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Manual de instrucciones Apollo 60

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  • Apollo 60 - page 1

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  • Apollo 60 - page 2

    No part of this document may be reproduced in any form or by any means without the express written consent of UPS Aviation Technologies, Inc. II Morrow, UPS Aviation Technologies, and Apollo are trademarks of UPS Aviation Technologies, Inc. © 2001 by UPS Aviation Technologies, Inc. All rights reserved. Printed in the U.S.A. UPS Aviation Technologi ...

  • Apollo 60 - page 3

    Welcome ... Welcome to a new era of aviation navigation. Once again, II Morrow Inc. has set new standards in features and ease of use for the general aviation public. The Apollo GX-series of products are unequaled in providing the features, level of performance, and reliability that aviation users require. The Apollo GX-series sets a precedent that ...

  • Apollo 60 - page 4

    History of Revisions Revision Date Software Ver. Manual P/N January 1998 2.1 560-0961-00 June 1998 2.2 560-0961-01 January 1999 2.2 560-0961-01a March 1999 3.0 560-0961-02 July 2001 3.3 560-0961-03 Ordering Information To receive additional copies of the Apollo GX50/55/60/65 manuals order the following part numbers: User’s Guide 560-0961-xx Appro ...

  • Apollo 60 - page 5

    Important Notice iii The Global Positioning System (GPS) is operated by the United States Department of Defense which is solely responsible for the accuracy, daily operation, and maintenance of the satellite constellation. System accuracy is affected by the Department of Defense’s Selective Availability (SA) and the Dilution of Precision (DOP) at ...

  • Apollo 60 - page 6

    Conventions The SMALL knob is the smaller, inner knob of the two concentric rotary knobs used to look at or change information on the display. When only the SMALL knob is shown next to an example, turn the SMALL knob. The LARGE knob is the larger, outer knob of the two concentric rotary knobs used to look at or change information on the display. Th ...

  • Apollo 60 - page 7

    Table of Contents Introduction ..............................................1 - 1 Apollo GX Features .................................1 - 1 Display ..............................................1 - 2 External Annunciators ...............................1 - 3 Controls ..............................................1 - 3 Keys ........................ ...

  • Apollo 60 - page 8

    Range (Rge) ........................................3 - 4 Course Deviation Indicator (CDI) and Distance Off Track . 3-5 TO/FROM Indicator ................................3 - 6 Desired Track (Dtk) .................................3 - 6 Leg (FROM-TO) Distance ...........................3 - 6 Track (Trk) Angle ...................................3 - 7 ...

  • Apollo 60 - page 9

    Approach GPSS Operation .......................... 3-38 GPSS Rules ....................................... 3-38 Tuned Station ........................................ 3-39 Tuning to a VOR ................................... 3-39 Tuning to a Localizer ............................... 3-40 Moving Map Functions ....................................4 - 1 ...

  • Apollo 60 - page 10

    Fly Direct To A US Grid ............................ 4-30 Create a User Waypoint By Basic Grid ................. 4-30 Fly Direct To A Basic Grid ........................... 4-32 Setting Up A Search Pattern .......................... 4-32 Waypoint Database ........................................5 - 1 Waypoint Information ........................... ...

  • Apollo 60 - page 11

    Delete Plan ........................................ 6-18 Hold ............................................. 6-18 Holding Patterns (GX50/60) ......................... 6-19 Continue .......................................... 6-21 Load Approach (GX50/60 Only) ...................... 6-22 Change Approach (GX50/60 Only) ................... 6-22 Unload A ...

  • Apollo 60 - page 12

    Encoding Altimeter ................................... 7-20 Air Data Info ......................................... 7-21 Air Speed ......................................... 7-21 Air Temperature ................................... 7-21 Altitude and Rate of Climb ........................... 7-21 Heading and Turn Rate ............................. 7-2 ...

  • Apollo 60 - page 13

    Manually Selecting a Flight plan Leg .................... 9-19 Flight Plan Waypoint Sequencing ....................... 9-20 Procedure Turns ...................................... 9-21 Procedure Turn at FAF ................................ 9-22 Holding Patterns ..................................... 9-24 DME Arcs (Arc Assist) ........................ ...

  • Apollo 60 - page 14

    User Stored Frequencies ............................. 10-7 Weather Channels .................................. 10-7 Emergency Channel ................................ 10-8 Intercom Function .................................... 10-8 Stuck Mic ........................................... 10-9 Com Radio System Information (GX60/65 Only) .......... 10-9 ...

  • Apollo 60 - page 15

    Introduction This guide describes the operation of the Apollo GX line of products. The GX50 and GX55 are GPS receivers. The GX60/65 models combine the GPS receiver with a VHF comm radio in a single package. Apollo GX Features The Apollo GX products are high performance GPS products with a high resolution moving map display configured in a 2 inch hi ...

  • Apollo 60 - page 16

    be saved with up to twenty legs for setting up custom tailored routes. The detailed Navigation information displays are also customizable and can be set to automatically scroll through the desired information. The Nearest/Emergency Search feature, invented by II Morrow (UPS Aviation Technologies), makes it easy to react to an emergency or change yo ...

  • Apollo 60 - page 17

    External Annunciators When external indicators are installed, the Apollo GX will also provide an external indication when Parallel Track (PTK) is activated or a Message (MSG) is received. The GX50/60 also have external annunciator controls for OBS/Hold and Approach Active. “Hold” refers to suspending waypoint sequencing. Controls The Apollo GX ...

  • Apollo 60 - page 18

    Keys There are two types of keys that allow you access to the functions in your Apollo GX: permanent “hard” keys and displayed “smart” keys. Seven back lighted permanent keys are used to reach the functions or perform other operations of the Apollo GX. The “smart” key labels are shown on the bottom of the display. There are two categori ...

  • Apollo 60 - page 19

    MAP (Graphic Moving Map) The Map key starts the Moving Map function. The entire display is used as a graphic map display. DIRECT-TO The DIRECT-TO key is used to define a direct course from your present position to a waypoint. Press once to select a waypoint. Press twice to enter an OBS desired track To or From the current active waypoint. ENTER The ...

  • Apollo 60 - page 20

    SYS (System Mode) Press the SYS key to reach the System mode functions. System mode is used to make system level adjustments and modify Nav function displays. SKIP (Start-Up Option) Press the SKIP key during the start-up procedure to bypass the start-up tests. This is for emergencies as the IFR tests must be completed to allow IFR flight. Map Funct ...

  • Apollo 60 - page 21

    Waypoint SCAN Key When the SCAN key is active (highlighted) in the Moving Map display, turning the LARGE knob will move between the nearest airports. You can then press INFO to view information about that airport. In an emergency press DIRECT-TO and ENTER to fly direct to the highlighted airport. Press the SCAN key again to return the LARGE knob to ...

  • Apollo 60 - page 22

    Communicati ons Radio Mode Smart Keys (GX60/65) The Recall (RCL), Monitor (MON), Memorize (MEM), and FLIP/FLOP (<->) keys are available in the GX60/65 after the COM soft key has been pressed. COM (GX60/65) Press the COM key to operate the Communications radio functions. Flip/Flop (GX60/65) Press the FLIP/FLOP key to switch between the active ...

  • Apollo 60 - page 23

    Apollo GX Features Navigation Features 30 Reversible Flight Plans of up to 20 Legs with Automatic Sequencing 500 User-Defined Waypoints Nav Displays Lat/Lon Bearing and Distance Ground Speed and Track Angle Desired Track and Distance Internal CDI Display 160 pixel wide by 80 pixel high electroluminescent display with moving map Automatic Display In ...

  • Apollo 60 - page 24

    Electrical Input voltage 10 VDC to 40 VDC, reverse polarity protected Input current (GPS navigation input) 500 mA typical, 750 mA max at 13.75 VDC 250 mA typical, 375 mA max at 27.5 VDC Input current (comm input - GX60/65 only) 270 mA typical, 2A max at 13.75 VDC, receive 130 mA typical, 900 mA max at 27.5 VDC, receive 2.1A typical, 3.2A max at 13. ...

  • Apollo 60 - page 25

    Serial Interface 2 RS-232 for GX50/60/65 1 RS-232 for GX55 Physical Specifications Height: 2.0 inches (5.08 cm) Width: 6.25 inches (15.88 cm) Depth: 11.125 inches (28.26 cm) behind panel, including mounting frame and connectors Weight (with mounting frame): GX50 and GX55 - 2.6 pounds (1.179 kg) GX60/65 - 3.1 pounds (1.409 kg) Environmental Specific ...

  • Apollo 60 - page 26

    VHF Comm Receiver Performance Specifications (GX60/65) Class D Frequency range - 118.000 to 136.975 MHz, 760 channels Sensitivity 1 microvolt (2 microvolt hard) for 6 dB S+N/N 30% modulation at 1000 Hz Selectivity <6 dB variation at ±22 kHz Speaker audio output level 12 watts into 4 ohms, 8 watts into 8 ohms Headphone audio output level 280 mW ...

  • Apollo 60 - page 27

    Getting Started This section explains how to get started using your Apollo GX. Information in this section explains how to: · Select a waypoint · Store waypoints · Find a Nearest Waypoint · Fly Direct-To a waypoint · Create a flight plan · Activate a flight plan · Use the Moving Map It is necessary to enter a seed position and the current ti ...

  • Apollo 60 - page 28

    2. The Waypoint Type will flash. Turn the SMALL knob to choose the Waypoint Type (Airport, VOR, NDB, INT, or USER). AIRPORT HIO PORTLAND city OR USA 3. Turn the LARGE knob to move the cursor (flashing character) to either the identifier or the city/facility name. Turn the SMALL knob to change the flashing character and show waypoints starting with ...

  • Apollo 60 - page 29

    3. In this case we’ll keep the “A” as the second character. Turn the LARGE knob to the third character and then turn the SMALL knob to select an “L.” AIRPORT 09C KAL AMAZOO city dup MI USA 4. Now, press the SEL key. Note that the entire name “KALAMAZOO” flashes. AIRPORT 09C KALAMAZOO city dup MI USA 5. Turning the SMALL knob will allo ...

  • Apollo 60 - page 30

    Duplicate Identifier, City, or Facility Names While performing Waypoint Identifier selection, you may see the word “dup” on the bottom line. This means that there is more than one waypoint for the displayed city or facility name. The same technique described above can be used to search for duplicate city and facility names. 1. While viewing the ...

  • Apollo 60 - page 31

    Storing a Waypoint Your Apollo GX can store up to 500 user-defined waypoints in the USER database. The waypoint can be created by providing a Lat/Lon position or by a Radial and Distance from a reference waypoint. Then, you can give your waypoint a name and even include a runway length. You can use up to six characters with upper case letters, numb ...

  • Apollo 60 - page 32

    Finding a Nearest Waypoint When you press the NRST key, your Apollo GX will search for the nearest 20 waypoints within 600 nm for each waypoint type. You can also be selective about the runway length, lighting, and surface type. See Setting Runway Limits on page 12. 1. Press the NRST key. The Nearest Waypoint function is displayed with the distance ...

  • Apollo 60 - page 33

    Flying Direct-To a Waypoint Pressing DIRECT-TO allows you to quickly make changes to your TO waypoint. When you press DIRECT-TO , the default waypoint shown will be the current TO waypoint in the Nav or Flight Plan functions or the waypoint displayed in the Database or Info functions. See page 31 for more details. 1. Press the DIRECT-TO key. The di ...

  • Apollo 60 - page 34

    Create a Flight Plan You can create up to 30 flight plans with up to 20 legs each. A flight plan name can have up to eight characters using upper case letters, numbers, or a space. 1. Press FPL . Turn the LARGE knob to reach the Create a New Flight Plan page. Then, press SEL . Press SEL to Create a New Flight Plan 2. The Plan Name page will appear ...

  • Apollo 60 - page 35

    5. The first flight plan leg page will be displayed. Press SEL to start inserting waypoints. ______ to ______ 1 Press SEL to Edit Leg 6. The Ins? prompt will flash. Press ENTER . This will take you to the waypoint database. Use the LARGE and SMALL knobs as described in the Select Waypoint section starting on page 1. Press ENTER after selecting a wa ...

  • Apollo 60 - page 36

    Using the Moving Map The Moving Map gives you a graphic presentation of your flight progress. You can select the type of waypoint displayed, a route line, ATC ring, airspace setup, type of airspace displayed, and map orientation. See the Moving Map section on page 1 for more details. Viewing the Moving Map 1. Press MAP . Turn the LARGE knob to view ...

  • Apollo 60 - page 37

    2-11 Getting Started Select (SEL) Direct-T o (D ) Enter (ENTER) Press SEL to edit information or to select options. Press ENTER to enter and save information. In the Comm function, ENTER saves the S tandby frequency . Press Direct-T o to define a direct course from your present position to a selected wa y point. Press the indicated button and then ...

  • Apollo 60 - page 38

    2-12 Getting Started Turn LARGE Knob to change MH z Turn SMAL L Knob to change kHz Press <-> to toggle Active & St andby Press MON to mo nitor S tandby Press MEM to me morize S tandby Press RCL to recall stored frequencies Press COM Turn the LARGE Knob to view frequency types Turn the SMAL L Knob to view frequencies for selected type Comm ...

  • Apollo 60 - page 39

    Navigation Basics This section explores the navigation function and describes the powerful features it contains. About the Navigation Function The navigation function is always active. When you use other functions, the navigation function continues to run “in the background” calculating your present position, navigating your programmed route (i ...

  • Apollo 60 - page 40

    Autonav The Autonav feature lets you select certain Nav display choices and have them rotate in sequence displaying each one from one to nine seconds. The selection of displays and sequencing time is performed in the Nav Info part of the System Functions (see page 1). 1. Start Autonav by pressing ENTER while displaying the Nav Home Page, or one of ...

  • Apollo 60 - page 41

    Relative Bearing Indicator The Relative Bearing Indicator is an arrow next to the Bearing value that indicates an approximate bearing to a waypoint or airspace relative to the aircraft’s current track when your current ground speed is more than 5 knots. The following illustration describes the bearing range for each arrow. MNOPQRT 23º to 67º 6 ...

  • Apollo 60 - page 42

    Estimated Time En Route (Ete) ETE is to the current TO (destination) waypoint from your present position based on the current ground speed. The units shown are in hours and minutes, 00:00 to 99:59, and in seconds when less than one hour is displayed. If the ground speed is less than or equal to 5 knots, the GPS receiver does not have a valid positi ...

