Elite AP-4000 User manual

O p e r a t o r ’ s M a n u a l
AP- 4 0 0 0 a v i o n i c m o d u l e s
R e l e a s e : O c t o b e r 2 0 1 9
w w w. f l y e l i t e . c h

Abstract
Thank you for purchasing an ELITE product. Since ELITE was rst introduced, each version has incorpo-
rated suggestions and ideas from our customers  student and academic general aviation and professional.
Through valuable customer feedback we were able to constantly enhance ELITE's PC-based simulation soft-
ware, so please let us know what you think of ELITE XTS.
ELITE (ELectronic IFR Training Environment) is a software that allows you to use your personal computer
to replicate the instrument panel, avionics and ight aerodynamics of specic aircraft to practice all proce-
dures and simulate elements of ight under instrument meteorological conditions.
This Operator's Manual is to give an insight of the options and training possibility that ELITE XTS oers.
If you have any questions or run into some trouble, please feel free to reach out to our Technical Support team.
ELITE Technical Support
www.flyelite.ch/support
support@yelite.ch

Contents
1 AP-4000 2
1.1 RadioNavigationReceivers ..................................... 2
1.1.1 COM/NAV.......................................... 3
1.1.2 DMEReceiver ........................................ 3
1.1.3 ADFReceiver......................................... 4
1.1.4 Marker Receiver and Audio Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4
1.1.5 Transponder ......................................... 5
1.2 EFS40-EADI/EHSI ........................................ 5
1.3 Autopilot ............................................... 6
1.3.1 KAP150/KFC150..................................... 6
1.3.2 APENG ........................................... 7
1.3.3 HDG.............................................. 7
1.3.4 NAV.............................................. 7
1.3.5 APR/GS/BC......................................... 7
1.3.6 ALT.............................................. 8
1.3.7 CWS.............................................. 8
1.3.8 FD............................................... 8
1.4 Altitude/Vertical Speed Selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8
1.4.1 AltitudePre-Select...................................... 8
1.4.2 Vertical Speed Pre-Select . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9
1.5 CRS/HDG.............................................. 9
2 Conclusion 10
2.1 Troubleshooting............................................ 10
2.2 Notes ................................................. 11

1|AP-4000
1.1 Radio Navigation Receivers
ELITE is equipped with up to four radio navigation receivers (NAV1, NAV2, ADF, DME), and two commu-
nication receivers (COM1, COM2). Instead of NAV1/COM1 a GPS device can be ordered, e.g. a GNS530
or a GTN750.
Figure 1.1: Radio Navigation
2

CHAPTER 1. AP-4000 1.1. RADIO NAVIGATION RECEIVERS
1.1.1 COM/NAV
On the "COM1/NAV1", "COM2/NAV2", and the "ADF" receivers, the displays on the right hand side show
the standby, the left displays show the active frequency. Setting a frequency is done in the same way as on
a real receiver. Use the inner/outer rotary to count up or down the standby frequency, or, if operating the
device with the mouse, click on the numbers themselves (Clicking on the right side of the number decreases
and clicking on the left side increases the value). Pushing the double-arrow button will toggle ("ip-op")
the frequencies. Each receiver may be switched on and o individually by turning (or dragging, if operated
with the mouse) the On/O button.
Figure 1.2: COM/NAV Module
The identication code of the currently selected "NAV" station will be audible over the connected speak-
ers, when the Ident button is pressed and the corresponding switch on the audio panel is on. When the
RAD button (Radial) on the NAV1 or NAV2 receiver is activated, the actual radial from the VOR station
is displayed in place of the standby frequency. While in the radial mode turning the knobs directly sets the
active frequency. There is no radial available when an ILS frequency is tuned.
1.1.2 DME Receiver
Figure 1.3: DME Receiver
The LED brightness can be adjusted by turning the DIM/BRT knob. The DME device has three dierent
operation modes, RMT, FREQ and GS/T.
RMT Mode
Distance, Ground Speed and TTS of remote frequency are displayed.
By activating the R1 or R2 button, the corresponding frequency is automatically taken from the NAV1 or
the NAV2 receiver. Search time is about one second. When no ground station can be locked, dashes will
be displayed. Distance, Ground Speed and TTS are only available if the station remotely tuned is DME
equipped.
Frequency Mode
Distance and selected frequency are displayed.
The DME receiver is in the frequency mode by default. It is then channelled internally with its own two
concentric frequency selection knobs (rotary dials) which set the active frequency. If a tuned station is DME
equipped, the relative distance to the station is indicated.
3

