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II Morrow Inc. Apollo NMC, Operating Manual

The II Morrow Inc. Apollo NMC Operating Manual is available for download free of charge from 88.208.23.73:8080. This comprehensive manual provides detailed instructions and essential information about the product, ensuring users have a seamless experience. Download your free manual today to optimize your use of the Apollo NMC.

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Important Notice

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) attributed to poor satellite geometry.

Due to implementation of Selective Availability by the United States Department of Defense (DoD),
all GPS receivers may suffer degradation of position accuracy. The DoD has stated that 95% of the
time horizontal accuracy will not be degraded more than 100 m and 99.9% of the time accuracy will
not be degraded more than 300 m.

Installations of TSO C-129a authorized GPS Navigation Management Systems (NMS) may be
approved for supplemental navigation only. The NMS may be used as the primary navigation data
display, however, other means of navigation appropriate to the intended route of flight must be
installed and operational. It is not required that these other systems be monitored.

FCC Notice

This equipment has been tested and found to comply with the limits for a Class B digital device,
pursuant to part 15 of the FCC Rules. These limits are designed to provide reasonable protection
against harmful interference during residential use. Operation is subject to the following two
conditions: (1) this device may not cause harmful interference, and (2) this device must accept any
interference received, including interference that may cause undesired operation. This equipment
generates, uses and can radiate radio frequency energy and, if not installed and used in
accordance with the instructions, may cause harmful interference to radio communications.
However, there is no guarantee that interference will not occur in a particular installation. If this
equipment does cause harmful interference to radio or television reception, which can be
determined by turning the equipment off and on, the user is encouraged to try to correct the
interference by one or more of the following measures:

·

Reorient or relocate the receiving antenna.

·

Increase the separation between the equipment and receiver.

·

Connect the equipment into an outlet on a circuit different from that to which the
receiver is connected.

·

Consult the dealer or an experienced radio/TV technician for help.

Changes or modifications to this equipment not expressly approved by II Morrow Inc. could void the
user’s authority to operate this equipment.

DOC Notice

This digital apparatus does not exceed the Class B limits for radio noise emissions from digital
apparatus as set out in the radio interference regulations of the Canadian Department of
Communications.

Le présent appareil numérique n’émet pas de bruits radioélectriques dépassant les limites
applicables aut appareils numérique de classe B prescrites dans le réglement sur le brouillage
radioélectrique édicté par le ministère des communications du canada.

Summary of Contents for Apollo NMC

Page 1: ...Apollo NMC Navigation Management Computer Operating Manual July 1999 P N 560 0164 01b ...

Page 2: ...t ups com U S A Toll Free 800 742 0077 Canada Toll Free 800 654 3415 International 503 391 3411 FAX 503 364 2138 Caution The Apollo NMS Navigation Management System is a powerful navigation tool but you should never rely solely on any one piece of navigation equipment It s important to maintain a constant awareness of the navigation picture by using all appropriate resources Your new NMC and perip...

Page 3: ...s device may not cause harmful interference and 2 this device must accept any interference received including interference that may cause undesired operation This equipment generates uses and can radiate radio frequency energy and if not installed and used in accordance with the instructions may cause harmful interference to radio communications However there is no guarantee that interference will...

Page 4: ...History of Revisions Revision Date Software Ver Manual P N April 1996 560 0164 00 December 1996 560 0164 00A June 1997 560 0164 01 March 1998 6 1 560 0164 01A July 1999 6 3 560 0164 01B ii ...

Page 5: ...g with a sample of the NMS display you will see while performing the procedure In this example the action is Press the SEL button and turn the Small knob Action Explanation 2 Pressing SEL activates editing The altimeter value flashes Turn the small knob to select the desired value ALTITUDE ASSIST LOCAL ALTIMETER SETTING 29 92 NAV iii Underlined characters are flashing Depicts the mode the system i...

Page 6: ...two concentric knobs Small knob refers to turning the small inner ring of the two concentric knobs The button graphics refer to the buttons you should press for the given examples Round button graphics refer to the mode buttons to press for the examples Audience This manual has been prepared with the following assumptions You are familiar with navigation instruments and displays The approach and i...

Page 7: ...truments will be compared to You can be confident in knowing that you are the owner of the state of the art in navigation Our products are built to last and to allow for upgrading as your needs change in the future It is important to note that only version 5 0 or later version of the Apollo NMC may be used for IFR GPS approach navigation You can determine your version by either the part number on ...

Page 8: ...perienced user of GPS navigation be sure to read the Basic Concepts and First Flight sections These two sections provide the rules for successful use of the Apollo NMC The rest of the manual contains important information that you can refer to as you need more detail on specific procedures or features Apollo NMC ...

Page 9: ... 2 Power Switch 2 LED Display 2 Knobs 2 Action Buttons 3 Mode Buttons 4 EMG Emergency Mode 4 MSG Message Mode 4 NAV Navigation Mode 4 DB Database Mode 4 FPL Flight Plan Mode 5 SYS System Mode 5 Features 5 Operating Logic 7 First Flight 9 Power Up 9 Direct Navigation 9 Navigation Displays 13 Power Up Sequence 15 EMG Emergency Mode 25 EMG Emergency Mode Organization 26 Emergency Mode Displays 27 v A...

Page 10: ...rocedures 79 Displaying Nav Information 79 Starting Stopping Auto Nav Scroll 79 Displaying Present Position 80 Selecting a Position Sensor 81 Automatic and Manual Position Sensor Selection 82 Clear RAIM Predict Ignore List 86 Altitude Sensor Selection 87 Setting the Altimeter Barometric Pressure 89 Setting Editing Hold and Buffer Altitudes 90 Starting Stopping Altitude Hold 91 Setting Editing Auto...

Page 11: ...DB Mode Procedures 115 Retrieving a Waypoint 115 Waypoint Retrieval by Identifier 115 Retrieving a Waypoint by City Facility Name 118 Waypoint Information and Comments 121 Displaying Waypoint Information 121 Entering Editing Waypoint Comments 122 Deleting a Waypoint Comment 125 User Waypoints 127 Creating a User Waypoint by Latitude Longitude 127 Creating a User Waypoint by Radial Distance 130 Edi...

Page 12: ...vigation Information Sub State 179 Airspace Alert Settings 181 Setting the Auto Nav Scroll Time 185 Programmable and Autonav Nav Pages 186 Restoring Default Nav Displays 190 Manually Entering Magnetic Variation 191 Changing the Oceanic Activation Altitude 194 Editing the Flight Timer Trigger Speed 195 Display Units 196 Description of the Direct To Entry Option 197 Editing the Direct To Entry Optio...

Page 13: ...uencing Details 239 Procedure Turns 241 Procedure Turn at an FAF 242 Holding Patterns 246 DME ARCs Arc Assist 249 Other Uses for the Arc Assist Function 253 Missed Approaches 254 GPS Approach Operations 259 Operations 259 NMS Approach Procedure 262 En route Operations 262 Approach Transition Operation Enabling Approach 264 Canceling An Approach 271 Repeating an Approach 272 Selecting a Different A...

Page 14: ...itations 328 Position Fix 330 Apollo NMC Flight Simulator 331 About the Flight Simulator 331 NMC Removal Panel Mount 332 NMC Removal Dzus Mount 333 Connecting the Power Supply 334 Starting the Flight Simulation 335 Flight Simulator Operations 340 After the NMC is Re Installed in the Aircraft 340 Operating Manual Supplement for the Apollo 2002 2102 Keypad 1 History of Revisions 2 Ordering Informati...

Page 15: ...ed for redundancy The system approach allows additional components to be added at any time Apollo Navigation Management System 1 Apollo NMS Apollo NMC Air Data Computer DTRK 013TO 00 00 FMS1 FMS2 HDG TTG M IN 1 NM ILS1 CDI Apollo NMS Sensors 2010 Apollo NMS VDI HSI V A L I D MCLS NAVNET PTK Autopilot NAV HDG GS GS APR MSG VFR Moving Map Shadin Digiflo Miniflo Fuel Flowmeters Altitude Encoder 2030 ...

Page 16: ...automatically adjusts the brightness of the LED Light Emitting Diode display The display consists of 3 lines with 16 characters each Knobs The Large knob has two functions First it is used to scroll through top level displays in each mode Second when part of the display is flashing i e editing is on the Large knob is used to choose which character or characters on the display will flash 2 Apollo N...

Page 17: ... accesses supplementary information about the displayed waypoint It is also used to access flight plan comments that you enter Pressing this button makes the current mode light flash indicating you are looking at waypoint or flight plan information Pressing this button again exits the INFO function Enter The ENT button enters and saves the information flashing on the display If ENT is not pressed ...

Page 18: ...ur aircraft MSG Message Mode MSG mode is used to display messages The NMC Nav Management Computer alerts you to important conditions such as arrival at a waypoint or degraded position accuracy The MSG light flashes when a new message condition occurs and is lit solid if any messages you have already viewed remain NAV Navigation Mode NAV mode is used to display navigation information such as the be...

Page 19: ...for position and other sensors Features Below is a brief explanation of the features available with the Apollo NMS Direct To Flights The NMS can provide course guidance from your location directly to any waypoint in any database Data cards Data cards contain listings of public use Airports VORs NDBs INTs intersections airspaces non precision approaches MSA MESA and magnetic variation information i...

Page 20: ...y with a specific sensor installed Flight Plans The NMC Nav Management Computer allows you to store up to 30 flight plans of up to 20 legs each These plans may be viewed activated reversed interrupted edited and deleted while en route or on the ground One of these flight plans is the Active flight plan From the first time a course is entered into the new unit there is always an Active flight plan ...

Page 21: ...imilar to the one below appears In this manual black characters such as the A in the display below indicate the item is flashing and editing is activated A I R P O R T A A P H O U S T O N CITY TX USA Whenever something on the display is flashing it may be changed by turning the Small knob To make something else on the display flash turn the Large knob The display shows the waypoint identifier and ...

Page 22: ...ANTILL Use the knobs to choose the remaining characters in the identifier until the desired waypoint is displayed VOR CCR CONCORD FACIL CA USA The last step is to press the ENT button As far as the system memory is concerned nothing has changed until ENT is pressed If you did not want to navigate to the displayed waypoint you would simply press any mode button Any time you want to abort a procedur...

Page 23: ...l remain blank Following initialization a power up sequence begins After the sequence the display below appears If the NMC Nav Management Computer has been removed from the panel and used in simulator mode or the unit has moved several hundred mile since the last time it was powered up your present position must be entered during the power up sequence See Operations Power Up Sequence ETE NAV FLAGG...

Page 24: ...displays other available items Turn the Small knob to choose the desired waypoint type In this example the VOR type is chosen VOR AAF NABB facil IN USA NAV 3 Turning the Large knob causes different items on the display to flash Turn the Large knob to make the first character in the waypoint ident flash AIRPORT AAF APALACHICOLA city FL USA NAV 10 Apollo NMS Underlined characters are flashing D The ...

Page 25: ...s the knob is turned because the NMC Nav Management Computer will not display an identifier that doesn t exist VOR DAG DAGGETT facil CA USA NAV 5 Turn the Large and Small knobs to choose the remaining characters in the waypoint identifier The desired waypoint is displayed VOR DLS THE DALLES facil OR USA NAV 11 Apollo NMS Heading_2 ...

Page 26: ...idance on a course from your present position to the chosen waypoint Navigation information is only displayed when position sensors have completed acquiring signals ETE DLS 00 00 Ã 0 00 BRG159 82 7NM NAV 12 Heading_2 Apollo NMS ENT Indicates additional displays sub pages may be viewed by turning the Small knob ...

Page 27: ...o until the system calculates position which takes from one to four minutes after power up and a To waypoint is entered ETE DLS 00 31 Ã 0 26 BRG 165 45 6NM TOP LINE The Estimated Time En route ETE to DLS is 31 minutes MIDDLE LINE The CDI indicator similar to a VOR CDI The desired course is towards the bar The selected course is 0 26nm to the left BOTTOM LINE The bearing to DLS is 165º the distance...

Page 28: ...E CDI The current UTC Coordinated Universal Time is 14 25 2 25 pm ETA DLS 14 56 MIN SAFEA 5700 ENRTSAFEA 13600 Estimated Time of Arrival ETA at DLS is 14 56 UTC MSA Minimum Safe Altitude MESA Minimum En route Safe Altitude BARO ALT 390FT ABOVE HOLD TO DESCENT Barometric Current Altitude The distance in feet above or below Hold altitude Time to beginning of Auto descent When Auto Descent has starte...

Page 29: ...e flying in In addition the NMC displays start up self test pages self test results and asks if you want to continue with the last used flight plan To acquire a position the system must know its approximate location and if using a GPS sensor the time UTC Coordinated Universal Time formerly called Greenwich Mean Time Hint The UTC and approximate position should be entered by the installer in which ...

Page 30: ...errors are found the affected User Waypoints are cleared from memory and the display shown below is displayed until the user presses ENT If no errors are found this page is not shown User DATABASE Memory Failure Press ENT NAV Next all Flight Plan information is checked If any errors are found the affected flight plans are cleared from memory and the display shown below is displayed until the user ...

Page 31: ...dicates a critical system error may exist In this case the following message is displayed and the NMC will not continue to function If this problem should occur return the NMC to the dealer for repairs Software Test Failed Contact Dealer NAV If a datacard is in the datacard slot it is tested next This test checks all of the datacard memory taking about 5 seconds to complete The test is accompanied...

Page 32: ...wner Information on page 209 Property Of ORVILLE WRIGHT KITTY HAWK NAV When a valid datacard is properly inserted in the datacard slot the database name expiration date and version number is displayed for 4 seconds West North Am Db Date 3 30 99 Version 1 11 NAV The display below only appears if the datacard is invalid or not inserted properly The magnetic variation value in bold is flashing Rotate...

Page 33: ...on the previous page is displayed then press ENT when the screen shown below appears or press SEL to cancel Press ENT To Turn Airspace Alerts On NAV If the Special Use Airspace SUA setups restricting which SUA alerts are displayed have been changed from the standard setups the screen shown below will be displayed for up to 4 seconds Airspace Setups Are Non Standard Setups NAV To reset the airspace...

Page 34: ...ergency Search Setups NAV If the 2030 Fuel Air Data Sensor is installed the NMC displays the next screen until SEL is pressed FUEL ON BOARD Must Be Verified Press SEL NAV Enter the total amount of fuel which is in the airplane s tanks including reserve by rotating the Small and Large knobs to edit the displayed values then press ENT If the cursor is flashing on the word FULL when ENT is pressed th...

Page 35: ... by pressing SEL within 4 seconds rotating the Large and Small knobs and pressing ENT to save the displayed values The UTC may also be reset in System Mode If using a GPS sensor the UTC and date must be accurate for the sensor to initialize in less than 30 minutes Date 11 APR 99 Time 15 14UTC SEL To Reset NAV The display below showing the present position in relation to the nearest airport appears...

Page 36: ...a GRI the system must know its approximate location If the NMC has been removed from the panel for use in Flight Simulator mode the display below appears after reinstallation in the aircraft and you must enter a reference position before the power up sequence will continue Press SEL to update the current position Reset Present Position Press SEL NAV Rotate the Large and Small knobs to edit the val...

Page 37: ...f Basic Concepts for detailed information on the Waypoint Retriever When the desired waypoint has been found using the Waypoint Retriever press ENT to exit the Waypoint Retriever and to display the current position of the retrieved waypoint If you are satisfied with the present position displayed press ENT again to save it as the NMC s current position The final power up screen shown below prompts...

Page 38: ... YES or NO Then press ENT CLEAR ACTIVE FLIGHT PLAN YES NAV At this point the power up sequence is complete North America EXPIRES 11 09 95 PRESS ENT NAV If your unit is installed for IFR GPS approach navigation a sequence of IFR output tests will be run to verify CDI andVDI annunciators as well as a display test STARTING IFR OUTPUT TESTS NAV 24 Power Up Sequence Operations ...

Page 39: ...ch database The feature also locates the 20 nearest SUAs Special Use Airspaces The Search Around a Waypoint feature is included in EMG mode and is very useful in flight planning It displays the nearest waypoints and SUAs relative to any waypoint in any database Runway limits can be used to display only those waypoints with adequate landing facilities Surface parameters can be Hard Hard Soft or Har...

Page 40: ... NEAREST Airport 1 NEAREST VOR 2 NEAREST VOR 3 NEAREST VOR 20 NEAREST VOR 1 NEAREST NDB 2 NEAREST NDB 3 NEAREST NDB 1 NEAREST INT 2 NEAREST INT 3 NEAREST INT USER 20 NEAREST 1 NEAREST USER 2 NEAREST USER 3 NEAREST USER CHOOSE SEARCH WAYPOINT RETRIEVER WAYPOINT 20 NEAREST Airport 1 NEAREST Airport ENT ENT RUNWAY LIMITS 1 NEAREST SUA 2 NEAREST SUA 3 NEAREST SUA 20 NEAREST SUA 20 NEAREST NDB 20 NEARE...