  • Apollo 60 - page 43

    Course Deviation Indicator (CDI) and Distance Off Track The triangle symbol ( “ ) referenced to a bar graph shows your position relative to being on-course. When the bar graph is to the right of the triangle, you must fly right to return on-course. In the example below, the bar graph indicates you are off-course to the right. Fly the aircraft in ...

  • Apollo 60 - page 44

    If the GPS sensor is not sending a valid position, or the current TO waypoint is blank, the CDI will display “—Nav Flagged—”. TO/FROM Indicator The triangle symbol is also used as a TO-FROM indicator. When the triangle is facing up, you are on the “TO” side of the destination waypoint. When the triangle is facing upside down, you are on ...

  • Apollo 60 - page 45

    resolution, 100.0 to 999.9 km at 0.1 km resolution, and 1000 to 9999 km at 1 km resolution. See page 6 for details on changing units of measurement. Track (Trk) Angle Track Angle is the angle of your actual direction of travel. Track is shown as a positive value from 0 to 359 degrees in one degree increments. Track is computed using the magnetic va ...

  • Apollo 60 - page 46

    ete aSLE 00:37 0.006 “ Ft01:23 137kts Minimum Safe Altitude (MSA) MSA is calculated by taking the Maximum Elevation Figure (MEF) from the sectional chart grid that corresponds to your current position. In areas below 3,000 feet, 1,000 feet is added. In areas above 3,000 feet, 2,000 feet is added. In the example below, the current aircraft would b ...

  • Apollo 60 - page 47

    database coverage area. In the example shown above, the MESA for the present position of the aircraft would be 16,800 ft. The mountainous terrain would add a 2,000 ft. buffer to the 14,800 ft. Maximum Elevation figure indicated from the sectional chart. Flight Time Flight Time shows the elapsed time in hours and minutes (00:00 to 99:59) from depart ...

  • Apollo 60 - page 48

    airport types you select, such as: runway length, lighting, and surface type. Press INFO while viewing a Nearest waypoint for more information about that waypoint. Starting Nearest Waypoint & Airspace Search 1. Press the NRST key. Turn the LARGE knob to display the waypoint type or options: Airport, VOR, NDB, Intersection (INT), User (USER), Ch ...

  • Apollo 60 - page 49

    2. The waypoint type will flash. Turn the SMALL knob to choose Airport, VOR, NDB, Intersection (INT) or User waypoint type. VOR PDX PORTLAND facil OR USA 3. Turn the LARGE knob to the waypoint identifier name. The first character of the identifier will flash. Turn the SMALL knob to change characters. Turn the LARGE knob to select the next character ...

  • Apollo 60 - page 50

    Setting Runway Limits for Nearest Waypoints Narrow the type of airports that you will accept by choosing the runway length, lighting, and surface type. The Runway Limits selection also controls the airports that are displayed in the Map function. 1. While in the Nearest Waypoint Search function, turn the LARGE knob to view the “Runway Limits” d ...

  • Apollo 60 - page 51

    4. Turn the LARGE knob to cause the runway surface type to flash. Turn the SMALL knob to choose from the Hard, Soft, or Water surface types. Soft refers to grass, dirt, or gravel runways. Choices include: Hard, Hard/Soft, and Hard/Soft/Water. Runway Limits HARD/SOFT Ft:3500 Lit:Yes 5. Press ENTER to save your choices or press SEL again to disable s ...

  • Apollo 60 - page 52

    1. Press the INFO key to view information about the airspace. Values for ceiling and floor may be any number of positive feet less than 100,000. Values may also be Unlimited, Ground, FL (Flight Level, followed by a number such as 050), Unknown, or NOTAM. KANSAS CITY Ceil: 8000’msl Floor: GROUND 2. Turn the SMALL knob to view more information abou ...

  • Apollo 60 - page 53

    In the Nav function, turn the LARGE knob to view the Altitude Assist page. The diamond in the corner notes that turning the SMALL knob will show the Encoder Altitude, Auto Descent, End Altitude, and Hold Altitude, and Buffer values. Altitude Assist Local Altimeter Setting 29.92" · Setting the Local Altimeter Value 1. While viewing the Altitud ...

  • Apollo 60 - page 54

    Setting Hold Altitude and Buffer The Hold Altitude is an altitude where you want to remain. The Buffer is the tolerance or range in altitude that you can move in vertically before a warning message is generated. 1. In the Nav function, turn the LARGE knob to the Hold Alt/Buffer page. Press SEL . The Hold Altitude value will flash. Hold Alt 5650ft B ...

  • Apollo 60 - page 55

    Auto Descent The Auto Descent feature allows you to input a desired End Altitude, an Offset Distance from a desired Auto Descent Waypoint from the Active flight plan, a desired Feet per Minute Descent rate, and an expected Ground speed. It then automatically calculates the distance remaining in your Active flight plan to the desired Auto Descent Wa ...

  • Apollo 60 - page 56

    Set up your Auto-Descent by selecting: · Distance from destination waypoint (0 - 99 nm) or Offset Distance · Ending altitude (-1,500 - 50,000’ in 50’ steps) · Descent rate (100 - 5,000’/min in 10’/min steps) · Estimated ground speed (50 - 600 kts) 1. While viewing either the Auto-Descent or End Alt page in the Altitude Assist function, ...

  • Apollo 60 - page 57

    Parallel Track Offset This function allows you to create a parallel course offset to the left or right from your current flight plan from 0.1 to 20.0 nm. You must have FROM and TO waypoints defined. Parallel Track cannot be activated if you set a course using Direct-To. Transitions between future flight plan legs cannot have turns greater than 120 ...

  • Apollo 60 - page 58

    1. In the Nav function, turn the LARGE knob to display Parallel Track. Parallel Track Offset: Standby RIGHT 12.4nm 2. Press SEL . The Offset field will flash. Two states are available: Use or Standby. If Parallel Track is in use, “Standby” will flash. If Parallel Track is on Standby, “Use?” will flash. If the direction and distance values a ...

  • Apollo 60 - page 59

    5. Turn the LARGE knob back to the “Offset” field. Press ENTER when the “Use?” prompt flashes to activate Parallel Track. A “p” will appear next to the waypoint identifier to indicate that Parallel Track is in use. The MSG annunciator will flash and a message will state that Parallel Track is in use. Press MSG to view the message. Paral ...

  • Apollo 60 - page 60

    Countdown Timer The Countdown Timer allows you to set a timer that will alert you when it expires with a flashing MSG annunciator. The maximum time is 99:59:59 (hours, minutes, seconds). The default time on power up is the previous time that was entered. The factory default time is 00:03:00 (3 minutes). You can stop the timer by pressing SEL twice ...

  • Apollo 60 - page 61

    Arc Assist The Arc Assist function will help you to navigate along an arc. In the GX50/60, Arc Assist will help you fly approaches with DME Arcs. Arc Assist can be used as a user-defined arc to avoid special use airspaces, or for conducting aerial searches using increasingly larger circles. The Arc Assist page shows the direction of the arc (left o ...

  • Apollo 60 - page 62

    2. Press SEL . Choose another waypoint using the LARGE and SMALL knobs. VOR CVO CORVALLIS facil OR USA 3. Select the Arc direction with the SMALL knob. Left Arc dtk 171 ref: CVO vor Rad 005° 14.0nm· Rght Arc dtk 351 ref: CVO vor Rad 005° 14.0nm 4. Press ENTER to accept the selections and start navigating. Note The DTK on the Arc Assist page is t ...

  • Apollo 60 - page 63

    Waypoint Distance Page This page shows the cumulative distance from your current position to each waypoint in the active flight plan starting with the active leg. Turn the SMALL knob to view the next set of waypoints in your active flight plan. The waypoint type is shown to the left of the identifier. The allowable waypoint types are: Airport (a), ...

  • Apollo 60 - page 64

    From/To/Next Waypoint The FROM/TO/NEXT Waypoint allows you to view and/or edit a three waypoint mini-flight plan, or view two legs of your flight plan, while within the Nav function. These waypoints are like a three waypoint window into your Active Flight Plan. Changes to the FROM/TO/NEXT page change the Active Flight Plan, and vice versa. You may ...

  • Apollo 60 - page 65

    2. Press SEL to start editing. Turn the LARGE knob to select the FROM (first) waypoint position. Turn the SMALL knob, if necessary, so the flashing selection shows “Ins?” (Insert). Press ENTER . From Ins? To ______ Next ______ 3. The Waypoint Type will flash. Choose the Waypoint Type with the SMALL knob. AIRPORT AAF APALACHIOCOLA city FL USA 4. ...

  • Apollo 60 - page 66

    6. Turn the LARGE knob clockwise one click to move to the next character. Turn the SMALL knob to select the desired character. Continue to select the needed characters. AIRPORT EUG EUGENE city OR USA 7. Press ENTER when you have selected the desired waypoint. From EUG arpt To ______ Next ______ B - Set the TO Waypoint 1. Press SEL and move to the T ...

  • Apollo 60 - page 67

    C - Set the NEXT Waypoint 1. Press SEL and move to the NEXT waypoint with the LARGE knob. The insert (Ins?) choice will flash. Press ENTER and then select the NEXT waypoint as you did for the FROM and TO waypoints. From EUG arpt To SLE Next Ins? 2. After selecting a NEXT waypoint, press ENTER . From EUG arpt To SLE arpt Next HIO arpt D - Editing FR ...

  • Apollo 60 - page 68

    3. Turn the SMALL knob to choose the type of editing you want to do. The flashing selection will ask you to choose between Ins (Insert), Chg (Change), or Del (Delete). The TO waypoint can also be placed on Hold. Press ENTER when you have selected the editing option. When a waypoint is deleted, its position will be replaced by dashes. The Chg and In ...

  • Apollo 60 - page 69

    Using Direct-To Pressing the DIRECT-TO key sets your present position as the FROM location. When using the Direct-To function, the FROM waypoint identifier is overwritten with the word “Direct.” If you remove the Direct-To position with the Del? option, the old FROM waypoint is returned to that position. If you edit the FROM position, Direct-To ...

  • Apollo 60 - page 70

    Direct-To Operation 1. Press the DIRECT-TO key. The waypoint type will flash. AIRPORT HIO PORTLAND city OR USA 2. Select the new destination (TO) waypoint using the SMALL and LARGE knobs. AIRPORT MMV MC MINNVILLE city OR USA 3. Press ENTER . Direct-To Examples The following three examples provide some of the more common ways that you can use the po ...

  • Apollo 60 - page 71

    1. You flew to the right to avoid a storm cloud and your CDI tells you to fly left, but you still have the same TO waypoint. Press DIRECT-TO . Your current TO waypoint is displayed and the Waypoint Type will flash. AIRPORT SLE SALEM city OR USA 2. Press ENTER . You will now fly direct from your present position to your desired TO waypoint. Your CDI ...

  • Apollo 60 - page 72

    1. While on the first leg of your active flight plan, you find out that you need to make another stop on the way but you don’t want to change the rest of your plan. Press FPL . While viewing the Active flight plan, turn the SMALL knob to the first leg. SLE to HIO 1** 345° 37.8nm arpt arpt 2. Press DIRECT-TO . Select the desired waypoint using th ...

  • Apollo 60 - page 73

    Direct-To OBS Pressing the DIRECT-TO key twice starts the OBS desired track editor. OBS Desired Track allows entry of a desired track to or from the current TO waypoint. The current desired track in the navigation pages will be replaced by the OBS Desired Track value entered. You may also select the reference waypoint from your active flight plan. ...

  • Apollo 60 - page 74

    4. Press ENTER when the choices are selected. Turn Anticipation The Apollo GX will provide information for you to smoothly transition from one flight plan leg to another. Turns are drawn on the moving map. You will receive a message about ten seconds before the turn. The message will count down to the beginning of the turn. The message shown below ...

  • Apollo 60 - page 75

    Turn anticipation will not be available when sequencing is on Hold; for the MAP or MAHP of an approach; or for the “flyover” waypoints in an approach. Wind and Turn Anticipation The graphic Turn Anticipation curve drawn on the map display is based on your current ground speed. Once you enter the turn, the graphic curve is no longer updated. You ...

  • Apollo 60 - page 76

    Approach GPSS Operation When the autopilot is directed by GPSS, there are few considerations when flying an approach. · GPSS information will not be provided after you pass the MAP. You need to follow the directions published on the approach plate. · When directed to the MAHP, use the Direct-To function. GPSS information will now once again be pr ...

  • Apollo 60 - page 77

    Tuned Station When your Apollo GX is connected to and configured to communicate with an Apollo SL30 Nav/Comm, your Apollo GX will provide information about the VOR or Localizer tuned by the SL30. The Apollo SL30 with SW version 1.2, or later, sends the Tuned Station information once every second. Earlier versions of the SL30 only sends data when th ...

  • Apollo 60 - page 78

    Tuning to a Localizer When the connected SL30 is tuned to a Localizer frequency, the SL30 sends the decoded Localizer identifier to the Apollo GX. The Apollo GX searches its LOC-DME database for an identifier match. If the Localizer is found to be a co-located LOC-DME, the Apollo GX will provide Distance, Speed, and Time information to the SL30 and ...

  • Apollo 60 - page 79

    Moving Map Functions Press the MAP key to reach the Moving Map function and view the progress of your flight on a graphic display. Your present position, nearby waypoints, and special use airspaces display options are user-selectable. Three main pages are available in the Moving Map function: full screen map, split screen with map and Nav info, Sea ...

  • Apollo 60 - page 80

    Controls The LARGE knob moves to different pages of the Map function and selects waypoints when scanning. The SMALL knob changes the map scale. Waypoint Type Keys The smart keys select the display of the waypoint types. The waypoint types selectable from the map view are: Airports, VORs, Intersections, User-defined, and NDBs. Press the smart key to ...

  • Apollo 60 - page 81

    Waypoint Scan Key The Waypoint Scan smart key allows you to select an airport to get information about while viewing the map. 1. Press the SCAN smart key. 2. Turn the LARGE knob to highlight the desired waypoint identifier. 3. Press INFO to get information about the waypoint. Press INFO to return to the map display. You may also press DIRECT-TO and ...