CHAPTER 1. AP-4000 1.1. RADIO NAVIGATION RECEIVERS
GS/T Mode
Distance, Ground Speed and TTS (Time-to-Station) are displayed.
Activating the Ground Speed (GS) button results in displaying the Ground Speed relative to the DME station
(in knots) instead of the DME frequency. In addition, the Time-to-Station (TTS) is displayed. Rotating the
frequency selector will have no eect on the display, because the DME is in "Frequency Hold". This mode
prevents accidental channelling of the DME when the frequency is not displayed.
1.1.3 ADF Receiver
Figure 1.4: ADF Receiver ADF KR 27 TSO
The Automatic Direction Finder Receiver (ADF) in ELITE selects a Non Directional Beacon (NDB)
in the frequency range ±600 Hz around the frequency set. This means that, for example, an NDB with a
frequency of 371.5 kHz may be received with the ADF set to either 371 or 372.
Note: When a receiver is tuned to a frequency, the closest NAVaid with this frequency is received. When
two facilities in the same area have identical frequencies, ELITE will show a dialog box to select the desired
one.
1.1.4 Marker Receiver and Audio Panel
Figure 1.5: ELITE Marker Receiver
The Marker Receiver can be switched to LO, HI and TEST. The LO selection may be made to set
marker reception to low sensitivity, i.e. markers will only receive data at a short distance, such as during
the approach. The marker lamp panel consists of the conventional:
• A lamp (white when lit, airway marker, inner marker)
• O lamp (blue when lit, outer marker)
• M lamp (amber when lit, middle marker)
When passing a marker, the appropriate identication code is heard while the corresponding marker lamp
ashes. The duration of the marker reception as well as the reception range depends on the type of marker.
4

CHAPTER 1. AP-4000 1.2. EFS 40 - EADI/EHSI
Figure 1.6: Marker Receiver / Audio / ALT-Preselet Module
1.1.5 Transponder
Figure 1.7: Transponder
The Transponder is a radio transmitter and receiver which operates on radar frequencies. Receiving
ground radar interrogations at 1030 MHz, it returns a coded response of pulses to ground-based radar on
frequency of 1090 MHz.
1.2 EFS 40 - EADI/EHSI
The Bendix/King EFS 40 is an advanced Electronic Flight Instrumentation System (EFIS) designed to meet
the demands of today's complex ight environment. The actual real-world EFS 40 has numerous installation
options/congurations that can be tailored to an individual aircraft and owner's preferences. The ELITE
EFS 40 installation consists of the ED 461 control/display unit, ED 462 display unit, and the CP 470 control
panel. The ED 461 and ED 462 function as the EHSI (electronic horizontal situation indicator) and EADI
(electronic attitude direction indicator) respectively while the CP 470 is a separate control panel for the
EADI. The EFS 40 EFIS is selectable in all aircraft currently available.
To select and add the EFS 40 EHSI by itself or the EHSI/EADI combination to any aircraft, simply go to
the Conguration Page and select the corresponding option as desired under the Instrument Conguration
column.
The complete EFS 40 Pilot's Guide is on the Main ELITE USB Memory stick and is also available at
www.bendixking.com . Refer to the Pilot's Guide for specic operational techniques. Some of the EFS 40
functions are briey outlined in the following diagrams. Please note that although most of the actual EFS
40 features/functions have been implemented in the ELITE EFS 40 unit, due to the numerous real world
installation options/congurations possible, not all features/functions are available.
The EFS 40 EADI utilises the CP 470 control panel (as shown in image 1.9. Mode controls that are used
with the EHSI are located on the periphery of the EHSI instrument itself.
Some features include but are not limited to the following:
• Heading-Sync feature : Click on center of knob to automatically set heading bug to current aircraft
heading.
• Direct-To feature : Click on center of knob to automatically set course pointer and digital course
readout to the direct course of the selected NAVAID or active waypoint.
5

