Aspen Avionics EFD1000 E5 User manual

EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
DOCUMENT # 900-00041-001 PAGE 1-226 REVISION D
© Copyright 2019 Aspen Avionics Inc.
EFD1000 E5
Dual Electronic Flight Instrument (EFI)
Installation Manual
April 2019

EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
DOCUMENT # 900-00041-001 PAGE 2-226 REVISION D
© Copyright 2019 Aspen Avionics Inc.
Special Notes to the Installer
It is important to review the entire Installation Manual before installing the EFD1000 E5. The following
items are of special note and should be considered for planning and installation.
The installer must determine whether the design changes described in this document are
compatible with previously approved modifications.
This installation is not authorized in aircraft with a MTOW exceeding 6000 pounds.
Correct placement of the aircraft instruments is critical to maintain the aircraft
certification. Certain instruments can be removed. More importantly, certain instruments
must not be removed, See Section 4. The existing turn/bank instrument or a backup attitude
indicator must be retained for all installations except Aircraft Limited to VFR, See Section 4.5.
The RSM contains magnetic elements that are sensitive to magnetic fields on the
aircraft. Section 6.9 describes locating the RSM installation. Mounting the RSM over the cabin
can be problematic due to passengers using headsets with magnetic speakers. Exercise the
control cables while validating a location. Consider all the magnetic field variations. A
satisfactory RSM location is part of the Final Check Sheet. Use caution when installing the RSM
connector to avoid damaging the connector or wiring.
The RSM can be damaged if exposed to a magnet. Do not use magnetic tools or magnetic
levels near the RSM.
The EFD1000 E5 does not display Flight Director. The existing flight director indicator will
need to be retained and relocated. See section 4.4.3

EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
DOCUMENT # 900-00041-001 PAGE 3-226 REVISION D
© Copyright 2019 Aspen Avionics Inc.
DOCUMENT REVISIONS
Revisio
n
Description of Change
ECO
( )
Original Revision
5465
A
Updated manual for initial release to the field
5483
B
Removed Special Conditions for Aircraft Limited to VFR. Clarified regulatory wording and
typographical errors.
5578
C
Corrected the transmit rate for the ARINC 429 outputs. Added a date to the cover. Updated
paragraph 7.2.11 to add tubing.
5588
D
Added Figure 4-1A, “VFR Configuration”. Added Section 4.5, Special Considerations for Aircraft
Limited to VFR. Added Figure 9-4 “VFR Only - No GPS input Configurations”and updated Fig 9-
10 to add VFR config with NAV, no GPS. Added VFR configs to 10.4.6.8. Added step to Appdx B
–Final Check Sheet to verify aircraft is placarded for VFR- if limited to VFR.
5718
Prepared
By:
Tim McNany
Reviewed
By:
Mike Studley /
Penny Heinz
See ECO Record For Release Authorization

EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
DOCUMENT # 900-00041-001 PAGE 4-226 REVISION D
© Copyright 2019 Aspen Avionics Inc.
This manual contains FAA Approved installation instructions for installation of the Aspen™ EFD1000 E5
system under the AML STC for use as an electronic flight display during day/night IFR and VFR
operations in those Part 23 Class I and II aircraft (as defined in AC 23.1309-1E) listed on the
AML. Installation of the EFD1000 E5 into part 23 Class I or II aircraft not included in the AML, into any
14 CFR Part 23 Class III or IV aircraft, or into any part 25, 27, or 29 aircraft, or non-U.S. registered
aircraft requires separate airworthiness approval.
This document is protected by the Copyright Laws of the United States and other countries. Nevertheless,
authorized Aspen dealers and distributors are licensed to make a reasonable number of verbatim copies of this
document for use in their business as Aspen dealers.
Reproduction for any other purpose is strictly prohibited.
Public or fee-based copy centers need not inquire into the bearer's status as an Aspen dealer or distributor, into the
purposes for which reproductions are to be made, or into the reasonableness of the number of reproductions
requested.

EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
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© Copyright 2019 Aspen Avionics Inc.
Table of Contents:
LIST OF TABLES ........................................................................................................................... 12
LIST OF FIGURES.......................................................................................................................... 13
LIST OF DEFINITIONS, ACRONYMS, ABBREVIATIONS ...................................................................... 16
1INTRODUCTION ................................................................................................ 17
1.1 PART NUMBERS .................................................................................................... 17
1.1.1 LATEST APPROVED SOFTWARE VERSIONS...................................................................... 17
1.1.2 AML-STC DOCUMENT LIST .................................................................................... 18
1.2 INSTALLATION KIT CONTENTS................................................................................... 18
1.3 OPTIONAL LRU INSTALL KITS ................................................................................... 19
1.4 ACCESSORIES REQUIRED BUT NOT SUPPLIED –EFD1000 E5............................................. 20
1.5 OPTIONAL ACCESSORIES NOT SUPPLIED –EFD1000 E5 .................................................. 20
1.6 OPTIONAL ACCESSORIES REQUIRED BUT NOT SUPPLIED –EA100 ....................................... 20
1.7 SPECIAL TOOLS REQUIRED ....................................................................................... 21
1.8 VENDOR INFORMATION ........................................................................................... 21
1.9 WARRANTY REGISTRATION....................................................................................... 21
1.10 REGULATORY COMPLIANCE ...................................................................................... 21
1.10.1 TECHNICAL STANDARD ORDER ................................................................................. 21
1.10.2 PMA APPROVAL ................................................................................................... 21
1.10.3 SOFTWARE CERTIFICATION ....................................................................................... 22
1.10.4 ENVIRONMENTAL COMPLIANCE.................................................................................. 22
1.10.5 INSTALLATION APPROVAL ........................................................................................ 22
1.11 FIELD REPLACEABLE PARTS....................................................................................... 22
1.12 RESERVED ........................................................................................................... 22
2EQUIPMENT SPECIFICATIONS AND LIMITATIONS ................................................. 23
2.1 EFD1000 E5...................................................................................................... 23
2.1.1 GENERAL SPECIFICATIONS ........................................................................................ 23
2.1.2 OPERATIONAL SPECIFICATIONS .................................................................................. 23
2.1.3 I/O SPECIFICATIONS .............................................................................................. 23
2.1.4 CERTIFICATION SPECIFICATIONS ................................................................................ 23
2.1.5 EFD1000 E5 OUTLINE DRAWING ............................................................................. 24
2.1.6 DESIGN EYE VIEWING ENVELOPE ................................................................................ 24
2.2 REMOTE SENSOR MODULE (RSM) .............................................................................. 25
2.2.1 GENERAL SPECIFICATIONS ........................................................................................ 25
2.2.2 OPERATIONAL SPECIFICATIONS .................................................................................. 25
2.2.3 I/O SPECIFICATIONS .............................................................................................. 25
2.2.4 CERTIFICATION SPECIFICATIONS ................................................................................ 25
2.2.5 OUTLINE DRAWING: ............................................................................................... 26
2.3 CONFIGURATION MODULE (CM)................................................................................ 26
2.3.1 GENERAL SPECIFICATIONS ........................................................................................ 26
2.3.2 OPERATIONAL SPECIFICATIONS .................................................................................. 27
2.3.3 I/O SPECIFICATIONS .............................................................................................. 27
2.3.4 CERTIFICATION SPECIFICATIONS ................................................................................ 27
2.3.5 OUTLINE DRAWING ................................................................................................ 27

EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
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2.4 ANALOG CONVERTER UNIT (ACU) ............................................................................. 28
2.4.1 GENERAL SPECIFICATIONS ........................................................................................ 28
2.4.2 OPERATIONAL SPECIFICATIONS .................................................................................. 28
2.4.3 I/O SPECIFICATIONS .............................................................................................. 28
2.4.4 CERTIFICATION SPECIFICATIONS ................................................................................ 28
2.4.5 OUTLINE DRAWING: ............................................................................................... 29
2.5 ANALOG CONVERTER UNIT 2 ................................................................................... 29
2.5.1 GENERAL SPECIFICATIONS ........................................................................................ 29
2.5.2 OPERATIONAL SPECIFICATIONS .................................................................................. 29
2.5.3 I/O SPECIFICATIONS .............................................................................................. 29
2.5.4 CERTIFICATION SPECIFICATIONS ................................................................................ 30
2.5.5 OUTLINE DRAWING ................................................................................................ 30
3SYSTEM DESCRIPTION ....................................................................................... 31
3.1 EFD1000 E5 DUAL ELECTRONIC FLIGHT INSTRUMENT (EFI) SYSTEM................................... 31
3.2 EFD1000 E5 FLIGHT DISPLAY (EFD)......................................................................... 31
3.3 REMOTE SENSOR MODULE (RSM) .............................................................................. 32
3.4 CONFIGURATION MODULE (CM)................................................................................ 32
3.5 ANALOG CONVERTER UNIT (ACU) ............................................................................. 32
3.6 ANALOG CONVERTER UNIT 2(ACU2) ........................................................................ 32
3.7 SYSTEM ARCHITECTURE .......................................................................................... 33
4STC SPECIFIC REQUIREMENTS AND LIMITATIONS ................................................ 35
4.1 EFD1000 E5 SYSTEM LIMITATIONS ........................................................................... 35
4.2 EA100 INSTALLATION LIMITATIONS (EA100 IS OPTIONAL) .............................................. 35
4.3 AUTHORIZED CONFIGURATIONS................................................................................. 35
4.4 GENERAL STANDBY INSTRUMENT REQUIREMENTS FOR IFR-CAPABLE AIRPLANES ...................... 38
4.4.1 PNEUMATIC ATTITUDE (EXISTING) .............................................................................. 38
4.4.2 ELECTRIC ATTITUDE (EXISTING) ................................................................................. 38
4.4.3 EXISTING ATTITUDE POSITIONING (IF KEEPING)............................................................... 38
4.4.4 AIRSPEED AND ALTIMETER ....................................................................................... 40
4.4.5 BACK UP NAV INDICATOR........................................................................................ 40
4.4.6 PLACARDS........................................................................................................... 40
4.5 SPECIAL CONSIDERATION FOR AIRPLANES LIMITED TO VFR ............................................... 41
5PRE-MODIFICATION PLANNING ......................................................................... 42
5.1 PRE-MODIFICATION CHECKLIST ................................................................................ 42
5.1.1 DIRECTIONAL GYRO/HSI........................................................................................ 43
5.1.2 AIRCRAFT POWER REQUIREMENTS .............................................................................. 43
5.1.3 EQUIPMENT POWER REQUIREMENTS ............................................................................ 43
5.1.4 RESERVED ........................................................................................................... 43
5.1.5 CESSNA 190/195 SPECIAL CONSIDERATION ................................................................ 44
5.2 RESERVED ........................................................................................................... 44
5.3 CONVENTIONAL LANDING GEAR “TAIL DRAGGER”AIRCRAFT .............................................. 44
5.4 OPTIONAL INTERFACES ........................................................................................... 45
5.4.1 AUTOPILOT ......................................................................................................... 45
5.4.1.1 EA100 ADAPTER.................................................................................................. 45
5.4.2 GPS NAVIGATOR COMPATIBILITY............................................................................... 46

EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
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5.4.3 GPSS ................................................................................................................ 46
5.4.4 GPS/ NAV SWITCHING .......................................................................................... 46
5.4.5 HEADING OUTPUT ................................................................................................. 47
5.4.6 AIR DATA OUTPUTS............................................................................................... 47
5.4.6.1 EFD1000 E5 AS ENCODING ALTITUDE SOURCE ............................................................ 47
5.4.7 FLUSH OR RECESS MOUNTING THE EFD ....................................................................... 48
6MECHANICAL INSTALLATION............................................................................. 50
6.1 UNPACKING AND INSPECTING EQUIPMENT..................................................................... 50
6.2 EQUIPMENT LOCATION DOCUMENTATION..................................................................... 50
6.3 LOG BOOK ENTRY ................................................................................................. 50
6.4 WEIGHT AND BALANCE ........................................................................................... 50
6.5 MOUNTING LIMITATIONS ......................................................................................... 50
6.5.1 EFD1000 E5 MOUNTING LIMITATIONS (EFD) .............................................................. 51
6.5.2 RSM MOUNTING LIMITATIONS .................................................................................. 51
6.6 EQUIPMENT BONDING ............................................................................................. 51
6.7 COOLING ............................................................................................................ 52
6.8 EFD INSTALLATION ............................................................................................... 52
6.8.1 EFD MOUNTING LOCATION ..................................................................................... 52
6.8.2 SURFACE MOUNTING THE EFD AS PER FIGURE 6-2 ......................................................... 52
6.8.3 RECESS MOUNTING THE EFD AS PER FIGURE 6-4 ........................................................... 54
6.8.3.1 RECESS MOUNT MODIFICATION PROCEDURE ................................................................. 54
6.8.4 EFD BONDING STRAP ............................................................................................. 59
6.8.5 PITOT AND STATIC CONNECTIONS ............................................................................. 59
6.8.6 QUICK CONNECTOR INSTALLATION ............................................................................ 60
6.8.7 LEAK CHECK REQUIREMENTS .................................................................................... 60
6.9 RSM INSTALLATION ............................................................................................... 61
6.9.1 RSM INTERNAL MOUNTING...................................................................................... 61
6.9.2 RSM INVERTED OR BOTTOM MOUNTING ...................................................................... 61
6.9.3 RSM EXTERNAL TOP MOUNTING ............................................................................... 61
6.9.4 PROPOSED RSM LOCATION CHECK ............................................................................ 65
6.9.5 PRESSURIZED AIRCRAFT........................................................................................... 67
6.9.6 RSM MOUNTING ON NON-METAL OR DAMAGE-TOLERANT DESIGN AIRCRAFT....................... 68
6.9.7 RSM MOUNTING ANGLES ........................................................................................ 68
6.9.7.1 LONGITUDINAL AXIS .............................................................................................. 68
6.9.7.2 PITCH AXIS.......................................................................................................... 68
6.9.7.3 ROLL AXIS........................................................................................................... 69
6.9.8 RSM EXTERNAL MOUNT –ALUMINUM SKIN .................................................................. 70
6.9.8.1 RSM DOUBLER FABRICATION.................................................................................... 70
6.9.9 RSM INTERNAL MOUNT .......................................................................................... 72
6.9.10 RSM INSTALLATION ............................................................................................... 72
6.9.11 RSM SHIM FABRICATION (IF NECESSARY)...................................................................... 73
6.10 ACU/ACU2 INSTALLATION..................................................................................... 74
6.10.1 ACU/ACU2 MOUNTING ........................................................................................ 75
6.11 CONFIGURATION MODULE INSTALLATION ..................................................................... 78
7ELECTRICAL INSTALLATION............................................................................... 80

EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
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7.1 ELECTRICAL LOAD ANALYSIS .................................................................................... 80
7.2 ELECTRICAL INSTALLATION ...................................................................................... 80
7.2.1 EFD1000 E5...................................................................................................... 80
7.2.2 ACU OR ACU2 (OPTIONAL)..................................................................................... 80
7.2.3 MISCELLANEOUS WIRING ......................................................................................... 80
7.2.4 HIRF/LIGHTNING REQUIREMENTS .............................................................................. 81
7.2.5 EFD TO GPS/VLOC/ACU WIRING ........................................................................... 81
7.2.6 RSM WIRING ....................................................................................................... 82
7.2.6.1 ASSEMBLY USING ASPEN PREFABRICATED 35FT AND OPTIONAL 50FT CABLES .......................... 82
7.2.6.2 ASSEMBLY USING M27500-A24SD7T23 CABLE ......................................................... 82
7.2.6.3 EFD END........................................................................................................... 83
7.2.7 CONFIGURATION MODULE WIRING ............................................................................. 83
7.2.8 ACU WIRING ....................................................................................................... 84
7.2.9 BACK UP NAV INDICATOR WIRING............................................................................. 84
7.2.10 AUTOPILOT WIRING ............................................................................................... 84
7.2.11 BACKUP INSTRUMENT WIRING AND CABLE BUNDLE .......................................................... 84
8ELECTRICAL CONNECTIONS............................................................................... 86
8.1 EFD ELECTRICAL SPECIFICATIONS .............................................................................. 86
8.1.1 POWER INPUT....................................................................................................... 86
8.1.2 RS-232 GPS INPUT.............................................................................................. 86
8.1.3 RS-232 ADC OUTPUT .......................................................................................... 86
8.1.4 ARINC 429 GPS INPUTS........................................................................................ 86
8.1.5 ARINC 429 VLOC INPUT ...................................................................................... 87
8.1.6 ARINC 429 OUTPUT ............................................................................................ 87
8.2 ACU ELECTRICAL SPECIFICATIONS (910-00004 ALL DASH NUMBERS) ................................ 88
8.2.1 POWER INPUT....................................................................................................... 88
8.2.2 RESERVED ........................................................................................................... 88
8.2.3 VLOC RECEIVER ................................................................................................... 88
8.2.3.1 NAV COMPOSITE INPUT.......................................................................................... 88
8.2.3.2 ILS ENERGIZE DISCRETE INPUT .................................................................................. 88
8.2.3.3 GLIDE SLOPE DEVIATION INPUT ................................................................................. 88
8.2.3.4 GLIDE SLOPE FLAG INPUT ........................................................................................ 89
8.2.4 GPS RECEIVER...................................................................................................... 89
8.2.4.1 OBS SINE,COSINE,ROTOR...................................................................................... 89
8.2.4.2 TO/ FROM FLAG INPUT........................................................................................ 89
8.2.4.3 LEFT/ RIGHT INPUT............................................................................................. 89
8.2.4.4 LATERAL FLAG INPUT ............................................................................................. 89
8.2.4.5 VERTICAL DEVIATION INPUT ..................................................................................... 89
8.2.4.6 VERTICAL DEVIATION FLAG INPUT .............................................................................. 89
8.2.4.7 OBS/ LEG (HOLD) INPUT ...................................................................................... 89
8.2.4.8 APPR ACTIVE INPUT .............................................................................................. 90
8.2.4.9 FCS-LOC ENGAGE INPUT ....................................................................................... 90
8.2.5 AUTOPILOT ......................................................................................................... 90
8.2.5.1 LATERAL DEVIATION OUTPUT ................................................................................... 90
8.2.5.2 LATERAL FLAG OUTPUT .......................................................................................... 90

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8.2.5.3 VERTICAL DEVIATION OUTPUT .................................................................................. 90
8.2.5.4 VERTICAL FLAG OUTPUT ......................................................................................... 90
8.2.5.5 ILS ENERGIZE OUTPUT............................................................................................ 90
8.2.5.6 VOLT REFERENCE OUTPUT ....................................................................................... 91
8.2.5.7 KI-525A HEADING AND COURSE DATUM OUTPUT ........................................................ 91
8.2.5.8 NSD-360 HEADING AND COURSE DATUM OUTPUT ....................................................... 91
8.2.5.9 PN-101 HEADING AND COURSE DATUM OUTPUT ......................................................... 92
8.2.5.10 HEADING VALID OUTPUT......................................................................................... 92
8.2.5.11 GPS SELECTED OUTPUT .......................................................................................... 93
8.2.5.12 ARINC 429 OUTPUT ............................................................................................ 93
8.3 ACU2 ELECTRICAL SPECIFICATIONS (910-00004-10X ONLY)......................................... 93
8.3.1 HEADING SYNCHRO OUT ......................................................................................... 93
8.3.2 +/-15VDC POWER OUTPUT ................................................................................... 94
8.3.3 GLIDESLOPE FLAG (NARCO)...................................................................................... 94
8.3.4 ARINC 429 OUTPUT ............................................................................................ 94
8.4 EFD PIN OUT ...................................................................................................... 94
8.5 RSM PIN OUT...................................................................................................... 96
8.6 CONFIGURATION MODULE PIN OUT ............................................................................ 96
8.7 ACU/ACU2 PIN OUT............................................................................................ 97
9INSTALLATION WIRING DIAGRAMS................................................................... 102
9.1 LIST OF WIRING DIAGRAMS –EFD1000 E5 ............................................................... 102
9.2 OPTIONAL INTERFACES –ACU AND ACU2................................................................. 103
10 CONFIGURATION AND EQUIPMENT CHECKOUT ................................................ 134
10.1 WIRING CHECKS.................................................................................................. 134
10.2 BONDING CHECK –14CFR 23.867(B)..................................................................... 134
10.3 INITIAL SYSTEM TURN ON...................................................................................... 134
10.4 SYSTEM CONFIGURATION....................................................................................... 135
10.4.1 MAIN MENU ACCESS ............................................................................................ 135
10.4.2 MENU NAVIGATION ............................................................................................. 135
10.4.3 EDIT MODE ....................................................................................................... 135
10.4.4 MAIN MENU CONFIGURATION ................................................................................. 135
10.4.5 INSTALLATION MENU –UNIT CONFIGURATION............................................................. 135
10.4.6 EFD1000 E5 INSTALLATION MENU CONFIGURATION ................................................... 138
INSTALLATION MENU CONFIGURATION –EFD1000 E5 ................................................................ 138
10.4.6.1 INSTALLATION MENU PAGE -IAS CONFIG A ............................................................. 138
10.4.6.2 INSTALLATION MENU PAGE –IAS CONFIG B.............................................................. 140
10.4.6.3 INSTALLATION MENU PAGE –IAS CONFIG C ............................................................. 140
10.4.6.4 INSTALLATION MENU PAGE –IAS CONFIG D ............................................................. 140
10.4.6.5 INSTALLATION MENU PAGE –IAS CONFIG E.............................................................. 140
10.4.6.6 INSTALLATION MENU PAGE -IAS CONFIG F ............................................................. 141
10.4.6.7 INSTALLATION MENU PAGE -IAS CONFIG G............................................................. 141
10.4.6.8 INSTALLATION MENU PAGE –NAV SETUP A .............................................................. 142
10.4.6.9 INSTALLATION MENU PAGE –NAV SETUP B .............................................................. 142
10.4.6.10 INSTALLATION MENU PAGE –NAV SETUP C .............................................................. 143
10.4.6.11 INSTALLATION MENU PAGE –RS-232 CONFIG A....................................................... 143