Page 41: ...fier and the database The bottom line shows the bearing relative bearing and distance The relative bearing arrow shows the approximate direction relative to the current ground track In the example the second closest airport to your present position is SLE The bearing to SLE is 75o the relative bearing is straight ahead and the distance is 7 3 nm NEAR 2 TO PPOS SLE AIRPORT BRG 075 7 3NM Turning the...

Page 42: ...he middle line shows the type of SUA Inside means you are inside of the SUA The bearing and distance to the nearest edge of the airspace is shown on the bottom line In this example the second closest SUA to your position is the Portland Oregon ARSA and the nearest edge of the ARSA is 005o and 6 2 nm PORTLAND OR 2 ARSA INSIDE BRG 005 6 2NM The display below may be selected with the Large knob after...

Page 43: ...he requirements are not displayed while using the Emergency Search or Search Around a Waypoint features All nearest waypoints are displayed during Emergency Search if runway limits are set to zero RUNWAY LIMITS HARD SOFT WATER FT 1200 LIT YES If you attempt to set the lighting requirement when the runway length is set at 0 the display below appears for approximately 3 seconds ZERO RWY LENGTH CANNO...

Page 44: ...used to display the nearest waypoints to your position and navigate directly to any of them Flow Chart 30 Emergency Mode Displays Operations PRESS EMG TURN TO DISPLAY DESIRED DATABASE TYPE TURN TO DISPLAY THE DESIRED WAYPOINT PRESS ENT A DIRECT COURSE TO THE WAYPOINT IS ENTERED PRESS D ...

Page 45: ...IRPORT BRG 342 7 3NM If the NMC has not calculated a valid position the display below telling you the last known position is being used appears If you want to continue press ENT USING LAST KNOWN POSITION PRESS ENT 2 Turn the Large knob to display the desired database type Turn the Small knob clockwise to display the remaining nearest waypoints for each database type beginning with the closest and ...

Page 46: ...tinued 3 Pressing the DIRECT TO button activates the Waypoint Retriever VOR CVO CORVALLIS FACIL OR USA NAV 4 Pressing ENT enters a direct course to the waypoint ETE CVO 0 10 Ã 0 00 BRG 189 27 6NM NAV 32 Emergency Mode Displays Operations D ENT ...

Page 47: ...lity name 33 Operations Emergency Mode Procedures ENT PRESS ENT PRESS PRESS EMG THE CHOOSE WAYPOINT TO TURN TO DISPLAY SEARCH AROUND PAGE IS THE DESIRED WAYPOINT TO SEARCH AROUND DISPLAYED YES YES NO DATABASE TYPE FLASH TURN TO MAKE THE TURN TO DISPLAY DESIRED DATABASE TYPE TURN TO DISPLAY THE DESIRED CHARACTER IS THE DESIRED WAYPOINT IDENTIFIER DISPLAYED PRESS SEL PRESS SEL TURN TO MAKE THE IDENT...

Page 48: ... ENT 2 Pressing ENT activates the Waypoint Retriever and the first character in the waypoint identifier flashes VOR CVO CORVALLIS FACIL OR USA 3 Display the desired waypoint Use the Waypoint Retriever to display the desired waypoint The Waypoint Retriever is described in Operations Retrieving a Waypoint AIRPORT WA61 SPANAWAY CITY WA USA 34 Emergency Mode Procedures Operations EMG ENT ...

Page 49: ... knob to change the database type Turn the Small knob clockwise to scroll through the waypoints in order from the nearest to the most distant NEAR 2 TO WA61 GR NDB BRG 279 10 6NM Note Press INFO and then turn the Small knob to examine details about the displayed waypoint Press INFO again to return to the previous screen 35 Operations Emergency Mode Procedures ENT INFO INFO ...

Page 50: ...that meet or exceed the runway requirements you specify If a runway length of 0 feet is chosen you cannot set runway surface or lighting limits Flow Chart 36 Emergency Mode Procedures Operations ENT PRESS YES THE RUNWAY LIMITS PAGE TURN TO DISPLAY PRESS TO ACTIVATE EDITING SEL INFORMATION TO CHANGE FLASH TURN TO MAKE THE TURN TO DISPLAY THE DESIRED INFORMATION ARE THE DESIRED RUNWAY LIMITS DISPLAY...

Page 51: ... Small knob to display the desired runway length Runway length is selected in increments of 100 feet RUNWAY LIMITS HARD SOFT WATER FT 2500 LIT NO 3 Turn the Large knob to make the surface type or lighting requirement flash Turn the Small knob to choose the setting Repeat until the desired limits are displayed RUNWAY LIMITS HARD SOFT WATER FT 2500 LIT YES 37 Operations Emergency Mode Procedures EMG...

Page 52: ...mpt to edit the lighting or surface type when a runway length of 0 is selected one of the displays appears for 2 seconds ZERO RWY LENGTH CANNOT EDIT LIGHTING ZERO RWY LENGTH CANNOT EDIT SURFACE TYPE 4 Pressing ENT enters the displayed runway limits RUNWAY LIMITS HARD SOFT FT 2500 LIT YES 38 Emergency Mode Procedures Operations ENT ...

Page 53: ...g but remains lit as long as the message condition exists If more message conditions occur the MSG light will begin to flash again Messages are displayed in prioritized order the most important to the least important The figure below illustrates the organization of Message Mode 39 Operations Message Displays OLD MESSAGE SUMMARY NEW MESSAGE SUMMARY HIGHEST PRIORITY MESSAGE HIGHEST PRIORITY MESSAGE ...

Page 54: ...de Assist and Arc Assist functions are disabled during system setup New Message Summary The display below summarizes the number of new messages It shows the number of new messages to be viewed In the example there are 4 new messages to view If there are no new messages the display states there are no new messages 4 NEW MESSAGES TURN LARGE KNOB FOR OLD MSGS Old Message Summary The display below sho...

Page 55: ...new messages become old messages and the MSG light stops flashing but remains lighted while there are old messages Countdown Timer Expired 3 To view old messages turn the Large knob to display the Old Message Summary page 2 Old Messages Turn Large Knob For New Msgs 4 Turn the Small knob to scroll through the old messages If new message conditions occur while in MSG mode the MSG annunciator begins ...

Page 56: ... not receiving responses to commands sent to the GPS sensor this message is generated This problem indicates that the GPS is not receiving NMC transmissions and cannot be used for IFR flight You should switch to Loran if available for IFR flight It becomes an old message after viewing and remains an old message even if the condition does not persist Service is required TX TO GPS FAILED GPS NOT FOR...

Page 57: ...rm a warning is generated and NAV data will be flagged as invalid The top line indicates the current flight phase either Approach Terminal or En Route which directly affects RAIM alarm requirements It becomes an old message after viewing If the Abort Approach message is given you must abort the approach by pressing the OBS HOLD button and exercise the missed approach procedure ABORT APPROACH GPS R...

Page 58: ...l occur Parallel Track will be disabled when approach operation is enabled Pressing ENT will enable approach approach transition operation turn the APPRCH indicator solid lock on the GPS sensor and display a barometric alert PUSH ENT TO ENABLE APPROACH If Loran position inputs are available the bottom line of the message will also display and Lock on GPS indicating that automatic sensor selection ...

Page 59: ...s ENT to continue normal NMC operation The default value first displayed is the last entered altimeter reading ENTER LOCAL ALTIMETER SETTING 29 94 Altitude Inputs with Baro Correction If the altitude inputs are already baro corrected the following screen reminds the user to update the remote device altimeter setting CHECK LOCAL ALTIMETER SETTING No Altitude Inputs If the NMC is not receiving altit...

Page 60: ...tion for the FAF and the MAP If those predictions are not completed by the FAF then the following warning is given This does not become an old message after viewing You must abort the approach by pressing the OBS HOLD button and exercise the missed approach procedure ABORT APPROACH RAIM PREDICT NOT COMPLETED BY FAF MCLS Position Sensor Signal Failure When the in use MCLS Multi Chain Loran Sensor t...

Page 61: ...e in use Loran position sensor is greater than or equal to 2 8 nm this message is generated It becomes an old message after viewing If the EPE cannot be calculated this message is still generated and the EPE value is dashed ENROUTE LORAN ACCURACY ERROR EPE 02 9 Terminal Loran EPE Warning During terminal mode within 30 nm of departure or destination airport when the estimated position error EPE for...

Page 62: ... function will still be armed The message below will display when entering terminal airspace It will not become an old message after being read WITHIN 30NM OF DESTINATION OCEANIC CANCELED Themessagebelowwilldisplaywhentheaircraft saltitudedropsbelow the Oceanic Activation Altitude Pressing ENT will cause the NMC to change the flight phase to enroute Pressing any other button will cause the NMC to ...

Page 63: ...te or verify that it has excluded the faulty satellite This message becomes an Old message after being acknowledged and remains until the RAIM alarm condition ends NAV will be flagged but the NMC will continue to provide cross track information OCEANIC GPS RAIM ALARM POSITION ERROR MCLS Station Warnings The display below shows the Loran signals are unusable In this example MCLS 1 has a low SNR Sig...

Page 64: ...It does not become an old message after viewing Altitude Encoder Communications Failure F ADS Communications Failure Warning A five second transmission delay from the Fuel Air Data Sensor causes a communication failure message to be generated It does not become an old message after viewing Fuel Air Data Communications Failure F ADS Transducer Failure Warning The display below shows that the Fuel A...

Page 65: ...0 MIN CHECK Tanks Arrival at Hold Buffer Altitude Message The display below shows arrival at the Target Hold Buffer Altitude In the example below the Target Hold Altitude is 2 000 feet The Target Hold Altitude is the altitude you want to descend ascend to and is adjusted in NAV mode The Target Hold Buffer is the distance above below the Target Hold Altitude at which you want this message to activa...

Page 66: ...s 2 000 feet This message is immediately reset after viewing it does not become an old message after viewing Arrival At 2000ft Target Descent Altitude Arrival at Waypoint Messages The arrival message is generated when you are within 36 seconds of arrival at the current TO waypoint It is cleared after viewing The arrival condition will also go away without viewing the message after crossing the ang...

Page 67: ...ist TO Waypoint Sequence When a waypoint sequence occurs and you have not viewed the arrival alert one of the following alerts are provided Normal Sequence The alert is only provided if traveling faster than 5 knots This reduces the chance of nuisance alerts after power up The new waypoint identifier bearing and desired track are provided Sequence Alert New Wpt SLE BRG073 DTK069 DME Arc Sequence T...

Page 68: ...In the example below 3 User waypoints or comments were deleted This message clears after it is viewed User Database Memory Loss 3 Deleted Flight Plan Memory Corrupted Message The display below shows the memory storing one or more flight plans is corrupted and the affected flight plans were deleted The NMC tests all flight plans each time the unit is turned on In the example below 2 flight plans we...

Page 69: ... display below shows manual magnetic variation is in use If a valid data card is not properly inserted the magnetic variation must be entered manually during the power up sequence Manual magnetic variation may also be entered in System mode It becomes an old message after being viewed Using Manual Mag Var 13 E Battery Voltage The NMC checks the battery voltages every 15 seconds Low Battery Voltage...

Page 70: ...igh battery voltage message is generated when the NMC detects a high battery voltage The unit must be returned for service Continued operation is not recommended It becomes an old message after being viewed Internal Battery Failure Turn Off Unit Needs Srvc Countdown Timer Expired Message The display below shows the active countdown timer has expired The countdown timer is set in NAV mode The messa...

Page 71: ...essage after being viewed Flight Plan Transfer To NMC Failed RAM Data card Is Full This message is generated when an installed RAM data card cannot be written to because the RAM data region is full It does not become an old message after being viewed Note This message is only available for the 2101 NMC with a RAM data card installed RAM Datacard Is Full Flightdata Storage Complete 57 Operations Me...

Page 72: ...n of the SUA The top line of the display shows the ceiling The middle line shows the floor and the bottom line shows the bearing approximate relative bearing and the distance to the nearest edge of the SUA In this example the ceiling is 10 000 ft the floor is the surface ground the bearing is 154o the SUA is straight ahead and the distance is 8 9 nm CEIL 10000 MSL FLOOR GROUND BRG 154 8 9NM 3 Pres...

Page 73: ...e number of minutes before entering an SUA you want to be alerted may be edited in SYS mode WITHIN 10 MIN OF GABBS CENTRAL MOA SUA Close Message The display below shows you are within 2 nm of an SUA in this example the SUNDANCE MOA The number of miles from an SUA you want to be alerted may be edited in SYS mode WITHIN 2 NM OF SUNDANCE MOA SUA Close Altitude Message The display below shows you are ...

Page 74: ...Inside SUA Message The display below shows you are inside an SUA in this example the SAN DIEGO Class B airspace Inside of SAN DIEGO CLASS B 60 Message Displays Operations ...

Page 75: ...ctive flight plan without exiting NAV mode by using the From To Next page Altitude Assist features included in NAV mode allow the NMC to monitor your altitude while en route and guide you in descent or ascent The system must include an altitude encoder or a F ADS Fuel Air Data Sensor to function NAV mode also allows you to avoid obstacles or weather by entering a parallel course Position sensor se...

Page 76: ...T SETTINGS When ARINC 429 Air Data Sensor is Installed Displays Barometric Altitude Corrected For Local Altimeter Setting Not Available when ARINC 429 Air Data Sensor Is Installed Page displays only when Oceanic is enabled DME ARC ASSIST RAIM PREDICTION PRN01 PRN02 PRN32 PARALLEL TRACK MANUAL AIR SPEED LAST STANDBY SENSOR FIRST STANDBY SENSOR FROM TO NEXT Distance to Waypoint FROM TO NEXT ETA to W...

Page 77: ...le dot bar indicates that CDI sensitivity is set to 0 3 nm full scale per side The bar always extends towards the desired course steer in the direction of the bar The manual sensitivity of the CDI may be set to 0 3 1 0 or 5 0 nm full scale per side The table appearing at the top of the next page describes the sensitivity choices for the CDI bar The airplane symbol is used as a To From indicator wh...

Page 78: ...ation waypoint and ETA If the ETA changes by more than 10 minutes the NMC automatically re performs the RAIM prediction The user can perform a RAIM prediction for any waypoint in the data base for any date and time from 1980 to 2079 Manual RAIM prediction provides a RAIM availability indication using approach operation RAIM alarm requirements 0 3 nm alarm limit within 15 minutes of the provided da...

Page 79: ...o highlight choices on the second line and then press ENT to select a waypoint from the database using the Large and Small knobs Primary Oceanic Status Page When Primary Oceanic is enabled status will be displayed on the Oceanic status pages To display the Oceanic status pages 1 Press the NAV button 2 Rotate the Large knob to display the oceanic status page The page will display one of the followi...

Page 80: ... sucessful exclusion occurs the NMC will display the following message indicates a satellite PRN number POSITION UPDATED FOR FAILED GPS SV Altitude Assist Altimeter Setting Display ALTITUDE ASSIST LOCAL ALTIMETER SETTING 29 92 If an ARINC 429 Air Data Sensor is installed in the system the Altitude Assist Altimeter Setting Display shows automatically corrected barometric pressure altitude No altime...

Page 81: ...e the Latitude Longitude position and the EPE Estimated Position Error GPS Sensors do not display an EPE In this example the In Use position sensor is Loran 1 and the present Lat Lon is 45 27 45 N 122 51 32 W Position is displayed in degrees minutes and hundredths of a minute Seconds of Lat Lon are not used The EPE is 0 7 nm If position has not been calculated the top line of the display reads Las...

Page 82: ... NEXT waypoint i e the waypoint you will be flying to after arriving at the TO waypoint and the database that stores the waypoint After arriving at the To waypoint the waypoints will sequence and the NEXT waypoint will become the TO waypoint In this example the FROM waypoint is airport ARPT SLE the TO waypoint is the PDX VOR and the NEXT waypoint is airport HIO For procedural information see NAV M...

Page 83: ...3 0 51nm à TRK 128 TAE 000 ETE AAB 01 23 0 51nm à FT01 09 147KTS ETE AAB 01 23 0 51nm à 128 TRK132 ETE AAB 01 23 0 51nm à 14 07 UTC ETA AAB 15 30 MIN SAFEA 5000 ENRTSAFEA 9000 BARO ALT 6000FT 100 ABOVE HOLD 00 11 TO DESCENT 69 Operations NAV Displays ...

Page 84: ...se items are available when you customize your navigation displays The BRG Bearing Nav item depicted below shows the magnetic bearing to the To waypoint from your present location In this example the bearing is 253o BRG 253 The distance Nav items depicted below show the distance in nautical miles to the To waypoint from your present location In this example the distance is 116 nautical miles 116NM...

Page 85: ...t Timer Trigger Speed FT00 32 The Current To Waypoint Nav item is depicted below SLE The Blank Field Nav item is depicted below Selecting this item will result in a blank field display at the highlighted entry location on the Nav page being programmed _ _ _ _ _ _ Sixteen Character Nav Items The following navigation display items use a total of sixteen characters an entire display line The CDI Cour...

Page 86: ...n the From and To waypoints The desired track is the magnetic bearing to the To waypoint from the From waypoint In this example the DTK is 235 and the distance between the From and To waypoints is 97 8 nm Distance can also be displayed in kilometers Dtk 235 97 8NM The Minimum Safe Altitude MSA Nav item is depicted below The MSA is the elevation of the highest obstruction near the aircraft with 1 0...