  • Apollo 60 - page 82

    Map Setup The map setup function allows you to select the route line, map orientation, waypoint types that will be displayed, airspace type, and special use airspaces, as well as what airspace alerts will appear when an airspace is penetrated. Route Line A Route Line can be drawn for the legs of the active route when the selection is turned on. A r ...

  • Apollo 60 - page 83

    2. Turn the SMALL knob to choose On or Off. 3. Press ENTER when you made your selection, or turn the LARGE knob to the next item. Map Orient The Map Orient selection allows you to choose how the top of the map display is oriented. North Up - The display is oriented so that vertical lines on the map are aligned with magnetic north. The aircraft symb ...

  • Apollo 60 - page 84

    Map Reference The Map Reference selection allows you to choose either the Destination Waypoint (Dest) or your current position with an airplane icon (Plane) as the center point of the Moving Map display. 1. In the Map function, turn the LARGE knob to reach the Map Setup page. Press SEL . The value will flash. Turn the LARGE knob to choose Map Ref f ...

  • Apollo 60 - page 85

    Note Waypoints that are in an active flight plan will show up on the moving map even if its waypoint type is set as “Off.” 1. In the Map function, turn the LARGE knob to reach the Map Setup page. Turn the SMALL knob to the Identifier & Waypoint Type page. Press SEL to start editing the waypoint types. APT:¿ID INT:+ID VOR:ÂID NDB:ÁID Usr: ...

  • Apollo 60 - page 86

    Track History Your Apollo GX can store a record of its progress in memory that will be shown on the display. The Track History is shown as a series of points on the display following the path of the plane icon. Track history may be recorded by time or by distance at a selected interval. You may also select the Strategy for storing the track history ...

  • Apollo 60 - page 87

    Trk History:Off Save By:Distance Interval:0.5 2. Turn the SMALL knob to select On or Off. 3. Turn the LARGE knob to the Save By option. Turn the SMALL knob to choose Distance or Time. 4. Turn the LARGE knob to the Interval option. Turn the SMALL knob to choose the Interval value. If you chose to Save By Distance, select a distance between 0.1 and 1 ...

  • Apollo 60 - page 88

    Airspace Setup The Airspace Setup selections allows you to turn Airspace notification (Alerts) or map display of Airspaces On or Off, select the distance and time buffers for airspace alerts, turn ATC rings On or Off, and to choose the Airspace types that will be used. Airspace alerts will not be given during an approach. 1. In the Map function, tu ...

  • Apollo 60 - page 89

    Airspace Buffers Three values may be adjusted for Airspace Buffers for determining CLOSE information: distance, elevation, and time. CLOSE distance may be from 0 to 99 nm at one nm intervals. Altitude values are from 0 to 9900 feet in 100 foot intervals. Time values are from 0 to 20 minutes in one minute intervals. From the Map Setup page, turn the ...

  • Apollo 60 - page 90

    ATC Ring Selection When this choice is turned ON ,a5n m radius artificial “ATC Ring” is drawn on the Map display around airports that have a control tower. From the Map Setup page, turn the SMALL knob four clicks cw to reach the ATC Ring selection page. 1. While viewing the ATC Ring page, press SEL to start selection. 5 nm ATC Rings Map : Off 2 ...

  • Apollo 60 - page 91

    The Outer selection refers to the outline of the outside ring extended from the ground on up. Selecting Outer will be useful to VFR pilots who wish to avoid all airspaces. The sector selection refers to the outside edges of the sector from the ground on up unless you have altitude input which then allows for 3-dimensional information. The Sector se ...

  • Apollo 60 - page 92

    Search and Rescue When activated, the Search and Rescue (SAR) feature allows a simplified, automated method of performing search patterns. The search patterns supported include parallel line, creeping line, and expanding square. A line showing the route of the pattern may also be displayed on the screen of your GX. Patterns can be based on two grid ...

  • Apollo 60 - page 93

    Grid Line Display While viewing the Search and Rescue (SAR) map page, you can choose how the grid lines are displayed. Press the GRD smart key to change the Grid line view. Grid line selection options are slightly different for the two grid types, US and Basic. As you zoom out to approximately 40nm the grid lines will be removed. US Grid Type The U ...

  • Apollo 60 - page 94

    Basic Grid Type GRD – No grid lines G R D1–6 0 minute grid lines G R D2–3 0 minute grid lines G R D3–1 5 minute grid lines Search and Rescue Map Setup Page The SAR Map Setup page provides selection of SAR Map (Off/On), Grid Type (US/Basic), and the Position (area of operation). 1. From the Map Setup Page, turn the SMALL knob counterclockwis ...

  • Apollo 60 - page 95

    4. Turn the LARGE knob to Position. Turn the SMALL knob to choose the position information. If you selected the US Grid type, choose the desired sectional name with the SMALL knob or the POS smart key. See the following Sectional Aeronautical Chart Grids table for the location nearest you operation. For the Basic Grid type, select the Position quad ...

  • Apollo 60 - page 96

    Set the SAR Position (Basic Grid Type) 1. If you selected the Basic Grid Type, you need to set the SAR Position. From the SAR Map Setup page turn the SMALL knob clockwise to the SAR Position page. The SAR Position page only appears when the Basic Grid Type is selected. The Position location refers to the LAT/LON of the southeast starting corner for ...

  • Apollo 60 - page 97

    Sectional Aeronautical Chart Grids Chart Ident North Grid Limit South Grid Limit West Grid Limit East Grid Limit Total Grids Grids/ Row Seattle SEA 49 ° 00N 44 ° 30N 125 ° 00W 117 ° 00W 576 32 Great Falls GTF 49 ° 00N 44 ° 30N 117 ° 00W 109 ° 00W 576 32 Billings BIL 49 ° 00N 44 ° 30N 109°00W 101 ° 00W 576 32 Twin Cities MSP 49 ° 00N 44 ...

  • Apollo 60 - page 98

    Selecting A Pattern Three pattern types provide you with the ability to perform a search that best suits your needs. The three types include Parallel Line, Creeping Line, and Expanding Square. 1. While viewing the SAR Map page, press the PAT (Pattern) smart key. 2. Turn the SMALL knob to select the desired pattern type. Press ENTER to choose the pa ...

  • Apollo 60 - page 99

    Parallel Line Search Pattern The Parallel Line search pattern selection allows you to create a search pattern along parallel lines based on an established grid. · Select grid · Set spacing · Set direction · Activate pattern 1. While viewing the SAR Map page, press the PAT smart key. 2. Turn the SMALL knob to select the Parallel Line pattern typ ...

  • Apollo 60 - page 100

    4. Use the LARGE and SMALL knobs to select the desired Grid. 5. Turn the LARGE knob to the Spacing option. Turn the SMALL knob to select the desired pattern spacing. You may select between 0.2 and 9.9 nm. 6. Turn the LARGE knob to the Direction of Travel option. Turn the SMALL knob to select the desired Direction of Travel. You may select N/S or E/ ...

  • Apollo 60 - page 101

    Creeping Line Search Pattern The Creeping Line search pattern is similar to the Parallel Line Search. The starting point is any selected waypoint, rather than a designated grid based on aeronautical sectionals. The creeping line search pattern will straddle the center of your flight path. You may select the following options: · Starting Waypoint ? ...

  • Apollo 60 - page 102

    3. Press SEL . The Starting Waypoint field will flash “INS?” (insert) or “CHG?” (change). Press ENTER to start editing the Starting Waypoint selection. Start: Ins? Spacing :1.0 Direction :000· 4. Choose a waypoint using normal selection methods. Then, press ENTER . 5. The Spacing option will flash. Turn the SMALL knob to select the desired ...

  • Apollo 60 - page 103

    9. Select the Leg Length. Press SEL to start editing the Leg Length. Turn the SMALL knob to choose the Leg Length. You may select between 1.0 and 9.9 nm. Leg Length:5.0 Start:RIGHT Side 10. Turn the LARGE knob to the Start Side selection. Turn the SMALL knob to choose Left or Right. This selection sets the side for the start of the search pattern. ...

  • Apollo 60 - page 104

    Expanding Square Search Pattern The Expanding Square search pattern is similar to the Creeping Line Search. Rather than parallel lines, an expanding square is radiated from the Starting Waypoint according to the spacing between lines and at an angle selected for the Direction of Travel. You may select the following options: · Starting Waypoint · ...

  • Apollo 60 - page 105

    3. Press SEL . The Starting Waypoint field will flash “INS?” (insert) or “CHG?” (change). Press ENTER to start editing the Starting Waypoint selection. Start: Ins? Spacing :5.0 Direction :000 4. Choose a waypoint using normal selection methods. Then, press ENTER . 5. Turn the LARGE knob to the Spacing option. Turn the SMALL knob to select t ...

  • Apollo 60 - page 106

    Mark A Position When viewing the SAR Map page you may save a User waypoint to Mark a location of interest. Pressing the MRK (Marker) smart key saves a User waypoint at the present position of the aircraft when you save the waypoint. 1. While viewing the SAR Map page, press MRK . 2. The User waypoint creation page will appear with the current Lat/Lo ...

  • Apollo 60 - page 107

    Create A User Waypoint By US Grid This feature allows you to set a US Grid coordinate, such as the corner of a grid, as a User waypoint so you can fly Direct-To the starting point in a grid for flying a search pattern. You must have selected the US Grid type on the SAR Setup page to have this display available. 1. Press the DB smart key. Turn the L ...

  • Apollo 60 - page 108

    Fly Direct To A US Grid After creating a User waypoint for a US Grid, you can fly Direct-To, or set a flight plan to, the starting corner of that grid to begin a search pattern. 1. Press DIRECT-TO . Turn the SMALL knob to choose the User waypoint type, if necessary. 2. Use the LARGE and SMALL knobs to select the desired waypoint. 3. Press ENTER . 4 ...

  • Apollo 60 - page 109

    If you want to fly to the Bravo-Charlie 3 corner of the 45°N and 123°W grid, you would define the corner as a USER waypoint with the name “53BC3.” The SAR position is set to 40°N and 120°W. The “5” comes from the 5° added to 40°N. The next number, “3”, comes from the 3° added to 120°W. The first letter, “B”, notes the 30’ ...

  • Apollo 60 - page 110

    3. Press ENTER to save the displayed Grid location as a User waypoint. 53BC3 USER 44°30.00N 122°15.00W Fly Direct To A Basic Grid After creating a User waypoint for a Basic Grid, you can fly Direct-To, or set a flight plan to, the starting corner of that grid to begin a search pattern. 1. Press DIRECT-TO . Turn the SMALL knob to choose the User w ...

  • Apollo 60 - page 111

    Waypoint Database Waypoint Information The Apollo GX provides an extensive built-in database of waypoint information to aid the navigator. Waypoints in the database are divided into 5 categories. This structure allows you to easily select a waypoint as a destination, search for waypoint information, search for nearest waypoints, or insert waypoints ...

  • Apollo 60 - page 112

    · Sunrise/Sunset times · Waypoint comment VOR Waypoint Information · Identifier, name, state, & country · Radial and distance from the VOR · Bearing and distance from present position · Map · Operating frequency · Lat/Lon coordinates · Sunrise/Sunset time · Waypoint comment NDB Waypoint Information · Identifier, name, state, & co ...

  • Apollo 60 - page 113

    · Lat/Lon coordinates · Sunrise/sunset time · Waypoint comment USER Waypoint Information · Name/Identifier (User entered) · Lat/Lon coordinates (User entered) · Runway Length (User entered) · Bearing and distance from present position · Map · Sunrise/sunset time · Waypoint comment Getting Information About A Waypoint You can access the Wa ...

  • Apollo 60 - page 114

    3. Turn the LARGE knob to the first character of the waypoint name. The character will flash. Turn the SMALL knob to select the desired character. AIRPORT PAE EVERETT city WA USA 4. Turn the LARGE knob clockwise one click to move to the next character. Turn the SMALL knob to select the desired character. Continue to select the needed characters. PD ...

  • Apollo 60 - page 115

    7. Press INFO to view information about the selected waypoint. AIRPORT TTD PORTLAND-TROUTDA city dup OR USA 9. Press ENTER or INFO to leave the function. Airport Info Pages The Apollo GX database holds the most needed information about each waypoint. The Airport information is described below. Similar information is available for each waypoint type ...

  • Apollo 60 - page 116

    Bearing & distance from present position Turn the SMALL knob to show the Bearing and Distance from your present position. An arrow shows the Relative Bearing to the waypoint from your present position. ppos to SLE Bearing 341°² Distance 121nm Airport frequencies Turn the SMALL knob to view the available frequencies for the waypoint. In the GX ...

  • Apollo 60 - page 117

    Fuel Availability Turn the SMALL knob to view fuel availability. SLE AIRPORT Available Fuel: Avgas/Jet Map Turn the SMALL knob to view a map of the waypoint and location. If the waypoint is an airport, the runway map will be shown. You can change the map scale by pressing SEL and then turning the SMALL knob. Press SEL again to disable map scaling. ...

  • Apollo 60 - page 118

    Approach Info (GX50/60 only) Turn the SMALL knob to view information about each approach. Lat/Lon Position Turn the SMALL knob to view the Lat/Lon position. SLE AIRPORT lat 44°54.57N lon 123°00.15W Sunrise/Sunset Time Turn the SMALL knob to view the Sunset/Sunrise time for the waypoint in UTC time. You can change the day and month to view alterna ...

  • Apollo 60 - page 119

    Create User Waypoint by Lat/Lon The Apollo GX allows you to create up to 500 of your own waypoints to the waypoint database. You can create a waypoint based on a Lat/Lon or using a radial and distance from another waypoint. The starting Lat/Lon coordinates are your present position You can also add the runway length. Unlike normal database waypoint ...

  • Apollo 60 - page 120

    4. Press ENTER when you have finished entering the waypoint information. HOME USER 44°24.29N Rwlen 122°51.52W 3000’ Create User Waypoint by Radial/Distance A User waypoint may also be created where its position is referenced by a Radial and Distance from another waypoint. 1. Press the DB soft key. Turn the LARGE knob to view the “Create User ...

  • Apollo 60 - page 121

    SMALL knobs to choose the identifier. After the reference waypoint name is chosen, press ENTER . Ref Wpt: SLE 0 00.0° 000.0nm 5. The first character of the radial will flash. Now select the needed characters for the Radial and Distance. Turn the SMALL knob to change characters. Turn the LARGE knob to move to the next character. Ref Wpt: SLE 040.0? ...