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10.4.6.12 INSTALLATION MENU PAGE –RS-232 CONFIG B ....................................................... 144
10.4.6.13 INSTALLATION MENU PAGE –RS-232 CONFIG C....................................................... 144
10.4.6.14 INSTALLATION MENU PAGE –ACU CONFIG A ........................................................... 144
10.4.6.15 INSTALLATION MENU PAGE –ACU CONFIG B............................................................ 145
10.4.6.16 INSTALLATION MENU PAGE –MISC CONFIG A .......................................................... 145
10.4.6.17 INSTALLATION MENU PAGE –MISC CONFIG B........................................................... 145
10.4.6.18 INSTALLATION MENU PAGE –MISC CONFIG C .......................................................... 146
10.4.6.19 INSTALLATION MENU PAGE –MISC CONFIG D .......................................................... 146
10.4.6.20 INSTALLATION MENU PAGE –RSM CALIBRATION ...................................................... 146
10.4.6.21 INSTALLATION MENU PAGE –ACCEL BIAS CAL ......................................................... 148
10.4.6.22 INSTALLATION MENU PAGE –WX-500 ..................................................................... 148
10.4.6.23 INSTALLATION MENU PAGE –DFC A/P CONFIG PAGE A ............................................. 148
10.4.6.24 INSTALLATION MENU PAGE –DFC A/P CONFIG PAGE B ............................................. 148
10.4.6.25 INSTALLATION MENU PAGE –AOA CONFIG .............................................................. 148
10.4.6.26 INSTALLATION MENU PAGE –NETWORK PAGE.......................................................... 148
10.4.6.27 INSTALLATION MENU PAGE -DIAGNOSTICS ............................................................ 149
10.4.7 CONFIGURATION DEFINITIONS................................................................................. 149
10.4.7.1 IAS CONFIGURATIONS .......................................................................................... 149
10.4.7.2 PANEL TILT PITCH ADJ ..................................................................................... 150
10.4.7.3 PANEL ROLL ADJ.............................................................................................. 152
10.4.7.4 ATTITUDE REF SYMBOL ADJ ............................................................................. 152
10.4.8 NAV SETUP CONFIGURATION ................................................................................. 152
10.4.8.1 GPS/NAV#1 (ID#1) .......................................................................................... 152
10.4.8.2 COMPOSITE PHASE (VOR1, VOR2)..................................................................... 152
10.4.9 ACU CONFIGURATION.......................................................................................... 152
10.4.9.1 ACU HSI TYPE.................................................................................................. 152
10.4.9.2 ACU DATUM ................................................................................................... 153
10.4.9.3 EXITING /SAVING DATA .................................................................................. 153
10.5 RSM CALIBRATION .............................................................................................. 153
10.5.1 CALIBRATION OVERVIEW ....................................................................................... 153
10.5.1.1 SECOND PHASE RSM LOCATION EVALUATION ............................................................. 154
10.5.1.2 CONVENTIONAL GEAR RSM CALIBRATION PROCEDURE .................................................. 156
10.5.2 RSM CALIBRATION PROCEDURE .............................................................................. 158
10.5.3 HEADING OFFSET ADJUSTMENT ............................................................................... 160
10.5.3.1 HEADING OFFSET ADJUSTMENT ............................................................................... 160
10.5.4 HEADING ACCURACY TEST..................................................................................... 161
10.5.5 HEADING INTERFERENCE TEST................................................................................. 161
10.6 GROUND TEST PROCEDURE .................................................................................... 162
10.6.1 INDICATED AIRSPEED DISPLAY................................................................................. 162
10.6.2 ALTITUDE DISPLAY .............................................................................................. 163
10.6.3 SYSTEM LEAK TEST .............................................................................................. 163
10.6.4 AHRS SENSOR TEST ............................................................................................ 163
10.6.5 GPS1 SENSOR TEST (LABELED AS GPS1) ................................................................... 163
10.6.5.1 ALL GPS INTERFACES ........................................................................................... 163
10.6.5.2 ANALOG GPS INTERFACES ..................................................................................... 163