Page 87: ...ning your descent This item is used only when auto descent monitoring is active If Auto Descent monitoring is not active is displayed instead of a time When Auto Descent begins this item is replaced by the Glide Path Deviation item or the Feet Over End Altitudeitem Inthisexample thetimetodescentis1hourand9minutes 01 09 To Descent The Glide Path Deviation Nav item is depicted below This item shows ...

Page 88: ...he Fuel Remaining At the Current To waypoint Nav item is shown below This value is calculated using the current burn rates the amount of fuel in the regular non reserve fuel tanks and the distance remaining to the waypoint The units of fuel may be displayed in USG United States Gallons IMG Imperial Gallons L Liters or LBS Pounds depending on the fuel units selected in the System Mode System Info s...

Page 89: ...ing Nav item is depicted next This item takes into account wind factors magnetic variation and the desired track to calculate the heading necessary to maintain the desired track Requires F ADS or ARINC 429 Air Data sensor and XYZ heading input Desired Hdg 153 The Magnetic Heading Nav item is shown next Requires F ADS or ARINC 429 Air Data sensor and XYZ heading input MAG HEADING 127 The Wind Speed...

Page 90: ...tem which factors in wind speed relative to a 0 knot ground speed is depicted next In this example the True Air Temperature is 10 centigrade Requires F ADS TrueAir 10 C The True Air Speed Nav item which displays the air speed of the plane after correction for altitude and temperature factors is displayed next RequiresF ADSorARINC429Air DatasensorandXYZheadinginput TruAirSp 153kts The Indicated Air...

Page 91: ...m the RAIM prediction Press the SEL button and use the Large and Small knobs to select and change fields NOTE The NMC will automatically reinclude satellites whose out of service time has elapsed PRN01 TO IGNORE SAT PRESS SEL Clear RAIM Predict Ignore List The user has the option to clear the RPIL In the NAV mode use the Large knob to display the main RAIM prediction page Press SEL to display Sele...

Page 92: ...NOTES 78 NAV Displays Operations ...

Page 93: ...hrough the Nav Information displays Starting Stopping Auto Nav Scroll This feature automatically displays navigation screens sequentially for a specified amount of time from 1 to 9 seconds per display To select the amount of time each screen is displayed refer to Operations Setting Auto Nav Scroll Time Action Explanation 1 In NAV mode while viewing any information page press ENT to start Auto Nav ...

Page 94: ...y the Position Summary page This page displays the position information from the position sensor in use LORAN1 IN USE 45 27 45N EPE 122 51 32W 1 7 NAV 2 Turn the Small knob to display the position provided by each sensor Only one sensor is In Use and the rest are on Standby LORAN2 STANDBY 45 27 46N EPE 122 51 31W 2 9 NAV If a position sensor is no longer sending valid information the Last Valid Po...

Page 95: ... tochoose the InUse position sensor Action Explanation 1 In NAV mode turn the Large knob to display the Position Summary page This page displays the position latitude longitude determined by the In Use sensor LORAN1 IN USE A 45 27 45N EPE 122 51 32w 1 7 NAV 2 Turn the Small knob to display the position sensor you want to use LORAN2 STANDBY 45 27 46N EPE 122 51 31W 2 9 NAV 81 Operations Nav Mode Pr...

Page 96: ...sition sensors installed on the Navnet network to use for navigation Automatic Position Sensor Selection allows the NMC to automatically choose which position sensor is being used for navigation Manual Position Sensor Selection disables the automatic option and allows you to choose your position sensor While using Manual Position Sensor Selection the NMC will not choose a different position sensor...

Page 97: ...d described above it can also be canceled by manually selecting a different position sensor as follows Action Explanation 1 In NAV mode turn the Large knob to display the In Use Position Sensor page The A on the top right of the display indicates that Automatic Position Sensor Selection is in use LORAN1 IN USE A 44 55 30N EPE 123 00 08W 0 0 NAV 2 Turn the Small knob to display the Position Sensor ...

Page 98: ...vailabilityforanywaypoint date andtimecontainedbythedatabase 1 In NAV mode turn the Large knob to the RAIM Prediction page RAIM UNKNOWN AT SLE ARPT 02APR99 12 56 2 Press SEL to begin RAIM prediction editing PREDICT RAIM AT SLE ARPT 01MAY99 17 56 3 Turn the Large knob to highlight the field that you want to change waypoint month day year or time RAIM UNKNOWN SELECT WAYPOINT 01MAY99 17 56 84 Nav Mod...

Page 99: ...ination compute ETA and start RAIM prediction Editing RAIM Predict Ignore List The Apollo NMC allows the user to specify satellite outages for RAIM predictions using information presented in NOTAMs or NANUs 1 From the RAIM prediction page rotate the Small knob to the desired satellite page Press the SEL button 2 The screen below will initially display with the hours field flashing Rotate the Small...

Page 100: ...OF SERVICE Clear RAIM Predict Ignore List The user has the option to clear the RPIL available from the main RAIM prediction page 1 Press SEL to display Select Waypoint Use the Large knob to display Predict RAIM on the top line PREDICT RAIM AT SLE ARPT 01MAY99 12 56 2 Use the Small knob to display Clr Ignore List Press ENT to clear the RPIL This will make all satellites available for future RAIM pr...

Page 101: ... is automatically selected as the current sensor for altitude data No other altitude sensor may be selected Action Explanation 1 In NAV mode turn the Large knob to display the Altitude Assist page ALTITUDE ASSIST LOCAL ALTIMETER SETTING 29 92 NAV If an ARINC 429 Air Data sensor is installed in the system the Altitude Assist page appears as shown below ALTITUDE ASSIST BARO ALT 1000FT 2 Turn the Sma...

Page 102: ... Large knob to choose the desired sensor CURRENT SENSOR ENCODER 1020FT F ADS 1021FT NAV 4 Press ENT to enter the sensor choice CURRENT SENSOR ENCODER 1020FT F ADS 1021FT NAV 88 Nav Mode Procedures Operations ENT ...

Page 103: ...r Data sensor is installed in the system Action Explanation 1 In NAV mode turn the Large knob to display the Altitude Assist page ALTITUDE ASSIST LOCAL ALTIMETER SETTING 29 92 NAV 2 Pressing SEL activates editing and the current barometric pressure setting flashes ALTITUDE ASSIST LOCAL ALTIMETER SETTING 29 92 NAV 3 Turn the Small knob to adjust the barometric pressure Press ENT to enter the settin...

Page 104: ...Hold Altitude and the Buffer Altitude Flow Chart Action Explanation 1 In NAV mode turn the Large knob to display the Altitude Assist page If an ARINC 429 Air Data sensor is installed this page shows barometric altitude not the local altimeter setting ALTITUDE ASSIST LOCAL ALTIMETER SETTING 29 92 NAV 90 Nav Mode Procedures Operations NAV PRESS TO ACTIVATE EDITING THE ALTITUDE ASSIST PAGE TURN TO DI...

Page 105: ...s chosen in increments of 10 ft Pressing ENT enters the displayed values HOLD ALT 13600FT BUFFER 350FT ENT TO HOLD ALT NAV Starting Stopping Altitude Hold Altitude Assist features require the system include a F ADS or an altitude encoder sensor The following procedure is used to start or stop the Altitude Hold feature When active Altitude Hold alerts you with a message when you have ascended desce...

Page 106: ... ALTIMETER SETTING 29 92 NAV 2 Turn the Small knob to display the Hold Altitude page HOLD ALT 15000FT BUFFER 1000FT ENT TO HOLD ALT NAV 3 Pressing ENT activates Altitude Hold Pressing ENT again deactivates the feature HOLD ALT 15000FT BUFFER 1000FT ENT TO CANCEL NAV 92 Nav Mode Procedures Operations ENT NAV ENT ...

Page 107: ...ield displays information indicating how much time remains before you should begin Auto Descent and once Auto Descent begins whether you are above or below your intended Glide Path Glide Path data may also be output to an optional Vertical Deviation Indicator Each time you begin to edit the Auto Descent values the End Altitude is automatically reset to 1 000 feet over the altitude of the desired A...

Page 108: ...Setting Editing Auto Descent Values continued Flow Chart 94 Nav Mode Procedures Operations ...

Page 109: ...ltitude this page shows barometric altitude not the local altimeter setting ALTITUDE ASSIST LOCAL ALTIMETER SETTING 29 92 NAV 2 While viewing either the Auto Descent or End Alt page in the Altitude Assist function press SEL The Offset Distance value will flash Turn the SMALL knob to change the Descent Offset Distance value End 0nm before PDX at 1027 500 min 200kts NAV 3 Turn the LARGE knob to the ...

Page 110: ...ue The default value is 1000 ft above the airport elevation 5 Turn the SMALL knob to the Auto Descent page if necessary Your recommended glide slope and ending altitude are shown Press ENTER to activate ready Auto Descent Press ENTER again to cancel it 96 Nav Mode Procedures Operations ENT ...

Page 111: ...Notes 97 Operations Nav Mode Procedures ...

Page 112: ...cent Values Action Explanation 1 In NAV mode turn the Large knob to display the Altitude Assist page If an ARINC 429 Air Data sensor is installed this page shows barometric altitude not the local altimeter setting ALTITUDE ASSIST LOCAL ALTIMETER SETTING 29 92 NAV 2 Turn the Small knob to display the Auto Descent page Based on the descent rate defined in the preceding procedure a descent angle in d...

Page 113: ...Offset page The current status is displayed on the right side of the middle line There are two status options available In Use and Standby In this example the status is Standby meaning the feature is not in use PARALLEL COURSE OFFSET STANDBY LEFT 0 0NM NAV 2 Pressing SEL activates editing and a prompt for the alternate status option in this example Use flashes The current offset direction and valu...

Page 114: ...alue flash Turn the Small knob to choose the amount of the offset The offset is chosen in tenths of a mile up to a maximum of 20 0 nm PARALLEL COURSE OFFSET STANDBY RIGHT 2 2NM NAV 5 Turn the Large knob to make the status flash and press ENT to enter the status Anytime you want to change the status without adjusting the direction or amount of the offset simply press SEL then ENT PARALLEL COURSE OF...

Page 115: ...d True Wind Direction when these Nav items are selected See the section on Programmable Nav pages on page and page for details on Wind information This function is only available when a F ADC or the ARINC 561 board are NOT installed 1 In NAV mode turn the Large knob to display the Manual Air Speed page MANUAL AIRSPEED SELECTION 0KTS NAV 2 Turn the Small knob to choose the desired values 101 Operat...

Page 116: ...he Countdown Timer Setting Starting the Countdown Timer The following procedure isused toset and start the countdown timer Action Explanation 1 In NAV mode turn the Large knob to display the Countdown Timer page COUNTDOWN TIMER 00 03 00 NAV 2 Pressing SEL activates editing and the minutes value flashes Turn the Small knob to adjust the minutes value COUNTDOWN TIMER 00 04 00 NAV 3 Use the Large and...

Page 117: ...NDB n and VOR v The waypoint type symbol will not be shown if one of the following occurs the waypoint identifier is unknown it is an approach waypoint that is not one of the four used types it is a User waypoint the waypoint is not recognized by the current data card s database or the data card has been removed aSLE ____nm aPDX 43nm aSEA 154nm NAV Waypoint ETE Page This page displays the cumulati...

Page 118: ...ing at the current To waypoint These waypoints are contained in the Active flight plan Using the From To Next page these waypoints may be changed or deleted or a new waypoint may be inserted These modifications are made to the Active flight plan and do not affect the stored flight plan that was activated Also the Active flight plan may be put on Hold which stops the flight plan waypoints from sequ...

Page 119: ...POSITION THE TURN THE WAYPOINT RETRIEVER PRESS TO ACTIVATE ENT IS THE DESIRED WAYPOINT IDENTIFIER DISPLAYED YES NO YES DATABASE TYPE FLASH TURN TO MAKE THE TURN TO DISPLAY DESIRED DATABASE TYPE TURN TO DISPLAY THE DESIRED CHARACTER IS THE DESIRED WAYPOINT IDENTIFIER DISPLAYED PRESS SEL PRESS SEL TURN TO MAKE THE IDENTIFIER CHARACTERS FLASH TURN TO MAKE THE IDENTIFIER CHARACTER TO CHANGE FLASH NO ...

Page 120: ...splayed INS Insert appears instead CHG is used to replace the waypoint and INS is used to add a waypoint DEL Delete will remove the waypoint FROM EUG ARPT TO CVO VOR NEXT CHG ARPT NAV 3 Turn the Large knob to choose the waypoint to change or the location where a new waypoint is to be inserted To insert a waypoint turn the Small knob to display INS HOLD maybechosentoreplace TO HOLD is used to place...

Page 121: ...y the desired waypoint Use the Waypoint Retriever to display the desired waypoint The Waypoint Retriever is described in Operations Retrieving a Waypoint AIRPORT S12 ALBANY CITY OR USA NAV 6 Press ENT to enter the displayed waypoint into the Active flight plan FROM EUG ARPT TO S12 VOR NEXT CVO ARPT NAV 105 Operations NAV Mode Procedures ENT ENT ...

Page 122: ...ion Explanation 1 In NAV mode turn the Large knob to display the From To Next page The current From To and Next identifiers are displayed Blank lines appear in spaces where there are no waypoints FROM EUG ARPT TO CVO VOR NEXT SLE ARPT NAV 2 Pressing SEL activates editing CHG Change appears in place of the Next waypoint If no Next waypoint is displayed INS Insert appears FROM EUG ARPT TO CVO VOR NE...

Page 123: ...aypoints and information on User waypoints are stored in the Navigation Management Computer NMC not on the data card The Waypoint Retriever is used to access waypoints Use of the Waypoint Retriever is consistent in all six modes and is used whenever you need to display a waypoint User waypoints are created in DB mode by directly entering the Latitude Longitude creating the waypoint at the location...

Page 124: ...COMMENT ENT ENT MODIFY USER WAYPOINT USER WPT EDIT SCREEN RETRIEVER WAYPOINT MODIFY HOME PAGE ENT WAYPOINT RETRIEVER ACCESS DATABASE ENT CREATE LAT LON USER WPT USER WPT EDIT SCREEN ENT ENT CREATE RAD DIST USER WPT REFERENCE WAYPOINT RETRIEVER USER WPT EDIT SCREEN ENT DELETE USER WAYPOINT WAYPOINT RETRIEVER DELETE COMMENT DELETION WAYPOINT ...

Page 125: ... Airport Database These databases drawers contain Airports A folder is maintained for every public use airport located in the datacard coverage area Additional information such as available runways and frequencies is included for each waypoint VOR NDB Intersection Databases These databases drawers contain a folder for every VOR NDB and Intersection located in the datacard coverage area Additional ...

Page 126: ...on approach data User waypoints and waypoint comments you enter are stored in the NMC Database information may include Airport Database Identifier City State and Country Facility Name Bearing from your present position Distance from your present position Any special use airspace area such as a Class B airspace the waypoint is located in or beneath Waypoint Elevation Availability of Avgas Jet fuel ...

Page 127: ... or NDB Bearing from your from your present position Distance from your present position Latitude Longitude User Database Identifier Bearing from your your present position Distance from your present position User defined runway length Waypoint Latitude Longitude 111 Operations Databases ...

Page 128: ...e is Portland International located in Oregon USA PPOS TO PDX BEARING 005 DISTANCE 44 3NM Present position to PDX Bearing To PDX is 005o Distance to PDX is 44 3 nm PDX AIRPORT PUBLIC ELEV 27FT Portland airport is public use Elevation is 27 ft above sea level PDX AIRPORT AVAILABLE FUEL AVGAS JET Portland Airport Fuel available is Aviation Gas and Jet Fuel PDX ATIS 126 35 UNIC 122 95 TWR 118 70 ATIS...

Page 129: ...0 APPR 133 00 Approach frequency is 118 10 Approach frequency is 126 90 Approach frequency is 133 00 PDX DEP 118 10 DEP 133 00 Departure frequency is 118 10 Departure frequency is 133 00 PDX ILS 109 90 RUNWAY 10R ILS frequency is 109 90 Runway 10R PDX ILS 111 30 RUNWAY 28R ILS frequency is 111 30 Runway 28R PDX LOC 109 90 RUNWAY 28R LOC frequency is 108 90 Runway 20 113 Operations Databases ...

Page 130: ... runway is lighted PDX 02 20 7000FT HARD LOC LIGHTED PDX runway 02 20 7000 feet long with a hard surface and LOC The runway is lighted PDX AIRPORT LAT 45 35 33N LON 122 35 78W PDX latitude longitude in degrees minutes and hundredths of minutes 45o 35 33 North 122o 35 78 West VERY RAINY DURING WINTER BRING BOOTS Waypoint comment has been entered PDX AIRPORT PORTLAND CITY OR USA PDX is an airport lo...

Page 131: ... in the data card slot Once the waypoint is displayed If you want to navigate directly to the waypoint press DIRECT TO then NAV To display information about the waypoint press INFO and turn the Small knob to view the information displays To exit the information function press INFO again The Mode annunciator flashes while the information function is active To exit without entering any changes press...

