BendixKing SG 465 User Manual

Pilot’s Guide
EFS 40/50
Bendix/King®4-inch/5-inch
Electronic Flight
Instrumentation System
n
Registration
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.
4o
(check box) precedes each configuration option. A
Registration

Table of Contents

TABLE OF CONTENTS
Section I INTRODUCTION I.1
Section 1
SYSTEM CONFIGURATION 1.1
GENERAL 1.1 CONTROL PANEL 1.2 SYMBOL GENERATOR 1.3 EQUIPMENT INTERFACE & OPERATING CONFIGURATION 1.5 SOFTWARE 04 CONFIGURATION PAGES 1.6 SOFTWARE 05 CONFIGURATION PAGES 1.9 SOFTWARE 06 CONFIGURATION PAGES 1.12 SOFTWARE 07 CONFIGURATION PAGES 1.15 (includes both 0701 and 0702) SOFTWARE 08 CONFIGURATION PAGES 1.18 SOFTWARE 09 CONFIGURATION PAGES 1.21 SOFTWARE 10 CONFIGURATION PAGES 1.25 SOFTWARE 11 CONFIGURATION PAGES 1.29 SOFTWARE 12 CONFIGURATION PAGES 1.33 SOFTWARE 13 CONFIGURATION PAGES 1.37 SOFTWARE 14 CONFIGURATION PAGES 1.41 SOFTWARE 15 CONFIGURATION PAGES 1.45 SOFTWARE 16 CONFIGURATION PAGES 1.48
Section 2
EHSI OPERATION 2.1.1
DETAILED OPERATING CONTROLS 2.1.1 EHSI CONTROLS (ED 461 & CP 467/468) 2.1.1
1-2 NAVIGATION SYSTEM SELECT 2.1.3 NAV NAVIGATION SENSOR SELECT 2.1.3 HSI 360° MODE SELECTION 2.1.5 BEARING POINTER SELECT 2.1.6 ARC SECTORED MODE SELECTION 2.1.7 RANGE SELECTION 2.1.8 TST/REF 2.1.8
TST— 2.1.8 REF GROUND SPEED or TIME-TO-STATION selection 2.1.8
REF MAP FORMAT 2.1.9 COURSE SELECT KNOB 2.1.10 HEADING SELECT KNOB 2.1.10 DISPLAY BRIGHTNESS CONTROL 2.1.10
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EADI OPERATION 2.2.1
EADI DETAILED OPERATING CONTROLS 2.2.1
BRIGHTNESS 2.2.2 DH SET 2.2.2 RALT TST 2.2.2
RADAR OPERATION 2.3.1
RADAR CONTROLS, (CP 466A & CP 466B) 2.3.1
OFF-STBY-TST-ON 2.3.2
OFF 2.3.2 STBY 2.3.2 TST 2.3.2
ON 2.3.2 WX 2.3.2 WXA 2.3.2 GND MAP 2.3.2 LIGHTNING 2.3.3 VP 2.3.3 TRK 2.3.4 GAIN 2.3.5 PULL ARL 2.3.5 TILT 2.3.5
MFD OPERATION 2.4.1
MULTI FUNCTION DISPLAY CONTROL PANEL 2.4.1 CONTROL PANEL BUTTON OPERATIONS 2.4.2
COURSE SELECT KNOB/BUTTON 2.4.2 HSI BUTTON 2.4.2 ARC BUTTON 2.4.2 NAV BUTTON 2.4.2 1-2 BUTTON 2.4.3 BEARING #1 & #2 BUTTON 2.4.3 RANGE UP/DOWN BUTTON 2.4.3 JOYSTICK 2.4.3
WAYPOINT ENTRY OPERATION 2.4.3
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/REFERENCE 2.4.6 CHECKLIST SELECT (available with 08 and higher) 2.4.6 TCAS ONLY SELECT (available with 08 and higher) 2.4.6
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Table of Contents
Section 3 ABBREVIATED OPERATIONS 3.1
Section 4
EHSI DISPLAYS 4.1.1
EFS 40/50 COLOR STANDARDS 4.1.1 STANDARD EHSI DISPLAYS 4.1.1
NORMAL COMPASS CARD 4.1.1 NAVIGATION SOURCE ANNUNCIATION 4.1.2 SYMBOLIC AIRCRAFT 4.1.3 HEADING SELECT “BUG” 4.1.4 COURSE SELECT 4.1.4 LATERAL COURSE DEVIATION SCALE 4.1.5 LATERAL COURSE DEVIATION BAR 4.1.6 TO/FROM INDICATOR 4.1.6 DISTANCE, GROUNDSPEED and TIME-TO-STATION 4.1.6 DUAL MULTICHANNEL DME INSTALLATIONS 4.1.7 DME HOLD 4.1.8 BEARING POINTER 4.1.9 MAGNETIC/TRUE HEADING ANNUNCIATIONS 4.1.11 RADIO ALTITUDE 4.1.11 GLIDE SLOPE/VERTICAL NAVIGATION 4.1.11 WIND VECTOR 4.1.13 DRIFT ANGLE POINTER ( LNAV only) 4.1.13 LNAV MODE ANNUNCIATIONS 4.1.14
360 Map Displays 4.1.14
MAP 360 COMPASS CARD 4.1.15 SELECTED COURSE 4.1.15 MAP COURSE DEVIATION INDICATOR 4.1.16 TO/FROM 4.1.16 BEARING POINTER 4.1.16 REFERENCE WAYPOINT 4.1.16 RANGE RING 4.1.17 360-DEGREE MAP WX RADAR (IF EQUIPPED) 4.1.18 RDR 1400 WEATHER RADAR 4.1.19 LIGHTNING DETECTION 4.1.20 FULL TIME LNAV MAP 4.1.21
ARC (Expanded Sectored Mode) Displays 4.1.22
HDG BUG (ALL ARC FORMAT MODES) 4.1.22 COURSE DEVIATION INDICATOR (EHSI ARC NON-MAP FORMAT) 4.1.22
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Custom (Non-Standard EHSI) Displays 4.1.23
DOPPLER 4.1.23
COMPASS CARD 4.1.23
DOPPLER VELOCITY BARS 4.1.23
VELOCITY AND TARGET SCALE 4.1.23
LNAV GROUND SPEED AND READOUT 4.1.24
WIND VECTOR INFORMATION 4.1.24
TARGET WAYPOINT 4.1.24
TENDENCY CIRCLE 4.1.24
MEMORY 4.1.24
HEADING BUG 4.1.24 CABLE 4.1.25
COMPASS CARD 4.1.25
ANGLE BARS 4.1.25
FUNNEL SCALE 4.1.25
WIND VECTOR INFORMATION 4.1.25
OPTIMUM CABLE POSITION CIRCLE 4.1.26
THRUST COMMAND 4.1.26
HEADING BUG 4.1.26 HOMING 4.1.26
LATERAL DEVIATION BAR 4.1.27
EADI DISPLAYS 4.2.1
NORMAL ATTITUDE DISPLAY 4.2.1
PITCH ATTITUDE 4.2.1 ROLL ATTITUDE 4.2.1 ROLL INDICATOR 4.2.2
Sky Pointer Roll Scale 4.2.2
Roll Indicator Scale 4.2.2 PERSPECTIVE LINES 4.2.2 SYMBOLIC AIRCRAFT 4.2.2 HEADING TAPE 4.2.3 FLIGHT DIRECTOR COMMAND BARS 4.2.3 AUTOPILOT/FLIGHT DIRECTOR MODE ANNUNCIATION 4.2.4
STANDARD 429 AUTOPILOT/FLIGHT
DIRECTOR MODE ANNUNCIATION 4.2.4
SFIM CDV AUTOPILOT/FLIGHT
DIRECTOR MODE ANNUNCIATION 4.2.7 RADIO ALTIMETER 4.2.8 DECISION HEIGHT SET 4.2.9 DECISION HEIGHT ALERT 4.2.9 PRECISION APPROACH MODE FORMAT 4.2.9 EXPANDED LATERAL DEVIATION SCALE 4.2.9 RISING RUNWAY 4.2.10 GLIDESLOPE/VERTICAL NAVIGATION 4.2.11
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EADI OFF-SIDE ILS/MLS 4.2.11 MARKER BEACON ANNUNCIATION 4.2.12 FAST/SLOW OR COLLECTIVE DISPLAY 4.2.12 MACH DISPLAY 4.2.13 RATE OF TURN DISPLAY 4.2.13 CATEGORY II ANNUNCIATOR 4.2.14
CATEGORY II OPERATION ANNUNCIATIONS 4.2.14 DUAL EFS SYSTEM 4.2.14 SINGLE EFS SYSTEM 4.2.15
CATEGORY II THRESHOLDS 4.2.16 ATTITUDE MONITOR 4.2.17 CROSS COMPARATOR ANNUNCIATORS 4.2.17
RA 4.2.17
LOC 4.2.17
GS 4.2.17
ATT 4.2.17
HDG 4.2.18
COMPOSITE DISPLAYS 4.3.1
COMPOSITE MODE 4.3.1 HEADING TAPE 4.3.1 SELECTED COURSE 4.3.1 HEADING BUG SELECT 4.3.1 NAVIGATION SOURCE ANNUNCIATION 4.3.2 LATERAL COURSE DEVIATION SCALE 4.3.2 LATERAL COURSE DEVIATION BAR 4.3.2 TO/FROM 4.3.3 DISTANCE INFORMATION 4.3.3 DME HOLD 4.3.3
MFD DISPLAYS 4.4.1
CRS, NOT CRS SELECT 4.4.1 WEATHER ONLY 4.4.1
TRACK LINE 4.4.1 VERTICAL PROFILE (VP) 4.4.1
SYMBOLIC AIRCRAFT 4.4.1
RANGE RINGS 4.4.2
ALTITUDE LINE 4.4.2
PROFILE ANGLE 4.4.2 PLAN VIEW NORTH-UP MAP 4.4.2 CHECKLIST INTERFACE 4.4.3
LOADING AND MODIFYING CHECKLIST DATA 4.4.3
CHECKLIST PAGE ORGANIZATION 4.4.4
ROOT INDEX PAGE 4.4.4
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SUB INDEX PAGES 4.4.5 CHECKLIST ITEM PAGES 4.4.5 NOTE PAGES 4.4.6 CLEARING CHECKLIST ITEMS 4.4.6 EMERGENCY PAGE ACTIVATION 4.4.6 CHECKLIST CONTROLS 4.4.7
Checklist: CHKLIST 4.4.7
Joystick 4.4.7
Enter : ENT 4.4.8
HSI 4.4.9
ARC 4.4.9
NAV 4.4.9
Up Arrow 4.4.9
Down Arrow 4.4.9
1-2 4.4.9
RMI 1 4.4.10
RMI 2 4.4.10
CRS (NOT) SEL 4.4.10
TST REF 4.4.10
CRS Knob 4.4.10
REMOTELY MOUNTED SWITCHES 4.4.10 FAULT ANNUNCIATIONS 4.4.10 TCAS INTERFACE 4.4.11
TCAS ONLY SELECTION 4.4.11 TCAS DISPLAY FORMAT 4.4.12 TCAS TRAFFIC SYMBOLOGY 4.4.12
Intruder Symbols 4.4.12
Vertical Speed Arrow 4.4.12
Data Tag 4.4.12
Off-Scale Traffic 4.4.13
TCAS DISPLAY ANNUNCIATIONS 4.4.13
Traffic 4.4.13
TCAS 4.4.13
TCAS Status 4.4.14
TCAS Mode 4.4.14
Range 4.4.15
Above/Norm/Below 4.4.15
No-Bearing Traffic 4.4.15
FLXXX and FL 4.4.15
EGPWS INTERFACE 4.4.16
EGPWS SELECTION 4.4.16 EGPWS DISPLAY FORMAT 4.4.16 EGPWS MODE/STATUS 4.4.16 EGPWS RANGE 4.4.16
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Table of Contents
Section 5
OPERATING INSTRUCTIONS 5.1
PREFLIGHT PROCEDURES 5.1
START UP 5.1
SELF TEST 5.1
PUSH BUTTON TEST 5.1 PRE-TAKEOFF PROCEDURES 5.2 IN-FLIGHT OPERATION 5.2
ADF 5.2
LNAV (RNAV) 5.3
VNAV 5.3 APPROACH PROCEDURES 5.3
ILS APPROACH 5.3
BACK COURSE APPROACH 5.4
ADF APPROACH 5.4
LNAV (RNAV) APPROACH 5.4
VNAV GPS PRECISION APPROACH 5.4
VOR APPROACH 5.5
DECISION HEIGHT SELECTION 5.5 LIMITATIONS 5.5
EMERGENCY PROCEDURES 5.5
Section 6
FAULT ANNUNCIATIONS 6.1
GENERAL 6.1
EXTERNAL SYSTEM FAILURES 6.1
HEADING 6.1
ATTITUDE 6.1
FLIGHT DIRECTOR 6.1 EFS 40/50 SYSTEM FAILURES 6.1
DU—DISPLAY UNIT LOSS OF COOLING 6.1
SG—SYMBOL GENERATOR LOSS OF COOLING 6.1
CP—CONTROL PANEL (CP 467, CP 468,
ED 461 OR CP 470) 6.2
HEADING SELECT “BUG” 6.2
COURSE SELECT 6.2
RCP—RADAR CONTROL PANEL (if equipped) 6.2
SG—SYMBOL GENERATOR 6.2 RAW DATA DEVIATION ANNUNCIATIONS 6.3
BEARING POINTER ANNUNCIATIONS 6.3
ALPHANUMERIC READOUT ANNUNCIATIONS 6.3
CHECK CONFIG 6.3
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WEATHER RADAR ANNUNCIATIONS 6.4
WX FLT 6.4 WX OFF 6.4 BUSY VP 6.4 RT FLT 6.4 STB LMT 6.4 TGTALRT 6.4 TGT 6.4 429 FLT 6.4 ANT FLT 6.5 TX FLT 6.5 RANGE 6.5 STB OFF 6.5
WAIT 6.5 CUSTOM DISPLAY FAILURE ANNUNCIATIONS 6.5 DOPPLER/CABLE 6.5
EXTERNAL SYSTEM FAILURES 6.5
FMS Warning 6.5 Autopilot Warning 6.5
TCAS FAULT MESSAGES 6.6
Fault Messages for TCAS Fail 6.6
Fault Messages for No TCAS 6.6 LIGHTNING DETECTION DISPLAY FAULT MESSAGES 6.6
Section 7
REVERSIONARY MODES 7.1
CMPST - COMPOSITE 7.2 COPY OFF-SIDE 7.3 DISPLAY (EADI) DOWN 7.4 STBY - STANDBY 7.5 REVERSIONARY MODE SELECTION 7.6
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
INDEX 9.1
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INTRODUCTION
Introduction
This pilots 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 1 Control display unit, 4" X 4"
E D 462 Display unit, 4" X 4" S G 4 6 4 EHSI/MFD-only symbol generator
(not available with software 08 or later) S G 4 6 5 EFIS symbol generator C P 4 6 6 A R D S 81/82/84 radar control panel C P 4 6 6 B R D S 86 radar control panel C P 4 6 7 EFIS control panel with DH set and test C P 4 6 8 EFIS control panel, less DH set and test C P 4 6 9 MFD control panel C P 4 6 9 A MFD control panel with Checklist,
TCAS and Joystick features C P 4 7 0 EADI brightness and DH set and test panel E D 5 5 1 Display unit, 5" X 5" (not available in current production) E D 5 5 1 A Display 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
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40/50 in minimal detail. The Abbreviated Operations section gives a brief visual overview of
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Introduction
features and push button opera­tions. However, it is necessary to read the entire Pilots 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 pilots 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.