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10.6.6 NAV RECEIVER SENSOR TEST (LABEL AS VLOC1)......................................................... 164
10.6.7 BACKUP NAVIGATION INDICATOR............................................................................. 164
10.6.8 AUTOPILOT SENSOR TEST ...................................................................................... 164
10.6.9 ANCILLARY EQUIPMENT HEADING CHECK ................................................................... 165
10.6.10 ANCILLARY EQUIPMENT AIR DATA CHECK .................................................................. 165
10.6.11 INTERNAL BATTERY TESTS ...................................................................................... 165
10.6.12 TAPES CONFIGURATION CHECK.............................................................................. 165
10.6.13 EMI TEST ......................................................................................................... 166
10.6.14 FLIGHT CONTROL INTERFERENCE CHECK .................................................................... 169
10.6.15 OBS MODE CHECK.............................................................................................. 169
10.6.16 EA100 ADAPTER TESTING .................................................................................... 170
11 POST INSTALLATION FLIGHT CHECK ................................................................ 171
11.1 ATTITUDE DISPLAY FLIGHT CHECKS.......................................................................... 171
11.2 HEADING CARD FLIGHT CHECKS.............................................................................. 171
11.3 ILS FLIGHT CHECKS ............................................................................................. 171
11.4 AUTOPILOT FLIGHT CHECKS (IF INSTALLED) ................................................................ 172
11.5 DOCUMENT OPERATIONAL CHECK ........................................................................... 172
12 OPERATING INSTRUCTIONS ............................................................................. 173
12.1 PILOT CONTROLS ................................................................................................ 173
12.1.1 OVERVIEW ......................................................................................................... 173
12.1.2 POWER CONTROL ................................................................................................ 173
13 ENVIRONMENTAL QUALIFICATION FORMS........................................................ 175
APPENDIX A : TROUBLESHOOTING ...................................................................................... 179
APPENDIX B : INSTALLATION FINAL CHECK SHEET............................................................... 185
APPENDIX C : SAMPLE OF AFMS SECTION 1.2 (INSTALLED EQUIPMENT CONFIGURATION MATRIX)
190
APPENDIX D : COMPONENT MAINTENANCE MANUAL (CMM)................................................. 193
APPENDIX E : EA100 ADAPTER ........................................................................................... 195
E1 GENERAL LIMITATIONS ......................................................................................................... 196
E2 EA100 SPECIFICATIONS......................................................................................................... 197
E3 OUTLINE DRAWING: .............................................................................................................. 198
E4 EA100 SYSTEM ARCHITECTURE ............................................................................................. 198
E5 EA100 INSTALLATION........................................................................................................... 199
E5.1 EQUIPMENT LOCATION DOCUMENTATION .......................................................................... 199
E5.2 WEIGHT AND BALANCE ...................................................................................................... 199
E5.3 MECHANICAL INSTALLATION.............................................................................................. 199
E5.4 ELECTRICAL INSTALLATION................................................................................................ 201
E5.5 FABRICATION OF TR1 OR TR2 TRANSFORMER ISOLATION BOX (CENTURY AUTOPILOTS ONLY)203
E5.6 ELECTRICAL CONNECTION ................................................................................................. 204
E5.7 WIRING DIAGRAMS............................................................................................................. 205
E5.8 CONFIGURATION ............................................................................................................... 220
E5.9 EA100 GROUND TEST PROCEDURE ..................................................................................... 220
E5.9 AUTOPILOT GYRO ALIGNMENT ........................................................................................... 222
E5.10 GROUND EMI TEST........................................................................................................... 222

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List of Tables
Table 1-1: Part Numbers....................................................................................................................17
Table 1-2: Latest Approved Software Version......................................................................................17
Table 1-3: AML-STC Additional Document List ...................................................................................18
Table 1-4: 903-00001-( ) EFD1000 EFD Install Kit..............................................................................18
Table 1-5: 903-00007-001 EFD Recess Mount Kit (optional) ..............................................................18
Table 1-6: 903-00002-( ) RSM Install Kits ..........................................................................................18
Table 1-7: 903-00003-001 ACU Install Kit.........................................................................................19
Table 1-8: 903-00003-002 ACU2 Install Kit.......................................................................................19
Table 1-9: 903-00011-( ) EA100 Install Kits.......................................................................................19
Table 1-10: EFD1000 E5 Accessories Required but Not Supplied .........................................................20
Table 1-11: E5 Optional Accessories Not Supplied ..............................................................................20
Table 1-12: EA100 Optional Accessories Required but Not Supplied....................................................20
Table 1-13: Special Tools...................................................................................................................21
Table 5-1: Pre-Modification Checklist ...............................................................................................42
Table 5-2: GPS Compatibility..............................................................................................................46
Table 5-3: Heading Sources ...............................................................................................................47
Table 5-4: Air Data Sources ...............................................................................................................47
Table 6-1: Component Weights..........................................................................................................50
Table 6-2: Parts Required to Recess Mount each EFD ..........................................................................54
Table 6-3: Static Load Table...............................................................................................................57
Table 6-4: RSM Mounting Hardware ...................................................................................................72
Table 7-1: Current Draw ....................................................................................................................80
Table 8-1: RS-232 ADC Outputs ........................................................................................................86
Table 8-2: EFD A429 GPS Input ..........................................................................................................87
Table 8-3: EFD A429 VLOC Input........................................................................................................87
Table 8-4: EFD1000 E5 A429 GPS Output ...........................................................................................88
Table 8-5: KI525A Emulation Specifications........................................................................................91
Table 8-6: NSD360A Emulation Specifications ....................................................................................92
Table 8-7: PN101 Emulation Specifications.........................................................................................92
Table 8-8: ACU A429 Output .............................................................................................................93
Table 8-9: ACU2 ARINC 429 Output ...................................................................................................94
Table 8-10: EFD Pin Out.....................................................................................................................95
Table 8-11: RSM Pin Out ....................................................................................................................96
Table 8-12: Configuration Module Pin Out..........................................................................................96
Table 8-13: ACU J1 Pin Out................................................................................................................97
Table 8-14: ACU J2 Pin Out................................................................................................................98
Table 8-15: ACU J3 Pin Out................................................................................................................99
Table 9-1: E5 Wiring Diagrams.........................................................................................................103
Table 9-2: Optional ACU/ACU2 Interfaces ........................................................................................103
Table 10-1 MOL Type and Parameter Descriptions............................................................................139
Table 10-2: Vertical Component Evaluation table..............................................................................154
Table 13-1: EFD1000 E5 Environmental Qualification Form ............................................................... 175
Table 13-2: RSM Environmental Qualification Form........................................................................... 176