Page 132: ... Access Database page ACCESS DATABASE PRESS ENT DB 2 Pressing ENT activates the Waypoint Retriever AIRPORT AAP HOUSTON CITY TX USA DB 3 Turn the Large knob to make the database type flash Turn the Small knob to display the desired database VOR ABA ARUBA FACIL ANTILL DB 116 DB Mode Procedures Operations DB ENT ...

Page 133: ...that exist VOR DAG DAGGET FACIL CA USA DB 5 Turn the Large knob to make the next character in the waypoint identifier flash Turn the Small knob to choose the character Repeat to choose the remaining character s in the identifier The desired waypoint is displayed VOR DEN DENVER FACIL CO USA DB Note If you see DUP on the 3rd line there are duplicate facilities with the same identifier Press SEL and ...

Page 134: ...or the facility name McNary Fld VORs NDBs and Intersections do not have city names Flow Chart 118 DB Mode Procedures Operations YES NO DESIRED CHARACTER TURN TO CHOOSE IS CITY FACILITY NAME CORRECT PRESS SEL THE CITY FACIL NAME FLASH TURN TO MAKE TURN TO MAKE CHARACTER TO CHANGE FLASH TURN TO DISPLAY ACCESS DATABASE PAGE PRESS DB PRESS THE CITY FACIL FLASH TURN TO MAKE PRESS SEL CITY NAME OR FACIL...

Page 135: ...NT DB 2 Pressing ENT activates the Waypoint Retriever VOR DEN DENVER FACIL CO USA DB 3 Turn the Large knob to make the database type flash Turn the Small knob to display the desired database AIRPORT AAP HOUSTON CITY TX USA DB 4 Turn the Large knob to make the Facility City designator flash AIRPORT AAP HOUSTON CITY TX USA DB 119 Operations DB Mode Procedures DB ENT ...

Page 136: ... will flash Turn the Small knob to scroll through all items similar to the selected characters For instance if you had selected M for the first character and E as the second character turning the Small knob will scroll through all names that start with ME 7 Turn the Large knob to make the next character flash Turn the Small knob to choose the character Repeat to choose the remaining character s in...

Page 137: ...INFO displays information about the To waypoint for the active leg In EMRG mode or DB mode pressing INFO displays information about the displayed waypoint When the INFO function is active you may scroll through the available information displays on a waypoint by turning the Small knob The mode annunciator flashes when the INFO function is active In all cases pressing INFO again exits the INFO func...

Page 138: ...NMC stores a maximum of 200 comments Flow Chart 122 DB Mode Procedures Operations DISPLAY THE DESIRED WAYPOINT PRESS INFO PRESS TO EXIT THE INFORMATION FUNCTION INFO TURN TO DISPLAY THE WAYPOINT COMMENT PRESS TO ACTIVATE EDITING SEL IS THE DESIRED WAYPOINT COMMENT DISPLAYED PRESS TO SAVE THE WAYPOINT COMMENT ENT TURN TO DISPLAY THE DESIRED CHARACTER CHARACTER SPACE TO CHANGE FLASH TO MAKE THE CHAR...

Page 139: ...displayed in DB mode AIRPORT PDX PORTLAND CITY OR USA DB 2 Pressing INFO activates the information function PDX AIRPORT PORTLAND INTL FACIL OR USA DB 3 Turn the Small knob to display the waypoint comment page If a comment on the waypoint has previously been entered the comment appears instead of the display below WAYPOINT COMMENT PRESS SEL DB 123 Operations DB Mode Procedures INFO ...

Page 140: ...blank display __ DB If the NMC is already storing the maximum of 200 comments the display below appears You must delete a comment to make room for a new comment WAYPOINT COMMENT NO MORE COMMENTS DB 5 Turn the Large knob to move the cursor and turn the Small knob to choose characters NUMEROUS BRIDGES AND CABLES CROSS COLUMBIA RIVER DB 6 Pressing ENT saves the waypoint comment Press INFO to exit the...

Page 141: ...r of waypoint comments currently entered DELETE WAYPOINT COMMENT 100 USED PRESS ENT DB 2 Pressing ENT activates the Delete Waypoint Comment function The top line shows the identifier and database of the associated waypoint The middle and bottom lines display the first 2 lines of the waypoint comment AVX AIRPORT GREAT PLACE TO SCUBA DIVE DB 3 Turn the Small knob to scroll to the comment to be delet...

Page 142: ...ressing ENT deletes the displayed waypoint comment Pressing any mode button instead of ENT exits the Delete Waypoint Comment function without deleting a comment DELETE WAYPOINT COMMENT 99 USED PRESS ENT DB 126 DB Mode Procedures Operations ENT ...

Page 143: ...Waypoint on page 115 Creating a User Waypoint by Latitude Longitude The following procedure is used to create a User waypoint by entering latitude longitude coordinates If there are already 500 User waypoints you must delete a previously entered User waypoint to make room for a new waypoint For more information refer to Operations Deleting a User Waypoint Flow Chart 127 Operations DB Mode Procedur...

Page 144: ... below appears and you must delete a User waypoint before you may create a new waypoint CREATE USER WPT BY LAT LON DATABASE FULL DB 2 Pressing the ENT button displays an open User waypoint page The waypoint identifier defaults to the next unused numerical identifier from 000 to 499 The latitude and longitude default to the present position and the runway length defaults to 0000 005 USER 44 54 58N ...

Page 145: ...e flash Repeat to edit the identifier Latitude longitude and the runway length The identifier may contain up to six characters When a waypoint is created at the location of the waypoint it is not necessary to edit the position coordinates Latitude Longitude HOME USER 44 54 58N RWLEN 123 00 08W 2800 DB 4 Press ENT to store the waypoint in memory CREATE USER WPT BY LAT LON PRESS ENT DB Ifaduplicatei...

Page 146: ...existing waypoint This reference waypoint may be in any database including the User database Do not chain radial distance waypoints If you create a waypoint by radial distance using another radial distance waypoint as the reference point position errors caused by rounding or conversion are cumulative 130 DB Mode Procedures Operations ...

Page 147: ...ENT DB If the maximum of 500 User waypoints already exist the display below appears and you must delete a User waypoint before you may create a new waypoint CREATE USER WPT BY RADIAL DIST PRESS ENT DB 2 Pressing ENT displays the Reference Waypoint Entry page If the desired reference waypoint identifier is displayed skip to step 8 REF WPT AAP 000 0 000 0NM DB 131 Operations DB Mode Procedures DB EN...

Page 148: ...EF WPT CHG 000 0 000 0NM DB 4 Pressing ENT activates the Waypoint Retriever AIRPORT AAP HOUSTON CITY TX USA DB 5 Display the desired waypoint Use the Waypoint Retriever to display the desired waypoint The Waypoint Retriever is described in Operations Retrieving a Waypoint AIRPORT ONP NEWPORT CITY OR USA DB 132 DB Mode Procedures Operations ENT ...

Page 149: ...t radial value number REF WPT ONP 100 0 000 0NM DB 9 Use the Large and Small knobs to choose the remaining numbers in the radial and distance values REF WPT ONP 165 0 011 1NM DB 10 Pressing ENT enters the displayed Radial Distance values The NMC calculates the latitude longitude and displays the User Waypoint Edit page 006 USER 44 23 72N RWLEN 124 04 21W 0000 DB 133 Operations DB Mode Procedures E...

Page 150: ...nway length The identifier may contain a maximum of six characters ALSEA USER 44 23 72N RWLEN 124 04 21W 1000 DB 12 Press ENT to store the waypoint in memory CREATE USER WPT BY RADIAN DIST PRESS ENT DB If a duplicate identifier is entered the display below appears for approximately 3 seconds The NMC then displays the waypoint editing page so you can change the identifier DUPLICATE USER WAYPOINT ID...

Page 151: ... 135 Operations DB Mode Procedures PRESS DB THE MODIFY USER WPT PAGE TURN TO DISPLAY ENT PRESS ENT PRESS DESIRED USER WAYPOINT TURN TO DISPLAY THE ENT PRESS CHARACTER TO CHANGE FLASH TURN TO MAKE THE DESIRED CHARACTER TURN TO DISPLAY THE IS THE WAYPOINT INFORMATION CORRECT YES NO DOES THE WAYPOINT HAVE A DUPLICATE IDENTIFIER NO THE WAYPOINT INFORMATION IS UPDATED YES ...

Page 152: ...ay below appears MODIFY USER WPT DATABASE EMPTY DB 2 The NMC displays the Find Waypoint to Modify page Turn the Small knob to display the desired waypoint If desired you may press SEL to activate character editing to display the waypoint however this is generally unnecessary unless there are a large number of User waypoints FIND WPT TO MOD HOME USER PRESS ENT DB 136 DB Mode Procedures Operations D...

Page 153: ...flight plan it cannot be modified and the display below appears for approximately 3 seconds The Find Waypoint to Modify page is then displayed WAYPOINT IS IN ACTIVE PLAN CANNOT MODIFY DB 4 Use the Large and Small knobs as necessary to edit the identifier Latitude Longitude and runway length HOME USER 44 54 58N RWLEN 123 00 10W 2300 DB 137 Operations DB Mode Procedures ENT ...

Page 154: ...After 3 seconds or if the waypoint is not in a flight plan the display below appears MODIFY USER WPT PRESS ENT DB If a duplicate identifier is entered the display below appears for approximately 3 seconds The NMC then returns to the waypoint editing page so you can change the identifier using the Small and Large knobs DUPLICATE USER WAYPOINT IDENT NOT ALLOWED DB 138 DB Mode Procedures Operations E...

Page 155: ...ENT DB If there are no User waypoints stored the display below appears DELETE USER WPT DATABASE EMPTY DB 2 The NMC displays the Find Waypoint to Delete page Turn the Small knob to display the desired waypoint If desired you may press SEL to activate character editing to display the waypoint however this is generally unnecessary unless there are a large number of User waypoints FIND WPT TO MOD HOME...

Page 156: ...ut deleting a waypoint DELETE USER WPT PRESS ENT DB The NMC will not delete any User waypoint included in a flight plan If this is attempted the following display appears for approximately 3 seconds The NMC then displays the Find Waypoint to Delete page WAYPOINT IS IN A FLIGHT PLAN CANNOT DELETE DB 140 DB Mode Procedures Operations ENT ...

Page 157: ...m and To waypoints One asterisk next to the leg number means that the displayed leg is in the Active flight plan Two asterisks means that the displayed leg shows the current From and To waypoints which are being used for navigation The third line of the Flight Plan Leg pages shows Leg Information This information may be customized to display one of several types of information related to the displ...

Page 158: ...e 142 Flight Plan FPL Mode Operations ACTIVE FLIGHT PLAN INFO HOME PAGE PLAN COMMENT LEG 2 UP TO LEG 20 LEG 1 PLAN COMMENT INFO LEG 2 LEG 1 UP TO LEG 20 PLAN COMMENT INFO LEG 2 LEG 1 UP TO LEG 20 CREATE FLIGHT PLAN INACTIVE FLIGHT PLAN UP TO 29 INACTIVE FLIGHT PLANS ...

Page 159: ...t plan above is named PDXTOSLE and the total distance of all legs in the flight plan is 50 8 nautical miles The flight status is Inactive not currently being used for navigation Action Explanation Press FPL to enter FLIGHT PLAN mode then rotate the Large knob to display the desired Flight Plan Summary page Turn the Small knob to view each of the Flight Plan legs PDX TO MMV 1 205 32 8NM ARPT ARPT F...

Page 160: ... flight plan creation The first character position will flash _ _ _ _ _ _ _ ENTER A NEW PLAN NAME FPL 3 Turn the Small knob to choose characters Turn the Large knob to move the cursor The flight plan name may have up to eight characters COA_____ ENTER A NEW PLAN NAME FPL 4 Press ENT to save the name and create a flight plan TURN SMALL KNOB TO INS WPTS OR SEL FOR OPTIONS FPL 144 Flight Plan FPL Mod...

Page 161: ...at any time in Flight Plan mode In addition the third line of the Flight Plan Leg pages may be customized to display one of several types of information INS allows you to insert a waypoint into the flight plan CHG allows you to change an existing waypoint in the flight plan DEL allows you to delete a waypoint in the flight plan Use the short description given previously to view the desired Flight ...

Page 162: ...egun CHG TO HIO 1 346 37 9NM ARPT ARPT FPL 3 Rotate the Large knob to move the cursor Turn the Small knob to view available fields CHG TO HIO 1 346 37 9NM ARPT ARPT FPL 4 Rotate the Large knob to move the cursor in this case to the To waypoint of the displayed leg SLE TO CHG 1 346 37 9NM ARPT ARPT FPL 5 Rotate the Small knob to view the desired option where the cursor is flashing 146 Flight Plan F...

Page 163: ...selection will often be required when operating with Radar vectors and there is the need to intercept an approach course It may also occur when flying a DME ARC to intercept an approach course 1 Press FPL twice to reach your active flight plan Then turn the Small knob to display the desired leg LGD TO BKE 2 146 28 2NM ARPT IAF 2 Press ENT LGD BKE PRESS ENT TO ACTIVATE LEG 3 Press ENT to accept the...

Page 164: ...s of their meanings is given next The Leg Information is viewed on the third line of the displayed Flight Plan Leg page Waypoint Type ARPT VOR FPL The Waypoint Type field displays which type of waypoint each waypoint in the flight plan is The example above shows that the From waypoint of the displayed leg is an Airport and the To waypoint of the displayed leg is a VOR The waypoint type option is l...

Page 165: ...o the displayed leg s To waypoint It uses the actual ground speed for calculations and is only available in the Active flight plan The time is dashed if the actual ground speed is 5 knots or less LEG ETE LEG ETE 02 21 FPL Leg ETE shows the Estimated Time En route to travel from the displayed leg s From waypoint to the displayed leg s To waypoint using the Estimated Ground Speed value described pre...

Page 166: ... knots in order to be valid If not valid the number is dashed The units of fuel displayed may be edited in System Mode to display in US Gallons Imperial Gallons Liters Pounds of Jet Fuel A Pounds of AvGas Pounds of JP4 Kilos of JP4 Kilos of Jet Fuel A or Kilos of AvGas FUEL TO FUEL TO 15USG FPL Fuel To works the same as the previous Fuel To description except the Estimated Fuel Flow described prev...

Page 167: ...t and save one screen of user input information for each flight plan This information is called the Flight Plan Comment and is accessed from a Flight Plan Summary page Action Explanation 1 Press FPL to enter FLIGHT PLAN mode then rotate the Large knob to display the desired Flight Plan Summary page All Flight Plan Summary pages are accessed by rotating the Large knob in Flight Plan mode VALLEY 364...

Page 168: ... Comment The first time the comment is edited the screen will be cleared as shown below and the cursor will be flashing on the first character of the screen Each time afterwards pressing SEL will allow you to edit the previously entered Flight Plan Comment _ FPL 4 Rotate the Small and Large knobs to input characters and move the flashing cursor USE PARALLEL COURSE OFFSET ON LEG 3 FPL 152 Flight Pl...

Page 169: ...light plans when the Flight Plan Summary page is displayed Shown below is a simple explanation for accessing these Flight Plan Summary Options A more detailed explanation of the purpose of each of these options is given later Action Explanation 1 Press FPL to enter FLIGHT PLAN mode then rotate the Large knob to display the desired Flight Plan Summary page VALLEY 364NM DEST WPT EUG INACTIVE FPL 2 W...

Page 170: ...sing ENT when Activate is displayed copies the Inactive flight plan into the Active plan The new Active flight plan is activated with the new waypoint information Waypoint sequencing then starts from leg 1 Navigation information such as Desired Track and CDI uses the newly activated flight plan s waypoints The original copy of the Inactive flight plan is not affected Load Approach ACTIVE 364NM DES...

Page 171: ...NT when Continue is displayed releases the Active flight plan from Hold allowing leg sequencing to continue beyond the current To waypoint Reverse ACTIVE 364NM DEST WPT EUG REVERSE FPL Pressing ENT when Reverse is displayed reverses the order of all waypoints in the Inactive flight plan Rev Activate ACTIVE 364NM DEST WPT EUG REV ACTIVATE FPL Pressing ENT when Rev Activate is displayed activates th...

Page 172: ... a flight plan s waypoints from an existing plan into the current flight plan You can also copy a flight plan s waypoints between another NMC when installed and the current plan After pressing ENT rotate the Small knob to select the name of the flight plan containing the waypoints you wish to copy Then press ENT to copy that flight plan s waypoints into the current flight plan The Copy Plan functi...

Page 173: ...speed is used by the Active flight plan whenever traveling faster than 20 knots On the other hand Inactive flight plans always use the Estimated Ground Speed value for ETA and ETE leg estimations This option is especially useful for pre flight planning After pressing ENT rotate the Small and Large knobs until the desired Estimated Ground Speed is displayed then press ENT again to store it Est Fuel...

Page 174: ...anges to show the Oceanic Activation Altitude flashing Press the ENT button to accept the altitude Rotate the Small knob CW to increase the altitude in 100 ft increments or CCW to decrease the altitude in 100 ft increments Press ENT when the desired altitude is displayed Cancel Oceanic ACTIVE 364NM DEST WPT EUG CANCEL OCEANIC FPL Pressing ENT when the Cancel Oceanic option is flashing deactivates ...