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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
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1.1
System Configuration
ED 551/A MFD & CP 469A
2 EA ED 462 & CP 467
2 EA ED 551A & CP 467 ED 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
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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 systems performance will be identical. Both mode con­trollers offer a simple means for the pilot to select the desired dis­play format, such as standard
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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
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Figure 1.2
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1.3
System Configuration
1.4
Figure 1.3
TYPICAL EFS 40/50 SYSTEM BLOCK DIAGRAM
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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 pilots guide.
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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 pilots side and side 2 (right side) as the co-pilots side.
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 01 2 I T E M 3 SG NUMBER _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 S I N G L E / D U A L _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 DU TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 ATTITUDE/HDG #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 ATTITUDE/HDG #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 RATE OF TURN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 ADF #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 ADF #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 VOR/ILS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 VOR/ILS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 02 2 I T E M 3 DME #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DME #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 MLS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 MLS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 FMS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 FMS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RNAV #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RNAV #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 TACAN #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 TACAN #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
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System Configuration
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 03 2 I T E M 3 V N A V _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 RADAR ALT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 AFCS TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 AFCS COMMAND BAR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 AFCS MODE ANN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 AIR DATA _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RADAR TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR CTL PNL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 RADAR INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 C H E C K L I S T _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 04 2 I T E M 3 J O Y S T I C K _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 RADAR GRAPHICS _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
— — — — — — — — — — | 1 VIEW/EDIT OPERATING CHAR PG 06 2 I T E M 3 VERT SCALE SIDE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DCLTR GS ON BC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 S P A R E _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DISPLAY WIND VEC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 DISPLAY DRIFT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 DG ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DME DIST ONLY _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 HOVER MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 . . M O R E . .
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1.7
System Configuration
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 07 2 I T E M 3 DISPLAY HDG TAPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 COMMAND BARS _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 ROLL INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DCLTR UNUS ATT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 CAT II AVAILABLE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 PERSPECTIVE LINES _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DH SELECT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 CABLE MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
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Issued 8/10
System Configuration
SOFTWARE 05 CONFIGURATION PAGES
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 pilots side and side 2 (right side) as the co-pilots side.
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 01 2 I T E M 3 SG NUMBER _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 S I N G L E / D U A L _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 DU TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 ATTITUDE/HDG #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 ATTITUDE/HDG #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 RATE OF TURN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 ADF #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 ADF #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 VOR/ILS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 VOR/ILS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 02 2 I T E M 3 DME #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DME #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 MLS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 MLS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 FMS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 FMS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RNAV #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RNAV #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 TACAN #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 TACAN #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
Issued 8/10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
1.9
System Configuration
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 03 2 I T E M 3 V N A V _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 RADAR ALT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 AFCS TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 AFCS COMMAND BAR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 AFCS MODE ANN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 AIR DATA _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RADAR TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR CTL PNL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 RADAR INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 C H E C K L I S T _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 04 2 I T E M 3 J O Y S T I C K _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 RADAR GRAPHICS _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 HOMING #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 HOMING #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
— — — — — — — — — — | 1 VIEW/EDIT OPERATING CHAR PG 06 2 I T E M 3 VERT SCALE SIDE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DCLTR GS ON BC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 FULL TIME FMS MAP _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DISPLAY WIND VEC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 DISPLAY DRIFT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 DG ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DME DIST ONLY _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 HOVER MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 MFD NAV CONTROL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
1.10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
System Configuration
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 07 2 I T E M 3 DISPLAY HDG TAPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 COMMAND BARS _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 ROLL INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DCLTR UNUS ATT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 CAT II AVAILABLE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 PERSPECTIVE LINES _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DH SELECT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 CABLE MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 SEL HDG SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 SEL CRS SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
Issued 8/10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
1.11
System Configuration
SOFTWARE 06 CONFIGURATION PAGES
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 pilots side and side 2 (right side) as the co-pilots side.
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 01 2 I T E M 3 SG NUMBER _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 S I N G L E / D U A L _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 DU TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 ATTITUDE/HDG #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 ATTITUDE/HDG #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 RATE OF TURN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 ADF #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 ADF #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 VOR/ILS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 VOR/ILS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 02 2 I T E M 3 DME #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DME #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 MLS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 MLS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 FMS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 FMS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RNAV #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RNAV #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 TACAN #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 TACAN #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
1.12
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
System Configuration
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 03 2 I T E M 3 V N A V _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 RADAR ALT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 AFCS TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 AFCS COMMAND BAR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 AFCS MODE ANN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 F/S AIR DATA _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RADAR TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR CTL PNL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 RADAR INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 C H E C K L I S T _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 04 2 I T E M 3 J O Y S T I C K _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 T C A S _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 HOMING #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 HOMING #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 LIGHTNING DET _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
— — — — — — — — — — | 1 VIEW/EDIT OPERATING CHAR PG 06 2 I T E M 3 VERT SCALE SIDE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DCLTR GS ON BC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 FULLTIME FMS MAP _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DISPLAY WIND VEC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 DISPLAY DRIFT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 DG ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DME DIST ONLY _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 HOVER MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 MFD NAV CONTROL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
Issued 8/10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
1.13
System Configuration
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 07 2 I T E M 3 DISPLAY HDG TAPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 COMMAND BARS _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 ROLL INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DCLTR UNUS ATT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 CAT II AVAILABLE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 PERSPECTIVE LINES _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DH SELECT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 CABLE MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 SEL HDG SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 SEL CRS SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 08 2 I T E M 3 NORTH UP MAP _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 VERT PTR TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 DISPLAY FMS MSG _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 SEL HDG COLOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 CMD BAR COLOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 REV MODE ANN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RISING RUNWAY _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 ADI DEV SRC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 CMD BAR FILTER _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
1.14
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
System Configuration
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 pilots side and side 2 (right side) as the co-pilots side.
——————————| 1 VIEW/EDIT EQUIPMENT PG 01 2 I T E M 3 SG NUMBER _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 S I N G L E / D U A L _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 DU TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 ATTITUDE/HDG #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 ATTITUDE/HDG #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 RATE OF TURN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 ADF #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 ADF #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 VOR/ILS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 VOR/ILS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 02 2 I T E M 3 DME #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DME #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 MLS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 MLS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 FMS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 FMS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RNAV #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RNAV #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 TACAN #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 TACAN #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
Issued 8/10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
1.15
System Configuration
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 03 2 I T E M 3 V N A V _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 RADAR ALT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 AFCS TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 AFCS COMMAND BAR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 AFCS MODE ANN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 F/S AIR DATA _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RADAR TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR CTL PNL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 RADAR INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 C H E C K L I S T _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 04 2 I T E M 3 J O Y S T I C K _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 T C A S _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 HOMING #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 HOMING #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 LIGHTNING DET _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 HOVER MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 CABLE MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
— — — — — — — — — — | 1 VIEW/EDIT OPERATING CHAR PG 06 2 I T E M 3 VERT SCALE SIDE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DCLTR GS ON BC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 FULL TIME FMS MAP _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DISPLAY WIND VEC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 DISPLAY DRIFT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 DG ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DME DIST ONLY _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 S P A R E _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 MFD NAV CONTROL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
1.16
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
System Configuration
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 07 2 I T E M 3 DISPLAY HDG TAPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 COMMAND BARS _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 ROLL INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DCLTR UNUS ATT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 CAT II AVAILABLE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 PERSPECTIVE LINES _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DH SELECT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 CTL PNL SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 SEL HDG SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 SEL CRS SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
1 VIEW/EDIT OPERATING PG 08 2 I T E M 3 NORTH UP MAP _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 VERT PTR TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 DISPLAY FMS MSG _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
6 SEL HDG COLOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 CMD BAR COLOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 REV MODE ANN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RISING RUNWAY _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 ADI DEV SRC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 CMD BAR FILTER _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
Issued 8/10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
1.17
System Configuration
SOFTWARE 08 CONFIGURATION PAGES
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 as the pilots side and side 2 as the co-pilots side.