  • Apollo 60 - page 122

    Update User Wpt with Present Pos Update the Lat/Lon coordinates of an existing User waypoint to your present position. You may also change the name and other info for the waypoint. 1. Press the DB key. 2. Turn the LARGE knob to view the “Update User Waypoint” page. Press ENTER . Update User Wpt with PPos Press ENT 3. The waypoint identifier wil ...

  • Apollo 60 - page 123

    3. Press ENTER . The waypoint identifier will flash. Turn the SMALL knob to view the User waypoints. Find Wpt to Del CABIN user Press ENT 4. When the waypoint to delete is displayed, press ENTER . Modify User Waypoint 1. Press the DB key. Turn the LARGE knob to view the “Modify User Wpt” page, and then press ENTER . Modify User Wpt Press ENT 2. ...

  • Apollo 60 - page 124

    5. Turn the SMALL knob to select the desired character. Continue using the SMALL knob to change characters and the LARGE knob to move to the desired character. After the correct characters are chosen, press ENTER . Creating Waypoint Comments You may add comments to up to 200 waypoints. The comments are added while viewing the Info for any waypoint. ...

  • Apollo 60 - page 125

    Deleting Waypoint Comments You may delete any of the waypoint comments that you have created. 1. Press DB and then turn the LARGE knob to the “Delete Waypoint Comment” page. Delete Waypoint Comment: 5 used Press ENT 2. Press ENTER to view the waypoint comments. The first waypoint comment page will show the waypoint identifier, waypoint type, an ...

  • Apollo 60 - page 126

    Update User Waypoint The Update User Waypoint function allows you to change the position of an existing User waypoint to your present position. 1. In the Database function, turn the LARGE knob to “Update User Wpt With Ppos.” Then, press ENTER . Update Usert Wpt With Ppos Press ENTER 2. A list of the User waypoints is available. The User waypoin ...

  • Apollo 60 - page 127

    Flight Plan Functions Flight plans are specific routes between waypoints you may store in the Apollo GX memory. This information is used to calculate useful flight statistics. The Flight Plan function allows you to have up to 30 stored flight plans. Each flight plan may have up to 20 legs. The Active flight plan is always used for the current fligh ...

  • Apollo 60 - page 128

    Flight Plan pages. The active leg is the default page you will see when pressing FPL once. *Active* 259nm Dest Wpt: PDT Active · 2. Turn the SMALL knob to view the individual legs of a flight plan. Two asterisks indicate the active leg. EUG to SLE 1** 353° 48.0nm arpt arpt Active Flight Plan The first plan in the Flight Plan function is the Activ ...

  • Apollo 60 - page 129

    1. Press the FPL key. Turn the LARGE knob to view the “Create a New Flightplan” page. Press SEL to Create a New Flight Plan 2. Press SEL . The first character will flash. Turn the SMALL knob to select the first flight plan name character. R_______ Enter a New Plan Name 3. Turn the LARGE knob clockwise one click to move to the next character pos ...

  • Apollo 60 - page 130

    7. Press SEL to insert a FROM waypoint. The Ins? prompt will flash. Press ENTER to insert a FROM waypoint. Ins? to ______ 1 ___° __._nm ____ ____ 8. Turn the SMALL knob to select the waypoint type. Turn the LARGE knob to the waypoint identifier. Turn the SMALL knob to select the first character of the waypoint identifier. AIRPORT EAA EAGLE city AK ...

  • Apollo 60 - page 131

    11. Repeat steps 7-10 for the remaining waypoints in your flight plan. SLE to Ins? 2 ___° __._nm ____ ____ 12. Press SEL when your flight plan is complete. Turn the SMALL knob to view the legs in your flight plan. Press SEL while viewing a flight plan leg page to make changes. Press SEL and then turn the SMALL knob while viewing the flight plan na ...

  • Apollo 60 - page 132

    Flight Plan Leg Information Two types of information are available within flight plan legs: waypoint and flight information. Pressing INFO will provide information about the destination waypoint. Information about the ETA, ETE, Ground Speed, and Fuel is also available for each leg by selecting which option you like to view in the leg display. 1. Wh ...

  • Apollo 60 - page 133

    ETA Estimated Time of Arrival is for the displayed TO waypoint and requires an actual ground speed of more than 5 knots. If there is no valid ETA for the leg, dashes will replace the value. EUG to SLE 1 353° 48.0nm ETA 17:36 ETA? ETA? is the same as ETA, except the Estimated Ground Speed is used for the calculation. EUG to SLE 1 353° 48.0nm ETA? ...

  • Apollo 60 - page 134

    no valid ETE for the leg, dashes will replace the value. EUG to SLE 1 353° 48.0nm ETE 00:27 ETE? ETE? is the same as ETE, except the Estimated Ground Speed is used for the calculation. See Estimated Ground Speed on page 16 for more details. EUG to SLE 1 353° 48.0nm Leg ETE? 00:24 Fuel To? Fuel shows the amount of fuel required to get from the FRO ...

  • Apollo 60 - page 135

    Direct-To If the leg page displayed is the currently active leg of the Active flight plan, and a Direct-To waypoint has been entered, the From waypoint will say “Direct.” The leg just prior to the currently active leg displays the leg as if the “Direct” waypoint did not exist. After sequencing, the “Direct” disappears, and the currently ...

  • Apollo 60 - page 136

    Flight Plan Editing You can alter any of the information you entered into the flight plans. The editing options include: Chg?, Ins?, and Del? · Chg? - An existing waypoint can be changed if at least one valid waypoint exists in the database. · Ins? - A waypoint can be inserted before an existing waypoint if at least one valid waypoint exists in t ...

  • Apollo 60 - page 137

    Changing Existing Flight Plan Legs 1. In the Flight Plan function, turn the LARGE knob to a flight plan and then use the SMALL knob to display the leg of the plan that you want to edit. HIO to TTD 3 070° 23.0nm arpt arpt 2. Press SEL . The FROM waypoint will flash with the Chg? prompt. Turn the LARGE knob to the desired waypoint. HIO to Chg? 3 070 ...

  • Apollo 60 - page 138

    2. Press SEL . The From waypoint will flash with the Ins? prompt. Turn the LARGE knob, if necessary, to the waypoint you want changed. HIO to Chg? 3 067° 75.0nm arpt arpt 3. If another option was last used, turn the SMALL knob to choose Ins?. HIO to Ins? 3 067° 75.0nm arpt arpt 4. Press ENTER . Use the LARGE and SMALL knobs to select the desired ...

  • Apollo 60 - page 139

    2. Press SEL . The From waypoint will flash with the Chg? prompt. Turn the LARGE knob to the waypoint you want changed. HIO to Chg? 3 070° 23.0nm arpt arpt 3. Turn the SMALL knob to choose Del?. HIO to Del? 3 070° 23.0nm arpt arpt 4. Press ENTER . The waypoint will be deleted. Each flight plan leg will shift back to replace the deleted leg, i.e. ...

  • Apollo 60 - page 140

    Flight Plan Options In the Flight Plan function you may make changes to a flight plan. 1. In the Flight Plan function turn the LARGE knob to a flight plan name page. 2. Press SEL and then turn the SMALL knob to view the available functions. 3. Press ENTER to activate the option. Activate Pressing ENTER when the “Activate” option is displayed co ...

  • Apollo 60 - page 141

    Rev Activate Pressing ENTER when the “Rev Activate” option is displayed copies the selected flight plan to the active plan in reverse waypoint order and starts it at leg 1. Route 2 259nm Dest: Wpt: PDT Rev Activate? Reactivate Press ENTER when the “Reactivate” option is displayed to reset the active leg to leg 1 and allow waypoint sequencin ...

  • Apollo 60 - page 142

    Copy Plan Pressing ENTER when the “Copy Plan” option is displayed allows you to copy any existing plan into the current plan, overwriting all of the current plan’s waypoints. You may choose the active or any inactive flight plan. 1. While viewing the desired flight plan, press SEL and then turn the SMALL knob to the “Copy Plan?” option. P ...

  • Apollo 60 - page 143

    Clear Waypoints Pressing ENTER will delete all waypoints in the selected flight plan. The plan name will remain. Route 2 259nm Dest: Wpt: PDT Clear Wpts? Reverse Flight Plan Pressing ENTER when the “Reverse” option is displayed reverses all the waypoints in the current flight plan. This option is available only on inactive flight plans with two ...

  • Apollo 60 - page 144

    plan or “Fuel To Uses Est Gr Speed” when the current flight plan is an inactive, stored flight plan. Delete Plan Pressing ENTER when the “Delete Plan” option is displayed deletes the current flight plan. The display returns to the previous flight plan’s name (or first) page. The *Active* flight plan cannot be deleted, in which case this o ...

  • Apollo 60 - page 145

    3. Press ENTER to place the active flight plan on hold. Waypoint sequencing will be inhibited on the current leg. Pressing OBS/HLD will also work. *Active* 259nm Dest: Wpt: PDT Holding Holding Patterns (GX50/60) A holding pattern is operationally the same as a procedure turn except that you usually intend to make repeated crossings of the waypoint ...

  • Apollo 60 - page 146

    selected inbound course and through the waypoint. The CDI will indicate “fly-left” if the aircraft is to the right of the desired track with reference to the selected inbound course. The CDI will indicate “fly-right” if the aircraft is to the left of the desired track with reference to the selected inbound course. As with traditional VOR na ...

  • Apollo 60 - page 147

    with 020° inbound selected as the “OBS” course to UBG. Continue The Continue option is available for the Active flight plan when the flight plan status is Holding (waypoint sequencing is not allowed). Pressing ENTER when this option is displayed restarts the Active flight plan and enables waypoint sequencing. 1. In the Flight Plan function, tu ...

  • Apollo 60 - page 148

    3. Press ENTER to continue the active flight plan. Waypoint sequencing will be enabled. *Active* 259nm Dest: Wpt: PDT Active · Load Approach (GX50/60 Only) This option is available for the Active flight plan when a datacard with approach information is inserted into the GX50/60. Press ENTER to show the available approaches for the destination airp ...

  • Apollo 60 - page 149

    Enable Approach (GX50/60 Only) This option is available on the Flight Plan home page when an approach is already loaded, but not enabled, and you are within approximately 30 nm of the destination airport. Press ENTER to enable the approach. *Active* 56.1nm Dest Wpt: PDX Enable Approach? Disable Approach (GX50/60 Only) This option is available on th ...

  • Apollo 60 - page 150

    1. While viewing the desired flight plan, press INFO . Turn the SMALL knob to reach the Comment page. Waypoint Comment Press SEL 3. Press SEL . Turn the SMALL knob to select the first character. _ 4. Turn the LARGE knob clockwise one click to move to the next character position. Turn the SMALL knob to select the next comment character. GOOD RESTAUR ...

  • Apollo 60 - page 151

    2. Press SEL and then use the LARGE and SMALL knobs to enter a new plan name. After entering the name, press ENTER . PLAN 9__ Enter a New Plan Name 3. Press ENTER a second time or turn the SMALL knob twice to return to the Inactive Flight Plan name page. Don’t insert any waypoints. PLAN 9 0.0nm Dest wpt: —— Inactive · 4. Press SEL and turn t ...

  • Apollo 60 - page 152

    An old navigation method 1. While holding your watch horizontal, point the hour hand at the sun. 2. Halfway between the hour hand and 12:00 is south. Don’t always depend on this method, but it is kind of fun. 6-26 Flight Plan Functions ...

  • Apollo 60 - page 153

    System Functions Pressing the SYS key allows you to access the System functions. After pressing the SYS key, turn the LARGE knob to view the available functions: Navigation Info, System Info, Position Sensors, Misc Sensors, and Comm Info (GX60/65 only). Press ENTER when viewing the desired System function. Navigation Information The Navigation Info ...

  • Apollo 60 - page 154

    1. While viewing the Autonav Time page, press SEL . Autonav Time: 4 Seconds/Page 2. Turn the SMALL knob to select the delay time. Autonav Time: 7 Seconds/Page 3. Press ENTER when finished. 4. Press NAV . While viewing the Nav functions, Press ENTER to start Autonav scrolling. Press ENTER again to stop Autonav scrolling. Navigation Mode Programmable ...

  • Apollo 60 - page 155

    4. Press SEL to activate editing. The first Nav field will flash. ete SLE 00:20 2.00 “¼¼ Dtk 353 48.0nm 5. Turn the SMALL knob to select the desired Nav information to be displayed in that field. GroundSp 100 kts 2.00 “¼¼ Dtk 353 48.0nm 6. Turn the LARGE knob to move to the next field to edit. Turn the SMALL knob to select the Nav informati ...

  • Apollo 60 - page 156

    Selecting Autonav Pages 1. While you are viewing a Nav page information page, press SEL and then ENTER . See page 5 for a listing of Nav Page choices. 2. You will be prompted to decide if you want to include this page in the Autonav scrolling. Turn the SMALL knob to choose between Yes and No. Nav Page 4 in Autonav Pages? Yes 3. Press ENTER . Restor ...

  • Apollo 60 - page 157

    Nav Page Choices The following displays are available when customizing your Nav displays. Page references are shown in parentheses. Ete aUAO 02:27 Estimated Time En Route to TO 4wpt () Eta aUAO 00:02 Estimated Time of Arrival to TO wpt (9) Eta aCVO 00:22 Estimated Time of Arrival to last wpt in plan Ft00:04 Elapsed Flight Time (9) Trk 318 357 Track ...

  • Apollo 60 - page 158

    Setting Units of Measurement Nav displays that show distance may be selected to show either nautical miles, statute miles, or kilometers. 1. In the Navigation section of the System function, turn the LARGE knob to the Nav Mode Display Pages. Nav Mode Display Programmable and Autonav Pages · 2. Turn the SMALL knob to reach a programmable Nav page. ...

  • Apollo 60 - page 159

    Magnetic Variation Automatic or Manual Magnetic Variation can be set in this page. Automatic is the default setting on power-up, unless the database is invalid. Manually set Magnetic Variation to 0° to orient your navigation to True North. 1. In the Navigation section of the System function, turn the LARGE knob to the Magnetic Variation page and t ...

  • Apollo 60 - page 160

    Flight Timer Trigger The following procedure is used to edit the flight timer trigger speed. The flight timer may be set to start at power-up, or when the ground speed exceeds from 10 to 500 knots. The default (factory) setting is 60 knots. The feature may also be turned off. 1. In the Navigation section of the System function, turn the LARGE knob ...