Page 175: ...any time by deleting the DIRECT signifier from the Flight Plan Leg page This is done exactly as if you were deleting a waypoint The old waypoint which was previously entered as the leg s From waypoint will then be redisplayed In some cases you may wish to fly Direct To a waypoint in the Active flight plan which is not the current To waypoint You may easily do this by viewing the Flight Plan Leg pa...

Page 176: ...NOTES 160 Flight Plan FPL Mode Operations ...

Page 177: ...Display Programming and Autonav time System Info Functions pertaining to the Apollo NMS such as displaying the Software Version and entering the Owner s name Position Sensors Functions pertaining to the position sensors such as displaying Loran or GPS sensor data Miscellaneous Sensors Functions pertaining to the F ADS Fuel Air Data Sensor and the altitude encoder Important When you enter SYS mode ...

Page 178: ...zation of SYS Mode 162 System SYS Mode Operations ENT ENT ENT ENT POSITION SENSORS POSITION SENSORS SUB STATE SYSTEM INFORMATION SYS INFO SUB STATE NAV INFO SUB STATE MISCELLANEOUS SENSORS HOME PAGE NAVIGATION INFORMATION MISCELLANEOUS SENSORS SUB STATE ...

Page 179: ...fo sub state and the knobs are then used to access displays pertaining to navigation data and settings Navigation Information Pressing ENT when the screen below is displayed provides access to Airspace Setup Autonav Time NAV Mode Display Programming Mag Variation Magnetic Variation the Flight Timer Trigger and Direct To Entry option NAVIGATION INFO PRESS ENT SYS System Information Pressing ENT whe...

Page 180: ...on information sub state screens are used to display and edit various navigation settings The display below is used to turn Airspace Alerts ON OFF AIRSPACE SETUP ALERTS ON SYS Airspace Buffers Airspace Alert provides alert messages based on distance altitude and time The page below is used to set the airspace buffers In this example you will be alerted when the aircraft is 2 nm from a SUA Special ...

Page 181: ...ass B OUTER or Class C OUTER is chosen only one alert message is generated when multiple Class B or Class C airspaces overlap i e the system considers the overlapping airspaces to be a single SUA AIRSPACE SELECT CLASSB OFF B OUTER ON SYS Autonav Time The display below is used to set the Autonav Scroll time In this example Autonav Scroll will display each Nav information page sequentially at 4 seco...

Page 182: ...d must be entered manually if a valid data card is not inserted MAG VARIATION AUTO 09 W SEL TO EDIT SYS Changing Oceanic Activation Altitude The display below shows the Oceanic Activation Altitude currently set to 16000 feet Activation altitude is adjustable in 100 foot increments over the range of 0 to 18000 feet OCEANIC ALTITUDE 16000 FT SEL TO EDIT SYS Flight Timer Trigger The display below is ...

Page 183: ... Universal Coordinated Time formally called Greenwich Mean Time to locate satellites and determine position In this example the current UTC is 15 14 and the date is February 11 1999 DATE 11 FEB 99 TIME 15 14 UTC SEL TO RESET SYS Fuel Measure Units The screen below is used to choose the measurement units used in fuel data displays The system must be interfaced with a F ADS Fuel Air Data Sensor or a...

Page 184: ... servicing troubleshooting the NMC In this example the NMC software version is 6 30 and part number is 139 0197 063 Turn the Small knob to display data base Gateway Keypad GPS Sensor Loran Sensor and AirData Computer information APOLLO NMC 139 0197 063 SYS Data card Version The display below shows the installed data card is North America version 1 10 The expiration date for this version is March 3...

Page 185: ...00 ANTENNA MT TOP SYS AirData Computer Version This display shows the version of the AirData Computer AIRDATA COMPUTER SW VERS 1 00 02 FW VERS 90 01 01 SYS Display Test The screen below is used to test the NMC display TO TEST DISPLAY PRESS ENT SYS Owner Name The display below shows the owner s name is Clark Kent The NMC allows you to enter your name address phone number and aircraft number into th...

Page 186: ...s Auto means the GRI selection process is automatic 93 describes the grade relative usefulness of the signals from 0 to 99 The higher the grade the more useful the data LORAN1 GRI1 9940 US WEST COAST GRADE 93 AUTO SYS No Data Available If the NMC is not receiving data from Loran 1 the display below appears LORAN1 GRI1 ____ NO DATA AVAILABLE SYS Master Station Information The display below shows Ma...

Page 187: ...s in a blink BNK condition or the SNR is too low In this example Loran 1 GRI1 is 9940 The Master station is in cycle the SNR is 8 and the Cycle 1 2 data is 48 51 The Station shows a low SNR condition LORAN1 GRI1 9940 MASTER CYCLE 08 48 51 SNR SYS Secondary Station Information The display below shows the signal information for secondary station W Whisky A similar display appears for each secondary ...

Page 188: ...ions are selected manually or automatically LORAN1 9940 MWX AUTO 5990 MYZ AUTO SYS GPS Status The screen below displays information concerning a GPS Global Positioning System Sensor The top line shows the GPS number and whether the position is 2D or 3D 2 Dimensional or 3 Dimensional If the position is 2D altitude is not calculated if the position is 3D the sensor is calculating both position and a...

Page 189: ...ation SNR and Azimuth for each satellite A similar display appears for each satellite a GPS sensor is tracking In this example satellite SV24 is in search status with an elevation of 56 an SNR of 38 and an azimuth of 173o Elevation describes the position in degrees above the horizon Azimuth refers to the horizontal position of the satellite in degrees measured from true north The SNR measurement i...

Page 190: ... ENT TO DO A NORMAL GPS RESET SYS Miscellaneous Sensors Sub State Displays These displays pertain to systems that include miscellaneous sensors The miscellaneous sensors are the F ADS Fuel Air Data Sensor Fuel Sensor and or encoding altimeter Air Data Sensor Information If the system does not include a F ADS the next display is the only page shown for the Air Data Sensor information AIR DATA INFO ...

Page 191: ...ts SYS The next display page shows True Air Temperature which compensates for wind chill factors Outside Air Temperature which does not compensate for wind chill Mach in this case 0 405 mach TrueAir 24 C OutAir 14 C Mach 405 SYS The next display shows Density Altitude Pressure Altitude Rate of Climb Dens Alt 13155ft Pres Alt 13300ft ROC 160ft min SYS The next Air Data Sensor display shows Magnetic...

Page 192: ... for the Fuel Data Sensor Information Fuel Info No Data Available SYS If the Fuel Data Sensor information is available the next screens are available for information on the Fuel Data Sensor The first Fuel Data Sensor display shows Estimated Fuel Endurance based on the current amount of fuel in the regular non reserve tanks and the current burn rates Nautical Miles per Fuel Unit Remaining fuel not ...

Page 193: ...the right engine Amount of Fuel Used by the right engine Right Engine Burn 7 3usg hr Used 30usg SYS The next Fuel Data Sensor display shows Burn Rate for the left engine Amount of Fuel Used by the left engine Right Engine Burn 7 0usg hr Used 28usg SYS The next display shows grand total of fuel which all tanks may hold amount of fuel which the reserve tanks may hold Fuel Warning Message time period...

Page 194: ...nged value The display page is also available in the System Info sub state Fuel Measure usg US Gallons SYS Altitude Encoder Information If the system does not include an altitude encoder the next display is shown for the encoding altimeter information Encoding Altimeter No Data Avail SYS If the encoding altimeter information is available it will be shown as displayed below This screen displays the...

Page 195: ... page is displayed during Auto Nav scroll Programmable Nav Information Displays Used to choose the specific navigation items displayed on the Nav information pages Magnetic Variation Used to choose auto or manual variation Oceanic Altitude Used to set the altitude where the NMC starts and stops the Oceanic flight phase Flight Timer Trigger Speed Used to adjust the ground speed at which the flight ...

Page 196: ...rations OCEANIC ALTITUDE MAGNETIC VARIATION SETTING FLIGHT TIMER TRIGGER SPEED DIRECT TO ENTRY CDI SCALING HOMEPAGE NAVIGATION INFORMATION SYSTEM INFORMATION POSITION SENSORS MISCELLANEOUS SENSORS AIRSPACE ALERT SETUP AIRSPACE BUFFERS AIRSPACE ALERT SELECT AIRSPACE ALERT SELECT AUTONAV TIME NAVIGATION PROGRAMMING PAGES FIRST PROGRAMMABLE PAGE LAST PROGRAMMABLE PAGE ENT ...

Page 197: ...SELECTED ENT PRESS ARE ALL DESIRED AIRSPACE ALERTS SELECTED PRESS SYS YES THE BUFFER TO CHANGE FLASH TURN TO MAKE TURN TO DISPLAY THE DESIRED AIRSPACE BUFFER ARE THE DESIRED BUFFERS DISPLAYED ENT PRESS PRESS TO ACTIVATE EDITING SEL TURN TO DISPLAY THE AIRSPACE BUFFERS PAGE THE NAVIGATION INFO PAGE TURN TO DISPLAY ENT PRESS PRESS SYS PRESS TO ACTIVATE EDITING SEL ENT PRESS AIRSPACE SETUP PAGE TURN ...

Page 198: ... the Navigation Info Sub State functions Turn the Large knob to display the Airspace Setup page Airspace Setup Alerts ON SYS 3 Pressing SEL activates editing Turn the Small knob to display ON or OFF Choosing OFF turns all airspace alert messages off Press ENT to save the displayed setting Airspace Setup Alerts ON SYS 182 Navigation Information Sub State Operations ENT SEL SYS ...

Page 199: ...g SUAs Airspace Buffers Dist Alt Time 2nm 500 10min SYS 5 Pressing SEL activates editing Turn the Small knob to display the desired distance setting Airspace Buffers Dist Alt Time 5nm 500 10min SYS 6 Turn the Large knob to make the altitude setting flash Turn the Small knob to display the desired altitude Airspace Buffers Dist Alt Time 5nm 400 10min SYS 183 Operations Navigation Information Sub St...

Page 200: ...Airspace Select Class B OFF B Outer ON SYS 9 Turn the Large knob to make the setting you want to change flash Turn the Small knob to display the desired setting Press ENT to save the changes Airspace Select Class B ON B Outer OFF SYS 10 Repeat steps 8 and 9 as required Use the Small and Large knobs and the SEL and ENT buttons to edit the remaining Airspace Select pages Airspace Select Restrict ON ...

Page 201: ...e knob to display the Navigation Info page Navigation Info Press ENT SYS 2 Pressing ENT activates the Navigation Info sub state functions Turn the Large knob to display the Autonav Time page Autonav Time 4 Seconds Page SYS 3 Pressing SEL activates editing Autonav Time 4 Seconds Page SYS 4 Turn the Small knob to display the desired time Press ENT to save the setting Autonav Time 6 Seconds Page SYS ...

Page 202: ...emaining Distance to the current To waypoint You may also decide which of the Nav Information pages will be displayed when the Autonav feature is being used The Navigation Info display is divided into six fields of eight characters each FIELD 1 FIELD 2 FIELD 3 FIELD 4 FIELD 5 FIELD 6 The Eight Character Nav Items will fit into any of fields 1 through 6 The Sixteen Character Nav Items span two fiel...

Page 203: ...EL activates editing The first Navigation Info page is not programmable Pressing SEL when the first Navigation Info page is displayed causes the next screen to be displayed If this page is displayed skip to step 5 or press SEL again to cancel SELECTED PAGE IS NOT PROGRAMMABLE EDIT AUTONAV Pressing SEL when any of the other Navigation Info pages are displayed starts the editor for updating the Nav ...

Page 204: ...plays the Autonav Pages prompt NAV PAGE 2 IN AUTONAV PAGES YES SYS 6 Turning the Small knob displays the available choices you have for keeping this page in the Autonav sequence NAV PAGE 2 IN AUTONAV PAGES NO SYS 7 Pressing ENT saves the Autonav choice and displays the Navigation Info page with the updated fields ETE SLE 00 32 ETA SLE 20 59 DTK 084 87NM SYS 188 Navigation Information Sub State Ope...

Page 205: ...mpletely blank the page will not appear in the Navigation Info pages of NAV mode nor will the page appear in the Autonav sequence You now have maximum control over the Navigation Info pages for satisfying your individual requirements You now have the capability of customizing the Navigation Info pages to display only desired fields see pages 70 through 76 remove pages customize which pages are dis...

Page 206: ...ion Info Sub state functions Turn the Large knob to display the NAV Mode Display Programmable and Autonav page NAV MODE DISPLAY PROGRAMMABLE AND AUTONAV PAGES SYS 3 Turn the Small knob to display the Restore Default Nav Pages screen PRESS ENT TO RESTORE DEFAULT NAV PAGES SYS 4 Pressing ENT restores the default Nav displays and displays the next page NAV MODE DISPLAY PROGRAMMABLE AND AUTONAV PAGES ...

Page 207: ...er the magnetic variation during power up For the procedure used to enter magnetic variation during power up see Operations Power Up Sequence Flow chart 191 Operations Navigation Information Sub State THE NAVIGATION INFO PAGE TURN TO DISPLAY ENT PRESS PRESS SYS MAG VARIATION PAGE TURN TO DISPLAY THE PRESS TO ACTIVATE EDITING SEL ENT PRESS TURN TO DISPLAY MANUAL TURN TO MAKE THE MAG VARIATION FLASH...

Page 208: ... ENT SYS 2 Pressing ENT activates the Navigation Info sub state functions Turn the Large knob to display the Mag Variation page MAG VARIATION AUTO 09 W SEL TO EDIT SYS 3 Pressing SEL activates editing MAG VARIATION AUTO 09 W SYS 4 Turn the Small knob to display Manual MAG VARIATION MANUAL 09 W SYS 192 Navigation Information Sub State Operations SYS ENT SEL ...

Page 209: ...ARIATION MANUAL 15 W SYS 6 Turn the Large knob to make the direction character flash Turn the Small knob to display E East or W West Pressing ENT enters the displayed Mag Variation MAG VARIATION AUTO 15 W SEL TO EDIT SYS 7 Pressing ENT saves the magnetic variation setting MAG VARIATION MANUAL 15 W SEL TO EDIT SYS 193 Operations Navigation Information Sub State ENT ENT ...

Page 210: ...de turn the Large knob to display the Navigation Info page Navigation Info Press ENT SYS 2 Press ENT to activate the Navigation Info sub state functions Turn the Large knob to display the Oceanic Altitude page OCEANIC ALTITUDE 16000FT SEL TO EDIT SYS 3 Press SEL to activate editing 4 Turn the Small knob to display the desired activation altitude The altitude is changed in 100 foot increments Press...

Page 211: ...ion Info page Navigation Info Press ENT SYS 2 PressingENTactivatestheNavigationInfo sub state functions Turn the Large knob to display the Flight Timer Trigger page FLIGHT TIMER TRIGGER AT 60 KTS SYS 3 Pressing SEL activates editing FLIGHT TIMER TRIGGER AT 60 KTS SYS 4 Turn the Small knob to display the desired trigger speed The trigger speed is chosen in increments of 10 kts OFF or AT POWER ON ma...

Page 212: ...function turn the Large knob to the Display Units Page Display Units Distance nm kts Altitude ft 2 Press SEL to activate selection The Distance value will flash Turn the Small knob to change the value Display Units Distance nm kts Altitude ft 3 Turn the Large knob to move to the Altitude selection Turn the Small knob to change the value Display Units Distance sm mph Altitude ft 4 After completing ...

Page 213: ... will be inserted in the Active flight plan and all of the other waypoints will be deleted from the Active flight plan With the Never Clears Direct To option the Direct To waypoint is inserted before the current To waypoint The May Clear option is useful for the pilot who uses the Direct To function for the majority of flight planning and doesn t want to be bothered with a steadily increasing numb...

Page 214: ...activates the Navigation Info sub state functions Turn the Large knob to display the Direct To Entry Option page DIRECT TO ENTRY NEVER CLEARS ACTIVE PLAN SYS 3 Pressing SEL activates editing DIRECT TO ENTRY NEVER CLEARS ACTIVE PLAN SYS 4 Turn the Small knob to display the desired Direct To Entry Option Press ENT to save the option DIRECT TO ENTRY NEVER CLEARS ACTIVE PLAN SYS 198 Navigation Informa...

Page 215: ...d will change according to your distance to the destination waypoint for the approach operation flight phase The following procedure isused toedit the Auto CDI Scaling Option Action Explanation 1 In SYS mode turn the Large knob to display the Navigation Info page Navigation Info Press ENT SYS 2 Pressing ENT activates the Navigation Info Sub State functions Turn the Large knob to display the CDI Sc...

Page 216: ... to save your choice CDI SCALING MANUAL ªªªªª 5 00nm SYS 5 Change the manual resolution while MANUAL is flashing Turn the Large outer knob The sensitivity value will flash CDI SCALING MANUAL ªªªªª 5 00nm SYS 6 Turn the Small inner knob to select 0 30 1 00 or 5 00 nm full scale deflection per side Press ENT to save your choice CDI SCALING AUTOMATIC ªªªªª 0 30nm SYS 200 Navigation Information Sub St...