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Table 13-3: ACU Environmental Qualification Form...........................................................................177
List of Figures
Figure 2-1: EFD1000 E5 Outline Drawing (inches) ...............................................................................24
Figure 2-2: RSM Outline Drawing (inches)...........................................................................................26
Figure 2-3: Configuration Module Outline Drawing (inches) ................................................................27
Figure 2-4: ACU Outline Drawing (inches)...........................................................................................29
Figure 2-5: ACU2 Outline Drawing (inches).........................................................................................30
Figure 3-1: EFD1000 E5 System Architecture ......................................................................................33
Figure 4-1: EFD1000 E5 Authorized IFR Configuration ........................................................................36
Figure 4-2: Flight Director/Backup Nav/Placard placement..................................................................39
Figure 6-1: EFD Mounting Location ....................................................................................................52
Figure 6-2: EFD and Bracket Installation .............................................................................................53
Figure 6-3: Single Display Recess Mount Cutout (inches).....................................................................55
Figure 6-4: Single Display Recess Mount Bracket Installation...............................................................56
Figure 6-5: Ground Strap Attachment Points.......................................................................................57
Figure 6-6: Recess Mounting Bracket Dimensions (inches) ..................................................................58
Figure 6-7: EFD Mounting Bracket (inches) .........................................................................................58
Figure 6-8: EFD Bonding Strap Connection .........................................................................................59
Figure 6-9: Pitot & Static Quick Connector..........................................................................................59
Figure 6-10: Pitot & Static Line Connections .......................................................................................60
Figure 6-11: RSM-External Mounting Locations (Top/Side View) –all aircraft types ..............................63
Figure 6-12: RSM Internal Mounting Locations –Composite/Fabric Aircraft .........................................64
Figure 6-13: RSM-003 External Mounting Locations (Bottom view) ......................................................65
Figure 6-14: RSM Top View longitudinal Alignment.............................................................................68
Figure 6-15: RSM Fore or Aft Max Tilt.................................................................................................69
Figure 6-16: RSM Fore or Aft Max Tilt (Shim installed).........................................................................69
Figure 6-17: RSM Side to Side Max Tilt ...............................................................................................69
Figure 6-18: RSM Side to Side Max Tilt (Shim installed) .......................................................................69
Figure 6-19: RSM Doubler P/N 503-00015-001 .................................................................................70
Figure 6-20: Masking of Doubler........................................................................................................71
Figure 6-21: Doubler Installation .......................................................................................................72
Figure 6-22: RSM Mounting ...............................................................................................................73
Figure 6-23: Example Shim Top View .................................................................................................73
Figure 6-24: Example Shim Side View.................................................................................................73
Figure 6-25: Masking of Shim for Priming ..........................................................................................74
Figure 6-26: ACU/ACU2 Mount to Flat Metal Shelf ..............................................................................75
Figure 6-27: ACU Dimensions (inches) ...............................................................................................76
Figure 6-28: ACU2 Dimensions (inches) .............................................................................................77
Figure 6-29: Configuration Module Dimensions (inches) .....................................................................78
Figure 6-30: Configuration Module Tie Wrapped to Harness................................................................78
Figure 7-1: EFD Back Shell Grounds....................................................................................................81
Figure 7-2: RSM Connector assembly .................................................................................................83
Figure 7-3: EFD Back Shell Grounds/RSM............................................................................................83
Figure 8-1: EFD Connector (as viewed from rear of unit) .....................................................................95

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Figure 8-2: RSM Mating Connector –Install Side ..................................................................................96
Figure 8-3: Configuration Module Connector (Install side)...................................................................96
Figure 8-4: ACU J1 Connector (as viewed from front of unit) ...............................................................97
Figure 8-5: ACU J2 Connector (as viewed from front of unit) ...............................................................98
Figure 8-6: ACU J3 Connector (as viewed from front of unit) ...............................................................99
Figure 8-7: ACU2 J4 Connector (ACU2 only)......................................................................................101
Figure 9-1: EFD1000 E5 Main Connections .......................................................................................104
Figure 9-2: ACU/ACU2 Input Power.................................................................................................. 105
Figure 9-3: Reserved .......................................................................................................................105
Figure 9-4: VFR Only No GPS input configurations ............................................................................ 105
Figure 9-5: ARINC 429 GPS without ACU ..........................................................................................105
Figure 9-6: GNAV without ACU ("Tracker" or no Autopilot) ................................................................106
Figure 9-7: GNAV with ACU (Autopilot).............................................................................................107
Figure 9-8: Reserved .......................................................................................................................107
Figure 9-9: Reserved .......................................................................................................................107
Figure 9-10: ARINC 429 GPS with ACU (Analog Nav and/or Autopilot) ............................................... 108
Figure 9-11: RS-232 GPS with ACU (Analog Nav and/or Autopilot) ....................................................109
Figure 9-12: KLN89B & KLN94 RS-232 and Analog to ACU Interface..................................................110
Figure 9-13: KLN-90/A/B RS-232 and Analog to ACU Interface ........................................................111
Figure 9-14: GX-50/60 & GX-55/65 RS-232 and Analog to ACU Interface ........................................112
Figure 9-15: Analog NAV Interface ...................................................................................................113
Figure 9-15A: Narco and Cessna ARC Navigation Radios ...................................................................114
Figure 9-16: KI525A Emulation (Bendix/King autopilot to ACU).........................................................115
Figure 9-17: S-TEC Autopilot to ACU Interface .................................................................................116
Figure 9-18: Century Autopilot to ACU Interface (minus HDG/CRS Datum).........................................117
Figure 9-18A: NSD360A Emulation (Century 21/31/41/2000/4000) .................................................117
Figure 9-18B: NSD360A Emulation Century 1C388/M, 1C388C/MC Radio Couplers ...........................118
Figure 9-18C: NSD360A Emulation Century 1C388-2/-3 Radio Couplers .......................................... 119
Figure 9-18D: NSD-360A Emulation Century IV (DC version)............................................................. 120
Figure 9-19: Cessna ARC 300B/400B/800B Autopilot to ACU Interface..............................................121
Figure 9-19A: Cessna Navomatic 300/400/800 IFCS to ACU Interface ............................................... 122
Figure 9-19B: NAVOMATIC 400/400A Autopilot to ACU Interface......................................................123
Figure 9-19C: Cessna ARC 300A AC & DC version to ACU Interface ................................................... 124
Figure 9-19D: Cessna 300 Navomatic to ACU Interface ..................................................................... 125
Figure 9-20: Bendix FCS-810 Autopilot to ACU ................................................................................126
Figure 9-21: Reserved .....................................................................................................................127
Figure 9-22: Reserved .....................................................................................................................127
Figure 9-23: Reserved .....................................................................................................................127
Figure 9-24: Back-up NAV Indicator (Internal Converter)................................................................... 127
Figure 9-25: Back-up NAV Indicator (OBS Resolver) .......................................................................... 128
Figure 9-26: Back-up NAV/GPS Indicator (GNS-430/530) ................................................................. 129
Figure 9-27: Non-Aspen Equipment Configuration Notes.................................................................. 130
Figure 9-28A: Digital Heading/ADC Outputs ....................................................................................131
Figure 9-28B: ARINC 407 Synchro Output (ACU2 only) ...................................................................... 132
Figure 10-1: Installation Menu Access ..............................................................................................136