——————————| 1 VIEW/EDIT EQUIPMENT PG 01 2 I T E M 3 SG NUMBER _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 S I N G L E / D U A L _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 DU TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 ATTITUDE/HDG #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 ATTITUDE/HDG #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 RATE OF TURN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 ADF #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 ADF #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 VOR/ILS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 VOR/ILS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 02 2 I T E M 3 DME #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DME #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 MLS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 MLS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 FMS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 FMS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RNAV #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RNAV #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 TACAN #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
1 2 TACAN #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
1.18
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
System Configuration
— — — — — — — — — — |
1 VIEW/EDIT EQUIPMENT PG 03 2 I T E M 3 FMS VNAV _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 RADAR ALT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 AFCS TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 AFCS COMMAND BAR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 AFCS MODE ANN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 F/S AIR DATA _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RADAR TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR CTL PNL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 RADAR INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 C H E C K L I S T _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 04 2 I T E M 3 J O Y S T I C K _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 T C A S _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 HOMING #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 HOMING #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 LIGHTNING DET _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 HOVER MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 CABLE MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
— — — — — — — — — — | 1 VIEW/EDIT OPERATING CHAR PG 06 2 I T E M 3 VERT SCALE SIDE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DCLTR GS ON BC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 FULL TIME FMS MAP _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DISPLAY WIND VEC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 DISPLAY DRIFT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 DG ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DME DIST ONLY _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 S P A R E _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 MFD NAV CONTROL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
Issued 8/10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
1.19
System Configuration
— — — — — — — — — — |
1 VIEW/EDIT OPERATING PG 07 2 I T E M 3 DISPLAY HDG TAPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 COMMAND BARS _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 ROLL INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DCLTR UNUS ATT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 CAT II AVAILABLE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 PERSPECTIVE LINES _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DH SELECT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 CTL PNL SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 SEL HDG SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 SEL CRS SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — |
1 VIEW/EDIT OPERATING PG 08 2 I T E M 3 NORTH UP MAP _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 VERT PTR TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 DISPLAY FMS MSG _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 SEL HDG COLOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 CMD BAR COLOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 REV MODE ANN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RISING RUNWAY _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 ADI DEV SRC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 CMD BAR FILTER _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 MLS VRT ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — |
1 VIEW/EDIT OPERATING PG 09 2 I T E M 3 DATUM SCALING _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 HDG FAIL ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 VNAV APR SCALE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 LNAV CRS CTRL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 SG #1 SIDE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 AIRCRAFT SYMBOL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 TACAN ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 TCAS DISPLAYS _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 CAT II SENSORS _______________
1.20
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
System Configuration
SOFTWARE 09 CONFIGURATION PAGES
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 as the pilots side and side 2 as the co-pilots side.
——————————| 1 VIEW/EDIT EQUIPMENT PG 01 2 I T E M 3 SG NUMBER _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 S I N G L E / D U A L _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 DU TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 ATTITUDE/HDG #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 ATTITUDE/HDG #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 RATE OF TURN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 ADF #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 ADF #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 VOR/ILS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 VOR/ILS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 02 2 I T E M 3 DME #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DME #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 MLS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 MLS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 FMS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 FMS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RNAV #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RNAV #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 TACAN #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 TACAN #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
Issued 8/10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
1.21
System Configuration
— — — — — — — — — — |
1 VIEW/EDIT EQUIPMENT PG 03 2 I T E M 3 FMS VNAV _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 RADAR ALT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 AFCS TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 AFCS COMMAND BAR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 AFCS MODE ANN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 F/S AIR DATA _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RADAR TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR CTL PNL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 RADAR INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 C H E C K L I S T _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 04 2 I T E M 3 J O Y S T I C K _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 T C A S _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 HOMING #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 HOMING #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 LIGHTNING DET _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 HOVER MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 CABLE MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
— — — — — — — — — — | 1 VIEW/EDIT OPERATING CHAR PG 06 2 I T E M 3 VERT SCALE SIDE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DCLTR GS ON BC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 FULL TIME FMS MAP _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DISPLAY WIND VEC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 DISPLAY DRIFT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 DG ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DME DIST ONLY _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 S P A R E _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 MFD NAV CONTROL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
1.22
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
System Configuration
— — — — — — — — — — |
1 VIEW/EDIT OPERATING PG 07 2 I T E M 3 DISPLAY HDG TAPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 ADI PLANE/CMD BAR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 ROLL INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DCLTR UNUS ATT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 CAT II AVAILABLE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 PERSPECTIVE LINES _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DH SELECT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 CTL PNL SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 SEL HDG SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 SEL CRS SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 08 2 I T E M 3 NORTH UP MAP _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 VERT PTR TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 DISPLAY FMS MSG _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 SEL HDG COLOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 CMD BAR COLOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 REV MODE ANN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RISING RUNWAY _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 ADI DEV SRC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 CMD BAR FILTER _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 MLS VRT ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 09 2 I T E M 3 DATUM SCALING _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 HDG FAIL ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 VNAV APR SCALE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 LNAV CRS CTRL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 SG #1 SIDE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 AIRCRAFT SYMBOL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 TACAN ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 TCAS DISPLAYS _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 CAT II SENSORS _______________ 1 2 RADAR SCAN _______________
Issued 8/10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
1.23
System Configuration
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 10 2 I T E M 3 RADAR SDI _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
1.24
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
System Configuration
SOFTWARE 10 CONFIGURATION PAGES
The EHSI, EADI, MFD and Reversion software will display the follow-
ing 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 as the pilots side and side 2 as the co-pilots side.
——————————| 1 VIEW/EDIT EQUIPMENT PG 01 2 I T E M 3 SG NUMBER _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 S I N G L E / D U A L _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 DU TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 ATTITUDE/HDG #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 ATTITUDE/HDG #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 RATE OF TURN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 ADF #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 ADF #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 VOR/ILS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 VOR/ILS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 02 2 I T E M 3 DME #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DME #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 MLS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 MLS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 FMS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 FMS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RNAV #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RNAV #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 TACAN #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 TACAN #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
Issued 8/10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
1.25
System Configuration
— — — — — — — — — — |
1 VIEW/EDIT EQUIPMENT PG 03 2 I T E M 3 FMS VNAV _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 RADAR ALT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 AFCS TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 AFCS COMMAND BAR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 AFCS MODE ANN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 F/S AIR DATA _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RADAR TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR CTL PNL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 RADAR INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 C H E C K L I S T _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 04 2 I T E M 3 J O Y S T I C K _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 T C A S _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 HOMING #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 HOMING #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 LIGHTNING DET _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 HOVER MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 CABLE MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
— — — — — — — — — — | 1 VIEW/EDIT OPERATING CHAR PG 06 2 I T E M 3 VERT SCALE SIDE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DCLTR GS ON BC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 FULL TIME FMS MAP _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DISPLAY WIND VEC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 DISPLAY DRIFT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 DG ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DME DIST ONLY _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 S P A R E _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 MFD NAV CONTROL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
1.26
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
System Configuration
— — — — — — — — — — |
1 VIEW/EDIT OPERATING PG 07 2 I T E M 3 DISPLAY HDG TAPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 ADI PLANE/CMD BAR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 ROLL INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DCLTR UNUS ATT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 CAT II AVAILABLE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 PERSPECTIVE LINES _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DH SELECT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 CTL PNL SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 SEL HDG SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 SEL CRS SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 08 2 I T E M 3 NORTH UP MAP _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 VERT PTR TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 DISPLAY FMS MSG _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 SEL HDG COLOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 CMD BAR COLOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 REV MODE ANN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RISING RUNWAY _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 ADI DEV SRC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 CMD BAR FILTER _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 MLS VRT ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 09 2 I T E M 3 DATUM SCALING _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 HDG FAIL ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 VNAV APR SCALE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 LNAV CRS CTRL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 SG #1 SIDE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 AIRCRAFT SYMBOL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 TACAN ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 TCAS DISPLAYS _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 CAT II SENSORS _______________ 1 2 RADAR SCAN _______________
Issued 8/10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
1.27
System Configuration
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 10 2 I T E M 3 RADAR SDI _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 PITCH SYNC DISC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
1.28
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
System Configuration
SOFTWARE 11 CONFIGURATION PAGES
The EHSI, EADI, MFD and Reversion software will display the follow-
ing 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 as the pilots side and side 2 as the co-pilots side.
——————————| 1 VIEW/EDIT EQUIPMENT PG 01 2 I T E M 3 SG NUMBER _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 S I N G L E / D U A L _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 DU TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 ATTITUDE/HDG #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 ATTITUDE/HDG #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 RATE OF TURN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 ADF #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 ADF #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 VOR/ILS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 VOR/ILS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 02 2 I T E M 3 DME #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DME #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 MLS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 MLS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 FMS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 FMS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RNAV #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RNAV #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 TACAN #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 TACAN #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
Issued 8/10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
1.29
System Configuration
— — — — — — — — — — |
1 VIEW/EDIT EQUIPMENT PG 03 2 I T E M 3 FMS VNAV _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 RADAR ALT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 AFCS TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 AFCS COMMAND BAR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 AFCS MODE ANN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 F/S AIR DATA _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RADAR TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR CTL PNL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 RADAR INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 C H E C K L I S T _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 04 2 I T E M 3 J O Y S T I C K _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 T C A S _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 HOMING #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 HOMING #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 LIGHTNING DET _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 HOVER MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 CABLE MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 VARIABLE LNAV _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
— — — — — — — — — — | 1 VIEW/EDIT OPERATING CHAR PG 06 2 I T E M 3 VERT SCALE SIDE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DCLTR GS ON BC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 FULL TIME FMS MAP _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DISPLAY WIND VEC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 DISPLAY DRIFT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 DG ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DME DIST ONLY _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 S P A R E _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 MFD NAV CONTROL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
1.30
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
System Configuration
— — — — — — — — — — |
1 VIEW/EDIT OPERATING PG 07 2 I T E M 3 DISPLAY HDG TAPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 ADI PLANE/CMD BAR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 ROLL INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DCLTR UNUS ATT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 CAT II AVAILABLE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 PERSPECTIVE LINES _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DH SELECT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 CTL PNL SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 SEL HDG SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 SEL CRS SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 08 2 I T E M 3 NORTH UP MAP _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 VERT PTR TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 DISPLAY FMS MSG _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 SEL HDG COLOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 CMD BAR COLOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 REV MODE ANN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RISING RUNWAY _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 ADI DEV SRC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 CMD BAR FILTER _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 MLS VRT ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 09 2 I T E M 3 DATUM SCALING _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 HDG FAIL ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 VNAV APR SCALE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 LNAV CRS CTRL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 SG #1 SIDE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 AIRCRAFT SYMBOL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 TACAN ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 TCAS DISPLAYS _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 CAT II SENSORS _______________ 1 2 RADAR SCAN _______________
Issued 8/10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
1.31
System Configuration
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 10 2 I T E M 3 RADAR SDI _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
1.32
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
System Configuration
SOFTWARE 12 CONFIGURATION PAGES
The EHSI, EADI, MFD and Reversion software will display the follow-
ing 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 as the pilots side and side 2 as the co-pilots side.
——————————| 1 VIEW/EDIT EQUIPMENT PG 01 2 I T E M 3 SG NUMBER _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 S I N G L E / D U A L _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 DU TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 ATTITUDE/HDG #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 ATTITUDE/HDG #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 RATE OF TURN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 ADF #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 ADF #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 VOR/ILS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 VOR/ILS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 02 2 I T E M 3 DME #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DME #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 MLS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 MLS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 FMS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 FMS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RNAV #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RNAV #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 TACAN #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 TACAN #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
Issued 8/10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
1.33
System Configuration
— — — — — — — — — — |
1 VIEW/EDIT EQUIPMENT PG 03 2 I T E M 3 FMS VNAV _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 RADAR ALT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 AFCS TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 AFCS COMMAND BAR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 AFCS MODE ANN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 F/S AIR DATA _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RADAR TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR CTL PNL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 RADAR INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 C H E C K L I S T _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 04 2 I T E M 3 J O Y S T I C K _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 T C A S _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 HOMING #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 HOMING #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 LIGHTNING DET _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 HOVER MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 CABLE MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 VARIABLE LNAV _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
— — — — — — — — — — | 1 VIEW/EDIT OPERATING CHAR PG 06 2 I T E M 3 VERT SCALE SIDE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DCLTR GS ON BC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 FULL TIME FMS MAP _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DISPLAY WIND VEC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 DISPLAY DRIFT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 DG ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DME DIST ONLY _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 S P A R E _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 MFD NAV CONTROL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
1.34
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
System Configuration
— — — — — — — — — — |
1 VIEW/EDIT OPERATING PG 07 2 I T E M 3 DISPLAY HDG TAPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 ADI PLANE/CMD BAR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 ROLL INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DCLTR UNUS ATT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 CAT II AVAILABLE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 PERSPECTIVE LINES _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DH SELECT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 CTL PNL SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 SEL HDG SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 SEL CRS SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 08 2 I T E M 3 NORTH UP MAP _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 VERT PTR TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 DISPLAY FMS MSG _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 SEL HDG COLOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 CMD BAR COLOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 REV MODE ANN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RISING RUNWAY _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 ADI DEV SRC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 CMD BAR FILTER _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 MLS VRT ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 09 2 I T E M 3 DATUM SCALING _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 HDG FAIL ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 VNAV APR SCALE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 LNAV CRS CTRL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 SG #1 SIDE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 AIRCRAFT SYMBOL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 TACAN ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 TCAS DISPLAYS _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 CAT II SENSORS _______________ 1 2 RADAR SCAN _______________
Issued 8/10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
1.35
System Configuration
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 10 2 I T E M 3 RADAR SDI _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
1.36
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
System Configuration
SOFTWARE 13 CONFIGURATION PAGES
The EHSI, EADI, MFD and Reversion software will display the follow-
ing 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 as the pilots side and side 2 as the co-pilots side.
