This pilot's guide has been tailored by the installation and or certification agency to cover the following EFS 40/50 installation:
AIRCRAFT TYPE
AIRCRAFT TAIL OR SERIAL NUMBER
AIRCRAFT OWNER
EFIS TYPE (EFS 40 or EFS 50)
EFIS SYSTEM CONFIGURATION
EFIS SYSTEM SOFTWARE LEVEL
EFIS DISPLAY UNIT TYPE
EFIS CONTROL PANELS
REVERSIONARY MODES
Throughout this pilot's guide various configuration options are
described. A
check mark may be placed in the appropriate boxes to define which
configuration options are available in a given installation.
PLAN VIEW OPERATION (available with 07 and higher) 2.4.4
CHECKLIST OPERATION(available with 08 and higher) 2.4.5
ENT BUTTON 2.4.5
WAYPOINT ENTRY OPERATION 2.4.5
PLAN VIEW OPERATION(available with 07 and higher) 2.4.5
CHECKLIST OPERATION(available with 08 and higher) 2.4.6
TEST/REFERENCE2.4.6
CHECKLIST SELECT (available with 08 and higher) 2.4.6
TCAS ONLY SELECT (available with 08 and higher) 2.4.6
TOC.2
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
Table of Contents
Section 3
ABBREVIATED OPERATIONS3.1
Section 4
EHSI DISPLAYS4.1.1
EFS 40/50 COLOR STANDARDS 4.1.1
STANDARD EHSI DISPLAYS4.1.1
THREE TUBE EFS 40/50 7.6
FOUR TUBE EFS 40/50 7.7
FIVE TUBE EFS 40 7.8
FIVE TUBE EFS 50 7.9
Section 8
GLOSSARY 8.1
ABBREVIATIONS 8.1
Section 9
INDEX9.1
TOC.8
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
INTRODUCTION
Introduction
This pilot’s guide describes the
components, operation, and
operational procedures of the
BENDIX/KING EFS 40/50 Electronic Flight Instrumentation System (EFIS) containing system
software 04, 05, 06, 07, 08, 09,
10, 11, 12, 13, 14, 15, and 16.
The EFS40 system uses either a
single control display unit, four
inch ED 461, or a separate
C P 467 mode controller and four
inch ED 462 display unit for control and display of navigation data
and sensor selection. When a
Multi-Function Display is incorporated in the system, the
C P 469/A will control and select
navigation data for display on the
MFD. A CP 466A or CP 4 6 6 B
Equipment covered in this pilot's guide includes:
E D 4 6 1Control display unit, 4" X 4"
E D 462 Display unit, 4" X 4"
S G 4 6 4EHSI/MFD-only symbol generator
(not available with software 08 or later)
S G 4 6 5EFIS symbol generator
C P 4 6 6 AR D S 81/82/84 radar control panel
C P 4 6 6 BR D S 86 radar control panel
C P 4 6 7EFIS control panel with DH set and test
C P 4 6 8EFIS control panel, less DH set and test
C P 4 6 9MFD control panel
C P 4 6 9 AMFD control panel with Checklist,
TCAS and Joystick features
C P 4 7 0EADI brightness and DH set and test panel
E D 5 5 1Display unit, 5" X 5" (not available in current production)
E D 5 5 1 ADisplay unit, 5" X 5" (~16% larger symbols
compared with ED 461/2 presentation)
provides the radar control function when an RDS 81/82/84 or 86
weather radar is interfaced with
the system, and the associated
radar control/display unit is not
i n s t a l l e d .
The EFS 50 system uses a
remote CP 467 mode controller
and an ED 551/A display unit for
control and display of navigation
data and sensor selection. The
remote SYMBOL GENERATOR,
S G 464 or SG 465, interfaces
with the navigation sensors to
compute the display and EFIS
output data required by other
systems on board the aircraft.
The SG 464 is no longer available and has not been produced
with software versions 08 or later.
An Abbreviated Operations
section included in this manual
covers the functions of the EFS
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
40/50 in minimal detail. The
Abbreviated Operations section
gives a brief visual overview of
I.1Issued 8/10
Introduction
features and push button operations. However, it is necessary to
read the entire Pilot’s Guide for a
full understanding of the
E F S 40/50 system.
N o t e : The EFS 40/50 display
illustrations used in this pilot's
guide are artist's reproduc tions. Extreme care has been
taken to ensure the accuracy
of symbology placement and
relative size. However, it is
impossible to exactly duplicate
the display of a CRT and com pensate for all brightness lev els, as line width displayed on
the CRT varies with bright ness. In many cases, unrealis tic displays provide the most
informative display possible on
a single display. Therefore,
we ask that you use and treat
the graphic illustrations con taine
d in this pilot's guide as
they were intended. These
illustrations are to familiarize
the pilot with the type and
placement of data to be provid ed by the EFS 40/50.
ED 551A is the only version in
current production.
The data presented in this
pilot’ s guide is general in
nature and not tailored toward
a specific installation. Not all
equipment interfaces nor dis play options presented are cer tifiable in all aircraft types or by
all certification agencies. Each
installation may incorporate
different equipment comple ments and use different dis play options. For the unique
certified operating procedure
of a particular aircraft, refer to
the appropriate approved
Flight Manual Supplement for
that aircraft.
I.2
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
SYSTEM CONFIGURATION
System Configuration
GENERAL
Various configurations of the
E F S 40/50 system are currently
available to fulfill the particular
needs of the user. These configurations are differentiated by the
number of display units, type of
mode controller, number of symbol generators and the interfacing equipment.
