Name: Aspen Avionics EFD1000 E5
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EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual

DOCUMENT # 900-00041-001 PAGE 1-226 REVISION D

EFD1000 E5

Dual Electronic Flight Instrument (EFI)

Installation Manual

April 2019

Table of Contents5
List of Tables12
List of Figures13
List of Definitions, Acronyms, Abbreviations16
Introduction17
- Part Numbers17
- Latest Approved Software Versions17
- Table 1-1: Part Numbers17
- Table 1-2: Latest Approved Software Version17
- Aml-Stc Document List18
- Installation Kit Contents18
- Table 1-3: AML-STC Additional Document List18
- Table 1-4: 903-00001-( ) EFD1000 EFD Install Kit18
- Table 1-5: 903-00007-001 EFD Recess Mount Kit (Optional)18
- Table 1-6: 903-00002-( ) RSM Install Kits18
- 1.3 Optional LRU Install Kits19
- Table 1-7: 903-00003-001 ACU Install Kit19
- Table 1-8: 903-00003-002 ACU2 Install Kit19
- Table 1-9: 903-00011-( ) EA100 Install Kits19
- Accessories Required but Not Supplied - Efd1000 E520
- Optional Accessories Not Supplied - Efd1000 E520
- Optional Accessories Required but Not Supplied - Ea10020
- Table 1-10: EFD1000 E5 Accessories Required but Not Supplied20
- Table 1-11: E5 Optional Accessories Not Supplied20
- Table 1-12: EA100 Optional Accessories Required but Not Supplied20
- Special Tools Required21
- Vendor Information21
- Warranty Registration21
- Regulatory Compliance21
- Technical Standard Order21
- Pma Approval21
- Table 1-13: Special Tools21
- Software Certification22
- Environmental Compliance22
- Installation Approval22
- Field Replaceable Parts22
- Reserved22
Equipment Specifications and Limitations23
- Efd1000 E523
- General Specifications23
- Operational Specifications23
- I/O Specifications23
- Certification Specifications23
- Efd1000 E5 Outline Drawing24
- Design Eye Viewing Envelope24
- Figure 2-1: EFD1000 E5 Outline Drawing (Inches)24
- Remote Sensor Module (Rsm)25
- General Specifications25
- Operational Specifications25
- I/O Specifications25
- Certification Specifications25
- Outline Drawing26
- Configuration Module (CM)26
- General Specifications26
- Figure 2-2: RSM Outline Drawing (Inches)26
- Operational Specifications27
- I/O Specifications27
- Certification Specifications27
- Outline Drawing27
- Figure 2-3: Configuration Module Outline Drawing (Inches)27
- Analog Converter Unit (Acu)28
- General Specifications28
- Operational Specifications28
- I/O Specifications28
- Certification Specifications28
- Outline Drawing29
- Analog Converter Unit 229
- General Specifications29
- Operational Specifications29
- I/O Specifications29
- Figure 2-4: ACU Outline Drawing (Inches)29
- Certification Specifications30
- Outline Drawing30
- Figure 2-5: ACU2 Outline Drawing (Inches)30
System Description31
- Efd1000 E5 Dual Electronic Flight Instrument (Efi) System31
- Efd1000 E5 Flight Display (Efd)31
- Remote Sensor Module (Rsm)32
- Configuration Module (CM)32
- Analog Converter Unit (Acu)32
- Analog Converter Unit 2 (Acu2)32
- System Architecture33
- Figure 3-1: EFD1000 E5 System Architecture33
Stc Specific Requirements and Limitations35
- Efd1000 E5 System Limitations35
- EA100 Installation Limitations (EA100 Is Optional)35