——————————| 1 VIEW/EDIT EQUIPMENT PG 01 2 I T E M 3 SG NUMBER _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 S I N G L E / D U A L _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 DU TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 ATTITUDE/HDG #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 ATTITUDE/HDG #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 RATE OF TURN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 ADF #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 ADF #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 VOR/ILS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 VOR/ILS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 02 2 I T E M 3 DME #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DME #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 MLS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 MLS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 FMS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 FMS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RNAV #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RNAV #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 TACAN #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 TACAN #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
Issued 8/10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
1.37
System Configuration
— — — — — — — — — — |
1 VIEW/EDIT EQUIPMENT PG 03 2 I T E M 3 FMS VNAV _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 RADAR ALT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 AFCS TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 AFCS COMMAND BAR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 AFCS MODE ANN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 F/S AIR DATA _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RADAR TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR CTL PNL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 RADAR INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 C H E C K L I S T _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 04 2 I T E M 3 J O Y S T I C K _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 T C A S _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 HOMING #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 HOMING #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 LIGHTNING DET _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 HOVER MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 CABLE MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 VARIABLE LNAV _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
— — — — — — — — — — | 1 VIEW/EDIT OPERATING CHAR PG 06 2 I T E M 3 VERT SCALE SIDE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DCLTR GS ON BC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 FULL TIME FMS MAP _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DISPLAY WIND VEC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 DISPLAY DRIFT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 DG ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DME DIST ONLY _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 S P A R E _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 MFD NAV CONTROL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
1.38
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
System Configuration
— — — — — — — — — — |
1 VIEW/EDIT OPERATING PG 07 2 I T E M 3 DISPLAY HDG TAPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 ADI PLANE/CMD BAR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 ROLL INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DCLTR UNUS ATT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 CAT II AVAILABLE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 PERSPECTIVE LINES _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DH SELECT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 CTL PNL SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 SEL HDG SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 SEL CRS SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 08 2 I T E M 3 NORTH UP MAP _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 VERT PTR TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 DISPLAY FMS MSG _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 SEL HDG COLOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 CMD BAR COLOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 REV MODE ANN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RISING RUNWAY _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 ADI DEV SRC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 CMD BAR FILTER _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 MLS VRT ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 09 2 I T E M 3 DATUM SCALING _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 HDG FAIL ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 VNAV APR SCALE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 LNAV CRS CTRL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 SG #1 SIDE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 AIRCRAFT SYMBOL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 TACAN ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 TCAS DISPLAYS _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 CAT II SENSORS _______________ 1 2 RADAR SCAN _______________
Issued 8/10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
1.39
System Configuration
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 10 2 I T E M 3 RADAR SDI _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 PITCH SYNC DISC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 ADF PTR HOLD DST _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
1.40
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
System Configuration
SOFTWARE 14 CONFIGURATION PAGES
The EHSI, EADI, MFD and Reversion software will display the follow-
ing 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 as the pilots side and side 2 as the co-pilots side.
——————————| 1 VIEW/EDIT EQUIPMENT PG 01 2 I T E M 3 SG NUMBER _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 S I N G L E / D U A L _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 DU TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 ATTITUDE/HDG #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 ATTITUDE/HDG #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 RATE OF TURN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 ADF #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 ADF #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 VOR/ILS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 VOR/ILS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 02 2 I T E M 3 DME #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DME #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 MLS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 MLS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 FMS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 FMS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RNAV #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RNAV #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 TACAN #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 TACAN #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
Issued 8/10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
1.41
System Configuration
— — — — — — — — — — |
1 VIEW/EDIT EQUIPMENT PG 03 2 I T E M 3 FMS VNAV _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 RADAR ALT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 AFCS TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 AFCS COMMAND BAR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 AFCS MODE ANN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 F/S AIR DATA _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RADAR TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR CTL PNL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 RADAR INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 C H E C K L I S T _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 04 2 I T E M 3 J O Y S T I C K _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 T C A S _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 HOMING #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 HOMING #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 LIGHTNING DET _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 HOVER MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 CABLE MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 VARIABLE LNAV _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 E G P W S _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
— — — — — — — — — — | 1 VIEW/EDIT OPERATING CHAR PG 06 2 I T E M 3 VERT SCALE SIDE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DCLTR GS ON BC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 FULL TIME FMS MAP _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DISPLAY WIND VEC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 DISPLAY DRIFT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 DG ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DME DIST ONLY _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 S P A R E _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 MFD NAV CONTROL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
1.42
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
System Configuration
— — — — — — — — — — |
1 VIEW/EDIT OPERATING PG 07 2 I T E M 3 DISPLAY HDG TAPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 ADI PLANE/CMD BAR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 ROLL INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DCLTR UNUS ATT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 CAT II AVAILABLE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 PERSPECTIVE LINES _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DH SELECT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 CTL PNL SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 SEL HDG SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 SEL CRS SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 08 2 I T E M 3 NORTH UP MAP _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 VERT PTR TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 DISPLAY FMS MSG _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 SEL HDG COLOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 CMD BAR COLOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 REV MODE ANN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RISING RUNWAY _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 ADI DEV SRC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 CMD BAR FILTER _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 MLS VRT ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 09 2 I T E M 3 DATUM SCALING _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 HDG FAIL ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 VNAV APR SCALE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 LNAV CRS CTRL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 SG #1 SIDE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 AIRCRAFT SYMBOL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 TACAN ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 TCAS DISPLAYS _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 CAT II SENSORS _______________ 1 2 RADAR SCAN _______________
Issued 8/10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
1.43
System Configuration
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 10 2 I T E M 3 RADAR SDI _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 PITCH SYNC DISC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 ADF PTR HOLD DST _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 FMS OUTPUT BUS _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
1.44
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
System Configuration
SOFTWARE 15 CONFIGURATION PAGES
The EHSI, EADI, MFD and Reversion software will display the follow-
ing 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 as the pilots side and side 2 as the co-pilots side.
——————————| 1 VIEW/EDIT EQUIPMENT PG 01 2 I T E M 3 SG NUMBER _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 S I N G L E / D U A L _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 DU TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 ATTITUDE/HDG #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 ATTITUDE/HDG #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 RATE OF TURN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 ADF #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 ADF #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 VOR/ILS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 VOR/ILS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 02 2 I T E M 3 DME #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DME #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 MLS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 MLS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 FMS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 FMS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RNAV #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RNAV #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 TACAN #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 TACAN #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
Issued 8/10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
1.45
System Configuration
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 03 2 I T E M 3 FMS VNAV _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 RADAR ALT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 AFCS TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 AFCS COMMAND BAR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
7 AFCS MODE ANN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 F/S AIR DATA _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RADAR TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR CTL PNL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 RADAR INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 C H E C K L I S T _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 04 2 I T E M 3 J O Y S T I C K _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 T C A S _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 HOMING #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 HOMING #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 LIGHTNING DET _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 HOVER MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 CABLE MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 VARIABLE LNAV _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 E G P W S _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 V A R I A B L E V N A V _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
— — — — — — — — — — | 1 VIEW/EDIT OPERATING CHAR PG 06 2 I T E M 3 VERT SCALE SIDE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DCLTR GS ON BC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 FULL TIME FMS MAP _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DISPLAY WIND VEC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 DISPLAY DRIFT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 DG ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DME DIST ONLY _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 S P A R E _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 MFD NAV CONTROL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
1.46
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
System Configuration
— — — — — — — — — — |
1 VIEW/EDIT OPERATING PG 07 2 I T E M 3 DISPLAY HDG TAPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 ADI PLANE/CMD BAR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 ROLL INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DCLTR UNUS ATT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 CAT II AVAILABLE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 PERSPECTIVE LINES _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DH SELECT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 CTL PNL SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 SEL HDG SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 SEL CRS SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 08 2 I T E M 3 NORTH UP MAP _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 VERT PTR TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 DISPLAY FMS MSG _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 SEL HDG COLOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 CMD BAR COLOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 REV MODE ANN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RISING RUNWAY _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 ADI DEV SRC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 CMD BAR FILTER _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 MLS VRT ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 09 2 I T E M 3 DATUM SCALING _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 HDG FAIL ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 VNAV APR SCALE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 LNAV CRS CTRL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 SG #1 SIDE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 AIRCRAFT SYMBOL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 TACAN ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 TCAS DISPLAYS _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 CAT II SENSORS _______________ 1 2 RADAR SCAN _______________
Issued 8/10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
1.47
System Configuration
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 10 2 I T E M 3 RADAR SDI _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 PITCH SYNC DISC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 ADF PTR HOLD DST _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 FMS OUTPUT BUS _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 LNAV VERT APR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 L/VNAV VERTA P R _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 LP VERT A P R _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 LPV VERT APR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 LNAV SELECT OUT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
1.48
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
System Configuration
SOFTWARE 16 CONFIGURATION PAGES
The EHSI, EADI, MFD and Reversion software will display the follow-
ing 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 as the pilots side and side 2 as the co-pilots side.
——————————| 1 VIEW/EDIT EQUIPMENT PG 01 2 I T E M 3 SG NUMBER _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 S I N G L E / D U A L _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 DU TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 ATTITUDE/HDG #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 ATTITUDE/HDG #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 RATE OF TURN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 ADF #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 ADF #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 VOR/ILS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 VOR/ILS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 02 2 I T E M 3 DME #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DME #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 MLS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 MLS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 FMS #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 FMS #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RNAV #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RNAV #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 TACAN #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 TACAN #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
Issued 8/10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
1.49
System Configuration
— — — — — — — — — — |
1 VIEW/EDIT EQUIPMENT PG 03 2 I T E M 3 FMS VNAV _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 RADAR ALT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 AFCS TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 AFCS COMMAND BAR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 AFCS MODE ANN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 F/S AIR DATA _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RADAR TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR CTL PNL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 RADAR INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 C H E C K L I S T _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT EQUIPMENT PG 04 2 I T E M 3 J O Y S T I C K _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 T C A S _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 HOMING #1 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 HOMING #2 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 LIGHTNING DET _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 HOVER MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 CABLE MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 VARIABLE LNAV _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 E G P W S _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 V A R I A B L E V N A V _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
— — — — — — — — — — | 1 VIEW/EDIT OPERATING CHAR PG 06 2 I T E M 3 VERT SCALE SIDE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 DCLTR GS ON BC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 FULL TIME FMS MAP _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DISPLAY WIND VEC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 DISPLAY DRIFT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 DG ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DME DIST ONLY _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 RADAR ONLY MODE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 S P A R E _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 MFD NAV CONTROL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
1.50
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
System Configuration
— — — — — — — — — — |
1 VIEW/EDIT OPERATING PG 07 2 I T E M 3 DISPLAY HDG TAPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 ADI PLANE/CMD BAR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 ROLL INDICATOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 DCLTR UNUS ATT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 CAT II AVAILABLE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 PERSPECTIVE LINES _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 DH SELECT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 CTL PNL SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 SEL HDG SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 SEL CRS SYNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 08 2 I T E M 3 NORTH UP MAP _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 VERT PTR TYPE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 DISPLAY FMS MSG _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 SEL HDG COLOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 CMD BAR COLOR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 REV MODE ANN _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 RISING RUNWAY _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 ADI DEV SRC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 CMD BAR FILTER _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 2 MLS VRT ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 3 . . M O R E . .