  • Apollo 60 - page 161

    With the May Clear Direct-To Entry Option, the Direct-To waypoint will be inserted in the Active flight plan, and all of the other waypoints will be deleted from the Active flight plan, including approaches. With the Never Clears Direct-To option, the Direct-To waypoint is inserted before the current TO waypoint. This is the normal, default setting ...

  • Apollo 60 - page 162

    CDI Scaling The CDI Scaling option allows you to select manual or automatic full scale deflection of the internal CDI. Manual full scale deflection options include: 0.30 nm, 1.00 nm, and 5.00 nm. Automatic scaling will use 5.00 nm as the setting. In an enabled approach operation (GX50/60), scaling is locked in automatic and will change to the appro ...

  • Apollo 60 - page 163

    System Information The System Information area provides the following pages: Software and Database Version, Display test, Owner Info, and Date and Time, . Date and Time 1. Press the SYS key. Turn the LARGE knob to reach the System Information function and press ENTER . Turn the LARGE knob to the Date and Time page. System Info Press ENTER 2. This i ...

  • Apollo 60 - page 164

    5. Turn the LARGE knob to move to the Month value. Turn the SMALL knob to choose the month. Date: 24 APR 97 Time: 23:24 UTC SEL to Reset 6. Turn the LARGE knob to move to the Year value. Turn the SMALL knob to choose the year. Date: 24 APR 97 Time: 23:24 UTC SEL to Reset 7. Turn the LARGE knob to move to the Time-Hours value. Turn the SMALL knob to ...

  • Apollo 60 - page 165

    2. Turn the SMALL knob cw one click to view the Database Version page. Americas DB Expires mm/dd/yy Version: x.xx 3. Turn the SMALL knob cw one click to view the GPS Software Version page. GPS Sensor SW Version x.x PN:123456789 Fuel Measure Units (GX50/60 Only) The GX50/60 allows you to choose the units of measure for your fuel displays. Fuel units ...

  • Apollo 60 - page 166

    Barometric Measure Units (GX50/60 Only) This function allows you to choose the units of measure for the Local Altimeter Settings. The choices are inches (“) or millibars (MB). 1. In the System Information section of the System function, turn the LARGE knob to reach the Baro Measure page. Baro Measure usg US Gallons 2. Press SEL to enable selectio ...

  • Apollo 60 - page 167

    2. Turn the SMALL knob to choose Default, High, or Low. Press ENTER to store the desired choice. Your choice is kept until you change it. Viewing Owner Information The Owner Information function allows the user to enter their Name, Address, City, Phone, and Aircraft. As a security feature, the user must enter a password to enable editing of the Own ...

  • Apollo 60 - page 168

    Editing Owner Information It is necessary to enter a password before editing owner information. Editing is then enabled until the unit is turned off. 1. Start editing by pressing SEL . User Must First Enter Password.. 2. The password entry page is then ready. Select the characters with the SMALL knob and move to the next character to the right by t ...

  • Apollo 60 - page 169

    5. Turn the SMALL knob to go to the next Owner Information page you want to edit. Press SEL to start editing. Select the characters with the SMALL knob and move to the next character to the right by turning the LARGE knob cw. Press ENTER to save the information. GPS Sensor The GPS Sensor selection provides information about GPS satellite health, th ...

  • Apollo 60 - page 170

    3. Turn the SMALL knob to view the GPS Satellites Used for Position fixes page. SV means space vehicle, which is the same as a GPS satellite in this case. GPS SVs for Fix 28, 31, 27, 26, 19, 07, 02, 18 4. Turn the SMALL knob again to view the GPS Satellite Status, Elevation, SNR, and Azimuth page. Continue turning the SMALL knob to view information ...

  • Apollo 60 - page 171

    GPS Date and Time Page In the GPS Sensor Information function, turn the SMALL knob to view the GPS Date and Time page. This page is not shown when using the Simulator. GPS Time (UTC) May 24, 1997 17:54:27 GPS Normal Reset Page Resetting the GPS receiver resends current time, date, and position to the GPS receiver. This forces a new search of the sa ...

  • Apollo 60 - page 172

    Miscellaneou s Sensors The Miscellaneous Sensor section of the System function displays information concerning the Fuel/Air Data Sensor (F/ADS), fuel sensor, and altitude encoder when they are installed. The F/ADS includes a fuel sensor and altitude encoder. The F/ADS monitors fuel flow, air speed, outside air temperature/pressure, and magnetic hea ...

  • Apollo 60 - page 173

    Air Data Info If the Air Data Sensor is installed, the following information is available. Air Speed True Airspeed - speed of the aircraft relative to the surrounding air speed. Indicated Air Speed - Speed of the aircraft as shown on the airspeed indicator. Air data Info TruAirSp 163kts IndAirSp 149kts· Air Temperature True Air Temperature - Tempe ...

  • Apollo 60 - page 174

    Wind Direction and Speed True Wind Direction, Magnetic Wind Direction, and the outside Wind Speed are displayed. Wind Dir 000°Tru Wind Dir 342°Mag Wind Spd 15kts Fuel Info An installed Fuel Data Sensor will provide the following information. Fuel Endurance · Estimated fuel Endurance based on the current amount of fuel in the regular (nonreserve) ...

  • Apollo 60 - page 175

    Right Engine Fuel · Burn rate for the right engine in fuel units per hour · Amount of fuel used by the right engine since power up Right Engine Burn 17.7usg/hr Used 11usg Left Engine Fuel · Burn rate for the leftt engine in fuel units per hour · Amount of fuel used by the left engine since power up Left Engine Burn 16.8usg/hr Used 10usg Total F ...

  • Apollo 60 - page 176

    Fuel Measure The GX50/60 allows you to choose the units of measure for your fuel displays. Fuel units may be displayed as US Gallons (USG), Imperial Gallons (IMG), Liters (L), Pounds (LBS), or Kilos (KGS). Fuel Measure usg US Gallons Press SEL to enable selection. Turn the SMALL knob to choose the desired units and then press ENTER . 7-24 System Fu ...

  • Apollo 60 - page 177

    Message Function Message function is responsible for warning the user of changing conditions which require immediate attention. Press the MSG smart key to view the message. Press the MSG key again to return to the previous function. However, if a new message occurs, pressing MSG will not return to the previous function until all new messages have b ...

  • Apollo 60 - page 178

    While any old message exists, the MSG annunciator remains steadily on at all times unless new messages arrive or all old message conditions go away. The home page in message mode is the first new message, if one exists, or the New Message Summary page if no new messages exist. New Messages The New Message page shows how many new messages are stored ...

  • Apollo 60 - page 179

    Messages The following is a summary of the conditions that cause a message warning, and examples of the messages generated for each condition. Special Use Airspace Messages Following is a list of the types of airspace messages which can be generated. All of the airspace messages become old messages after they are viewed. The Airspace Messages are u ...

  • Apollo 60 - page 180

    CLOSE Altitude This condition occurs when the airspace boundary is within 500 feet, or a user-selected limit in the System function. Within 500’ of NORTON AFB Class C INSIDE This condition occurs when the plane penetrates the airspace. Inside of SAN DIEGO Class B Empty TO Waypoint: Cannot Compute Nav Anytime the current To waypoint is empty, this ...

  • Apollo 60 - page 181

    GPS Sensor Lat/Lon Failure When the GPS sensor cannot compute the latitude and longitude, the following message displays. It becomes an old message after viewing. GPS Position Sensor Cannot Compute Lat/Lon GPS RAIM Not Available When RAIM detection is not available for the GPS sensor, a warning is generated. The current flight phase is displayed fi ...

  • Apollo 60 - page 182

    GPS Communications Failure GPS HDOP Position Error When the HDOP for the GPS sensor exceeds current flight phase HDOP requirements, a warning is generated and Nav data will be flagged as invalid. The current flight phase is displayed first (either Terminal or En route). Approach warnings are for the GX50/60 only. Messages become an old message afte ...

  • Apollo 60 - page 183

    Set Barometer (GX50/60 Only) When an approach is enabled, you are prompted to enter the local altimeter setting. Enter Local Altimeter Setting 29.92in No Valid Altitude Input for Approach (GX50/60 Only) An approach is not valid unless an altitude value is available. Abort Approach No Valid Altitude Input Approach RAIM Unavailable (GX50/60 Only) An ...

  • Apollo 60 - page 184

    Altitude Range Error When the altitude encoder reports an altitude that is out of range, the following message is created. Altitude Out of Range Altitude Encoder Communications Failure This message appears when communications fail between the Apollo GX and the altitude encoder. Altitude Encoder Communications Failure Fuel/Air Data Sensor Communicat ...

  • Apollo 60 - page 185

    Outside Hold Altitude Buffer You have gone above or below the selected Hold Altitude Buffer. Altitude Alert 500ft Above Hold Altitude Start Auto Descent Begin Descent To NOONS 500ft/min 130kts Arrival At Auto Descent Altitude Arrival At 2000ft Target Descent Altitude Arrival At The TO Waypoint The arrival message is generated when you are within 36 ...

  • Apollo 60 - page 186

    Apollo GX with F/ADS Wind Info Arrival: SLE Next DTK 321° Desired Hdg 324° In addition to the arrival waypoint identifier, the next leg’s desired track is shown when available; otherwise, it is dashed. If wind factors (from the Fuel/Air Data Sensor) and a next waypoint are available, the desired heading is also shown on line three; otherwise, l ...

  • Apollo 60 - page 187

    Holding at the TO Waypoint This form of the Arrival Alert is provided when holding at the current TO waypoint. Arrival: SLE - Holding - Next Leg is DME Arc This type of Arrival Alert is provided when the next TO waypoint is the end of a DME Arc holding at the current TO waypoint. Press ENTER to transition directly to the NAV mode DME Arc Assist pag ...

  • Apollo 60 - page 188

    DME Arc Sequence (GX50/60 Only) This form of Sequence Alert is provided when the next TO waypoint is the end of a DME Arc in a nonprecision approach. Press ENTER to transition directly to the NAV mode DME Arc Assist page. Sequence Alert DME Next-Use ARC Assist? Enter Auto OBS Crossing Holding Waypoint When a waypoint on hold is crossed to the From ...

  • Apollo 60 - page 189

    User Memory Failure This message indicates that one or more user settings were not within valid limits at power-up and needed to be reset. This message is cleared after the message is viewed. Memory Failure User Setups Have Been Reset Database Expired This message indicates that the datacard expiration date is before the current UTC date. This mess ...

  • Apollo 60 - page 190

    Low Internal Battery Voltage This message is generated when low internal battery voltage is detected. It becomes an old message after being viewed. Battery voltage is checked every 15 seconds. This battery backs up the memory for information added by the user, such as user waypoints and stored flight plans. Low Battery Voltage: Unit Needs Service H ...

  • Apollo 60 - page 191

    Approach Basics (GX50/60) The Apollo GX50/60 may be used to navigate GPS non-precision approaches. These consist of overlay approaches, GPS approaches which overlay an existing non-precision approach procedure such as a VOR, an RNAV, or an NDB approach, and GPS-only approaches. GPS approaches may overlay any type of non-precision approach procedure ...

  • Apollo 60 - page 192

    Approach Transition Approach Transition operations occur after you enable approach operation. The APPRCH annunciator will turn on. The CDI sensitivity will gradually scale from 5.0 to 1.0 nm full scale per side automatically. The IAF is usually in the Approach Transition operation area. The ACTIVE annunciator will start flashing when you are within ...

  • Apollo 60 - page 193

    CAUTION The Apollo GX and the U.S. GPS Satellites use the World Geodetic System 1984 (WGS-84) horizontal datum for latitudes and longitudes. Approach plate or approach procedure data must be referenced to the WGS-84 or North American Datum 1983 (NAD-83) in order to use the approach. NAD-83 is for all practical purposes identical to the WGS-84 datum ...

  • Apollo 60 - page 194

    9-4 Approach Basics (GX50/60) ...

  • Apollo 60 - page 195

    Approach Procedure There are three general types of Apollo GX operation: · En Route ü Load Destination Waypoint ü Load Approach Information · Approach Transition (or Approach Enabled) ü Enable approach (Method 1 or 2) ü 30 nm from Destination Airport ü Initial Approach Fix ü Final Approach Fix · Approach Active ü Crossing the Final Approa ...

  • Apollo 60 - page 196

    Load a Destination Airport The destination must be an airport. 1. Load your flight plan. You may activate or edit an existing flight plan. Press the FPL key to reach FLIGHT PLAN mode. If the desired flight plan is active, go to the next section “Load Approach Information.” 2. If the desired flight plan is not displayed, turn the LARGE , outer k ...

  • Apollo 60 - page 197

    Load Approach Information 1. When a flight plan is active, press SEL while in the Nav function or the Moving Map to go directly to this display. In the Flight Plan function with the active flight plan displayed, press SEL to reach the “Load Approach?” selection. *Active* 44.2nm Dest Wpt: PDX Load Approach? 2. Press ENTER . The approach name is ...

  • Apollo 60 - page 198

    Approach Transition Operation (Enabling Approach) Approach Transition Operation begins when you enable an approach that has already been selected from the database and loaded into the active flight plan. The Approach annunciator will be on (and the Approach Active annunciator will be off) to indicate that your Apollo GX is operating in Approach Tra ...

  • Apollo 60 - page 199

    the FAF if the approach has not yet been enabled. You will then get a message to enter the local altimeter setting. Enable Approach - Method 2 When an approach has been loaded, the aircraft is less than 30 nm from the destination airport, and the approach has not yet been enabled, pressing FPL will result in the “Enable Approach?” prompt. If yo ...

  • Apollo 60 - page 200

    Initial Approach Fix (IAF) 1. Prior to the Initial Approach Fix (IAF), the MSG indicator will light to announce a Waypoint Arrival Alert. Press MSG to acknowledge the message and view the instructions to the next approach point. 2. Press MSG to return to the previous function. 3. Prior to reaching the IAF, determine if a procedure turn or a course ...

  • Apollo 60 - page 201

    Approach Active Operation Approach Active Operation begins when you cross the Final Approach Fix (FAF) inbound if an approach has been loaded and enabled, the FAF is the active waypoint, and there are no system-detected reasons not to continue the approach (see Message Mode starting on page 1 ). The Approach Active annunciator is illuminated for Ap ...