- Authorized Configurations35
- Figure 4-1: EFD1000 E5 Authorized IFR Configuration36
- General Standby Instrument Requirements for Ifr-Capable Airplanes38
- Pneumatic Attitude (Existing)38
- Electric Attitude (Existing)38
- Existing Attitude Positioning (if Keeping)38
- Figure 4-2: Flight Director/Backup Nav/Placard Placement39
- Airspeed and Altimeter40
- Back up Nav Indicator40
- Placards40
- 4.5 Special Consideration for Airplanes Limited to VFR41
Pre-Modification Planning42
- Pre-Modification Checklist42
- Table 5-1: Pre-Modification Checklist42
- Directional Gyro/ HSI43
- Aircraft Power Requirements43
- Equipment Power Requirements43
- Reserved43
- Cessna 190/195 Special Consideration44
- Reserved44
- Conventional Landing Gear "Tail Dragger" Aircraft44
- Optional Interfaces45
- Autopilot45
- 5.4.1.1 EA100 Adapter45
- Gps Navigator Compatibility46
- Gpss46
- Gps/ Nav Switching46
- Table 5-2: GPS Compatibility46
- Heading Output47
- Air Data Outputs47
- 5.4.6.1 EFD1000 E5 as Encoding Altitude Source47
- Table 5-3: Heading Sources47
- Table 5-4: Air Data Sources47
- Flush or Recess Mounting the Efd48
Mechanical Installation50
- Unpacking and Inspecting Equipment50
- Equipment Location Documentation50
- Log Book Entry50
- Weight and Balance50
- Mounting Limitations50
- Table 6-1: Component Weights50
- Efd1000 E5 Mounting Limitations (Efd)51
- Rsm Mounting Limitations51
- Equipment Bonding51
- Cooling52
- Efd Installation52
- Efd Mounting Location52
- Surface Mounting the Efd as Per Figure 6-252
- Figure 6-1: EFD Mounting Location52
- Figure 6-2: EFD and Bracket Installation53
- Recess Mounting the Efd as Per Figure 6-454
- 6.8.3.1 Recess Mount Modification Procedure54
- Table 6-2: Parts Required to Recess Mount each EFD54
- Figure 6-3: Single Display Recess Mount Cutout (Inches)55
- Figure 6-4: Single Display Recess Mount Bracket Installation56
- Table 6-3: Static Load Table57
- Figure 6-5: Ground Strap Attachment Points57
- Figure 6-6: Recess Mounting Bracket Dimensions (Inches)58
- Figure 6-7: EFD Mounting Bracket (Inches)58
- Efd Bonding Strap59
- Pitot and Static Connections59
- Figure 6-8: EFD Bonding Strap Connection59
- Figure 6-9: Pitot & Static Quick Connector59
- Quick Connector Installation60
- Leak Check Requirements60
- Figure 6-10: Pitot & Static Line Connections60
- Rsm Installation61
- Rsm Internal Mounting61
- Rsm Inverted or Bottom Mounting61
- Rsm External Top Mounting61
- Figure 6-11: RSM-External Mounting Locations (Top/Side View) - All Aircraft Types63
- Figure 6-12: RSM Internal Mounting Locations - Composite/Fabric Aircraft64
- Proposed Rsm Location Check65
- Figure 6-13: RSM-003 External Mounting Locations (Bottom View)65
- Pressurized Aircraft67
- RSM Mounting on Non-Metal or Damage-Tolerant Design Aircraft68
- Rsm Mounting Angles68
- 6.9.7.1 Longitudinal Axis68
- 6.9.7.2 Pitch Axis68
- Figure 6-14: RSM Top View Longitudinal Alignment68
- 6.9.7.3 Roll Axis69
- Figure 6-15: RSM Fore or Aft Max Tilt69
- Figure 6-16: RSM Fore or Aft Max Tilt (Shim Installed)69
- Figure 6-17: RSM Side to Side Max Tilt69
- Figure 6-18: RSM Side to Side Max Tilt (Shim Installed)69
- Rsm External Mount - Aluminum Skin70
- 6.9.8.1 RSM Doubler Fabrication70