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 09 2 I T E M 3 DATUM SCALING _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 HDG FAIL ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 VNAV APR SCALE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 LNAV CRS CTRL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 SG #1 SIDE _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 AIRCRAFT SYMBOL _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 TACAN ANNUNC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 TCAS DISPLAYS _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 CAT II SENSORS _______________ 1 2 RADAR SCAN _______________
Issued 8/10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
1.51
System Configuration
— — — — — — — — — — | 1 VIEW/EDIT OPERATING PG 10 2 I T E M 3 RADAR SDI _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 4 PITCH SYNC DISC _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 5 ADF PTR HOLD DST _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 6 FMS OUTPUT BUS _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 7 LNAV VERT APR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 8 L/VNAV VERTA P R _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 9 LP VERT A P R _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 0 LPV VERT APR _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ 1 1 LNAV SELECT OUT _ _ _ _ _ _ _ _ _ _ _ _ _ _ _
1.52
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
EHSI OPERATION
DETAILED OPERATING CONTROLS
EHSI Operation
All possible EFS 40/50 Interfac-
ing Equipment is described in the Detailed Operating Controls sec­tion of the EFS 40/50 Pilots Guide, however, all may not be active in a specific installation.
This section, EHSI Operation, will describe the operation of both
the ED 461 control display unit, C P 468 EHSI control panel and the EHSI section of the CP 4 6 7 EHSI/EADI control panel. The EADI operation of the CP 467 is covered in section 2.2, EADI Operation. The CP 466A/B radar control panels are covered in section 2.3, RADAR Operation.
Figure 2.1
ED 461 EHSI
2.1.1Issued 8/10 SW 04/05/06/07/08/09/10/11/12/13/14/15/16
EHSI Operation
Figure 2.2
ED 462 Display Unit & Companion
CP 468 Control Panel
For clarification on a particular display or operational feature, refer to section IV. EHSI DIS­PLAYS or section V. OPERAT­ING INSTRUCTIONS. Figure
2.1 shows the ED 461 combined
2.1.2
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
control/display unit and figure 2.2 shows the CP 468 dedicated stand-alone EHSI mode con­troller and companion ED 4 6 2 display unit.
Issued 8/10
EHSI CONTROLS (ED 461 & CP 467/468)
1-2
1 2
NAV
N A
V
EHSI Operation
1-2 NAVIGATION SYSTEM SELECT
The 1-2 button is used to cycle between primary navigation sen­sor system #1 and #2 for display. The primary NAV system select­ed is annunciated as sensor 1 or sensor 2 on the EHSI. Example, if VOR 1 is being displayed and the 1-2 button is pressed, VOR 2 will become the displayed sen­sor. If only one sensor is installed, the display will not cycle and the sensor annunciation will not show a system number. For example ADF would be displayed (not ADF 1) in installations con­taining a single ADF.
Note: The cross-side sensor for
VOR could be TCN, for LNAVs it could be a combination of FMS, GPS, OMG or LOR. Beginning with software 08, the 1-2 button no longer selects between sources.
unlike LNAV
NAV NAVIGATION SENSOR SELECT
During installation, the EFS 40/50 symbol generator was pro­grammed with the type and quantity of each piece of interfac­ing equipment. Not all the equipment interfaced to the EFS 40/50 is usable for primary navi­gation. The EFS 40/50 creates and maintains in permanent memory a list of the interfacing navigation sensors.
The NAV push button is used to select which NAV sensor pro­vides primary navigation data. A press of the NAV sensor select button sequentially selects the next available sensor from the list of those installed. Primary Navi­gation Data is defined as the dis-
tance in the upper right corner, selected cour and deviation.
se, course pointer
Software release 0402 added “FUNCTION NOT IMPLE ­MENTED” annunciation when either the 1-2, RMI or NAV sensor select button is pressed and it is not active in the sys ­tem. A yellow FUNCTION NOT IMPLEMENTED will be displayed in the center of the screen.
2.1.3Issued 8/10 SW 04/05/06/07/08/09/10/11/12/13/14/15/16
EHSI Operation
DOPP
MLS
NAV (KNS 81 ONLY)
LNAV, (FMS, LOR or OMG)
TCN (Control head)
ADF
CAB
HOM
TCN (Control head)
VOR (VOR, LOC, TCN or RNV)
VOR (VOR, LOC, TCN or RNV)
LNAV, (FMS, LOR or OMG)
NAV (KNS 81 ONLY)
MLS
ADF
HOM
ON-SIDE EFS CROSS-SIDE EFS
1-2
1-2
1-2
1-2
1-2
1-2
N A V
NAV
NAV
NAV
NAV
NAV
NAV
NAV
NAV
NAV
1-2
NAV
NAV
NAV
NAV
NAV
NAV
DOPP
MLS
NAV (KNS 81 ONLY)
ADF
CAB
HOM
NAV (KNS 81 ONLY)
MLS
ADF
HOM
1-2
1-2
1-2
1-2
N A V
NAV
NAV
NAV
NAV
NAV
NAV
NAV
NAV
NAV
NAV
LNAV, (FMS, LOR, OMG or GPS)
TCN (Control head) TCN (Control head)
VOR (VOR, LOC, TCN or RNV)
VOR (VOR, LOC, TCN or RNV)
ON-SIDE EFS CROSS-SIDE EFS
1-2
1-2
NAV
NAV
NAV
NAV
LNAV, (FMS, LOR, OMG or GPS)
NAV
The Primary Navigation Sensor is annunciated at the side of the display unit opposite the vertical scale. Only those sensors inter­faced to the EFS 40/50 in a spe­cific installation will be selectable for use and display.
For installations with dual VOR/ILS receivers and a KNS 81, the KNS 81 will be pro­grammed as an RNAV. The annunciation displayed on the EHSI for this configuration will be NAV and will not change as modes on the KNS 81 are changed. The sensor annuncia­tion and associated navigation data colors will change to match the normal enroute or approach
color scheme, green for on-side approach navigation data, cyan for on-side non approach naviga­tion data and yellow for off-side navigation data.
S o f t w a r e 04 added two new heli­copter navigation sensor options, Doppler (DOPP) and Cable (CAB). These sensors require unique display formats, therefore when they are selected for dis­play their unique format will be presented and are not change­able by the HSI or ARC button.
The following is an all-inclusive list, in order, of primary naviga­tion sensors that may be inter­faced with the EFS 40/50:
SOFTWARE 04/05/06/07 SOFTWARE 08 OR LATER
2.1.4
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
EHSI Operation
HSI
H
S
I
See Section 4 for display details
on Doppler, Cable and Homing.
Note: If a number 2 NAV sen -
sor has been selected for dis ­play on the number 1 EHSI by pressing the 1-2 button and the number 1 EHSI NAV push button is pressed, the next available number 1 NAV sen ­sor will be selected.
ADF D-Bar presentation may not be available if the ADF does not provide a suitable flag output.
Software 08 treats unlike LNAV sources (i.e. FMS, LOR, OMG, or GPS) as single sen ­sors. When two unlike LNAV sources are configured, the EFS will display both the on­side LNAV and the off-side LANV without a system num ­ber and the NAV button is used to select between them.
HSI 360° MODE SELECTION
The display selection list may include the following:
DG and WEATHER are options selected at the time of installation and are included in the system certification. Software 06 added lightning detection presentation.
If a compatible weather radar or lightning detection is not installed, the weather option will not be in the sequence.
The EFS 40/50 EHSI has four possible 360-degree display for­mats: standard HSI compass rose, NAV map, NAV map with weather, and DG mode. Each press of the HSI button sequen­tially selects the next display for­mat. A press of the HSI button while in the ARC mode will change the display to the stan­dard HSI compass rose.
Software release 05 added a Heading Bug to the DG mode. Primary use of this display format is for training or as an option to provide an uncluttered display for an NDB approach (using the EHSI as an ADF RMI).
Software release 07 provides the additional, optional display format of "Plan View" which can be con­figured for display on the MFD o n l y .
2.1.5Issued 8/10 SW 04/05/06/07/08/09/10/11/12/13/14/15/16
EHSI Operation
DECLUTTER, (NO #1 OR #2 BEARING POINTER INFORMATION IS DISPLAYED)
VOR, (VOR OR TCN)
TCN, (ONLY AVAILABLE WHEN THE TACAN HAS AN INDEPENDENT CONTROL HEAD)
LNAV, (FMS, LOR, OMG or *GPS)
NAV (KNS 81 ONLY)
MLS
ADF
DME ONE DISTANCE ONLY, (OPTIONAL)
OR
*SW 08 OR LATER
BEARING POINTER SELECT
The bearing pointer select but­tons work in a similar manner as the NAV sensor select button. A press of the bearing pointer but­ton sequentially selects the next available sensor for display. The bearing pointer sensor list con­tains only those sensors which have bearing information capabil­ities. If the selected sensor has distance information paired with it, that distance will also be dis­played below the sensor annun-
ciation. An optional push button sequence allows independent selection and display of the respective DME distance without the presence of the bearing p o i n t e r .
E x a m p l e : For a single ADF
installation, the ADF bearing pointer may be displayed on either the single or double bar pointer. The annunciation associated with either bearing pointer will be ADF, not ADF 1 or ADF 2.
The following is an all-inclusive list, in order, of the bearing point­er sensors that may be interfaced with the EFS 4 0 / 5 0 :
Only those sensors interfaced to the EFS 40/50 will be included in the sequence.
2.1.6
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
N o t e : Software release 0 5
allows single bearing sensors to be displayed on either bear ­ing pointer. Software release 07 and high ­er, the DME only field can be configured to annunciate DME or NAV.
Issued 8/10
EHSI Operation
ARC
A R C
A
R
C
ARC COMPASS ROSE
ARC NAV MAP
ARC NAV MAP WITH WEATHER (OPTIONAL)
ARC COMPASS ROSE WITH WEATHER (OPTIONAL)
ARC WEATHER ONLY (OPTIONAL ON MFD)
ARC SECTORED MODE SELECTION
The ARC mode provides the pilot a large scale view of the CDI by presenting an approximate 85­degree sector display of the com­p a s s .
The EFS 40/50 EHSI has five possible ARC sectored display formats: standard HSI compass rose, NAV CDI map, NAV CDI map with weather and standard HSI compass rose with weather. Software release 05 provides a configuration option, selectable at
the time of installation and certifi­cation, that allows a weather only mode to be selected on the MFD. A press of the ARC button will sequentially select the possible display formats.
A press of the ARC button while in the 360-degree mode will result in an ARC presentation of the same format. For example, if the 360 NAV MAP WITH WEATHER mode is being dis­played and the ARC button is pressed, the resulting display for­mat will be ARC NAV MAP WITH W E A T H E R .
The ARC display selection list may include the following:
WEATHER is an option selected at the time of installation and is included in the system certifica­tion. If a compatible weather radar is not installed, the weather option will not be in the s e q u e n c e .
Software release 05 provides MFD, multi function display, capabilities. If an MFD is installed, an additional ARC for­mat option is offered, selectable at the time of installation and cer­tification, which provides an
2.1.7Issued 8/10 SW 04/05/06/07/08/09/10/11/12/13/14/15/16
EHSI Operation
RNG
RNG
SYS REF
TST
REF
uncluttered weather radar pre­sentation. The MFD ARC weath­er only format provides a typical weather radar presentation, no navigation data is presented when this mode is selected.
Refer to radar controls in this section for details on weather radar operation.
RANGE SELECTION
A press of the RANGE DOWN button selects the next lower range to be displayed while in the NAV MAP or WEATHER modes of operation. Once the lowest selectable range is reached, the RANGE UP button must be used for a range change.
The operation of the RANGE UP button is similar to the RANGE DOWN except it selects the next higher while in the NAV MAP or WEATHER modes of operation.
range to be displayed
TST/REF
The TST/REF button will per­forms SELF TEST display, Ground speed, Time-to-Station or LNAV formatting selections with software 04/05/06/07. The TST/REF button will per­forms SELF TEST or LNAV for­matting selections with software release 08 and higher.
2.1.8
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
w
TST—
To display the EHSI system SELF TEST, press and hold the TST/REF button for three sec­onds. Upon entering Self Test, a test pattern will be displayed. In the center of the test pattern, either a SELF TEST PASS or SELF TEST FAIL will be annun­ciated. With 04/05/06 software, the SELF TEST display will remain until the TST/REF button is pressed again. Beginning with 07 software, the EFS will cancel the test mode and return both the EADI and EHSI to normal opera­tion after 5 seconds.