CHAPTER 1. AP-4000 1.3. AUTOPILOT
Figure 1.8: EFS 40
Figure 1.9: CP 470 Control Panel
1.3 Autopilot
1.3.1 KAP 150 / KFC 150
The KFC 150 and KAP 150 are both two-axis automatic pilot systems that operate almost identically. These
autopilots each provide pitch and roll stabilization and automatic trim, as well as automatic response to all
selected autopilot modes. The only dierence being the KFC 150 also has a ight director (FD) function.
Since the KAP 150 does not have a FD function it uses a standard attitude reference without V-bar com-
mands.
To use the KAP 150 and KFC 150 autopilots refer to the instructions within the next few sections
Note: Press the TEST button and wait for the system to perform its self-test function, before
you start using the Autopilot.
6

CHAPTER 1. AP-4000 1.3. AUTOPILOT
Figure 1.10: KAP 150 / KFC 150
1.3.2 AP ENG
The most basic form of autopilot operation is to engage only the autopilot engage (AP ENG) mode button.
In this mode, with no other modes selected, the aircraft will maintain the pitch attitude existing at the time
of AP ENG engagement and will y with the wings level. Use of the vertical trim (UP/DN) switch in this
mode will aect an approximate 0.9 degree per second pitch change.
1.3.3 HDG
In heading (HDG) mode the aircraft will maintain the heading selected by the heading bug. Be sure to place
the heading bug in the desired position before engaging the HDG button, as the aircraft will immediately
begin turning in the shortest direction toward the bug.
1.3.4 NAV
In navigation (NAV) mode the autopilot will intercept and track VOR courses. To use the autopilot with
a conventional CDI-type VOR indicator rst make sure the autopilot is in HDG mode and then tune the
desired navigation frequency. Set the OBS to the desired course and then depress the NAV button causing
the NAV indicator to ash signifying the mode is armed. Within ve seconds move the heading bug to the
same value as selected on the OBS. The autopilot will then y a 45 degree intercept heading until course
capture whereupon the system will track the desired course.
Note: The NAV indicator will not ash if the NAV mode is selected while the aircraft is level
within ±4 degrees and 2-3 dots of course deviation, but will rather go immediately into NAV
mode directly.
To use the navigation feature of the autopilot with a HSI, rst tune the navigation frequency. Use the
Course Set Knob to select the desired course line value. Set the intercept angle by placing the heading
bug on the desired heading and press the HDG button, if not already in HDG mode. Now press the NAV
button and y the selected heading until course capture. The NAV light will ash until course interception
to indicate that it is armed.
1.3.5 APR/GS/BC
To use the autopilot in approach (APR) mode st make sure that the system is in HDG mode if using a
conventional CDI-type VOR indicator. Tune the appropriate ILS, LOC or VOR frequency. Set the OBS to
the nal approach course. Note that if intending to y a back course be sure to use the front course setting.
Press the BC (Back Course) button after pressing the APR button. Press the APR button causing the APR
light to ash indicating it is armed. Turn the heading bug to the inbound course within ve seconds. The
system will y a 45◦ degree intercept heading until capturing the course. If ying an ILS the GS will be
captured automatically causing the GS light to illuminate.
If using the APR mode with an HSI please tune the appropriate ILS, LOC or VOR frequency rst. Use the
Course Set Knob to set the desired nal approach course. Turn the heading bug and press the HDG button
if not already in HDG mode. Press the APR button. The autopilot will y the desired heading until course
capture. The BC and GS features operate the same way as described above.
7