The basic EFS 40 ( 2 tube four
inch Electronic Flight Instrumentation System) consists of:
• 1ea EHSI Control/Display
Unit (ED 4 6 1 )
• 1 ea EADI Display
Unit (ED 4 6 2 )
• 1 ea EADI control
panel (CP 4 7 0 )
• 1 ea Symbol Generator
( S G 4 6 5 )
• Or 1 ea remote EFIS
Control Panel (CP4 6 7 )
• 1 ea EHSI Display
Unit (ED 4 6 2 )
• 1 ea EADI Display
Unit (ED 4 6 2 )
• 1 ea Symbol Generator
( S G 4 6 5 )
The basic EFS 50 (2 tube five
inch Electronic Flight Instrumentation System) consists of:
• 1
ea remote EFIS Control
Panel (CP 467)
• 1 ea EHSI Display
Unit (ED 5 5 1 A ) ,
• 1 ea EADI Display
Unit (ED 5 5 1 A )
• 1 ea Symbol Generator
( S G 4 6 5 )
Beginning with software 09, a
configuration option was added
allowing an MFD only installation.
This option removes the heading
bug from the display allowing the
MFD SG to stand alone without
any other symbol generator in
the installation. The display unit
in this case can be either an ED
462 or ED 551A. The control
panel must be a CP 469A.
o MFD ONLY - no selected
heading bug.
Two new configuration options
for display unit (DU) type were
also added with software 09.
These options allow the MFD SG
to drive a 5” ED 551A MFD during normal operation and change
to eit
her ED 461 or ED 462 EHSI
and ED 462 EADI during standby
o p e r a t i o n .
o
MFD - ED 551A
EHSI - ED 461
EADI - ED 462
o
MFD - ED 551A
EHSI - ED 462
EADI - ED 462
Issued 8/10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
1.1
System Configuration
ED 551/A MFD & CP 469A
2 EA ED 462 & CP 467
2 EA ED 551A & CP 467ED 461, ED 462, & CP 470
Figure 1.1
CONTROL DISPLAY OPTIONS
CONTROL PANEL
The ED 461 Control/Display Unit
incorporates the EHSI mode controller in the bezel of the display,
reducing the required panel
space to 4” X 4”. For those installations that are not sensitive to
panel space, an independent display unit, ED 462, ED 551A, and
mode controller, CP 467, are
1.2
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
offered. Figure 1.1 depicts the
E F S 40/50 Control Display
O p t i o n s .
Regardless of which display unit
and method of control is selected, the system’s performance will
be identical. Both mode controllers offer a simple means for
the pilot to select the desired display format, such as standard
Issued 8/10
System Configuration
compass rose or sectored compass rose, 360-degree map or
sectored map and weather radar
overlay. Also incorporated on
the mode controller is the course
and heading select knobs with
auto sync. The auto sync feature
SYMBOL GENERATOR
The SG 464 EHSI/MFD-only
symbol generator is a remotemounted processing unit packaged in an ARINC 1/4 ATR short
form factor. The SG 4 6 5
EADI/EHSI/MFD symbol generator is a remote-mounted processing unit packaged in an ARINC
3/8 ATR short form factor. A version of the SG 465 3/8 ATR short
symbol generator is offered with
EHSI/MFD-only provisions.
will slew the heading bug to the
lubber line or the course pointer
to the DIRECT TO course for the
selected NAV sensor providing a
centered D-Bar. The CP 4 6 7
and CP 470 incorporate Decision
Height Set and Radio Altimeter
T e s t .
The SG 464 or SG 465 with software version 05 and above will
drive either the 4” X 4” (ED 4 6 1
or 462) or 5” X 5” (ED 551A) displays. Software version 06 incorporates the capability to drive the
E D 551 display. The SG 464 is
no longer available and has not
been produced with software versions 08 or later.
SG 464 AND SG 465 SYMBOL GENERATORS
Issued 8/10
Figure 1.2
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
1.3
System Configuration
1.4
Figure 1.3
TYPICAL EFS 40/50 SYSTEM BLOCK DIAGRAM
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
EQUIPMENT INTERFACE &
OPERATING CONFIGURATION
System Configuration
The EFS 40/50 equipment interface and operating configuration
is established at the time of
installation and certification. The
following pages are provided to
document the certified configura-
tion of a specific aircraft. Those
pages referring to software configuration versions not applicable
to this aircraft are to be removed
from this pilot’s guide.
Issued 8/10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
1.5
System Configuration
SOFTWARE 04 CONFIGURATION PAGES
The EHSI, EADI, and Reversion software will display these pages. All
items will be identical among all 3 displays, however, the ADI will not
be able to show the rack configurations, instead it will show the configuration data coming from the HSI and the data in its own EEPROM.
The descriptions given in this section refer to side 1 (left side) as the
pilot’s side and side 2 (right side) as the co-pilot’s side.
The EHSI, EADI, MFD and Reversion software will display the following pages. All display information will be identical on the EHSI and
MFD, however, the EADI will not display the rack configurations, it will
display a comparison of the EHSI and EADI configuration data. The
descriptions given in this section refer to side 1 (left side) as the pilot’s
side and side 2 (right side) as the co-pilot’s side.
The EHSI, EADI, MFD and Reversion software will display the following pages. All display information will be identical on the EHSI and
MFD, however, the EADI will not display the rack configurations, it will
display a comparison of the EHSI and EADI configuration data. The
descriptions given in this section refer to side 1 (left side) as the pilot’s
side and side 2 (right side) as the co-pilot’s side.
SOFTWARE 07 CONFIGURATION PAGES
(includes both 0701 and 0702)
The EHSI, EADI, MFD and Reversion software will display the following pages. All display information will be identical on the EHSI and
MFD, however, the EADI will not display the rack configurations, it will
display a comparison of the EHSI and EADI configuration data. The
descriptions given in this section refer to side 1 (left side) as the pilot’s
side and side 2 (right side) as the co-pilot’s side.