Page 217: ... hour clock Fuel Measure Units Used to choose the units used to display fuel information Baro Measure Units Used to choose inches or millibars for air pressure display Software Versions Used to display the software version and database for the NMC and each sensor Display Testing Used to test each LED in the display Owner Information Used to enter edit the owner s name address phone number and airc...

Page 218: ...System Information Sub State continued The figure below illustrates the organization ofthe Sys Info sub state 202 System Information Sub State Operations ...

Page 219: ...y also be adjusted during the power up sequence The NMC will update itself from GPS satellite data during power up after it gets a 3 D fix For the procedure used to adjust the time and date during power up see Operations Power Up Sequence 203 Operations System Information Sub State ENT PRESS PRESS SYS PRESS TO ACTIVATE EDITING SEL ENT PRESS THE SYSTEM INFO PAGE TURN TO DISPLAY TIME AND DATE PAGE T...

Page 220: ...nob to display the desired date DATE 21 APR 99 TIME 13 16 UTC SYS 4 Turn the Large knob to make the next item you want to change flash Turn the Small knob to display the desired item DATE 21 FEB 99 TIME 13 16 UTC SYS 5 Repeat step 4 Use the Large and Small knob to edit the items Pressing ENT saves the changes Pressing SEL exits editing without saving any changes DATE 21 FEB 99 TIME 14 18 UTC SEL T...

Page 221: ...b to display the System Info page SYSTEM INFO PRESS ENT SYS 2 Pressing ENT activates the Navigation Info sub state functions Turn the Large knob to display the Fuel Measure page FUEL MEASURE USG US GALLONS SYS 3 Pressing SEL activates editing Turn the Small knob to choose the desired fuel measure units FUEL MEASURE LBS POUNDS AVGAS SYS 4 Press ENT to save the selection FUEL MEASURE LBS POUNDS AVGA...

Page 222: ...vigation Info page SYSTEM INFO PRESS ENT SYS 2 Pressing ENT activates the Navigation Info sub state functions Turn the Large knob to display the Barometric Pressure Units page BARO MEASURE INCHES SYS 3 Pressing SEL activates editing BARO MEASURE INCHES SYS 4 Turn the Small knob to display the desired Direct To Entry Option Press ENT to save the option BARO MEASURE MB MILLIBARS SYS 206 System Infor...

Page 223: ...to this test have the NMC serviced Action Explanation 1 In SYS mode turn the Large knob to display the System Info page SYSTEM INFO PRESS ENT SYS 2 Pressing ENT activates the System Info sub state functions Turn the Large knob to display the Test Display page TO TEST DISPLAY PRESS ENT SYS 3 Pressing ENT activates display testing SYS 207 Operations System Information Sub State ENT SYS ENT ...

Page 224: ...n SYS mode turn the Large knob to display the System Info page SYSTEM INFO PRESS ENT SYS 2 Pressing ENT activates the Navigation Info sub state functions Turn the Large knob to display the Apollo NMC Software Version page APOLLO NMC 139 0197 030 SYS 3 Turn the Small knob to scroll through the displays showing version information for the various system components WEST NORTH AM DB DATE 03 31 99 VERS...

Page 225: ... entered Caution To change the owner information you must remember your password The password can only be cleared by II Morrow technicians Action Explanation 1 In SYS mode turn the Large knob to display the System Info page and press ENT to activate the System Info functions Turn the Large knob to display the Owner Name page OWNER NAME SEL TO EDIT SYS 2 Pressing SEL activates editing The display b...

Page 226: ... remaining characters in the password Characters chosen are not displayed when another character space is flashing To review the characters turn the Large knob Press ENT to enter the password The display below appears for approximately 3 seconds CAUTION PASSWORD MUST BE VERIFIED SYS After 3 seconds the display below appears VERIFY OWNER PASSWORD ______ SYS 210 System Information Sub State Operatio...

Page 227: ...assword If a mistake is made the NMC asks you to try again The following display appears for approximately 3 seconds PASSWORD MATCHED EDITING ENABLED SYS After 3 seconds the display below appears OWNER NAME SEL TO EDIT SYS 8 Pressing SEL enables editing Turn the Small knob to display the first character in the owner name OWNER NAME A SYS 211 Operations System Information Sub State ENT SEL ...

Page 228: ...name Press ENT to save the name OWNER NAME AMELIA JEAN EARHART SYS 11 Turn the Small knob to display the next Owner Information page OWNER ADDRESS SEL TO EDIT SYS 12 Repeat steps 8 through 11 Use the Large and Small knobs and the ENT button to edit the remaining Owner Info pages Once the password has been verified Owner Info displays may be edited without entering the password until the NMC is pow...

Page 229: ...es OSC Reference Oscillator frequency and temperature GRI s and Triads If GPS sensor s are installed this information includes the number of healthy satellites the number of visible satellites present altitude track ground speed identifiers of the satellites used the UTC Coordinated Universal Time satellite status satellite elevation SNR Signal to Noise Ratio and Azimuth 213 Operations ...

Page 230: ...ellites used the UTC Coordinated Universal Time satellite status satellite elevation SNR Signal to Noise Ratio and Azimuth Displaying Position Sensor Information The following procedure is used to display position sensor data 1 In SYS mode turn the Large knob to display the Position Sensors page POSITION SENSORS PRESS ENT SYS 2 Pressing ENT activates the Position Sensor sub state functions Turn th...

Page 231: ...s page POSITION SENSORS PRESS ENT SYS 2 Pressing ENT activates the Position Sensor sub state functions Turn the Large knob to display the desired Loran GRI page LORAN1 GRI 9940 US WEST COAST GRADE 93 AUTO SYS 3 Pressing SEL activates editing LORAN1 GRI 9940 US WEST COAST GRADE 93 AUTO SYS 4 Turn the Small knob to choose MANUAL LORAN1 GRI 9940 US WEST COAST GRADE 93 MANUAL SYS 215 Operations Headin...

Page 232: ...ection The following procedure is used to manually select the Loran triad Prior to using this procedure you must manually select the GRI s Only one triad may be manually selected for each Loran sensor 1 In SYS mode turn the Large knob to display the Position Sensor page POSITION SENSORS PRESS ENT SYS 2 Pressing ENT activates the Position Sensor sub state functions Turn the Large knob to display th...

Page 233: ...isplayed LORAN1 STATIONS 5990 9940 MWX MANUAL SYS 5 Turn the Large knob to make the first station designator flash Turn the Small knob to display the desired station LORAN1 STATIONS 5990 9940 M MANUAL SYS 6 Turn the Large knob to make the next station designator flash Turn the Small knob to display the desired station Repeat to choose the remaining station LORAN1 STATIONS 5990 9940 MXY MANUAL SYS ...

Page 234: ...NT to enter the triad Pressing any Mode button or the SEL button instead exits editing without saving the changes LORAN1 STATIONS 5990 MXYZ AUTO 9940 MXY MANUAL SYS 218 Loran Sensor Sub State Operations ENT SEL ...

Page 235: ... fuel sensor and altitude encoder monitors fuel flow air speed outside air temperature pressure and magnetic heading The F ADS data is used to compute TAS pressure altitude density altitude heading wind direction velocity rate of climb and fuel usage Miscellaneous Sensor Sub State The figure below illustrates the organization of the SYS Mode Miscellaneous Sensors Sub State 219 Operations Heading_2...

Page 236: ...the Miscellaneous Sensor sub state functions Turn the Large knob to display the Air Data Sensor top page the Fuel Data Sensor top page or the altitude encoder page AIR DATA INFO TruAirSp 385kts IndAirSp 304kts SYS 3 If the diamond character is displayed on the lower right hand corner of the display page rotate the Small knob to view sub pages of the current page TrueAir 24 C OutAir 14 C Turn 3 Sec...

Page 237: ...uidance during a non precision approach without actively monitoring the applicable navaid s which define the approach being used However the traditional ground based navaid s required for the published approach and alternate should be operational and the associated avionics should be installed and operational The approach should be requested and approved by its published name such as NDB Runway 24...

Page 238: ...irport You may execute a GPS approach to a required alternate but you must plan for the possibility that GPS navigation will not be available FAA guidelines on IFR use of GPS and GPS approaches are contained in an FAA Advisory Circular AC AC 90 94 You should be familiar with the information in this AC before attempting GPS approaches In order to use the Apollo NMS for an approach the approach must...

Page 239: ...re charts however these names are usually not included on National Ocean Service NOS charts TSO C129 Overlay specific TSO C129 requires the equipment to prompt the pilot to enter the local altimeter setting if not already entered at 3 nm inbound to Final Approach Fix FAF It also requires that the equipment change RAIM alarm limits from 1 nm to 0 3 nm and to begin changing CDI sensitivity from 1 nm...

Page 240: ...h procedure chart but not on the National Ocean Service NOS approach procedure chart for this approach This is especially important to understand when a procedure turn or course reversal is required If you are inbound from the CASHS intersection a procedure turn is required You must execute this procedure turn on your Apollo NMS relative to FF285 the TSO C129a FAF not relative to the EAT VOR as de...

Page 241: ...Charts have been reduced for illustrative purposes 225 Operations Approach Procedures Reproduced with permission of Jeppesen Sanderson Inc NOS Chart ...

Page 242: ... 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 NMS database as D164N D for DME 164 for 164 radial and N the 14th letter of the alphabet for 14 nm It is also depicted on Jeppesen approach procedure charts with this name however this name is not found on NOS charts 226 Approach Procedures Operations ...

Page 243: ...Charts have been reduced for illustrative purposes 227 Operations Approach Procedures Reproduced with permission of Jeppesen Sanderson Inc NOS Chart ...

Page 244: ...ext page located one click to the left of the home navigation page always shows the waypoint names and types for this two leg window view of your active flight plan Most of the waypoint types for en route waypoints are quite familiar They include ARPT for Airport VOR NDB INT for intersection and USER for a user defined waypoint The approach waypoint types will usually also have familiar types but ...

Page 245: ...nt could be the IAF the MAP and the MAHP however TSO C129a non precision approaches require that there always be a distinct FAF to MAP leg Intermediate waypoints of type APPR or ARC may be anywhere in the sequence except between the FAF and the MAP The following example uses the VOR DME RWY 12 GPS overlay approach to Baker City Oregon The Apollo NMS has a flight plan loaded from the Salem Oregon a...

Page 246: ...8 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 3 2NM FAF MAP MA12 TO BKE 8 120 0 8NM MAP MAHP Notice that these waypoints are all depicted on the example Jeppesen Approach plate however only BKE is depicted as such on the NOS plate shown on the following page 230 Approach Procedures Operations ...

Page 247: ...Charts have been reduced for illustrative purposes 231 Operations Approach Procedures NOS Chart Reproduced with permission of Jeppesen Sanderson Inc ...

Page 248: ...ed to the nearest whole mile A waypoint on the BKE VOR 272 radial at 25 nm would then be named D272Y as is the IAF in the Baker Oregon approach example above When the distance is greater than 26 miles such as for the Topeka KS VOR DME RWY 3 approach the waypoint is named by using the first two characters of the reference navaid ID followed by the bearing from the navaid The IAF at the Topeka VOR T...

Page 249: ...Bearing and Distance Waypoints Distance bearing waypoints sometimes called Rho Theta waypoints that are defined as a bearing and distance from a VHF navaid are named with the character D followed by the radial on which they are positioned followed by a single alpha character from A to Z that corresponds to a distance from 1 to 26 nm Thus a waypoint that is on a 350 radial at 10 nm will be named D3...

Page 250: ...hese are most often used for identifying bends in airways that occur at unnamed positions and other enroute uses It is unlikely that you will often see this convention used to name any approach waypoints but you will occasionally 234 Approach Procedures Operations ...

Page 251: ...rse to the current active waypoint Entering a desired inbound course to a waypoint automatically suspends leg sequencing at that waypoint and lights the OBS HLD annunciator OBS DTK 001 TO BTG BRG 002 DTK 001 Subsequent pressing of DIRECT TO toggles between the two first uses The Direct To feature defaults to the current active waypoint the current displayed waypoint or in FLIGHT PLAN mode the wayp...

Page 252: ... approach course It may also occur when flying a DME ARC to intercept an approach course 1 Press FPL twice to reach your active flight plan Then turn the Small knob to display the desired leg LGD TO BKE 2 146 28 2NM ARPT IAF 2 Press ENT LGD BKE PRESS ENT TO ACTIVATE LEG 3 Press ENT to accept the displayed destination waypoint The unit will then go to NAV mode ETE BKE 00 05 Ã 0 006 BRG 146 27 7NM 2...

Page 253: ...e 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 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 237 Operations Approach Procedures ...

Page 254: ...pears to indicate the leg number An Asterisk is used after the number of each leg to indicate the active flight plan SLE TO BTG 1 001 53 2NM ARPT VOR Two asterisks after the leg number indicate the active leg of the active flight plan SLE to BTG BTG TO OLM 2 331 74 4NM VOR VOR Turn the Small knob until the leg you wish to activate is shown and then press ENT twice Now fly the ATC assigned heading ...

Page 255: ...rcept a leg that you will want to select a leg that according to the rule for sequencing you are already past In order to keep the NMS from immediately sequencing when such a leg is selected place your flight plan on hold by pressing the OBS HLD button prior to selecting the leg It is then necessary to re enable sequencing by pressing the OBS HLD button again when established inbound on the desire...

Page 256: ...ur selected leg as soon as the leg is selected To prevent sequencing press OBS HLD before manually selecting the leg The OBS HLD annunciator will turn on Manually select the desired flight plan leg and navigate to the waypoint Point B When the leg is intercepted press OBS HLD again to enable sequencing Point C The OBS HLD annunciator will then turn off 240 Approach Procedures Operations ...

Page 257: ...he FAF and the final approach course FAF to MAP course In this case the NMS will automatically suspend sequencing and the OBS HLD annunciator will light Note The only other time the NMS will automatically suspend sequencing for you is when the active waypoint is either the Missed Approach Point MAP or the Missed Approach Holding Point MAHP When you know that a procedure turn or course reversal is ...

Page 258: ...are past the waypoint on the From side Procedure Turn at an FAF A special condition occurs when a procedure turn is made at an IAF which is also the FAF In this case the Apollo NMS will treat the waypoint as the IAF until sequencing is enabled when established inbound When you enable sequencing by pressing the OBS HLD button thereby extinguishing the OBS HLD annunciator light the IAF FAF waypoint ...

Page 259: ...4 procedure with IAF OED VOR using the OED 157 10 transition see point A 1 At point A press OBS HLD to suspend sequencing 2 At point B press DIRECT TO twice Use the Small and Large knobs to select 153 and then press ENT to establish an inbound course Note that your CDI will reverse sense while outbound just like a VOR with 153 TO selected on the OBS 3 At point C make your procedure turn 4 243 Oper...

Page 260: ...e the VOR or GPS B approach for Wenatchee Washington You will start the approach using the CASHS transition Illustration Points Point A Between CASHS and EAT Point B A heading of 105 between EAT and FF285 Point C Continue on a heading of 105 between FF285 and the procedure turn until beyond FF285 Point D Make the procedure turn Point E Intercept the 285 inbound to FF285 1 Point A A heading of 073 ...

Page 261: ...ss ENT 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 Point C 9 At point D make the procedure turn 10 At the intercept of the inbound course to the FAF press OBS HLD to allow sequencing at the FAF Waypoint FF285 now becomes the FAF Point E 245 Operations Approach Procedures ENT D D ...

Page 262: ...exit the holding pattern press OBS HLD while still on the To side of the waypoint to enable sequencing the next time you cross the waypoint While you are in a holding pattern the CDI HSI cross track deviation display and the TO FROM flag will behave almost exactly the way they would if you were holding at a VOR The TO FROM flag will display TO prior to reaching the waypoint The TO FROM flag will d...

Page 263: ...cross the waypoint If you are on the FROM side of the waypoint the flight plan will sequence immediately The following example shows holding at the Newburg VOR VBG with020 inboundselectedasthe OBS coursetoUBG A special case exists when holding at the FAF The waypoint will not be treated as the FAF until sequencing is resumed inbound to the 247 Operations Approach Procedures ...

Page 264: ...utton as soon as you are established inbound when you want the waypoint to become the FAF in order to allow as much time for this transition as possible This example shows holding at the FAF SL TURNO for the NDB or GPS Runway 31 Salem McNary Airport SLE Press OBS HLD to release the hold as soon as you intercept the inbound course point A This will allow you as much time as possible for transition ...

Page 265: ...e is selected in navigation mode with the Large knob The nearest VOR will display as the default reference point ARC ASSIST REF LMT VOR PRESS ENT OR SEL 2 Before you reach the starting waypoint of a DME Arc press ENT to accept the displayed VOR or press SEL and select the desired waypoint The selected waypoint is now used as the center of the arc LEFT ARC DTK 031 REF ILR VOR RAD 121 131NM 3 Turn t...

Page 266: ...and intercepting a new course is very similar to the information and techniques used to fly a DME Arc with traditional equipment except easier DME Arcs are flown using an Apollo NMS Arc Assist page and the aircraft heading for primary guidance This makes them nearly identical to flying a DME Arc with traditional DME equipment The NMS and your CDI should provide guidance on the course or leg that y...