CHAPTER 1. AP-4000 1.4. ALTITUDE/VERTICAL SPEED SELECTOR
1.3.6 ALT
To operate in altitude hold (ALT) mode rst y to and level o at the desired altitude and then press ALT.
Altitude adjustments may be made in ALT mode by using the vertical trim (UP/DN) switch. Moving this
switch in either direction while in ALT mode will cause the aircraft to climb or descend at approximately
500 fpm. When the switch is released the autopilot will maintain the new altitude.
1.3.7 CWS
The control wheel steering (CWS) button located on the control yoke allows the pilot to manoeuvre the
aircraft in pitch and roll with out disengaging the autopilot. The autopilot resumes control when the button
is released.
1.3.8 FD
KFC 150 only
The KFC 150 has a ight director (FD) function that the KAP 150 does not. ELITE aircraft modules using
this autopilot have a V-bar that appears on the attitude indicator anytime the FD or AP ENG features are
selected. If the FD function only is selected the V-bar will command the user to make control inputs to
satisfy the system requirements by manoeuvring the orange delta wing into the V-bar.
1.4 Altitude/Vertical Speed Selector
Figure 1.11: Altitude/Vertical Speed Selector
This feature is available only for the Bonanza, Baron, Seneca III and King Air (King radio option) aircraft
modules. The KAS 297B oers the user the ability to pre-select altitudes and vertical speeds while using
the autopilot.
1.4.1 Altitude Pre-Select
To pre-select an altitude the unit must rst be indicating ft. If it does not indicate ft then either push in the
inner concentric knob if using a mouse or ip the toggle switch to ALT if using an ELITE avionics panel.
8

CHAPTER 1. AP-4000 1.5. CRS / HDG
Using the knob(s), choose the desired altitude and then press the ARM button to arm the altitude capture
mode. This will cause ARM to appear on the indicator. Use pitch attitude hold or select a vertical speed to
guide the aircraft to the desired altitude. As the aircraft nears the desired altitude the system computes a
roundout and will indicate altitude capture (CAPT) as the aircraft levels o. Once the aircraft has levelled
o, the vertical speed mode disengages and the CAPT indication disappears.
Altitude alerting is provided by the KAS 297B and alerts the user with a two second aural tone at ±1000
ft from the target altitude. An alert annunciation comes on with the tone and stays on until 300 ft from
the target altitude. The aural tone also sounds again for two seconds when the aircraft reaches its selected
altitude. The system also provides an aural warning any time the aircraft's altitude varies more than 300
feet from the selected altitude after level o.
1.4.2 Vertical Speed Pre-Select
To pre-select a vertical speed the unit must rst be indicating ft/min. If not, pull the inner concentric knob
when using a mouse or ip the toggle switch to V/S when using an ELITE avionics panel. Use the knob(s)
to select the desired vertical speed. The indicated up/down arrows show whether a climb or descent has
been selected. To engage the selected rate press ENG and VS will appear on the indicator. Engaging the
vertical speed function will cancel the ALT mode if being used. There are several ways to change the rate
of vertical speed once the function is engaged:
1. By rotating the knob while in V/S mode
2. By pressing the CWS button on the yoke and pitching to a new vertical speed value
3. By pressing the vertical trim switch on the autopilot. Using the vertical trim switch will aect a 100
feet per minute change in vertical speed for every second it is pressed
1.5 CRS / HDG
Figure 1.12: ELITE Course / Heading
The Course/Heading panel of the Avionics stack is used to set course and headings using either the HSI/
ight director (if equipped) or using VOR #1 OBS and VOR #2.OBS.
The barometric pressure can be set by turning the ALT knob.
The MDI knob has dierent functions, depending on the aircraft module loaded. In aircraft equipped with
an radio magnetic compass the MDI button selects the course, on aircraft equipped with a radio altimeter
(e.g. the Beech King Air) the MDI button selects the radio altimeter bug.
A 2-position switch (CRS or OBS) is used to assign the CRS knob to function as a course selector for HSI
or OBS.
The module also includes buttons for Freeze, the Instrument Panel and the Map page to speed up the
selection of the most important pages.
9

2|Conclusion
2.1 Troubleshooting
As this document is to give an overview of the possibilities within ELITE and how to handle the software,
it does not include any troubleshooting topics nor steps to resolve this.
In case you run into any issues, please check the document "Troubleshooting" on your USB Card / Download
File.
If there are any open questions regarding the installation or the setup of the software, please refer to the
installation manual. The most common issues that occur during the setup are also included in this documents.
The most frequent questions and issues are discussed in these documents. Please feel free to contact the
ELITE Support Team if the topic is not discussed in either of the two manuals.
ELITE Technical Support
www.flyelite.ch/support
support@yelite.ch
10

CHAPTER 2. CONCLUSION 2.2. NOTES
2.2 Notes
Please feel free to add any notes here:
11