- Figure 6-19: RSM Doubler P/N 503-00015-00170
- Figure 6-20: Masking of Doubler71
- Rsm Internal Mount72
- Rsm Installation72
- Table 6-4: RSM Mounting Hardware72
- Figure 6-21: Doubler Installation72
- RSM Shim Fabrication (if Necessary)73
- Figure 6-22: RSM Mounting73
- Figure 6-23: Example Shim Top View73
- Figure 6-24: Example Shim Side View73
- Acu/Acu2 Installation74
- Figure 6-25: Masking of Shim for Priming74
- Acu/Acu2 Mounting75
- Figure 6-26: ACU/ACU2 Mount to Flat Metal Shelf75
- Figure 6-27: ACU Dimensions (Inches)76
- Figure 6-28: ACU2 Dimensions (Inches)77
- Configuration Module Installation78
- Figure 6-29: Configuration Module Dimensions (Inches)78
- Figure 6-30: Configuration Module Tie Wrapped to Harness78
Electrical Installation80
- Electrical Load Analysis80
- Efd1000 E580
- ACU or ACU2 (Optional)80
- Miscellaneous Wiring80
- Table 7-1: Current Draw80
- Hirf/Lightning Requirements81
- Efd to Gps/Vloc/Acu Wiring81
- Figure 7-1: EFD Back Shell Grounds81
- Rsm Wiring82
- 7.2.6.1 Assembly Using Aspen Prefabricated 35Ft and Optional 50Ft Cables82
- 7.2.6.2 Assembly Using M27500-A24SD7T23 Cable82
- Efd End83
- Configuration Module Wiring83
- Figure 7-2: RSM Connector Assembly83
- Figure 7-3: EFD Back Shell Grounds/Rsm83
- Acu Wiring84
- Back U Pnav Indicator Wiring84
- Autopilot Wiring84
- Backup Instrument Wiring and Cable Bundle84
Electrical Connections86
- Efd Electrical Specifications86
- Power Input86
- RS-232 GPS Input86
- Adc Output86
- Arinc 429 Gps Inputs86
- Table 8-1: RS-232 ADC Outputs86
- Arinc 429 Vloc Input87
- Arinc 429 Output87
- Table 8-2: EFD A429 GPS Input87
- Table 8-3: EFD A429 VLOC Input87
- ACU Electrical Specifications (910-00004 All Dash Numbers)88
- Power Input88
- Reserved88
- Vloc Receiver88
- 8.2.3.1 NAV Composite Input88
- 8.2.3.2 ILS Energize Discrete Input88
- 8.2.3.3 Glide Slope Deviation Input88
- Table 8-4: EFD1000 E5 A429 GPS Output88
- 8.2.3.4 Glide Slope Flag Input89
- Gps Receiver89
- 8.2.4.1 OBS Sine, Cosine, Rotor89
- 8.2.4.2 TO/ from FLAG Input89
- 8.2.4.3 LEFT/ RIGHT Input89
- 8.2.4.4 Lateral Flag Input89
- 8.2.4.5 Vertical Deviation Input89
- 8.2.4.6 Vertical Deviation Flag Input89
- 8.2.4.7 OBS/ LEG (HOLD) Input89
- 8.2.4.8 APPR Active Input90
- 8.2.4.9 FCS-LOC Engage Input90
- Autopilot90
- 8.2.5.1 Lateral Deviation Output90
- 8.2.5.2 Lateral Flag Output90
- 8.2.5.3 Vertical Deviation Output90
- 8.2.5.4 Vertical Flag Output90
- 8.2.5.5 ILS Energize Output90
- 8.2.5.6 Volt Reference Output91
- 8.2.5.7 KI-525A Heading and Course Datum Output91
- 8.2.5.8 NSD-360 Heading and Course Datum Output91
- Table 8-5: KI525A Emulation Specifications91
- 8.2.5.9 PN-101 Heading and Course Datum Output92
- Heading Valid Output92
- Table 8-6: NSD360A Emulation Specifications92
- Table 8-7: PN101 Emulation Specifications92
- Gps Selected Output93
- Arinc 429 Output93
- Acu2 Electrical Specifications (910-00004-10 X Only )93
- Heading Synchro out93
- Table 8-8: ACU A429 Output93
- +/- 15Vdc Power Output94
- Glideslope Flag (Narco)94
- Arinc 429 Output94
- Efd Pin out94
- Table 8-9: ACU2 ARINC 429 Output94
- Table 8-10: EFD Pin out95
- Figure 8-1: EFD Connector (as Viewed from Rear of Unit)95
- Rsm Pin out96
- Configuration Module Pin out96