N o t e : If the SELF TEST FAIL
message is annunciated, the system should be serviced.
REF GROUND SPEED
w
or TIME-TO-STATION s e l e c t i o n
With software 04/05/06/07, the TST/REF button allows alternate selection of Ground speed or Time-to-station as calculated by the selected primary NAV sys­tem. When Ground speed or Time-to-station information is available it will be displayed below the distance information in the upper right corner of the dis­play. If the information is not pro­vided, the associated annuncia­tor will be removed. The alternate selection of Ground speed and Time-To-Station will not be allowed in the MAP mode with an LNAV selected as the pri­mary navigation source. Begin­ning with software 08, both
Issued 8/10
EHSI Operation
FPL ID
AIRPORT
NAVAIDS
TEST
REF
(FLIGHT PLAN WITH FULL ICAO IDENTIFIERS)
(TO WAYPOINT AND NEAREST AIRPORTS WITH ICAO IDENTIFIERS)
(TO WAYPOINT AND NEAREST NAVAIDS WITH ICAO IDENTIFIERS)
ground speed and time-to-station are displayed simultaneously. Time-To-Station is displayed immediately below the Ground Speed using the format of hours and minutes separated by a colon (H:MM).
Note: The Time-To-Station field
used with software 08 can also be used for an abnormal DME annunciation which has priori ­ty.
The EFS 40/50 will calculate ground speed and time-to-station in installations which use an A R I N C 568 type DME. If a con­ventional DME indicator is also used, differences in ground speed and time-to-station display may be noticed.
N o t e : Time-To-Station is
replaced with Time-To-Way ­point when the selected prima ­ry n
av is an LNAV providing
this information.
w
REF MAP FORMAT
When the selected EFS 4 0 / 5 0 display is LNAV MAP, the TST/REF button allows selection of the desired NAV MAP format. To determine the present MAP format momentarily press the TST/REF button. The momen­tary button press will activate the present MAP format annuncia­tion. If the displayed format is desired, no additional action is required; the format message will be removed within 5 seconds. If a different format is desired, sequence through the list by momentarily pressing the TST/REF button until the desired format is d
isplayed. Approxi­mately 5 seconds after the last button press, the map format annunciation will be removed.
The following is an all-inclusive list, in order, of the possible NAV MAP formats:
Note: Depending upon the Flight Management System installed,
the above format options may not be fully supported. Systems such as the BENDIX/KING KNS 660, KLN 88, and KLN 90, that support the GAMA 429 LNAV data bus will provide the above for ­mat options.
2.1.9Issued 8/10 SW 04/05/06/07/08/09/10/11/12/13/14/15/16
EHSI Operation
BRT
COURSE SELECT KNOB
Rotation of the COURSE SELECT knob allows the course pointer and digital course to be set at the desired course.
The ED 461, CP 467 and CP 468 provide a ”DIRECT TO” fea­ture. Pushing the center of the E D 461 Course Select knob or pulling the CP 467 or CP 4 6 8 COURSE SELECT knob will cause the course pointer and dig­ital course readout on the EHSI to slew to the direct course to the selected NAVAID or active way­p o i n t .
If the selected NAV sensor is an LNAV system, it may have modes of operation that control the selected course.
During these LNAV modes of operation the EFS 4 0 / 5 0 COURSE SELECT knob will be inactive.
HEADING SELECT KNOB
Rotation of the HEADING SELECT knob allows the head­ing bug on the EHSI to be rotated to the desired heading.
The ED 461, CP 467 and CP 468 provide a “HEADING SYNC” feature. Pushing the cen­ter of the ED 461 heading select knob or pulling the CP 467 or C P 468 HEADING SELECT knob will cause the heading bug on the EHSI to slew to the pre­sent aircraft heading (lubber line).
DISPLAY BRIGHTNESS CONTROL
The BRT knob controls the dis­play brightness.
Note: The display brightness
control provides full range dim ­ming to allow night operation in no- or low-light situations. The
2.1.10
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
lower limit of the display bright ­ness may appear as an inoper ­ative tube during normal day ­light operation. It is therefore advisable to check the BRT knob setting during preflight test.
To ensure maximum display tube life, it is highly recom ­mended that the display be operated at the lowest accept ­able brightness level.
Issued 8/10
EADI OPERATION
DH
BRT
ADI
RALT
TST
SET
EADI DETAILED OPERATING CONTROLS
EADI Operation
This section, EADI Operation, of the EHI 40/50 Pilots Guide describes the EADI operational controls of the CP 467 and CP 470 used with an ED 462 or ED 551/A EADI.
EADI controls are limited to three basic functions: EADI display brightness adjustment, DH (deci­sion height) set and Radio Alti­tude test.
For clarification on a particular display or operational feature refer to section IV, EADI DIS­PLAYS or section V, OPERAT­ING INSTRUCTIONS.
The CP 467 shown in Figure
2.2.1 is used in EFIS installations utilizing an ED 462 or ED 5 5 1 / A as the EHSI. The CP 4 7 0 shown in Figure 2.2.2 is used in EFIS installations utilizing the ED 461 EHSI control display unit with an ED 462 EADI.
Figure 2.2.1
CP 467 EFIS CONTROL PANEL
Figure 2.2.2
CP 470 EADI CONTROL PANEL
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
2.2.1Issued 8/10
EADI Operation
DH
BRT
ADI
RALT
TST
BRT
DH
DH
RALT
TST
RALT TST
BRIGHTNESS
The BRT knob controls the dis-
play brightness.
N o t e : The display brightness
control provides full range dim ­ming to allow night operation in no- or low-light situations. The lower limit of the display bright ­ness may appear as an inoper ­ative tube during normal day ­light operation. It is therefore advisable to check the BRT knob setting during preflight test.
To ensure maximum display tube life, it is highly recom ­mended that the display be operated at the lowest accept ­able brightness level.
DH SET
increments up to 500 feet and then in 10 foot increments to 2,500 feet.
Once the desired DH is selected, push in the DH set knob to lock the selected DH altitude. If DH is set to OFF, the “DH” annuncia­tion will not be displayed.
RALT TST
Pressing the RALT TST (Radio Altimeter Test) push button pro­vides a discrete output to the Radio Altimeter initiating its self test function.
The height displayed on the EADI will depend on the type of Radio Altimeter installed. For details on this information refer to the Radio Altimeter Pilot’s Guide of approve Flight Manual Sup­p l e m e n t .
To set the Decision Height, pull out and turn the DH knob. Turn­ing clockwise will increase the Decision Height selected, turning counter clockwise will decrease the Decision Height. The DH set knob is variable rate, the faster the knob is turned the greater the change
in a given amount of rotation. The Decision Height range is from “OFF” to 2,500 feet and will be displayed in one foot
2.2.2
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
RADAR OPERATION
DN
PULL STAB OFF
ON
TST
STBY
OFF
GAIN
Wx WxA
GND MAP
UP
TILT O
DN
PULL STAB OFF
BRT
OFF
GND MAP
TRKVP
TRK
ON
TST
STBY
OFF
GAIN
Wx WxA
GND
MAP
UP
TILT O
DN
PULL AUTO
PULL ARL
BRT
OFF
GND MAP
TRKVP
TRK
RADAR CONTROLS, (CP 466A & CP 466B)
Radar Operation
The following section provides general operating information on E F S 40/50 radar control panels, C P 466A & CP 466B. Figure
2.3.1 shows the CP 466A used with an RDS 81, RDS 82 or R D S 82VP, RDS 84 or RDS
Figure 2.3.1
CP 466A
84VP, RDR 2000. Figure 2.3.2 shows the CP 466B used with an RDS 86, RDS 86VP or RDR
2100. For detailed information on the specific weather radar functions, refer to the appropriate radar pilots guide.
Figure 2.3.2
Note: The CP 466A and B shown include the push buttons required
CP 466B
for the Vertical Profile radars. For non-VP installations using the CP 466A or B the VP and two track buttons will not be present.
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Radar Operation
BRT
Wx WxA
GND MAP
TRKVP
TRK
ON
TST
STBY
OFF
BRT
Wx WxA
GND MAP
BRT
GND MAP
BRT
GND MAP
OFF-STBY-TST-ON
The rotary OFF-STBY-TST-ON knob selects the desired operat­ing condition for the radar.
w
OFF
Disables the ART (Antenna, Receiver and Transmitter) power supply. “OFF” is displayed below the NAV source annunciator on the radar mode line.
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STBY
After 30 seconds in this mode, the system is in a state of readi­ness. No radar transmission occurs, and the antenna is parked in the down position. “STBY” is displayed below the NAV source annunciator on the radar mode line, if a weather mode is selected.
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TST
Causes the test pattern to be dis­played on the indicator, if a weather mode “TEST” is displayed below the NAV source annunciator on the radar mode line.
ON
w
is selected.
ation. Depending on the select­ed mode of operation, WX,WXA or MAP is displayed below the NAV source annunciator on the radar mode line.
Note: If “ON” is selected on the
C P 466 radar control panel, the radar Antenna, Receiver and Transmitter (ART) is oper ­ational. However, if a weather radar mode is not selected for display on one of the indicators the ART is placed in standby by the EFIS.
WX
Selects the weather mode (WX) when pressed. “WX” will be dis­played below the NAV source annunciator on the radar mode line, if a weather mode is select­e d .
WXA
Selects the weather-alert mode when pressed. The magenta area of a storm will flash between magenta and black. “WXA” will be displayed below the NAV source annunciator on the radar mode line, if a weather mode is s e l e c t e d .
GND MAP
Selects the condition of normal operation, allowing for weather detection or other modes of oper-
2.3.2
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Places the radar in ground map­ping mode of operation; disables weather-alert feature and acti-
Issued 8/10
Radar Operation
BRT
OFF
Wx WxA
GND MAP
TRKVP
TRK
vates gain control. “MAP” will be displayed below the NAV source annunciator on the radar mode line. (Magenta is not active in the GND MAP mode.)
LIGHTNING
o (Optional) Enables the Light-
ning display when pressed if a weather mode is selected for dis­p l a y .
VP
o
azimuth is selected with the TRK button, press the VP button to enter the Vertical Profile mode of operation. The Vertical Profile Screen will appear. The weather mode of operation (WX, WXA or GND MAP) displayed in the lower left corner of the display will be the same as existed just prior to selecting VP. To select a different weather mode once in Vertical P desired mode (WX, WXA or GND MAP) by pressing the appropri­ate button.
Note: A brief period of time will
The operation of scanning the antenna vertically (+/- 20 or +/-
(Optional) Once the desired
rofile, simply select the
normally elapse before the dis ­play will “paint” the Vertical Profile “picture”. This time delay is due to the fact that the radar continues its normal azimuth scan after the VP but ­ton is pressed.
30 degrees depending on the Radar) is referred to as taking a vertical “slice”.
Once Vertical Profile is selected, the desired profile-azimuth angle may be changed in two degree increments by pressing and hold­ing the appropriate TRK button. One of two things will happen when a TRK button is pressed: (1) If the radars antenna is already profiling, the antenna will move in the two-degree incre­ments, “slicing” in the direction determined by the TRK button; or (2) A “WAIT” annunciation will be displayed indicating that the radars antenna will perform the desired “slicing” function as soon as the antenna returns to the last selected prof
iling-azimuth angle.
Depending on the software ver­sion of the RDS VP radar and the system installation, the anten­na may also scan horizontally while in the VP mode. If the antenna is not sweeping vertical­ly when the TRK button is pressed, a “WAIT” annunciation will be displayed until the anten­na returns to the last vertical “slice” azimuth.
To terminate the Vertical Profile mode and return to the normal mode (horizontal scan), press the VP button. The radar system will retain its existing weather mode and return to horizontal scanning. A track line will be present on the screen for 15 seconds to indicate the location of the last profiling­azimuth angle.
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Radar Operation
BRT
OFF
GND MAP
TRKVP
TRK
Beginning with EFS software ver­sion 09, a Split Screen mode is added to the VP button selection sequence immediately following the Vertical Profile mode. During this Split Screen mode the EFS will toggle the antenna between vertical and horizontal scans every 6 seconds, allowing both to be displayed simultaneously on the MFD. See Figure 4.4.4.