Page 267: ...he flightplanandthenloadanapproach Select the VOR DME 14 LANKS approach ACTIVE 52 2NM VORDME 14 LANKS APPROACH MFR 2 In NAV Mode view the home NAV page and watch your progress to the first waypoint LANKS ETE LANKS 00 10 0 05 BRG 270 28 1NM 251 Operations Approach Procedures NAV ...

Page 268: ...om D333O to OED11 We are going to manually activate this leg and we don t want to sequence immediately 5 Now manually select the flight plan leg from D333O to OED This is the inbound course this Arc will intercept Press FPL Turn the Small knob to display the leg from D333O to OED Press ENT Press ENT a second time to activate the leg D3330 TO OED11 PRESS ENT TO ACTIVATE LEG 6 Press NAV Turn the Lar...

Page 269: ...or the Arc Assist feature and it can be used at any time not just during approach or terminal operations This allows the Arc Assist feature to be used for a variety of uses other than flying DME arcs to intercept an approach course It can of course be used to navigate DME arcs that are part of a published missed approach procedure It can also be used for difficult operations such as conducting an ...

Page 270: ...sed approach are as follows 1 Begin your missed approach This usually includes a procedural clearance such as Fly runway heading to altitude or climbing left turn to a heading of xxx 2 Cancel the approach on your Apollo NMS Press OBS HLD to enable sequencing and to cancel the approach As soon as you enable sequencing the Apollo NMS will sequence to the next waypoint in the flight plan This is the ...

Page 271: ... inbound course to the active waypoint is to be intercepted or flown press DIRECT TO twice 5 Enter the desired the inbound course with the Large and Small knobs Then press ENT Selecting an inbound course in this manner will suspend flight plan sequencing and the OBS HLD annunciator will light 6 If you do not wish to hold or execute a procedure turn at the next waypoint press OBS HLD to enable sequ...

Page 272: ...to waypoint While this guarantees that the new selected destination is the last waypoint in the flightplan itwillalsoresultinaNav Flaggedconditionimmediatelyafter delete waypoints is selected This is because the Apollo NMS has no waypoint to navigate to Therefore all navigation data is invalid until you select a new TO waypoint Select a New Destination by Activating Another Flight plan Method 2 Yo...

Page 273: ...n inbound course to the IAF select the inbound course and then remember to enable sequencing when established inbound on that course 6 If you are being vectored to intercept an approach leg manually select the leg you are intercepting Press FPL twice Turn the Small knob to display the desired leg Press ENT The message displayed is Press ENT to activate leg Press ENT Note If you are on the FROM sid...

Page 274: ...Notes 258 Approach Procedures Operations ...

Page 275: ...s 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 in the Approach Transition operation area The ACTIVE annunciator will start flashing when you are within 3 nm inbound to the FAF and not on hold When you are 2 nm from the FAF CDI sensitivity willgraduallyscalefrom1...

Page 276: ... charts meet this criterion Prior to using the Apollo NMS for any GPS approach other than a published U S or Canadian approach you must first verify that the approach charts and approach waypoints use the WGS 84 or NAD 83 reference system If the approach data is referenced to any other coordinate system it can result in an unsafe position error The Apollo NMS database contains approach information...

Page 277: ...ration CDI Scale 5nm CDI Scale 1 0nm CDI Scale 2nm to FAF 3nm to FAF CDI Scale Transitions 1 0 to 0 3nm CDI Scale Transitions 5 0 to 1 0nm ACTIVE Annunciator Flashes ACTIVE Annunciator on Steady 30nm to Airport APPRCH Annunciator On IAF FAF MAP MAHP Proceed to Selected Waypoint 0 3nm CDI Scale 1 0nm Intermediate waypoints not illustrated OBS Hold Annunciator on Steady CDI Scale Transitions 0 3 nm ...

Page 278: ...ur destination airport Your Apollo NMS is providing En route operation whenever the Approach annunciator light is not on The default CDI sensitivity for en route is 5 0 nm however you may manually select other CDI sensitivities Generally you will select your destination airport prior to departure or while en route and you will usually select and load an anticipated approach from the database into ...

Page 279: ...ach Information 2 If the desired flight plan is not displayed turn the Large outer knob to display the desired flight plan RTE 1 1020NM DEST WPT SEA INACTIVE 3 Press SEL Activate will flash Press ENT to activate the selected flight plan RTE 1 1020NM DEST WPT SEA ACTIVATE Load Approach Information 1 Press FPL 2 Press SEL to reach the Load Approach selection ACTIVE 1020NM DEST WPT SEA Load Approach ...

Page 280: ...e off to indicate that your NMS is operating in Approach Transition The CDI sensitivity is locked at 1 0 nm for Approach Transition After an approach has been loaded into the active flight plan you will be prompted with a message to enable the approach This prompt occurs when you are 30 nm from your destination assuming the approach was loaded prior to that The enable approach message occurs immed...

Page 281: ...m the destination airport This message prompt is repeated at 3 nm inbound to the FAF if the approach has not yet been enabled 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 displaying the Enable Approach prompt Press ENT when this prompt is displayed to enable the approach ...

Page 282: ...ill verify that you have enabled the selected approach You will now be prompted to enter the local altimeter setting Turn the Small knob to change the barometric pressure values and turn the Large knob to move the cursor Press ENT ENTER LOCAL ALTIMETER SETTING 30 02 3 Press NAV to return to the Navigation Mode Initial Approach Fix IAF 1 Prior to the Initial Approach Fix IAF the MSG indicator will ...

Page 283: ...h the Large and Small knobs When finished press ENT 5 Press OBS HLD again to resume sequencing and to continue your approach when you have established an inbound heading Final Approach Fix FAF 1 When you are 3 nm inbound to the Final Approach Fix FAF and not on Hold the Active light will flash to 267 Operations Approach Operations Approach Transition Operation CDI Scale 1 0nm 2nm to FAF 3nm to FAF...

Page 284: ...or will flash and a standard Waypoint Arrival Alert will turn on Press MSG to acknowledge the message and then press NAV to return to Navigation Mode ARRIVAL CVO NEXT DTK 018 268 Approach Operations Operations MSG NAV Before At or After MAP Press OBS Hold for Missed Approach Approach Active Operation CDI Scale ACTIVE Annunciator on Steady FAF MAP 0 3nm OBS Hold Annunciator on Steady NOTE If ACTIVE...

Page 285: ...iding approach guidance As soon as you cross the FAF the active flight plan sequences and the Missed Approach Point MAP becomes the active waypoint Sequencing is now automatically suspended and the OBS HLD annunciator will be on Anytime the Apollo NMS is in Approach Active Operations the approach may be canceled by pressing the OBS HLD button Canceling the Approach will result in returning to Appr...

Page 286: ... 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 Follow the published missed approach instructions or clearance as appropriate Press the OBS HOLD annunciator to deselect HOLD and 270 Approach Operations Operations MSG NAV At or After MAP Press OBS Hold for Missed Approach Transition...

Page 287: ...h instructions 1 Press the OBS HLD button Canceling an approach does the following Sequencing is enabled The unit returns to Approach Transition operations Approach Active annunciator turns off Approach annunciator remains turned on CDI scales to 1 nm full scale deflection RAIM alarm limit goes from 0 3 nm to 1 0 nm Though you have canceled the active approach it is still loaded and enabled You ma...

Page 288: ...IAF VOR UBG NEWBERG FACIL OR USA or 3 Press the DIRECT TO button twice to set a new Desired Track DTK to the selected waypoint This also activates the OBS HLD annunciator so remember to press the OBS HLD annunciator to enable waypoint sequencing when you have established your inbound course Turn the Small knob to change the flashing value Turn the Large knob to move the cursor Press ENT when finis...

Page 289: ...ur intended destination airport 1 Press FPL and then the SEL button Turn the Small knob to display a flashing Change Approach ACTIVE 82 5nm APPR ARPT SLE CHANGE APPROACH 2 Press ENT to change the approach The center row showing the approach choices will flash ACTIVE 82 5nm NDB 31 SL APPROACH SLE 3 Turn the Small knob to display the approach choices If desired press INFO to display a list of the ap...

Page 290: ...Notes 274 Approach Operations Operations ...

Page 291: ...hat you may encounter while using approaches is included in this section This section expands on the previous Approach Basics section Use this section to familiarize yourself with the procedures that you expect to use in normal flight operations 275 ...

Page 292: ...Reproduced with permission of JeppesenSanderson Inc Reduced for illustrative purposes 276 ...

Page 293: ... with the Apollo NMS as there is Note It is good planning to always consider what you would do in the event of any equipment failures that may occur during flight operation including your navigation system Always make yourself aware of other available navaids should you need to select an alternate method of navigation 277 PARMO EMETT IAF 1 2 3 2 0 5 º 1 1 5 º 110º DEFKI RW11 1 1 0 º 110º NEMEW 290...

Page 294: ...Altimeter Setting with the SMALL knob and then press ENTER Press NAV to return to NAV mode Point A Between EMETT and PARMO 1 Fly the segment 2 Verify that the Approach annunciator is on Point B Between PARMO and DEFKI 1 Fly the segment 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...

Page 295: ...come the TO waypoint The inbound course to NEMEW is already the same as the approach inbound so you do not need to enter it 3 NEMEW is the MAHP and will automatically become a holding waypoint Verify that the OBS HLD annunciator is lighted Point E Holding Pattern 1 After crossing NEMEW you will be prompted to set the OBS course Turn the LARGE and SMALL knobs to select 290 and press ENTER 2 Fly the...

Page 296: ...Reproduced with permission of JeppesenSanderson Inc Reduced for illustrative purposes 280 ...

Page 297: ...e the Klamath Falls Oregon VOR LMT and the Medford airport Illustration Points A Inbound to OED from the south B Outbound on the procedure turn C On the procedure turn D Inbound to OED E Between OED and MA14 F Turning right and climbing to 6100 feet G Outbound from OED to enter the holding pattern H Inbound to OED in the holding pattern 281 ...

Page 298: ... ENT 3 Load the VOR or GPS A approach to MFR In flight plan mode press SEL The display will flash Load Approach Press ENT Select VOR A OED with the Small knob if necessary and press ENT Turn the Small knob to view the waypoint legs Press NAV to view NAV info ACTIVE 112NM VOR A OED APPROACH MFR 30 nm from Medford MFR 1 At 30 nm from your destination MFR the MSG annunciator will light Press MSG At t...

Page 299: ...n 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 FROM OED will remain the active waypoint 2 Select the desired inbound course to OED Press DIRECT TO twice Turnthe Large andSmallknobstodisplay162 Press ENT OBS DTK 162 TO OED BRG 175 DTK 020 Point C On the procedure turn 1 Flyoutboundviathe342radialofOEDtoexecuteapr...

Page 300: ...ED the CDI sensitivity will begin changing from 1 nm to 0 3 nm full scale deflection 3 As you cross OED the Approach Active annunciator will come on solid to indicate that approach operation is active and you may continue the approach to the FAF Point E Between OED and MA14 1 Continue to the missed approach point Verify that the OBS HLD and Approach Active annunciators are lighted steady 2 If you ...

Page 301: ... decide to miss the approach 2 The CDI will scale out to 1 nm and OED will become the active waypoint As you reach 6100 press DIRECT TO and then press ENT to establish a direct route to the active waypoint OED 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 s...

Page 302: ...Reproduced with permission of JeppesenSanderson Inc Reduced for illustrative purposes 286 ...

Page 303: ...ple was chosen primarily because of the unusual published missed approach instructions and to illustrate how to navigate this missed approach with the Apollo NMS Illustration Points A Between Parmo IAF and BO FAF B Between BO FAF and RW10R MAP C Just past RW10R MAP D Turn inbound to BO MAHP E Just past BO MAHP 287 ...

Page 304: ...le3 flight plan Press SEL and the ENT ACTIVE 43 7NM DEST WPT ACTIVE 3 Load the NDB approach to BOI In flight plan mode press SEL The display will flash Load Approach Press ENT Select NDB 10R PARMO with the Small knob and press ENT ACTIVE 48 9NM NDB 10R PARMO APPROACH BOI 30 nm from Boise BOI 1 At 30 nm from your destination the MSG annunciator will light Press MSG At the Enable Approach prompt pre...

Page 305: ...annunciator lights at BO Verify that the OBS HLD annunciator is lighted at BO Point B Nearing MAP Fly the final approach and descend to MDA Point C Missed Approach 1 When the decision has been made to execute the published missed approach press OBS HLD The active waypoint will become BO Missed Approach Point The CDI will gradually scale out to 1 0 nm full scale deflection The OBS HLD annunciator a...

Page 306: ...n 4 When you reach 4200 or when your bearing to BO matches your current heading press DIRECT TO and then ENT This will establish a new inbound course direct to BO NDB BO USTIK BOISE FACIL ID USA Point D Inbound to BO Fly inbound on the new direct course to BO The OBS HLD annunciator will remain lighted Point E Missed Approach Hold Point As you pass BO establish the new inbound holding course and e...

Page 307: ...Note If you want to reshoot the approach following your missed approach hold reactivate the flight plan leg from PARMO IAF to BO FAF or select DIRECT TO PARMO IAF as appropriate 291 ...

Page 308: ...Reproduced with permission of JeppesenSanderson Inc Reduced for illustrative purposes 292 ...

Page 309: ...referenced to a VOR that is not co located with the MAP and because of the published missed approach instructions Illustration Points A Approaching MUGGZ IAF B On the DME Arc between MUGGZ and D185O ARC C Inbound between D185O and CF005 APPR D Between CF005 and FF005 FAF E Between FF005 and MA005 MAP F Turning to intercept 165 to MUGGZ G Inbound to MUGGZ MAHP H In the holding pattern at MUGGZ En R...

Page 310: ...urn the Large knob to display the Example4 flight plan Press SEL and then ENT EXAMPLE4 147NM DEST WPT DLS ACTIVATE 3 Load the VOR DME A approach to DLS In flight plan mode press SEL The display will flash Load Approach Press ENT Select VORDME A MUGGZ with the Small knob and press ENT EXAMPLE4 147NM VORDME A MUGGZ APPROACH DLS 294 ...

Page 311: ... 121 84 1NM Note Always suspend sequencing before manually activating an inbound leg to intercept with a DME Arc if you are already on the FROM side of that leg This ensures that the flight plan will not sequence if you are currently at a point on the arc that is past the TO waypoint on the leg that you are manually selecting Re enable sequencing when you are established on the inbound path Althou...

Page 312: ... knob to the Arc Assist page Point B On the arc between MUGGZ and D1850 1 Make sure that you are viewing the Right Arc Assist page Turn the Small knob if necessary RGHT ARC DTK 270 REF LTJ VOR RAD 180 16 1NM 2 Use the Arc Assist page and your aircraft heading display to navigate to the selected inbound leg The Desired Track DTK is your tangent to the arc on your present radial For the right turn a...

Page 313: ...an sequencing Press NAV twice or turn the Large knob until you display your primary NAV page 2 Press OBS HLD to reenable flight plan sequencing if you suspended it prior to activating the inbound leg Point D Between CF005 to FF005 1 Note that the flight plan waypoints used as step down fixes are depicted on the Jeppesen Approach Plate but not on the NOS charts 2 If you are using an NOS chart you m...

Page 314: ...and MA005 1 Continue to the Missed Approach Point MA005 2 Verify that the OBS HLD and Approach Active annunciators are lighted Point F Turning to intercept 165 to MUGGZ 1 When you reach the Missed Approach Point and you wish to fly the published Missed Approach procedure press OBS HLD as you start your climbing right turn 2 The CDI will scale back to Approach Transition CDI sensitivity The MAP MUG...

Page 315: ...GGZ 1 As we already have selected 165 as the inbound to MUGGZ and sequencing is suspended we are set up for the hold 2 Enter and fly the published holding pattern just as you would if MUGGZ was a VOR and you had selected 165 on your OBS Point H Holding Pattern Fly the holding pattern Note If you are going to reshoot the approach select MUGGZ as the IAF in your approach sequence again While holding...

Page 316: ...Notes 300 ...

Page 317: ...phase is in addition to the currently provided En Route Terminal and Approach flight phases and is used for primary navigation in oceanic and or remote airspaces Definitions The following paragraphs define various terms that relate to the NMC s primary oceanic remote airspace operation Arm ing ed The manual entry sequence you use to instruct the NMC to change to the oceanic remote flight phase whe...

Page 318: ... flight phase when entering terminal airspace Deactivate The NMC s action that changes the state from active to armed and stops flying in the oceanic remote flight phase NOTE The NMC changes states from active to armed automatically if the aircraft enters terminal airspace In this case the NMC will change to the terminal flight phase NOTE The NMC changes states from active to armed if you press EN...

Page 319: ...ainty will be reported as Not Available As the operator of the NMC you can only arm or cancel the oceanic remote mode of operation The NMC does the rest The diagram below illustrates the different NMC flight phases except approach and their relationship for flight through terminal en route and oceanic remote airspace The diagram shows the NMC was armed before leaving terminal airspace and below th...