  • Apollo 60 - page 202

    Canceling the Approach will result in returning to Approach Transition operation. The Approach Active light will go out and the CDI will smoothly scale back to 1.0 nm sensitivity. Once Approach Active has been canceled by the pilot, it cannot be made active again except by again crossing the FAF inbound. Note Verify that the Approach Active annunci ...

  • Apollo 60 - page 203

    2. The OBS/HLD annunciator will remain lighted solid. CDI resolution is maintained at 0.3 nm. The To/From flag will switch from “TO” to “FROM” as you cross the MAP. 3. If desired, and conditions allow, land the aircraft. 4. If you do not choose to land, cancel the approach by pressing the OBS/HLD button. Follow the published missed approach ...

  • Apollo 60 - page 204

    approach. You will now return to Approach Transition mode. The Approach Active light will go out and the CDI will gradually go back to Approach Transition CDI sensitivity (from 0.3 nm to 1.0 nm full-scale). As soon as you enable sequencing, the Apollo GX will sequence to the next waypoint in the flight plan. This is the next waypoint in the publish ...

  • Apollo 60 - page 205

    OBS DTK: 151° to ROARK iaf man brg 356 dtk 356 6. If you do not wish to hold or execute a procedure turn at the next waypoint, press OBS/HLD to enable sequencing at the active waypoint. You may also want to manually select a flight plan leg to intercept. In this case, press FPL , turn the SMALL knob to the desired leg and press ENTER . Press ENTER ...

  • Apollo 60 - page 206

    leg or waypoint and navigate to try the approach again. Your flight plan remains unchanged. Note After an active approach has been canceled, you cannot immediately reactivate it. The approach can only be reactivated by crossing the FAF inbound, when the FAF is the active waypoint. Repeating an Approach You must cross the FAF inbound with the FAF se ...

  • Apollo 60 - page 207

    OBS DTK 159° UBG iaf auto brg 159 dtk 159 Note If you wish to intercept an approach leg, manually activate that leg. This is useful when receiving radar vectors back to intercept an approach leg. See “Manually Selecting a Flight Plan Leg” on page 19. Selecting a Different Approach After a missed approach, you may want to select one of the othe ...

  • Apollo 60 - page 208

    Direct-To The Direct-To function is used for several purposes. Especially during approach operations, you should be very comfortable with how this feature works. Review the Direct-To section on page 31 if you need a refresher before proceeding with approaches. If you select a waypoint that is not one of the waypoints already in the active flight pl ...

  • Apollo 60 - page 209

    suspends leg-sequencing at that waypoint and lights the OBS/HLD annunciator. Subsequent pressing of DIRECT-TO toggles between the waypoint selection and OBS DTK choices. Manually Selecting a Flight plan Leg Approach operations often result in the need to manually select a leg of the active flight plan. Manual leg selection will often be required wh ...

  • Apollo 60 - page 210

    Flight Plan Waypoint Sequencing A flight plan will sequence to the next leg of the flight plan as the aircraft crosses to the bisector that runs through the “TO” waypoint. The bisector is defined as the angle that is half of the angle between the current leg and the next leg. When the unit is on Hold, or there is no next leg, the bisector is pe ...

  • Apollo 60 - page 211

    Procedure Turns A procedure turn is a way of crossing the same waypoint more than once in order to accomplish a course reversal. First, make sure that flight plan leg sequencing is suspended. Second, after crossing the waypoint, set the correct inbound course to intercept. Finally, enable sequencing when you are established inbound. Suspend Sequenc ...

  • Apollo 60 - page 212

    2. Set the desired inbound course with the LARGE and SMALL knobs. Then, press ENTER . OBS DTK: 000° to BTG ifaf auto brg 000 dtk 000 3. Verify that waypoint sequencing is set to “auto.” 4. Fly the procedure-turn or course reversal and intercept the selected inbound course. Note While flying outbound, the CDI is reverse sensing. Many pilots are ...

  • Apollo 60 - page 213

    are less than 2 nm from the FAF when you enable sequencing, then transition to Approach Active, i.e., the CDI sensitivity will begin changing to 0.3 nm full-scale deflection immediately. The approach annunciator will begin flashing immediately if all the conditions exist to allow the approach to go to the active condition (RAIM available, etc.). It ...

  • Apollo 60 - page 214

    Holding Patterns A holding pattern is operationally the same as a procedure turn except that you usually intend to make repeated crossings of the waypoint on a specific inbound course. Like the procedure turn, the steps will always be: · First, suspend sequencing · Second, set the inbound course. · Third, enable sequencing. 1. Verify that sequen ...

  • Apollo 60 - page 215

    4. Finally, when you are ready to exit the holding pattern, press OBS/HLD . Caution While flying outbound, your CDI will provide reverse sensing. Holding at the FAF Holding at the FAF is different from other holding patterns. You must be inbound and have sequencing enabled to allow proper transition to Approach Active at the FAF. This example shows ...

  • Apollo 60 - page 216

    DME Arcs (Arc Assist) DME-Arcs are usually used as a method for pilots to intercept a flight plan leg, or a course to a fix. They are sometimes used as a method for reaching a subsequent fix such as a missed approach holding waypoint. The Apollo GX automates your DME-Arc procedure. As you near the start of the DME-Arc rather than a typical arrival ...

  • Apollo 60 - page 217

    Note The desired track shown on an Arc Assist page is relative to the arc, not to the flight plan legs. The DME-Arc is always perpendicular to the present radial and it shows the desired track at the current radial if the aircraft was on the arc. It is the desired no-wind heading if established on the arc. If your distance from the reference waypoi ...

  • Apollo 60 - page 218

    3. The Course Intercept alert will appear as you become established inbound on the final approach course. Course Intercept Next Dtk 312° Navigating to a DME The Apollo GX may be used to help guide you to near the start of an ILS approach by using the location of a DME as a destination waypoint. The waypoint type is labeled “LOC-DME,” which sta ...

  • Apollo 60 - page 219

    RAIM RAIM stands for Receiver Autonomous Integrity Monitor. It is a way a GPS receiver can verify when the signals it is receiving from one or more of the satellites are useable. It does this by using more satellites than are required for a position solution. In essence, the receiver compares the pseudo-ranges, or calculated distance measurements, ...

  • Apollo 60 - page 220

    to predict whether RAIM will be available at the estimated time of arrival at the destination. Your Apollo GX provides you with a RAIM prediction page. This page allows you to determine if RAIM should be available at any location and time. If it says RAIM will be available, it actually means that it will be available at your predicted time of arriv ...

  • Apollo 60 - page 221

    En Route RAIM, or a 2.0 nm alarm limit is provided at all other times. Note that the three different equipment operation states: En route, Approach-Transition, and Approach-Active are somewhat but not directly related to the three RAIM alarm limits of En route, Terminal, and Approach. The equipment states are defined by the CDI sensitivity and oper ...

  • Apollo 60 - page 222

    navigation as long as you verify the accuracy of your position by other means at least every 15 minutes until RAIM becomes available again. This can be accomplished by cross-checking your GPS position against that of other navigation instruments. Even during times of no RAIM, if your Apollo GPS determines that it cannot provide an accurate position ...

  • Apollo 60 - page 223

    directly from that satellite’s transmissions. An integrity monitor, such as RAIM when it is available, protects you from false or misleading navigation displays resulting from bad satellite information. RAIM Nav Page (GX50/60 Only) The Apollo GX50/60 allows you to manage your RAIM prediction process, besides allowing for automatic prediction. You ...

  • Apollo 60 - page 224

    4. Press SEL . The “Predict RAIM?” choice will flash. Press ENTER to perform manual RAIM prediction now. The top line will display the result of the calculation of whether RAIM is available or not available. Excluding Satellites The Apollo GX50/60 allows you to specify satellite outages for RAIM predictions using information from NOTAMs or NANU ...

  • Apollo 60 - page 225

    Clearing the Exclusion List You can also easily clear the Exclusion List. 1. While viewing the RAIM home page, press SEL . The “Predict RAIM?” choice will flash. Turn the SMALL knob to the “CLR Ignore List?” option. Clr Ignore List? at: SLE arpt 10Nov97 22:06 · 2. Press ENTER to clear all satellite exclusions. Emergency (Alternate) Approac ...

  • Apollo 60 - page 226

    Fly Direct-To a Nearest Airport 1. Press the NRST key. Turn the SMALL knob to choose the nearest desired airport. Near 1 to PPos CVO AIRPORT Brg 154°± 5.4nm 2. Press DIRECT-TO . Press ENTER . You have now set a Direct-To course. AIRPORT CVO CORVALLIS city OR USA Set New Approach 1. Press SEL . The Load Approach option will appear. *Active* 0.0nm ...

  • Apollo 60 - page 227

    Approach Examples This section expands on the previous Approach Basics section. A variety of the situations that you may encounter while using approaches is included in this section. Use this section to familiarize yourself with the procedures that you expect to use in normal flight operations. What you will see · A description of the approach · ...

  • Apollo 60 - page 228

    Reproduced with permission of JeppesenSanderson Inc. Reduced for illustrative purposes. 9-38 Approach Examples ...

  • Apollo 60 - page 229

    Approach Example 1 - Straight In This example illustrates the approach to Nampa, Idaho. This example was selected because it is a new approach designed especially for TSO C-129 GPS equipment. It is probably as simple an approach to fly with the Apollo GX as there is. Note It is good planning to always consider what you would do in the event of any ...

  • Apollo 60 - page 230

    Illustration Points A - Between EMETT (IAF) and PARMO (APPR) B - Between PARMO (APPR) and DEFKI (FAF) C - Between DEFKI (FAF) and RW11 (MAP) D - Between RW11 (MAP) and NEMEW (MAHP) E - In Holding Pattern En Route Load and activate your flight plan, then load the approach. Select the Nampa Municipal GPS Rwy 11 approach. 30 nm From Nampa Municipal Ai ...

  • Apollo 60 - page 231

    2. The Approach Active annunciator will begin flashing 3 nm from DEFKI (FAF) indicating that approach RAIM prediction is beginning. The transition to approach active is starting. 3. At 2 nm from DEFKI the CDI scale will begin changing from 1 nm to 0.3 nm full scale deflection. Point C (Between DEFKI and RW 11) As you cross DEFKI, verify that the Ap ...

  • Apollo 60 - page 232

    9-42 Approach Examples ...

  • Apollo 60 - page 233

    Reproduced with permission of JeppesenSanderson Inc. Reduced for illustrative purposes. 9-43 Approach Examples ...

  • Apollo 60 - page 234

    Approach Example 2 - Holding at IFAF This example uses an active flight plan ending at the Medford, Oregon airport (MFR). The last two waypoints in this example are the Klamath Falls, Oregon VOR (LMT) and the Medford airport. This approach example involves a procedure turn, a combined IAF and FAF (IFAF), and a MAHP holding pattern at the FAF. This ...

  • Apollo 60 - page 235

    En route to Medford (MFR) 1. Create a flight plan named “Example 2” with the last two waypoints as the Klamath Falls VOR (LMT) and the Medford airport (MFR). 2. Activate the flight plan. Press FPL . Turn the LARGE knob to display the “Example 2” flight plan. Press SEL and then ENTER . 3. Load the VOR or GPS-A approach to MFR. In Nav or Flig ...

  • Apollo 60 - page 236

    Point A (Inbound to OED from the east) 1. Flight plan sequencing at OED is disabled because it is an IFAF in preparation for a procedure turn. The combined IAF/FAF waypoint is noted on your Apollo GX as IFAF. 2. Verify that the Hold annunciator is ON. Point B (Outbound on the procedure turn) 1. After crossing OED, the To/From flag will indicate FRO ...

  • Apollo 60 - page 237

    Point D (Inbound to OED) 1. As you intercept the 162 inbound a course intercept alert is given. Sequencing is automatically enabled. Turn to intercept the desired course. At 3 nm inbound to OED, the Approach Active annunciator will begin flashing to indicate that approach RAIM prediction is beginning. The transition to approach active is starting. ...

  • Apollo 60 - page 238

    3. Because OED is the MAHP, it is automatically a Hold waypoint and flight plan sequencing is suspended. Verify that the OBS/HLD annunciator is lighted. Point G (At the MAHP) 1. Upon crossing OED, press ENTER when prompted to set the inbound holding course (153°). Use the LARGE and SMALL knobs to select 153°. Then, press ENTER . OBS DTK: 153° to ...

  • Apollo 60 - page 239

    Reproduced with permission of JeppesenSanderson Inc. Reduced for illustrative purposes. 9-49 Approach Examples ...

  • Apollo 60 - page 240

    9-50 Approach Examples ...

  • Apollo 60 - page 241

    Approach Example 3 - Missed Approach This approach example describes an NDB approach from PARMO (IAF) to the Boise, Idaho airport (BOI). This example was chosen primarily because of the unusual published missed approach instructions and to illustrate how to navigate this missed approach with the Apollo GX. Illustration Points A - Between Parmo (IAF ...

  • Apollo 60 - page 242

    3. Load the NDB approach to BOI. In flight plan mode active plan or Nav mode home page, press SEL . The display will flash “Load Approach?” Press ENTER . Select “NDB 10R:PARMO” with the SMALL knob and press ENTER . 30 nm from Boise (BOI) 1. At 30 nm from your destination, the MSG annunciator will light. Press MSG . At the “Enable Approach ...

  • Apollo 60 - page 243

    2. Now press DIRECT-TO twice. Turn the LARGE knob to reach the reference waypoint. Turn the SMALL knob to select BO. OBS DTK: 150° to BO mahp man brg 162 dtk 162 3. Turn the LARGE knob to select the OBS course. Select 105° with the SMALL knob as the desired inbound course. Press ENTER . The CDI will indicate FROM and will provide guidance on the ...

  • Apollo 60 - page 244

    Reproduced with permission of JeppesenSanderson Inc. Reduced for illustrative purposes. 9-54 Approach Examples ...

  • Apollo 60 - page 245

    9-55 Approach Examples ...

  • Apollo 60 - page 246

    Approach Example 4 - VOR Reference This example for the VORDME A:MUGGZ approach uses a flight plan with the last two waypoints as VOR IMB (Kimberly, Oregon) to The Dalles, Oregon (DLS). This example is illustrates the following points: the step down fixes are referenced to a VOR that is not co-located with the MAP, the nature of the published misse ...