Note: This Split Screen mode is
an operational enhancement added to EFS 09 software that does not require any modifica ­tion to the existing RDS 82VP/84VP/86VP/RDR 2000 weather radar systems. Since this feature was not part of the original design of these radars, the transition between horizon ­tal and vertical scans is not synchronized to the antenna scan and will therefore occur at random scan positions.
Horizontal (azimuth) and vertical (tilt) track lines are dis the MFD full time during the split screen mode to indicate the antenna scan position in each p l a n e .
played on
TRK
o
(Optional) If the weather only mode is selected on the MFD, pressing the TRK button acti­vates and slews a yellow dashed azimuth line. It also activates a digital display showing the num­ber of degrees the azimuth line is located left or right from the nose
of the aircraft. In any other map weather presentation, only the yellow dashed line will be dis­played.
For VP operations, the TRK but­ton performs two functions. 1.) Prior to engaging VP, the appro­priate button (left or right) is used to place the track line at the desired azimuth angle to be verti­cally scanned (sliced). When VP is engaged, the slice will be taken at the last position of the track line, whether it is visible or not. If the track line has not been selected after power has been applied to system and VP is engaged, the slice will be taken at 0 degrees (directly in front of the aircraft). 2.) When mode, pressing the TRK will change the selected azimuth two-degrees left or right, depend­ing on which button is pressed. Continuously holding the TRK button will result in the system “slicing” in two-degree incre­ments, called continuous profile. Continuous profile is not used on the RDR2 0 0 0 .
Beginning with EFS software ver­sion 09, the Drift Angle Track fea­ture can be activated on the MFD by pressing both TRK buttons simultaneously. While active, this feature places the track line at the drift angle provided by an LNAV. The track line always indi­cates the azimuth angle at which a vertica VP operation.
l scan is performed for
in VP
Note:Approximately 15 seconds
after drift angle track is select -
2.3.4
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Issued 8/10
Radar Operation
BRT
OFF
UP
TILT
GAIN
ON
Wx WxA
GND MAP
TRKVP
TRK
BRT
OFF
UP
TILT
DN
PULL AUTO
GAIN
PULL ARL
ON
Wx WxA
GND MAP
TRKVP
TRK
BRT
OFF
UP
TILT
DN
ed, the track line will disap ­pear, however, the weather radar will continue to use the drift angle even though the track line is not displayed.
The EFS must be receiving valid drift angle information from an LNAV and have the drift angle bug displayed before the Drfit Angle Track feature can be acti­v a t e d .
o
A configuration option was added with software 09 to allow the drift angle bug to be dis­played full time, in addition to the original option which displayed this bug only when the LNAV providing drift angle was selected as the primary na
v sensor on
E F S . Drift angle track is de-activated
and manual control returned by pressing either TRK left or TRK right buttons individually.
GAIN
Manual gain control becomes active when GND MAP is select­ed. In all other modes, gain is internally set.
tems where weather detection is no longer possible because of attenuation.
TILT
Permits manual adjustment of antenna tilt 15 degrees up or down to enable the pilot to ana­lyze the weather presentation. The tilt angle is displayed below the NAV source annunciator on the radar tilt annunciator line.
If a CP 466A is installed, pull the Tilt selector knob, PULL STAB OFF, for “STAB OFF” opera­tions. “STAB OFF” will appear on the Radar Fault/Warning line displayed below the NAV source annunciator just under the Anten­na Tilt annunciation line.
If a CP 466B is installed, pull the Tilt selector knob, PULL AUTO, for Auto Tilt. If selected, an “A” will follow the tilt direction indica­tion
arrow preceding the internal­ly calculated Auto tilt angle sup­plied by the ART.
PULL ARL
Only present when an RDS 8 6 or RDS 86VP is installed. Auto­matic Range Limit displays a blue area behind weather sys-
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2.3.5Issued 8/10
Radar Operation
*This page intentionally left blank.
2.3.6
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Issued 8/10
MFD Operation
MFD OPERATION
MULTI FUNCTION DISPLAY CONTROL PANEL
The EFS 40/50 Multi Function Display Control Panel provides for display of a more meaningful variety of data than was previ­ously accessible on EFIS MFD displays. In fact, the EFS 4 0 / 5 0 MFD may be used as a second EHSI by the pilot or copilot, pro­viding them the ability to cross check their primary EHSI, pre­view or set up for a potential nav­igation scenario, and still function as a primary weather radar or LNAV map display.
CP469
The CP 469, MFD control panel, provides control of the selection of Nav source selection, display format and course selection. Starting with software release 08, the CP 469A MFD control panel replaces the CP 469 and pro­vides additional control of Check­list, Joystick and TCAS functions. Weather radar control functions and mode selection are per­formed by the CP 466A/B, an independent weather radar con­trol panel.
CP 469A
WITH CHECKLIST & JOYSTICK
Note: Software levels 04, 05, 06 and 07 do not support Checklist or
TCAS functions.
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MFD Operation
ENT C-LTCS ARCHSI NAV
ENT C-L
CONTROL PANEL BUTTON OPERATIONS
Those push buttons which have common operation between the MFD and EHSI control panels, E D 461, CP 467 and CP 4 6 8 , will function as defined in the section 2.1, EHSI Operation unless otherwise noted in this section. For detailed operational information on those buttons please refer section 2.1.
COURSE SELECT
KNOB/BUTTON
The course select knob will func­tion identical to, but independent of the one on the EHSI control panel, ED 461, CP 467 or CP 468, when the CRS SEL button is activated. This provides inde­pendent selection of course on the MFD referenced to the same or a different nav sensor.
If the CRS SEL button is not acti­vated, the course select kn
the CP 469 will not be active. In this mode the MFD will obtain selected course data from the pilot EHSI control panel. In this mode the course on the EHSI and MFD will be synchronized, unless the selected sensor on the MFD is a LNAV providing D T K .
When the MFD course select knob is not active, a bar the color of the CRS annunciator will be placed above it. This will alert the
ob on
pilot that the MFD CRS knob is not active and is referenced to the pilot’s EHSI selected course.
Example: C R S 1 3 5
HSI BUTTON
Will function identical to, but inde­pendent of, the one on the ED 461, CP 467 or CP 468. Begin­ning with software 07, an addi­tional "Plan View" display format can be configured for presenta­tion on the MFD. When config­ured, this display format is added to the end of the HSI button selection list provided in section 2 . 1 .
Refer to section 2.1 EHSI OPER­ATION for detailed information.
ARC BUTTON
Will function similar to, but inde­pendent of, the one on the ED 461, CP 467 or CP 468. The MFD ARC button will allow the selection of an optional radar only MFD display. This display will not contain navigation or map data and is added to the end of the ARC button selection list pro­vided in
section 2.1.
NAV BUTTON
The NAV button may be config­ured at the time of installation and certification to operate in one of two methods.
2.4.2
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Issued 8/10
MFD Operation
o Configuration option number
one will slave the MFD to the #1 EHSI. The NAV push button will cause the MFD to display either the same NAV sensor as dis­played on the EHSI or the LNAV. When this configuration is select­ed the 1-2 push button allows selection between the on s i d e and off side sensors. Once a side is selected, that side will remain the selected side until the 1-2 button is pressed again. This allows the pilot the ability to select the off side sensor to pro­vide himself a constant visual cross comparison.
o Configuration option number
two enables the NAV button
function identical to, but indepen­dent of, the one on the ED 4 6 1 , C P 467 or CP 468. When this configuration option is selected the pilot can select any available nav sensor for display on the MFD independent of what is dis­played on the EHSI.
to
1-2 BUTTON
If NAV push button configuration option number one is selected, where the MFD is slaved to the EHSI, the 1-2 push button allows the pilot to select between on side and off side NAV sensors. Unlike the 1-2 push button on the EHSI control panel, it selects which side will be displayed until pushed again. A press of the NAV push button will not cause a selected off side sensor to cycle back to an on side sensor as it does on the EHSI.
If NAV push button configuration option number two is selected, the 1-2 button functions identical to, but independent of, the one on the ED 461, CP 467 or CP 4 6 8 .
BEARING #1 & #2 BUTTON
Will function identical to, but inde­pendent of, the one on the ED 461, CP 467 or CP 468.
Refer to section 2.1 EHSI OPER­ATION for detail information.
RANGE UP/DOWN BUTTON
Will function identical to, but inde­pendent of, the one on the ED 461, CP 467 or CP 4 6 8 .
Refer to section 2.1 EHSI OPER­ATION for detail information.
JOYSTICK
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W A Y P O I N T E N T R Y O P E R A T I O N
When the joystick is interfaced to an EFS 40/50 system, it can be used to generate and move sin­gle waypoint on the display unit. These waypoints can then be entered into the KNS 81, KNS 660, KLN other LNAV using an appropriate GAMA 429 interface. The KNS
88, KLN 90, or any
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2.4.3Issued 8/10
MFD Operation
81 must have the graphic output
b u s . With an LNAV, RNAV, (or KNS
81 configured as a NAV) select­ed for the primary nav sensor and during display of a NAV MAP on the MFD, initial movement of the joystick will create a waypoint cursor ahead of the aircraft on the half range ring at the current heading. This will be true for both HSI and ARC display formats. The cursor will be a standard white waypoint symbol. Move­ment of the waypoint will be in any of the eight directions com­manded by the joystick. The rate of movement will start off slow and increase in speed in two steps. Return of the joystick to its center, off position at any time will
reset the rate of movement to the slowest speed. The cursor location on the display screen and its rate of movement relative to the display screen will be inde­pendent of the display range selected. The cursor is not allowed to exit the compass. When an LNAV is selected as the primary navigation source, Lat/Lon coordinates of the cursor will be displayed in the lower cen­ter of the display. When a KNS 81 is the active primary naviga­tion source, and it is not in the ILS mode, radial and distance of the cursor from the navaid in use by the KNS 81 will be displayed instead of Lat/Lon coordinat
The cursor position information can be transferred to the LNAV or KNS 81 that is selected as the primary navigation sensor, by pressing the ENTER button while
es.
the cursor and its coordinates are displayed. The coordinates of the cursor will remain displayed for at least 10 seconds and disappear from the display within 15 sec­onds after activating the ENTER button. If the waypoint cursor is not moved for 20 seconds, it will disappear from view. The next time the joystick is moved, the cursor will re-appear in the same location on the display screen. However, a change of primary NAV sensor or display modes will reset the invisible cursor location to its initial starting position.
Note: Systems with an MFD can
have the joystick on the CP 469A MFD control panel or a stand alone joystick. Additional joysticks for the pilot or copilot normally will not be installed. Systems without an MFD may have up to t
wo joysticks that are completely independent of each other; one for the pilot and one for the copilot. The pilots joystick can create or move a waypoint only on the pilots EHSI, and any waypoint created by the pilot can only be loaded into the #1 RNAV or #1 LNAV. Likewise, the copi ­lots joystick can create or move a waypoint only on the copilots EHSI, and any way ­point created by the copilot can only be loaded into the #2 RNAV or #2 LNAV.
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PLAN VIEW OPERATION
(available with 07 and higher)
Plan View will be available in the HSI key selection sequence
2.4.4
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Issued 8/10
MFD Operation
ENT
immediately following “DG MODE”. In addition to selecting the plan view display mode, the operator must be using a nav source which will provide flight plan information like FMS, GPS, and LORAN sensors.
If joystick is not available, the center of the screen will repre­sent the aircraft present position when plan view mode is entered, and the map may not be moved from this reference. Range could be changed using the range but­tons. When a joystick is avail­able, it will control the flight plan view relative to the aircraft pre­sent position. Pressing the “ENT button wiil reset the display where the aircraft is displayed in the center of the display
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CHECKLIST OPERATION
.
(available with 08 and higher)
In the Checklist mode, the Joy­stick commands will be limited to four positions: UP, DOWN, LEFT and RIGHT. The 45° commands will be ignored.
A down push on the joystick will advance the cursor checklist line. A down push at the bottom of a checklist page will advance the cursor to the next page if avail­able. Continuous downward pushes will wrap the cursor within a checklist level.