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Figure 10-2: Installation Menu Warning ............................................................................................136
Figure 10-3: Notional Diagnostics Page............................................................................................ 149
Figure 10-4: Illustration of aircraft 2º nose high ...............................................................................151
Figure 10-5: Illustration of Zero degree pitch adjustment .................................................................151
Figure 10-6: GPS/NAV Example........................................................................................................152
Figure 10-7: HSI Type Example ........................................................................................................ 153
Figure 10-8: nT Example .................................................................................................................155
Figure 10-9: EFD1000 Diagnostic Page Magnetometer Row Example ................................................. 155
Figure 10-10: RSM Calibration Graphic............................................................................................. 157
Figure 10-11: RSM Calibration Page .................................................................................................158
Figure 10-12: Calibration in Process.................................................................................................159
Figure 10-13: Aircraft Turning .........................................................................................................159
Figure 10-14: Accept/Reject Results ................................................................................................159
Figure 10-15: Results Accepted .......................................................................................................160
Figure 10-16: Results Rejected.........................................................................................................160
Figure 10-17: Calibration Heading Before Adjustment ......................................................................160
Figure 10-18: Calibrated Heading After Adjustment.......................................................................... 161
Figure E1: EA100 Outline Drawing (inches) and center of gravity .......................................................198
Figure E2: EA100 Block Diagram (Bendix King Autopilots) .................................................................198
Figure E3: EA100 Block Diagram (Century Autopilots)........................................................................198
Figure E4: EA100 Mounting .............................................................................................................. 200
Figure E5: A/P AHRS FAIL Annunciator Location ................................................................................ 202
Figure E6: MS25041-4 Dimmable “Catseye” ......................................................................................203
Figure E8: EA100 Main Wiring Connections(King and Century) ...........................................................206
Figure E9: EA100 to KAP100/KAP150/KFC150 Attitude Source w/DISC .............................................. 207
Figure E10: EA100 to KAP/KFC200 Attitude Source w/DISC ...............................................................208
Figure E11: EA100 to KFC225 Attitude Source w/DISC.......................................................................209
Figure E12: EA100 to KFC250 (with KA141) Attitude Source w/DISC .................................................. 210
Figure E13: EA100 to KFC250 (without KA141) Attitude Source w/Disc ..............................................211
Figure E14: Reserved........................................................................................................................ 211
Figure E15: EA100 to Century IIB Attitude Source w/DISC ..................................................................212
Figure E16: EA100 to Century III Attitude Source w/DISC ...................................................................213
Figure E17: EA100 to Century IV Attitude Source w/DISC................................................................... 214
Figure E18: EA100 to Century 21 Attitude Source w/DISC..................................................................215
Figure E19: EA100 to Century 31 Attitude Source w/DISC..................................................................216
Figure E20: EA100 to Century 41 Attitude Source w/DISC..................................................................217
Figure E21: EA100 to Century 2000 Attitude Source w/DISC..............................................................218
Figure E22: EA100 to Century 4000 Attitude Source w/DISC..............................................................219

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List of Definitions, Acronyms, Abbreviations
ACU ................................................Analog Converter Unit
ADAHRS ..........................................Air Data Attitude Heading Reference System
ADC ................................................Air Data Computer
ADI .................................................Attitude Director Indicator
AI....................................................Attitude Indicator
AHRS ..............................................Attitude and Heading Reference System
AML ................................................Approved Model List
AMMD.............................................Aerodrome Moving Map Display (geo-referenced airport diagram)
AOA................................................Angle of Attack
A/P .................................................Autopilot
A429...............................................ARINC 429 interface
CM..................................................Configuration Module
DG ..................................................Directional Gyro
DH ..................................................Decision Height
EFD .................................................Electronic Flight Display
EFD1000 E5 ....................................EFD1000 E5 system
EFI ..................................................Electronic Flight Instrument
EHA ................................................Evolution Hazard Awareness
ESV .................................................Evolution Synthetic Vision
FAR.................................................Federal Aviation Regulations
FD...................................................Flight Director
FPM.................................................Flight Path Marker
GNAV..............................................Combined GPS and VOR radio (all A429 interface)
GPS .................................................Global Positioning System
GPSS ...............................................GPS Steering
GS...................................................Glide-slope or Groundspeed
HSI..................................................Horizontal Situational Indicator
ICA .................................................Instructions for Continued Airworthiness
IFR ..................................................Instrument Flight Rules
IOP .................................................Input/Output Processor (Aspen software)
LOC ................................................ILS Localizer
LRU.................................................Line Replaceable Unit
MAP ................................................Main Application Processor (Aspen software)
MOL................................................Maximum Operating Limit
MPS ................................................Minimum Performance Standard
OAT ................................................Outside Air Temperature
OBS.................................................Omni-Bearing Selector
PARAM............................................Parameter
RSM ................................................Remote Sensor Module
SEL..................................................Select
STC.................................................Supplemental Type Certificate
TAS.................................................True Airspeed
VFR .................................................Visual Flight Rules
VLOC ..............................................The VOR side of a GNAV radio
WAAS ..............................................Wide Area Augmentation System

EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
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1Introduction
This Installation Manual contains FAA Approved Data, but only when used to install the Aspen
Avionics EFD1000 E5 Dual Electronic Flight Instrument (EFI) system in accordance with AML-STC
SA10822SC. This document contains detailed instructions for installing the EFD1000 E5 System into
specific aircraft as listed in the AML-STC. There are regulations that must be complied with to
ensure an airworthy installation. Section 4 -STC Specific Requirements and Limitations and Section 5
-Pre-Modification Planning will guide you through these requirements.
1.1 Part Numbers
List of the major hardware components (by part number) that make up the EFD1000 E5
system.
Part Number
Description
910-00101-001
EFD1000 E5, Evolution Flight Display, PMA
910-00005-004
Configuration Module, Assy, TSO
910-00003-002
RSM Rev E or later, Remote Sensor Module, Top Mount, TSO
910-00003-003
RSM Rev E or later, Remote Sensor Module, Bottom Mount, TSO
903-00001-( )
EFD1000 EFD Install Kit, TSO
903-00002-( )
RSM Install Kit, TSO
Table 1-1: Part Numbers
Part Number
Description
910-00004-001
ACU, Analog Converter Unit, TSO
903-00003-001
ACU Install Kit, TSO
910-00004-101
ACU2 Analog Converter Unit–HDG Synchro, TSO
903-00003-002
ACU2 Install Kit, TSO
910-00013-001
EA100 Adapter, TSO
903-00011-( )
EA100 Installation Kit, TSO
Table 1-1A: EFD1000 E5 Optional LRUs
1.1.1 Latest Approved Software Versions
Description
Hardware Component
Software P/N and Revision
EFD1000 E5 Display
MAP (Main Application Processor)
IOP (Input/Output Processor)
910-00101-001
302-00032-001 MAP Version E5 2.10
302-00033-001 IOP Version E5 2.2
Analog Control Unit (ACU)
910-00004-001
Version 1.1
Analog Control Unit2 (ACU2)
910-00004-10x
Version 2.0
EA100
910-00013-001
Version 1.2
Table 1-2: Latest Approved Software Version

EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
DOCUMENT # 900-00041-001 PAGE 18-226 REVISION D
© Copyright 2019 Aspen Avionics Inc.
1.1.2 AML-STC Document List
The following list of documents contain engineering aspects that are a part of AML-STC
SA10822SC data.
Document
P/N
Description
ICA
900-00012-001
Instructions for Continued Airworthiness
AFMS
900-00038-001
Airplane Flight Manual Supplement
Table 1-3: AML-STC Additional Document List
1.2 Installation Kit Contents
Installation Kit, EFD1000 - Basic P/N 903-00001-004
Part Number
Description
Quantity
403-00002-001
Panel Mounting Bracket Assembly
1
116-00022-002
44 Pin HD D-Sub Connector with Contacts
1
116-00026-006
EMI Metal Backshell
1
275-00001-002
Pitot Quick Connector
1
275-00001-001
Static Quick Connector
1
273-00003-001
Tee Fittings for Pitot/Static, 0.25” x 0.17” x 0.25”
2
271-00001-001
Miniature Hose Clamps
8
412-00004-001
Configuration Module Cable Assembly
1
Table 1-4: 903-00001-( ) EFD1000 EFD Install Kit
Optional EFD Recess Mount Kit P/N 903-00007-001
Part Number
Description
Quantity
903-00007-001
EFD Recess Mount Installation Kit (1 required per EFD)
1
Table 1-5: 903-00007-001 EFD Recess Mount Kit (optional)
Installation Kit, RSM P/N 903-00002-( )
Part Number
Description
Quantity by Kit Variant
-001
-002
-003
-004
412-00005-001
RSM 35ft cable assembly w/connector
1
1
-
-
412-00006-001
RSM 50ft cable assembly w/connector
-
-
1
1
201-00004-001
Screw, Machined, Pan, Phillips, Brass,
8-32 11/4”, MS35214-47
4
4
4
4
212-00001-001
Nut, Hex, Locking, Nylon Insert, Brass,
8-32, MS21044B08
4
4
4
4
231-00001-001
Washer, Flat, #8, Brass, 11/64” ID,
3/8” OD, NAS1149B0832H
4
4
4
4
256-00001-001
O-Ring, AS568A-120
1
1
1
1
403-00004-001
RSM Doubler Installation Assy
-
1
-
1
Table 1-6: 903-00002-( ) RSM Install Kits

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1.3 Optional LRU Install Kits
Installation Kit, ACU P/N 903-00003-001
Part Number
Description
Quantity
116-00014-001
15 pin D-Sub connector
1
116-00014-002
25 pin D-Sub connector
1
116-00014-003
37 pin D-Sub connector
1
116-00026-002
DB15 EMI Back shell
1
116-00026-003
DB25 EMI Back shell
1
116-00026-005
DB37 EMI Back shell
1
116-00015-001
Crimp Sockets
77
Table 1-7: 903-00003-001 ACU Install Kit
Installation Kit, ACU2 P/N 903-00003-002
Part Number
Description
Quantity
116-00014-001
15 pin D-Sub connector
1
116-00014-002
25 pin D-Sub connector
1
116-00014-003
37 pin D-Sub connector
1
116-00052-001
62 pin high density D-Sub connector, contacts, back shell
1
116-00026-002
DB15 EMI Back shell
1
116-00026-003
DB25 EMI Back shell
1
116-00026-005
DB37 EMI Back shell
1
116-00015-001
Crimp Sockets
77
Table 1-8: 903-00003-002 ACU2 Install Kit
Installation Kit, EA100 P/N 903-00011-( )
Part Number
Description
Quantity by Kit Variant
-001
-002
-003
-004
116-00022-002
44 Pin HD D-Sub connector with contacts
1
1
1
1
116-00026-001
DB 25 EMI Metal Back shell
1
1
1
1
116-00014-001
15 pin D-sub connector
1
1
1
1
116-00026-007
DB15 EMI Back shell
1
1
1
1
116-00015-001
Crimp Sockets
15
15
15
15
122-00031-001
Diode Junction Splice, 200v
2
2
2
2
403-00009-001
Century II/III/IV supplemental parts
bag:
2ea. 126-00004-006 Cap 0.12uF. 400V
2ea. 132-00007-002 Resistor 1.21KΩ, 1/4W, 1%
2ea. 132-00007-004 Resistor 2.2KΩ, 1/4W, 1%
1
1
1
1
412-00013-001
EA100 10ft Ethernet Cable
-
1
-
-
412-00013-002
EA100 20ft Ethernet Cable
-
-
1
-
412-00013-003
EA100 30ft Ethernet Cable
-
-
-
1
Table 1-9: 903-00011-( ) EA100 Install Kits

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1.4 Accessories Required but Not Supplied –EFD1000 E5
Description
Manufacturer’s P/N or Specification
Circuit Breaker pull to open (EFD) 7.5 amp
MS 26574-7.5
Circuit Breaker (ACU) 2 amp
MS26574-2
EFD to GPS/ACU double shielded cable
M27500-22TG2V64
Unshielded wire 24, 22, 20 AWG
MIL-W-22759/16
Shielded Wire 22/20 AWG
MIL-C-27500
3/16” pitot/static tube (EFD to T fitting
MIL-DTL-5593
EFD Mounting Screws #6-32, 6 ea.
MS24693-S30
EFD Mounting Lock Nuts #6-32
MS21044N06
EFD Mounting Washers
NAS1149FN632P
ACU Mounting Screw #8-32
MS35206-XXX
ACU Mounting Lock Nuts #8-32
MS21044N08
ACU Mounting Washers
NAS1149FN832P
Table 1-10: EFD1000 E5 Accessories Required but Not Supplied
1.5 Optional Accessories Not Supplied –EFD1000 E5
Description
Manufacturer P/N or Specification
E5 Master switch –rated for 7.5 amps cont.
MS35058-22 SPST switch
Circuit Breaker/Switch 7.5amp
(optional –in lieu of separate C/B and switch)
MS24509-A- 7½
*Tinned Copper Over Braid
*used in lieu of double shielded wire
MIL-SPEC# AA59569R36T0250 ¼”
MIL-SPEC# AA59569R36T0500 ½”
RSM Doubler
Installer fabricated per Section 6.9.5
RSM Shim
(may be required on extreme mounting angles)
Installer fabricated per Section 6.9.9
RSM sealant non-pressure vessel mounting
MIL-A-46146, Dow 738
7 conductor shielded cable
For installer fabricated harness using
116-00020-001 connector.
M27500-A24SD7T23/
M27500-22TG7T14
Table 1-11: E5 Optional Accessories Not Supplied
1.6 Optional Accessories Required but Not Supplied –EA100
Description
Manufacturer P/N or Specification
A/P AHRS FAIL press-to-test indicator
“dimmable cat’s-eye”
Electroswitch Electronic Products
MS25041-4 (dimmable)
(also available from Aircraft Spruce)
EA100 Ethernet Cable
(Cat 5e Ethernet cable (MX100P-24)
Order Aspen Avionics EA100
Installation kits 903-00011-002,
-003, or -004 which include the cable.
EA100 Mounting Lock Nuts #8-32 (6)
MS21044N08
EA100 Mounting Washers (6)
NAS1149FN832P
EA100 Mounting Screw #8-32 (6)
MS35206-XXX
Circuit Breaker 2A
MS26574-2
Table 1-12: EA100 Optional Accessories Required but Not Supplied