  • Apollo 60 - page 247

    En Route 1. Create a flight plan named “Example4” with Kimberly VOR (IMB) as the last waypoint before The Dalles, Oregon (DLS) as the destination airport. 2. Activate the flight plan. Press FPL . Turn the LARGE knob to display the “Example4” flight plan. Press SEL , turn the SMALL knob to select “Activate,” and then press ENTER . EXAMPL ...

  • Apollo 60 - page 248

    2. If the reference VOR is LTJ, press ENTER .I ft h e reference is not LTJ, press SEL and select the LTJ VOR with the LARGE and SMALL knobs and then press ENTER . The Apollo GX will automatically provide guidance with the Arc Assist and Map pages. Arc Assist Ref: LTJ vor Press ENTER/SEL 3. Use the Arc Assist page as the primary guidance for flying ...

  • Apollo 60 - page 249

    Point C - Inbound between D1850 (ARC) and CF005 (APPR) 1. Flight plan sequencing will operate automatically for each of the remaining waypoints. You will receive arrival and next DTK messages as you cross each waypoint. Press MSG to view the message. Press MSG again to return to the previous display. Point D - Between CF005 (APPR) to FF005 (FAF) 1. ...

  • Apollo 60 - page 250

    Point F - Turning to intercept 165° to MUGGZ (MAHP) 1. When you reach the Missed Approach Point and you wish to fly the published Missed Approach procedure, press OBS/HLD to reactivate waypoint sequencing as you start your climbing right turn. 2. Press DIRECT-TO twice and set the outbound course to 165°. Turn the LARGE and SMALL knobs to select 1 ...

  • Apollo 60 - page 251

    Manual Flight Plan Leg Selection Example You are flying a section of an active flight plan from SLE to BTG to OLM. As you approach the Portland area, you are given Radar vectors to the West of your course. ATC then tells you: “Fly heading 360, resume own navigation, intercept V287 to OLM, then as filed...” 9-61 Approach Examples V23 SALEM TURNO ...

  • Apollo 60 - page 252

    Manually select the leg from BTG to OLM (which is V287). Even though you have not yet reached BTG, you will know when you have intercepted this course. 1. Press FPL twice to reach the active plan in Flight Plan Mode. This example uses a flight plan from the Salem (SLE) airport to the Battle Ground (BTG) VOR and then to the Olympia (OLM) VOR. Turn t ...

  • Apollo 60 - page 253

    Approach Example 5 - DME Arc The following example describes the process for intercepting and flying a DME-Arc. This example uses a flight plan from Klamath Falls (LMT) to Medford (MFR) and will navigate along the VOR DME Runway 14 approach. You may also use Ashland (S03) to make your flight a little quicker. 1. Create a flight plan from Klamath Fa ...

  • Apollo 60 - page 254

    2. Some approaches use additional intermediate waypoints not listed on the approach selection page, but are shown as small squares. Press INFO to view all waypoints in the approach. Turn the SMALL knob as necessary to view additional waypoints. Press INFO again to return to the previous page. LANKS ¾ D3330 ¾ OED11 ¾ CF14 ¾ OED ¾ MA14 ¾ 3. At ...

  • Apollo 60 - page 255

    Left Arc dtk 245 ref: OED vor Rad 335° 16.4nm· 3. Follow the Moving Map or Arc Assist page information to fly the arc. 4. Flight plan waypoint sequencing will operate normally. Note When intercepting and flying DME-ARCs, autopilots may be used only in the heading mode. Autopilots may be used in Nav mode if you manually update the course bug. Auto ...

  • Apollo 60 - page 256

    Approach Example 6 - Procedure Turn 1 This example uses a flight plan from Roseburg, OR (5S1) to Medford, OR (MFR) to demonstrate how to recover when you overshoot the point where you need to place sequencing on hold (Point B). If you cross an IAF without suspending sequencing (pressing OBS/HLD), the Apollo GX will automatically sequence to show MA ...

  • Apollo 60 - page 257

    1. Point A - At 30 nm west of the MFR airport, you will be prompted to “Enable Approach.” As the current Track Angle is less than 70° to the FAF-MAP leg, sequencing is not suspended. 2. As you cross over the OED VOR (IAF) at point E, the unit will sequence to MA14, because sequencing was not suspended prior to OED. 3. If you still need to fly ...

  • Apollo 60 - page 258

    Approach Example 7 - Procedure Turn 2 For this example, use the VOR or GPS-B approach for Wenatchee, Washington. You will start the approach using the CASHS transition. The example involves a procedure turn at the FAF that is not also the IAF. Illustration Points Point A - Between CASHS and EAT. Poin tB-A heading of 105° between EAT and FF285. Poi ...

  • Apollo 60 - page 259

    3. Point C - You will be prompted to enter the OBS DTK when you near the FAF. Select an OBS setting of 285° with the LARGE and SMALL knobs and then press ENTER to select an inbound course. Note that the CDI will be “reverse-sensing” just as it would when outbound from a VOR with the OBS set to the inbound course. 4. Point D - Make the procedur ...

  • Apollo 60 - page 260

    The following examples of typical approaches illustrate where the LOC-DME waypoint may be useful. In addition, examples using DME information from VOR waypoints are given. ILS with DME Data from ILS DME Antenna The following example uses the ILS Rwy 10L approach to Portland International airport. This procedure describes the use of your Apollo GPS ...

  • Apollo 60 - page 261

    The Apollo GPS CDI may not be aligned with the approach course, only the Nav receiver may be used for course guidance. 3. Press NAV on the Apollo GPS to display distance. Note the distance to the IVDG DME to identify the intersections TRAYL (D9.1 IVDG), BLAZR (D5.2 IVDG), D2.2 step down, and, D0.2. Note that if you enter the step-down waypoints int ...

  • Apollo 60 - page 262

    ILS DME with DME Data from Two VORs on the Field This example uses the ILS DME approach to Rwy 21 at Flagstaff, Arizona. The DME is co-located with the VOR. 1. Before commencing the approach, press DIRECT-TO . Select the Flagstaff (vFLG) VOR/DME waypoint using the LARGE and SMALL knobs, and then press ENTER . 2. Use your Nav receiver for Localizer ...

  • Apollo 60 - page 263

    The Apollo GPS CDI may not be aligned with the approach course, if the magnetic variation has changed since the VOR station was commissioned. Only the Nav receiver may be used for course guidance. 3. Press NAV on the GPS to display distance. Use your Apollo GPS for distance information to identify the REENY (IAF) intersection at D20.0, the D16.0, D ...

  • Apollo 60 - page 264

    identify FORRS (D13.0), CERAB (D18.0), and the missed approach point (D23.0). DME Arc Example The following example uses Baltimore’s VOR DME 15 to demonstrate the approach to Martin State Airport. The approach uses a 14.7 DME clockwise arc to guide the aircraft to Runway 15. 1. Before reaching SLOAF, tune the Nav receiver to the Baltimore VOR. In ...

  • Apollo 60 - page 265

    just plant your right wing on the bearing to BAL as displayed by the GPS and hold the arc. If the distance drifts lower than 14.7, widen the turn a few degrees by turning left. If the distance drifts higher than 14.7, tighten the turn a few degrees by turning right. 5. Dial the 021° radial on you Nav receiver to identify the CUMBE intersection, wh ...

  • Apollo 60 - page 266

    Notes 9-76 Approach Examples ...

  • Apollo 60 - page 267

    Approach Notes Waypoints The database waypoints which describe the TSO C129a GPS approaches correspond with the waypoints which appear on the approach procedure charts whenever possible. VORs, NDBs, and named Intersections will appear in the approach sequence as they are on the charts. The Rifle, Colorado VOR will be identified RIL, the Turno Locat ...

  • Apollo 60 - page 268

    underlying approach. There are many GPS overlay approaches, such as the VOR or GPS-B approach to Wenatchee Washington, where there is no FAF inbound. The EAT VOR is the Initial Approach Fix (IAF), Final Approach Fix (FAF), Missed Approach Point (MAP), and Missed Approach Holding Point (MAHP). When there is no FAF inbound waypoint for a GPS approach ...

  • Apollo 60 - page 269

    Reproduced with permission of JeppesenSanderson Inc. Reduced for illustrative purposes. 9-79 Approach Notes ...

  • Apollo 60 - page 270

    Another type of waypoint which will have a name in your Apollo GX database, but may or may not appear on your approach procedure chart is an IAF waypoint defined as a radial and distance from a VOR. An example would be the VOR DME RWY 4 approach to North Bend, Oregon. The IAF at the OTH 164 radial at 14 nm is contained in the Apollo GX database as ...

  • Apollo 60 - page 271

    Charts have been reduced for illustrative purposes. 9-81 Approach Notes ...

  • Apollo 60 - page 272

    There are several other types of waypoints which may appear in your Apollo GX loaded approach and which may or may not appear on your approach procedure charts. Following is a brief description of these types of waypoints and the naming convention followed. Identification Each waypoint in an Apollo GX flight plan has an identifying type and a name. ...

  • Apollo 60 - page 273

    or course reversal is required - this usually depends on the direction of flight). MAP Missed Approach Point MAHP Missed Approach Holding Point ARC A DME arc terminator. The preceding flight plan leg is described as an arc to this waypoint. An ARC waypoint may follow another ARC waypoint. APPR An intermediate approach waypoint. These are sometimes ...

  • Apollo 60 - page 274

    The following legs replace the BKE airport in the flight plan and describe the approach sequence. D272Y TO D297Y 3* 018° 10.8nm iaf arc D297Y to D297O 4* 118° 10.0nm arc appr D297O to CF12 5* 119° 5.0nm appr appr CF12 to FF12 6* 120° 6.0nm appr faf FF12 to MA12 7* 120° 6.0nm faf map MA12 to BKE 8* 120° 6.0nm map mahp Notice that these waypoin ...

  • Apollo 60 - page 275

    Reduced for illustrative purposes. 9-85 Approach Notes ...

  • Apollo 60 - page 276

    Charts have been reduced for illustrative purposes. 9-86 Approach Notes ...

  • Apollo 60 - page 277

    Naming Conventions When a name must be provided for an otherwise unnamed waypoint, the naming will use the ARINC-424, chapter 7 specified convention whenever possible. There are a few types of waypoints, DME arc waypoints greater than 26 nm from the reference and single character NDB idents, which are not adequately addressed by the ARINC-424 speci ...

  • Apollo 60 - page 278

    it; therefore, it would appear in the database as “GNB” at the second airport. Standard Naming Conventions In general, the following codes are used to correspond to a waypoint type. When they are associated with an approach to a specific runway, the runway is appended. When the approach is not to a specific runway, the approach bearing is appen ...

  • Apollo 60 - page 279

    Unnamed turn points, intersections, and bearing/distance waypoints: Idents for unnamed turn points, intersections, or bearing/distance waypoints (other than VHF navaid distance/bearing), that are not coincidental with named waypoints, are constructed by using the ident of the nearest navaid together with the distance (rounded to whole miles). If th ...

  • Apollo 60 - page 280

    Note Jeppesen Approach Procedure Charts identify Phase-2 overlay approaches by printing GPS contained in parenthesis, (GPS) along with the procedure name. Phase III GPS Approaches Phase III GPS approaches must contain GPS in the title of the GPS procedure such as VOR or GPS RWY 24. Neither the ground station navaid(s) nor the traditional aircraft a ...

  • Apollo 60 - page 281

    Start Up Displays The Start Up Sequence runs each time the unit is powered on. The Start Up Sequence varies between units due to installation differences. The initial start up message is displayed for about three seconds. Apollo GX By II Morrow Startup Bypass During the startup sequence, press the SKIP “smart” key to stop the initial testing. Y ...

  • Apollo 60 - page 282

    Owner Message If the owner name has been previously entered (in System Mode), this page with your name is displayed for three seconds. No owner info screen is displayed if the user has not entered the owner data . Property of: II Morrow Inc Memory Tests Your Apollo GX performs a number of tests at startup to ensure proper operation. Note In the eve ...

  • Apollo 60 - page 283

    Failure to pass the software checksum test indicates that the software memory is corrupted. The GPS board will not continue operation when the following screen is displayed. Software Test Failed: Contact IIMorrow Non-Volatile RAM Tests The non-volatile RAM validation code does the following checks every time the unit is powered up. Any tests which ...

  • Apollo 60 - page 284

    Miscellaneous NVRAM or EEPROM Memory Failure All other user input values which are held in non-volatile RAM are checked for validity, producing the following message if any of the values needed to be reset. The following message is then displayed until you press ENTER . Memory Test Failure Press ENTER Database Test This checksum test compares the d ...

  • Apollo 60 - page 285

    Database Message This page shows the database name and expiration date. If the database has expired, press ENTER to continue. Americas DB Expires mm/dd/yy Version: x.xx Seed Position Each time the Apollo GX is switched on, it must locate satellites in the sky to acquire signals before determining a position fix in a complex process involving length ...

  • Apollo 60 - page 286

    press ENTER to accept the current position, though this is not required. Ppos: 2.3nm 130° To Nrst Wpt SLE Ent-OK SEL-Chnge 2. Press SEL to change the Seed Position. 3. The current Reference Position will be displayed and the Chg? prompt will flash. Ppos: 44°54.46N 122°59.69W Ref Wpt: Chg ? Press ENTER to change the Reference Waypoint or turn the ...

  • Apollo 60 - page 287

    SMALL knob. Turn the LARGE knob to move to each character of the waypoint name. 4. When you have entered the waypoint name, press ENTER . Change Lat/Lon Reference Position 1. Set the latitude and longitude coordinates near to your current position. After setting the Reference Waypoint, the first character of the Reference Position Lat/Lon will flas ...

  • Apollo 60 - page 288

    4. After entering the Seed Position, you will be prompted next to clear the active flight plan. Choose Yes or No with the SMALL knob. Press ENTER to continue normal operations. Clear Active Flight Plan NO? IFR Output Tests A series of tests covering connections for IFR flight are tested if your Apollo GX has been installed and configured for IFR fl ...

  • Apollo 60 - page 289

    TO/FROM FLAG -To- To/From Flag tests and display screens are provided for the To, From, and Off conditions. Nav Valid and Nav Super Flag Tests The Nav Valid and Nav Super Flag outputs are tested next. Each of the following displays is shown for three seconds, during which the external Nav Valid and Nav Super flags should be driven as indicated by t ...

