Message Description 400HZ LOW Problem with main inverter Note 1 AIRCRAFT POWER Main power to unit out of specification AUTO SLEW ACTIVE Displayed when course knob...

Страница 35: ...iring short circuit in the aircraft Immediately monitor the lateral and vertical deviation indicators and disable the autopilot and flight director NAV or APPR mode for the duration of the flight if t...

Страница 36: ...is not installed MESSAGES 82005 PG D SANDEL SN3500 EHSI PILOT S GUIDE PAGE 10 6 Message Description OVERTEMP SHTDWN The internal temperature is continuously monitored An over temperature condition wi...

Страница 37: ...DE PAGE 10 7 is usually the source of Fluxgate power Note 3 Loss of the auxiliary 400HZ inverter will only cause the ADF to become invalid if installed MESSAGES 82005 PG D SANDEL SN3500 EHSI PILOT S G...

Страница 38: ...F2 X XXA Standard A2 F1 ZBABHXXXXXXZBABB WW M XX E2 F2 X XXA Physical Dimensions Form Factor 3ATI ARINC 408 Width 3 165 in 8 04 cm Height 3 165 in 8 04 cm Length 10 3 in 26 2 cm overall excluding con...

Страница 39: ...___________ Installer Phone ________________________________________ Work Order __________________________________________ Installer ______________________________________________ NAV Equipment Inputs...

Страница 40: ...associated with the same position as the installed pilot or copilot position Selectable Items Modifiable values multiple choice listings displayed on multiple lines and requests that an operator may...

Страница 41: ...eight Precision approach DME Distance Measuring Equipment EFIS Electronic Flight Instrument System FAA Federal Aviation Administration AVIONICS ACRONYMS 82005 PG D SANDEL SN3500 EHSI PILOT S GUIDE PAG...

Страница 42: ...ound track usually magnetic TSO Technical Standard Order USB Universal Serial Bus Vac Volts AC alternating current in aircraft typically 400Hz Vdc Volts DC direct current VDI Vertical Deviation Indica...

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