Page 320: ... and NANUs will indicate satellite outages in the following formats 1 PRNxx will be out of service FROM a date and time TO a date and time 2 PRNxx will be out of service FROM a date and time for hh hours 3 PRNxx will be out of service indefinitely FROM a date and time The RPIL pages permit you to specify satellite outages in any of these formats 304 Operations Introduction to Primary Oceanic Remot...

Page 321: ...ion may not be accurate due to bad or false satellite information GPS systems limited to VFR use must meet the exact same accuracy requirements as those authorized for IFR use Systems authorized for IFR use must also have an integrity monitor such as RAIM How Is Raim Used TSO C129a calls for three different levels of RAIM protection En route Terminal and Approach Plus the receiver has the ability ...

Page 322: ...ons 1 0 nm for Terminal operations and 0 3 nm for Approach operations What are En Route Terminal and Approach Operations Approach RAIM or 0 3 nm alarm limit is provided from 2 0 nm inbound to the FAF until you cancel the Approach Active operation usually at the MAP Approach RAIM is provided only if an approach is loaded into your active flight plan and it is enabled Terminal RAIM or 1 0 nm alarm l...

Page 323: ...ated to the three RAIM alarm limits of En route Terminal and Approach The equipment states are defined by the CDI sensitivity and operational requirements When you depart an airport the equipment is operating En route but it is providing Terminal RAIM integrity When you reach a point 30 nm from your destination airport 307 RAIM Operations ...

Page 324: ...nal satellites in the sky the time of day the location the receiver design the antenna mask angle and location and on the method of baro aiding The Apollo NMS has been designed such that with an optimal 21 satellites in operation Approach RAIM availability should exceed 95 There are currently at the time this manual was published at least 24 satellites in operation however the Federal Navigation R...

Page 325: ...may still be available even when Approach RAIM integrity is not If so your navigation display will again become valid and you may continue to use the Apollo GPS for missed approach navigation What does a RAIM alarm mean A RAIM alarm means that the navigation data can not be trusted to be within the alarm limit A RAIM alarm means that the Apollo NMS has determined that there is something wrong with...

Page 326: ...ellite can occur During that time there is no way for a GPS receiver to know that the information from that satellite is bad 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 310 Operations RAIM ...

Page 327: ...e flight plan sequences to the next waypoint as soon as I re enable sequencing 1 Press OBS HLD to disable sequencing 2 Press FPL Then turn the Small knob to show the waypoint you want active on the TO side 3 Press ENT twice to select the desired leg 4 Remember to press OBS HLD to re enable sequencing when established inbound Why do I sometimes see several degrees difference in what the Apollo NMS ...

Page 328: ...oach Tokyo you must travel southwest The effect of these small discrepancies is generally negligable over the relatively short distances used for most flight legs that you will navigate What if I manually activate a leg and it i m m e d i a t e l y sequences to a new leg This will happen if you were on the FROM side of the leg when you activated it if you did not press OBS HLD first to disable seq...

Page 329: ...service life of this type of battery is from 5 to 10 years This is not a user replaceable item The lithium battery must be replaced by the factory an authorized dealer or service center If You Have A Problem Please read the instructions again for the desired function If You Are Unable To Correct The Problem Record as much information as possible such as where and when the problem occured symptoms ...

Page 330: ...heck the static bonding straps on all control surfaces If the problem continues skin mapping may be necessary Indication Problem Same as above The aircraft is flying out of the coverage area for the selected chain Action Use Auto GRI or manually select a new GRI Indication Problem Same as above If the MSG light comes on and stays on after takeoff or run up noise from the aircraft alternator or mag...

Page 331: ...e problem clears Indication Problem MSGlightison Displayedmessageis LORAN1 or 2 TD SENSOR 1 or 2 FAILURE The Loran TD sensor has failed Action Return MCLS for service Indication Problem Bearinganddistance displaysappeartobe wrong A mistake was made in entering the Latitude Longitude coordinates of a User waypoint or the wrong waypoint is selected Action Verify that coordinates of the User waypoint...

Page 332: ...LORAN1 STATIONS HAVE LOW SNR The wrong Loran GRI is manually selected Action Use Auto GRI or manually select an appropriate GRI Indication Problem Same as above Required secondary is shut down Action Check Loran signals in SYS mode to see if unit is receiving signals from each station Indication Problem Same as above Signal is weak due to distance from transmitters Action You may not obtain lock o...

Page 333: ...t work inside a hanger Indication Problem MSG light stays on after power up Displayed message is IN USE POSITION SENSOR CANNOT COMPUTE LAT LON The In Use position sensor is not able to calculate a position Action Select a different position sensor Indication Problem MSG light is on after run up Displayed Message is LORAN1 or 2 EST POS ERROR EPE IS 1 8NM Noise generated from the aircraft alternator...

Page 334: ...prepared tooffer the following information about the installation Ö system configuration including number of NMCs sensor antennas etc Ö model numbers part numbers with mod level and serial numbers Ö software SW version numbers Ö firmware FW version numbers Ö description of problem Ö efforts made to isolate the problem Ö mounting location of each system component Ö computed lat long position shown ...

Page 335: ...t used for GPS nonprecision approaches that is concurrent with approach RAIM integrity and full scale deflection at 0 3 nm During approach active mode approach is enabled the MAP is the current TO waypoint and waypoint sequencing is on HOLD Approach Enabled A state that allows automatic transition to approach active mode When approach is first enabled the flight mode transitions from terminal to a...

Page 336: ...ired course of travel Course Deviation Indicator CDI A graphic indicator of course deviation typically shown as a graduated horizontal bar with an icon indicating the deviation distance left or right of course Common Traffic Advisory Frequency CTAF 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 NMC contains a...

Page 337: ...2 0 nm RAIM alarm limit EPE Estimated Precision Error Ephemeris A list of accurate positions or locations of a celestial object as a function of time Estimated Time of Arrival ETA Estimated Time Enroute ETE F FAF Final Approach Fix Fix A geographical location determined by either visual reference or by electronic navigation aids G GDOP Geometric Dilution of Precision The relationship between error...

Page 338: ...lel to the equator measured in degrees minutes and seconds north and south of the equator Longitude Lon Any line from the north to the south pole measured in degrees minutes and seconds of a circle east or west of the Prime Meridian Greenwich England M Magnetic North The region some distance from the geographic north pole where the earth s magnetic lines concentrate A magnetic compass points to th...

Page 339: ...dvisory to NAVSTAR Users 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 NAVigation System with Time And Ranging Non Directional Beacon NDB A low frequency medium frequency navigation aid sending non directional signals that can be used for...

Page 340: ...igational aid beginning at the navigational aid and proceeding outward in a straight line RAIM Receiver Autonomous Integrity Monitoring A method of predicting possible system accuracy errors that may be caused by bad satellite data The RAIM algorithm requires that more satellites are available and usable than required for a normal GPS position fix RAIM Alarm A signal that with RAIM available RAIM ...

Page 341: ...Route A predefined sequence of waypoints used before arrival procedures Statute Mile A distance measurement equal to 5 280 feet or 0 87 of a nautical mile T Terminal EPE Loran EPE limit of 1 7 nm Terminal Operations The phase of flight within 30 nm of the departure airport or the destination airport when approach is not enabled During terminal operations terminal RAIM integrity is used For Loran t...

Page 342: ... England Also referred to as Zulu time UTC Differential The difference in time between that at the present position and UTC Universal Transverse Mercator Map Projection System UTM Also known as Military Grid Coordinates the UTM grid consists of 60 north south east west zones each six degrees wide in longitude V Very High Frequency Omnirange VOR A navigational aid that transmits signals such that a...

Page 343: ...h satellite transmits at the same frequency 1575 42 MHz The GPS equipment in the Apollo Navigation Management System NMS only receives signals The receiver looks for the satellites by searching for the codes transmitted by each satellite Each satellite found is used to determine a position solution An additional satellite is used to determine the time differences between the time of signal transmi...

Page 344: ...acquire all of the required almanac information the first time it is turned on If you use your GPS receiver regularly it should always have a current almanac and you won t have to wait very long The almanac only provides an approximate location for each satellite so the receiver knows where to begin to look Information that pinpoints the exact location of the satellite is also transmitted about ev...

Page 345: ...all error will have an effect on overall accuracy Clock error can contribute a real distance error of about two feet Ephemeris information is a prediction of a satellite position in space The actual position of the satellite might differ slightly and can contribute to an error of about two feet at the GPS receiver The calculation of distance used to fix a position of a GPS receiver depends on know...

Page 346: ...l yield a 2D or horizontal position with only three satellites but is not as accurate as when four satellites are used A three dimensional fix 3D includes altitude information GPS altitude is calculated according to an ideal model WGS 84 spheroid The GPS altitude is determined by the distance calculated to be the height above an ideal ellipsoid model of the earth designed to closely approximate th...

Page 347: ...tion will remain constant throughout the simulation The NMC uses a simulated GPS sensor to provide position altitude speed and course information As no external sensors are connected while the simulation is running no information is displayed about external sensors The simulated altitude does not change while the Flight Simulator is running so the Altitude Assist functions will show that you are m...

Page 348: ... the flat blade screwdriver provided P N 555 0500 Insert the screwdriver blade into the face plate holes as shown in Figure 1 to reach the mounting rod screw heads 2 Pull the unit straight out of the mounting tube 332 Flight Simulator Apollo NMC Mounting screw holes APOLLONAVIGATION MANAGEMENT SYSTEM 2001 NAV DB FPL SYS M S G G E M ABQ PDX SLE ARPT VOR ARPT FROM TO NEXT INFO SEL ENT D Figure 1 Apo...

Page 349: ...NMC 1 Unscrew the four Dzus mount screws on the NMC front panel by turning them 1 4 turn counterclockwise with a flat blade screwdriver 2 Pull the unit out of the panel Disconnect the avionics connector ground wires and air flow tube from the back of the unit 333 Apollo NMC Flight Simulator Dzus mount screws Figure 2 Apollo NMS Dzus Mount Front Panel ...

Page 350: ...om your aircraft to use the Flight Simulator 1 Remove the NMC from the aircraft 2 Plug the external power supply into a 120 VAC socket 3 Insert the power cord into the power connector shown in Figure 3 or 4 334 Flight Simulator Apollo NMC Figure 3 Panel Mount Apollo NMC Rear Connections Figure 4 Apollo NMC Dzus Mount Rear Connections ...

Page 351: ...te functions Action Explanation 1 Push in or turn the power switch APOLLO NMC BY II MORROW NAV The owner name is displayed for approximately 2 seconds If you have not entered your name the display will read Property of No Name Entered PROPERTY OF WILBUR WRIGHT NAV The data card information is displayed for approximately 3 seconds WEST NORTHAM DB DATE 05 30 99 VERSION 1 11 NAV 335 Apollo NMC Flight...

Page 352: ...ATABASE ENTER MANUAL MAG VAR 09 W NAV Turn the Large knob to make the variation direction flash Turn the Small knob to display E or W Pressing ENT enters the displayed magnetic variation NO DATABASE ENTER MANUAL MAG VAR 09 E NAV If you have changed the default factory airspace alert settings the following display appears for approximately 3 seconds AIRSPACE SETTINGS ARE NON STANDARD NAV 336 Flight...

Page 353: ...ngs the following display appears for approximately 3 seconds EMERGENCY SEARCH SETTINGS ARE NON STANDARD NAV 3 Only if adjusting the Date Time The date and time are displayed for confirmation The time setting is displayed as UTC Universal Coordinated Time formerly Greenwich Mean Time If the date and time are incorrect press the SEL button to activate editing DATE 06 MAY 99 TIME 11 18 UTC NAV 337 A...

Page 354: ...to make the next information to change flash Turn the Small knob to display the desired information Repeat as necessary to edit the Time and Date DATE 09 JUN 99 TIME 11 18 UTC NAV Pressing ENT enters the displayed time and date The power up sequence will continue FLIGHT SIMULATOR NOT FOR FLIGHT PRESS SEL NAV 338 Flight Simulator Apollo NMC ENT ...

Page 355: ...AV Turn the Large knob to make the altitude value flash Turn the Small knob to display the desired altitude SIMULATOR SETUPS GR SPEED 240KTS ALTITUDE 4000FT NAV Pressing ENT enters the displayed ground speed and altitude values and starts the flight simulation The NMC is placed in NAV mode and a simulated GPS sensor begins tracking your position from the first FROM waypoint in the Active flight pl...

Page 356: ...e the simulator is running are retained when the NMC is reinstalled in the aircraft After the NMC is Re Installed in the Aircraft To acquire a position the system must know is approximate location and if using GPS sensor s the UTC time After using the Flight Simulator the NMC remembers the last simulated location it was at when the power was turned off At power up the NMC will use this location in...

Page 357: ... Keypad These pages supplement your Apollo NMC Operating Manual and includes information for use with the Apollo 2002 2102 Keypads Place these pages in the rear portion of your NMC Operating Manual behind the tab labeled Supplements Other P N 560 0168 00 ...

Page 358: ...138 History of Revisions January 1996 Original Release Ordering Information To receive additional copies of this document order part 560 0168 00 NMC Operating Manual Supplement for the Apollo 2002 Keypad The Apollo NMC Operating Manual ispart 560 0164 Warranty Information The Apollo 2002 2102 Keypads carrie the same II Morrow limited warranty as your Navigation Management Computer Refer to the ter...

Page 359: ...if a number value is flashing you can only enter a number A letter would not be allowed When the NMC accepts a character the next character to the right will flash This allows you to use the keypad to continue changing other characters without turning the knobs on the NMC The ENT button on the keypad serves the same function as on the front panel of the NMC Press the ENT button to save the entered...

Page 360: ...ill select the following waypoint types as shown below Press this Keypad Letter Waypoint Item Selected L Airport LFAC Landing Facility I Intersection V VOR N NDB R Runways if in your database Intersections will be displayed as INT x where x is the database type Pressing I will take you to the Intersection waypoint type You then turn the Large knob to move to the identifier field Pressing the lette...

Page 361: ...h Fix 267 Initial Approach Fix 266 Missed Approach Point 270 Procedures 259 Arc Assist 249 Auto Descent Setting Editing 93 Starting Stopping 98 Auto Nav Scroll 79 Time Setting 185 Auto Descent 95 B Barometric pressure 89 Barometric Pressure 206 Basic Concepts 1 Battery replacement 313 Buffer Altitude 91 Buttons 3 C CDI Scaling Automatic 199 CEP 328 Controls Direct To Button 3 ENT Button 3 INFO But...

Page 362: ...est Activation 207 Display Units 196 Displays LED Display 2 Sub page Indicator 3 Distance to waypoint 103 DME Arc 249 Dzus Mount 333 E Editing Display description 7 Emergency Mode 4 Emergency Search 20 30 EMG Displays 27 EMG Mode 25 Description 4 Displays 27 Organization 26 EMG Mode Procedures Runway Limits Setting 36 Ending Altitude 95 ENT button 3 Ephemeris 328 ETA to waypoint 104 ETE to waypoin...

Page 363: ...ce 327 Satellite Status 173 Status 173 GPS Altitude Calibration 87 GPS Status 172 GRI Manual Selection 215 Triad Manual Selection 216 H Hold Altitude Setting Editing 90 Hold Continue 106 I Intersection Database 111 Introduction to Primary Oceanic Remote Airspaces301 302 303 304 K Keypad 1 Knobs 2 L Large Knob 2 LED Display 2 Local Altimeter Setting 206 Loran Sensor 214 216 218 Loran Stations Manua...

Page 364: ...69 70 71 72 73 74 75 76 77 78 NAV Displays63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 Organization 62 Procedures 79 Sub Displays 68 Nav Mode Procedures Nav Information Displaying 79 NAV Mode Procedures Altimeter Setting 87 GPS Altitude Calibration 87 Present Position Displaying 80 Navigation Displays 13 Navigation Information 179 Default Navigation Displays 13 Eight Character Items 70 Sixteen ...

Page 365: ...way Limits 36 S Searching Around A Waypoint 33 SEL button 3 Selective Availability 329 Self Test 16 Setting Display Units 196 Small Knob 3 Software and Database Versions Displaying 208 Special Use Airspace 19 58 Status Options Active 144 SUA Information Displaying 58 SYS Mode Description 5 SYS Mode Displays 163 164 165 166 167 168 169 170 171 172 173 174 175 176 177 178 System Info Sub State 167 T...

Page 366: ...g 127 Deleting 139 Editing 135 V Viewing Messages 41 VOR Database 109 111 W Waypoint Searching 33 Waypoint Comments Displaying 125 Waypoint Comments 121 Deleting 125 Entering Editing 122 Waypoint Information 121 Waypoint Retriever 7 115 Using Identifier 115 Description 7 Using City Facility Name 118 Using Identifier 115 Waypoints Displays 112 What is Primary Oceanic 301 Index Apollo NMC ...

Page 367: ...nc 2345 Turner Rd S E Salem OR 97302 U S A Phone 503 581 8101 1 800 525 6726 FAX 503 364 2138 In Canada 1 800 654 3415 http www iimorrow com Part 560 0164 01b July 1999 II MORROW V I S I O N A R Y T H I N K I N G T O D A Y ...

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