  • Apollo 60 - page 290

    VDI tests and display screen are provided for VDI Full Up, VDI Half Up, VDI Level, VDI Full Down, and VDI Half Down. VDI Valid and VDI Super Flag Tests (GX50 and GX60/65 only) The VDI Valid and VDI Super Flag outputs are tested next. Each of the following displays is shown for three seconds, during which the external VDI Valid and VDI Super flags s ...

  • Apollo 60 - page 291

    Screen Test A full visual display test on each line of the display and all of the annunciators is run next, preceded for two seconds by the following screen. Starting Display Test... The visual display incrementally lights groups of pixels on the electroluminescent display. Checking GPS Signal Strength The unit shows the GPS signal strength screen ...

  • Apollo 60 - page 292

    3. Turn the SMALL knob to view the GPS Satellites Used for the Position fixes page. GPS SV’s for Fix 31, 27, 26, 19, 07, 02 4. Turn the SMALL knob again to view the GPS Satellite Status, Elevation, Signal Strength (SIG), and Azimuth page. Turn the SMALL knob to view information about each available satellite. The status will initially display as ...

  • Apollo 60 - page 293

    Flight Simulator Your Apollo GX is provided with a Flight Simulation program that allows you to “fly” your unit by simulating the speed and altitude. This section describes the procedures used to run the Flight Simulator. You may operate the Flight Simulator in the cockpit or in your home to familiarize yourself with the operation of the Apollo ...

  • Apollo 60 - page 294

    Removing and Replacing the Apollo GX The following procedure is used to remove the Apollo GX so you can operate it at a location of your choice. . While inserting or removing the GX, Do not exert excessive turning force at the end of the cam lock travel or the unit may be damaged. 1. Remove the Apollo GX from the front panel of your aircraft. Use t ...

  • Apollo 60 - page 295

    lock is hard to turn or the unit does not seat fully, the unit is probably binding and the mounting tube should be checked. Starting the Flight Simulation The following procedure is used to start the flight simulation. It is recommended that you have a data card properly inserted into the data card slot so you can use the appropriate functions. 1. ...

  • Apollo 60 - page 296

    6. You will be prompted to use or clear the previous Flight Plan. Turn the SMALL knob to choose Yes or No. Press ENTER . If you do nothing, the Apollo GX will automatically retain the previous Flight Plan and switch to the Nav function. The Apollo GX will go to the Nav function and a simulated GPS sensor begins tracking your position from the first ...

  • Apollo 60 - page 297

    Troubleshooting Or, what to do when nothing works! This section contains information to troubleshoot your Apollo GX product when improper operation is observed. The following table lists possible problems you could encounter while operating the unit. Examine the possible causes of the problem and take the action listed to correct the trouble. If yo ...

  • Apollo 60 - page 298

    To Ensure Trouble Free Operation Avoid high cockpit temperatures when the aircraft is not in use. Extreme heat shortens the life of any electronic equipment. Periodically check all antenna, power, and ground connections. Caution DO NOT clean the face plate with chemical cleaning agents, solvents, or harsh detergents. A soft cloth may be used to cle ...

  • Apollo 60 - page 299

    Problem Possible Cause Action No GPS signal reception Obstructed signal path Move aircraft out of hangar or away from buildings to provide an unobstructed view of the sky for the antenna Incorrect seed position, time, or UTC differential entered Check these settings, if necessary in the System Functions If using a wrong antenna: faulty external ant ...

  • Apollo 60 - page 300

    Problem Possible Cause Action Search for nearest waypoints reveals too few or wrong types of waypoints Incorrect selection of waypoint types to show after search Runway Limits are set for a value that is too large Check “Airspace Setup” function and verify that the desired waypoint type to search is “ON”, see page 10 Check the “Identifier ...

  • Apollo 60 - page 301

    GPS Navigation GPS Overview The Global Positioning System (GPS) is a constellation of 24, or more, satellites in six orbit lanes 10,898 nautical miles above the earth at an inclination angle of about 55 degrees from the equator. Each satellite orbits the earth twice in 24 hours. The GPS was developed and the satellites launched by the U.S. Departme ...

  • Apollo 60 - page 302

    processes the information to determine which satellites are “visible” to the receiver’s antenna. With this determination made, the receiver chooses satellites to calculate a position fix. Using information transmitted from three or more satellites, the unit can calculate latitude and longitude (usually abbreviated Lat/Lon); with four or more ...

  • Apollo 60 - page 303

    Glossary A Altitude (GPS ALT): Altitude, as calculated by the Apollo GX , based upon a mathematical model of the earth’s surface curvature. A substantial difference between this altitude value and altitude referenced to sea level may exist. Altitude Assist: An aid that provides guidance in descending from one altitude to another. See the Altitude ...

  • Apollo 60 - page 304

    Bearing (BRG): The direction to any point, usually measured in degrees relative to true or magnetic north. The direction from your present position to your destination waypoint. C CF: Final approach course Fix. This waypoint type is used when necessary to define a course to the FAF - all VOR DME approaches require a course fix waypoint. A code appe ...

  • Apollo 60 - page 305

    Cross Track Deviation: The distance that your are away from your intended course. CTAF: Common Traffic Advisory Frequency. D Database: A collection of data structured in such a way as to allow quick and convenient access to any particular record or records. The Apollo GX contains a built-in database of waypoints and waypoint information. Users may ...

  • Apollo 60 - page 306

    Desired Track (DTK): The desired course of navigation between a point of origin (FROM) and a destination (TO) waypoint. Destination: The last waypoint in the active route. Dilution of Precision (DOP) : A merit value for the calculated position based on the geometrical configuration of the satellites used; 3 is considered good, greater than 7 is con ...

  • Apollo 60 - page 307

    FDE: The F ault D etection and E xclusion column refers to the ability to identify and exclude a faulty satellite and still have suitable satellite geometry at that position. FF: Final Approach Fix. A code appended to a waypoint in the database that may not appear on a published map. Fix: A geographical location determined by either visual referenc ...

  • Apollo 60 - page 308

    Hold: Waypoint sequencing is disabled or suspended. A hold may be automatically or manually activated. This should not be confused with a “holding pattern.” Pressing the OBS/HLD key suspends waypoint sequencing. I IAF: Initial Approach Fix. Identifier: A name, typically abbreviated, assigned to a waypoint. The identifier may consist of numbers ...

  • Apollo 60 - page 309

    Magnetic North: The region, some distance from the geographic north pole where the earth’s magnetic lines concentrate. A magnetic compass points to the magnetic north. Magnetic Variation (Mag Var): The angle between the magnetic and true north. At various points on the earth it is different due to local magnetic disturbances. It is shown on chart ...

  • Apollo 60 - page 310

    N Nautical Mile (nm): A distance measurement equal to 6,076 feet, or 1.15 statute mile. One nautical mile is also equal to one minute of latitude. NAVSTAR: The name given to GPS satellites formed from the acronym for NAV igation S ystem with T ime And R anging. Non-Directional Beacon (NDB): A low frequency/medium frequency navigation aid sending no ...

  • Apollo 60 - page 311

    Relative Bearing Indicator: The Relative Bearing Indicator is an arrow next to the Bearing value that indicates an approximate bearing to a waypoint or airspace relative to the aircraft’s current track when your current ground speed is more than 5 knots. RW: Runway Fix. A code appended to a waypoint in the database that may not appear on a publis ...

  • Apollo 60 - page 312

    Track (TRK): The imaginary line that the flight path of an airplane makes over the earth. Track Angle: The angle of your actual direction of travel. Track angle is computed using the magnetic variation at the Present Position. Track Angle Error (TAE): The difference between the Desired Track and the Track Angle (Dtk - Trk = Tae). A letter is shown ...

  • Apollo 60 - page 313

    UTC Differential: The difference in time between that at the present position and UTC. UTM (Universal Transverse Mercator map projection system): Also known as Military Grid Coordinates, the UTM grid consists of 60 north-south/east-west zones, each six degrees wide in longitude. V VFR: Visual Flight Rules. VOR: Very High Frequency Omni-directional ...

  • Apollo 60 - page 314

    Notes 15-12 Glossary ...

  • Apollo 60 - page 315

    Index A Abbreviations .......... 10-4 Access database ..........5 - 3 Activate flight plan ....... 6-14 Air pressure ........... 7-20 Air speed ......... 7-20 - 7-21 Air temperature ..... 7-20 - 7-21 Airport elevation .........5 - 6 Airport frequency .........5 - 6 Airport Info ............5 - 1 Airspace Buffers ··········· 4-11 Ceiling ...

  • Apollo 60 - page 316

    CDI reverse sensing ....... 9-22 Change approach ........ 6-22 Cleaning ............. 13-2 Clear exclusion list ....... 9-35 Clear flight plan wpts ...... 6-17 Close ............ 4-11, 8-3 Close altitude ...........8 - 4 Com Headphone level ····· 10-12 Info ············· 10-9 Intercom squelch ····· 10-10 K e y ·······? ...

  • Apollo 60 - page 317

    Emergency channel ....... 10-8 Emergency search ........3 - 9 Empty TO waypoint .......8 - 4 En route operation ....... 9-30 Enable approach ...... 6-23, 9-8 Encoder altitude ......... 3-15 Encoding altimeter ....... 7-20 Ending Altitude ......... 3-18 Enroute ............ 9-1, 9-5 Error messages ..........8 - 3 Estimate ground speed ..... 6-16 Est ...

  • Apollo 60 - page 318

    Antenna ·········· 11-12 Azimuth ·········· 7-18 Communication failure · · · 8-5 Elevation ·········· 7-18 Error ·············8 - 5 Failure ············8 - 4 Health ········ 7-17, 11-11 Introduction ····· 14-1 - 14-2 Position ··········· 3-21 Reset ·········? ...

  • Apollo 60 - page 319

    Lat/Lon units ...........7 - 4 Left engine fuel ......... 7-23 Leg distance ............3 - 6 List key ..............1 - 6 Load approach ....... 6-22, 9-7 Load destination .........9 - 6 Local altimeter .......... 3-15 Localizer ......... 3-39 - 3-40 Low fuel ..............8 - 8 M Magnetic heading .... 7-20 - 7-21 Magnetic variation ..... 7-7, 8-13 ...

  • Apollo 60 - page 320

    I n U s e ············ 3-19 Standby ··········· 3-19 Part numbers ........... 1-ii Password ............. 7-16 Pattern .............. 4-20 PDOP .............. 3-21 Phase II Approach ........ 9-89 Phase III Approach ....... 9-90 Photocell .............1 - 2 Power knob ............1 - 3 Power Up .............2 - 1 Pressure alti ...

  • Apollo 60 - page 321

    Sunset/Sunrise time .......5 - 8 Symbol Triangle ···········3 - 5 System ...........7 - 1 - 7-24 Navigation Info ·······7 - 1 System Info ········· 7-11 T Technical assistance ....... 13-1 Terminal operation ....... 9-30 Tips ................ 6-26 T o ................ 6-19 TO waypoint .... 2-4, 3-6, 4-1, 8-9 TO-FROM flag ...

  • Apollo 60 - page 322

    Type ··········· 1-6, 4-6 Update User ········ 5-12 User info ···········5 - 3 VOR info ···········5 - 2 Waypoint alert .......... 8-10 Weather channel ........ 10-7 Web Page ............. 1-ii Wind direction .......... 7-22 Wind speed ........... 7-22 X X I T k e y ..............1 - 8 16-8 Index ...

  • Apollo 60 - page 323

    ...

  • Apollo 60 - page 324

    © 2001 by UPS Aviation Technologies, Inc. 2345 Turner Rd., S.E. Salem, OR 97302 U.S.A. Phone 503.581.8101 800.525.6726 In Canada 800.654.3415 FAX 503.364.2138 http://www.upsat.com Part #560-0961-03 July 2001 ...

Fabricante Apollo Categoría Stereo Amplifier

Los documentos del dispositivo Apollo 60 que obtenemos del fabricante se pueden dividir en varios grupos. Entre ellos están::
- dibujos técnicos Apollo
- manuales de instrucciones 60
- hojas de producto Apollo
- folletos informativos
- o etiquetas energéticas Apollo 60
Todos son importantes, pero lo más importante desde el punto de vista del usuario de un dispositivo lo encontraremos en el manual de instrucciones Apollo 60.

Un conjunto de documentos determinado como manual de instrucciones se divide también en tipos más detallados, tales como: instrucciones de montaje Apollo 60, instrucciones de servicio, instrucciones cortas o instrucciones de usuario Apollo 60. Dependiendo de la situación debes buscar el documento que necesitas. En nuestra página puedes consultar el manual de instrucciones más popular del producto Apollo 60.

Manuales de instrucciones parecidos

El manual de instrucciones del dispositivo Apollo 60, ¿cómo debería ser?
El manual de instrucciones, también determinado como el manual de usuario o simplemente instrucciones, es un documento técnico que tiene como objetivo ayudar a los usuarios a utilizar Apollo 60. Las instrucciones normalmente las realiza un escritor técnico pero en un lenguaje comprensible para todos los usuarios de Apollo 60.

El manual de instrucciones completo de Apollo debe contener unos elementos básicos. Una parte de ellos es menos importante, como por ejemplo: la portada / la página principal o las páginas de autor. Sin embargo, lo demás debe facilitarnos la información más importante desde el punto de vista del usuario.

1. Introducción y pistas sobre cómo orientarse con el manual Apollo 60 - Al principio de cada manual se deben encontrar las indicaciones acerca de la manera de usar un manual de instrucciones. Debe contener información sobre dónde encontrar el índice Apollo 60, preguntas frecuentes o problemas más comunes – son los apartados más buscados por los usuarios de cada manual de instrucciones.
2. Índice - listados de todos los consejos acerca de Apollo 60 que encontraremos en el documento
3. Consejos de uso de las funciones básicas del dispositivo Apollo 60 - que deben facilitarnos los primeros pasos durante el uso de Apollo 60
4. Troubleshooting - una secuencia sistematizada de acciones que nos ayudará a diagnosticar los problemas más importantes con Apollo 60
5. FAQ - las preguntas frecuentes
6. Datos de contacto Información acerca de cómo encontrar los datos de contacto del fabricante / servicio de Apollo 60 en cada país si no somos capaces de solucionar el problema por nuestra cuenta.

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