An up push on the joystick will move the cursor up one checklist line. An up push at the top of a checklist page will move the cur­sor to the previous page if avail-
able. Continuous upward pushes will wrap the cursor within a checklist level. A right push on the joystick will move the cursor to the top of the next checklist page. Continuous right pushes will wrap the cursor to the top of the next page within the list.
A left push on the joystick will move the cursor to the top of the previous checklist page. Contin­uous left pushes will wrap the cursor to the top of the previous page within the list.
ENT BUTTON
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W A Y P O I N T
ENTRY OPERATION
In the map mode the cursor posi­tion information can be trans­ferred to the LNAV or KNS 81 that is selected as the primary navigation senso the ENTER button while the cur­sor and its coordinates are dis­played. The coordinates of the cursor will remain displayed for at least 10 seconds and will disap­pear from the display within 15 seconds after the ENTER button is pressed.
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PLAN VIEW OPERATION
(available with 07 and higher)
In the Plan View mode the enter button will be used to reset the aircraft in the center of the dis­p l a y .
r, by pressing
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2.4.5Issued 8/10
MFD Operation
TST
REF
BRT
1-2
CHK LIST
TCAS ONLY
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CHECKLIST OPERATION
(available with 08 and higher)
In the Checklist mode the enter button will generally function to check items in the list. The checklist was designed such that the pilot can complete the entire checklist by using only the enter b u t t o n .
Normally, pressing the ENT but­ton will cause an unchecked checklist line to be checked and the cursor to advance to the next unchecked line. At the end of a page pressing the ENT button will cause the cursor to advance to the next page (if available) and to check the first unchecked line on that page. If no unchecked items exist between the cursor position and the end of the list, the cursor is placed on the first unchecked page which re
enced the specific list.
fer-
TEST/REFERENCE
CHECKLIST SELECT
(available with 08 and higher)
This button is not functional in Software 04, 05, 06 or 07.
Pressing the checklist button will display the root page of the checklist. If an emergency dis­crete is active, pressing the checklist button will display the emergency page
TCAS ONLY SELECT
(available with 08 and higher)
This button is not functional in Software 04, 05, 06 or 07.
The TCAS ONLY button will tog­gle the MFD display between the TCAS only presentation and the previously selected mode.
Will function identical to, but inde­pendent of, the one on the ED 461, CP 467 or CP 468.
With checklist active, this button will cause a checklist "help" page to be displayed on the MFD.
Refer to section 2.1 EHSI OPER­ATION for detailed information.
2.4.6
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TERRAIN SELECT
(available with 14 and higher)
This button is not functional in Software 04, 05, 06, 07, 08, 09, 10, 11, 12 or 13.
The TERRAIN SELECT button will to between the Terrain presentation and the previously selected weather mode.
ggle the MFD display
Issued 8/10
Abbreviated Operations
Issued 8/10
Figure 3.1
ED 461 EHSI CONTROL PANEL OPERATION
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3.1
Abbreviated Operations
Issued 8/10
Figure 3.2
CP 468 EFIS CONTROL PANEL OPERATION
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3.2
Abbreviated Operations
Issued 8/10
Figure 3.3
CP 467 EFIS CONTROL PANEL OPERATION
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3.3
Abbreviated Operations
Issued 8/10
Figure 3.4
CP 469 MFD CONTROL PANEL OPERATION
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3.4
Abbreviated Operations
Issued 8/10
Figure 3.5
CP 469A MFD CONTROL PANEL OPERATION
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3.5
EHSI Displays
Warnings Cautions/Abnormal Source Scales and associated figures On-side approach and navigation data Cross-side NAV data On-side non-approach navigation data (LNAV) On-side commanded data Cross-side commanded data Selected heading, DME HOLD annunciation Selected source
Selected active route/flight plan Cross-side selected active route/flight plan
Held DME distance display
Red Yellow White Green Yellow Cyan Green Yellow Orange
Green Yellow
White
Matches NAV data color
EHSI DISPLAYS
EFS 40/50 COLOR STANDARDS
The EFS 40/50 uses a defined color set which aids the pilot in inter­preting displayed information. A brief summary of the color set is as f o l l o w s :
For an example of the color usage, refer to figure 4.1.3 at the back of this section, Typical EFS 40/50 EHSI Color Displays.
STANDARD EHSI DISPLAYS
Refer to Figures 4.1.5 and 4.1.6 while reviewing STANDARD EHSI DISPLAYS.
NORMAL COMPASS CARD
360° rotating white compass scale indicates aircraft heading referenced to white triangular heading index (lubber line). The compass scale is divided in 5­degree increments with the 10­degree divisions being approxi­mately twice as long. Fixed
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45-degree index marks are adja­cent to the compass scale.
Free DG (directional gyro) opera­tion will be annunciated by a yel­low FDG (or FHDG) to the left of the lubber. The Free mode annunciation will only be support­ed in installations with an ARINC 429 AHRS (Attitude Heading Reference System) that supports the Free DG (directional gyro) mode of operation via the digital data bus.
4.1.1Issued 8/10
EHSI Displays
N o t e : Software release 06
changed the DG annunciation to HDG to better describe the variety of heading sources that may be interfaced with the E F S 40/50, ie. INS, AHRS and conventional gyros.
Dual selectable compass inputs are provided for. If a second compass system is installed, the cross-side source is selected by means of a remote mounted switch. Once the alternate com­pass source has been selected, a yellow DG1 (HDG1) or DG2 (HDG2) will be displayed to the left of the lubber line.
In a dual EFS 40/50 installation with software release 04 or 05, if both systems use the same heading source, annunciations will appear on both EHSIs alert­ing the pilots they have the
source selected. The EHSI that is using its normal heading source will annunciate a yellow “DG” with a yellow box around it to indicate that its primary heading source has been selected for use on the other EHSI. The EHSI that is using its alternate heading source will annunciate a yellow “DG1” or “DG2” as applicable with a yellow box around it to indicate the heading source being used is the same one being used by the other EHSI. For example, if the co-pilot were to select his alternate heading source, heading #1, “DG1” would appear with a box around it on th
e co-pilots EHSI and DG would
appear with a box around it on
same
the pilot’s EHSI. In a dual EFS 40/50 installation
with software release 06 and above, if both systems select the same heading source, a yellow “HDG1” or “HDG2” with a yellow box around it will appear on both EHSIs alerting the pilots that they have the same source selected.
Figure 4.1.1
SAME HEADING SOURCE
SELECTION
When two compass sources are available, the two inputs are compared for agreement. If the two inputs do not fall within 6­degrees of each other while in level flight, a yellow comparison warning, HDG under a double­ended arrow, will be annunciated to the right of the lubber line. See figure 4.1.5, EHSI SYMBOL DEFINITION.
NAVIGATION SOURCE ANNUNCIATION
A vertical three- or four-letter alphanumeric readout located on the left or right side of the dis­play, depending on vertical scale side selection, indicates the sys­tem selected as the primary navi­gation sensor.
For dual sensor installations the cross-side navigation system may be selected by pressing the 1-2 push button. Example: pilot
4.1.2
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Issued 8/10
EHSI Displays
selecting co-pilots navigation system or co-pilot selecting pilots navigation system. The 1-2 push button will not be active if the system configuration does not support two of the same type NAV sensors.
Green annunciations indicate an on-side approach NAV system or an enroute NAV system which has been approved for approach use is being displayed. Yellow indicates the cross-side system has been selected. Cyan annun­ciations apply to on-side non­approach LNAV systems. These color codes apply to the NAV source annunciator, CRS pointer, deviation bar, CRS line in MAP mode, CRS, distance, gro
speed, time-to-station, drift angle pointer and vertical deviation p o i n t e r .
und-
Software release 06 incorporated the ability to interface with the TACAN version of the KNS 8 1 and annunciate TCN when the K N S 81 is in the TACAN mode of operation.
If both sides select the same navigation source, (i.e., pilot and co-pilot select VOR 2) a yellow box is placed around the naviga­tion source annunciator on both E H S I s .
If both sides select their respec­tive cross-side navigation source (i.e., pilot selects system 2, co­pilot selects system 1) then both NAV source annunciators will be yellow with no yellow box.
N o t e : Same source annuncia -
tion rules also apply to the heading source.
Figure 4.1.2
SAME NAVIGATION SOURCE SELECTION ANNUNCIATION
SYMBOLIC AIRCRAFT
N o t e : Starting with software 08
The orange symbolic aircraft pro­vides a visual reference of the aircraft present position in rela­tionship to the deviation bar.
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a configuration option is avail ­able for the display of Fixed wing or Rotary Wing symbolic aircraft.
4.1.3Issued 8/10
EHSI Displays
HEADING SELECT “BUG”
A notched heading bug is manu­ally rotated around the compass scale by the heading select knob on the control panel. In the 360­degree compass mode a full time digital readout of the selected heading is displayed below the vertical deviation scale position. In the ARC mode, a digital head­ing readout is displayed when the heading bug is not completely in view. The digital readout will be positioned just inside the com­pass scale on the side nearest the heading bug. Once set, the heading bug rotates with the compass card. The heading bug is used to indicate desired head­ing and provides selected head­ing reference for autopilot steer­i n g .
A RED X will be drawn through the heading bug if there is a he
ading select knob failure on
the EFS 40/50 control panel. Software release 06 added the
options, selectable at the time of installation and certification, to select one of three heading bug and digital readout color choices:
o O r a n g e
C y a n
o
o
M a g e n t a
Prior to software 06, the heading bug and selected heading read­out are always orange. The heading bug is not displayed in MFD only installations. This became an EFS system configu­ration option with software 09.
COURSE SELECT
The CRS control knob rotates the course pointer about the com­pass scale and sets digital course readout. Once set, the course pointer rotates with the compass card. The selected course indicates desired naviga­tion course to be flown. Depend­ing on the LNAV (long range nav­igation) installed, the course pointer may automatically be positioned to the DTK (desired track) when LNAV is selected as the primary sensor. When LNAV is the selected sensor and DTK is displayed, the EFS 4 0 / 5 0 course select knob is disabled.
In the upper left corner of the dis­play, an alphanumeric annunciates the letters CRS and indicates the selected navigation course in degrees. When in a NAV map display mode, the course pointer will not be dis­played, the alphanumeric readout will be the only reference for the selected course.
N o t e : Desired track readout
(DTK) generated by an LNAV system replaces (CRS) in LNAV mode. Some LNAV systems may display CRS or DTK depending on the select ­ed mode. MLS may display AZ (azimuth) or BAZ (back azimuth) depending on the selected mode.
Systems with Software release 05 retain (remember) the manu­ally selected the CRS knob, when the selected
course, as set by
readout
4.1.4
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
Issued 8/10
EHSI Displays
primary NAV sensor is sequenced through the LNAV position. In previous software releases, once the LNAV sensor was displayed, its CRS or DTK would become the selected course, requiring the CRS to be reset when another primary Nav sensor was selected.
This change will allow an ILS inbound course to be selected prior to the completion of an LNAV flight leg that will be fol­lowed by an ILS approach.
zontal position, providing stan­dard course deviation information (CDI) referenced to the digital CRS selected. A RED X will be drawn through the CRS annunci­ation if there is a course select knob failure. In the event the selected course or desired track received from the LNAV becomes invalid, a RED X will be drawn through the digital r e a d o u t .
Note: The above heading failure
mode does not apply when ADF is the primary NAV sen -
In the event of a heading failure, the course pointer head and tail are removed and the course deviation scale is fixed in a hori-
sor. (ADF D-Bar is heading dependent and is non-opera ­tional without valid heading.)
LATERAL COURSE DEVIATION SCALE
The course deviation scale, two white dots evenly spaced on both sides of the symbolic aircraft, provides a reference for the course deviation bar to indicate the center line of the selected
navigation or localizer course in relation to the symbolic airplane.
The following represents the deviation scale for different navi­gation sources.
N o t e : D e p e n d i n g
on the type of LNAV installed, the Lateral Devia ­tion may be differ ­ent. GPS lateral deviation scale is for TSO C129 capable units only. SW 15 and later accepts C145/C146 equip ­ment variable deflection values.
SW 04/05/06/07/08/09/10/11/12/13/14/15/16
LATERAL DEVIATION SCALE
(Aircraft Displacement)
4.1.5Issued 8/10
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