- Table 8-11: RSM Pin out96
- Table 8-12: Configuration Module Pin out96
- Figure 8-2: RSM Mating Connector -Install Side96
- Figure 8-3: Configuration Module Connector (Install Side)96
- Acu/Acu2 Pin out97
- Table 8-13: ACU J1 Pin out97
- Figure 8-4: ACU J1 Connector (as Viewed from Front of Unit)97
- Table 8-14: ACU J2 Pin out98
- Figure 8-5: ACU J2 Connector (as Viewed from Front of Unit)98
- Table 8-15: ACU J3 Pin out99
- Figure 8-6: ACU J3 Connector (as Viewed from Front of Unit)99
- Figure 8-7: ACU2 J4 Connector (ACU2 Only)101
Installation Wiring Diagrams102
- List of Wiring Diagrams - Efd1000 E5102
- Optional Interfaces - Acu and Acu2103
- Table 9-1: E5 Wiring Diagrams103
- Table 9-2: Optional ACU/ACU2 Interfaces103
- Figure 9-1: EFD1000 E5 Main Connections104
- Figure 9-2: ACU/ACU2 Input Power105
- Figure 9-3: Reserved105
- Figure 9-4: VFR Only no GPS Input Configurations105
- Figure 9-5: ARINC 429 GPS Without ACU105
- Figure 9-22: Reserved105
- Figure 9-6: GNAV Without ACU ("Tracker" or no Autopilot)106
- Figure 9-7: GNAV with ACU (Autopilot)107
- Figure 9-8: Reserved107
- Figure 9-9: Reserved107
- Figure 9-23: Reserved107
- 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 Interface110
- Figure 9-13: KLN-90/A/B RS-232 and Analog to ACU Interface111
- Figure 9-14: GX-50/60 & GX-55/65 RS-232 and Analog to ACU Interface112
- Figure 9-15: Analog NAV Interface113
- Figure 9-15A: Narco and Cessna ARC Navigation Radios114
- Figure 9-16: KI525A Emulation (Bendix/King Autopilot to ACU)115
- Figure 9-17: S-TEC Autopilot to ACU Interface116
- 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 Couplers118
- Figure 9-18C: NSD360A Emulation Century 1C388-2/-3 Radio Couplers119
- Figure 9-18D: NSD-360A Emulation Century IV (DC Version)120
- Figure 9-19: Cessna ARC 300B/400B/800B Autopilot to ACU Interface121
- Figure 9-19A: Cessna Navomatic 300/400/800 IFCS to ACU Interface122
- Figure 9-19B: NAVOMATIC 400/400A Autopilot to ACU Interface123
- Figure 9-19C: Cessna ARC 300A AC & DC Version to ACU Interface124
- Figure 9-19D: Cessna 300 Navomatic to ACU Interface125
- Figure 9-20: Bendix FCS-810 Autopilot to ACU126
- Figure 9-21: Reserved127
- 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 Notes130
- Figure 9-28A: Digital Heading/Adc Outputs131
- Figure 9-28B: ARINC 407 Synchro Output (ACU2 Only)132
10 Configuration and Equipment Checkout134
- Wiring Checks134
- Bonding Check - 14Cfr134
- Onding Heck - 14Cfr 23.867( )134
- Initial System Turn on134
- System Configuration135
- Main Menu Access135
- Menu Navigation135
- Edit Mode135
- Main Menu Configuration135
- Installation Menu - Unit Configuration135
- Figure 10-1: Installation Menu Access136
- Figure 10-2: Installation Menu Warning136
- Efd1000 E5 Installation Menu Configuration138
Installation Menu Configuration - Efd1000 E5138
- Installation Menu Page - Ias Config a138
- Table 10-1 MOL Type and Parameter Descriptions139
- Installation Menu Page - Ias Config B140
- Installation Menu Page - Ias Config C140
- Installation Menu Page - Ias Config D140
- Installation Menu Page - Ias Config E140
- Installation Menu Page - Ias Config F141
- Installation Menu Page - Ias Config G141
- Installation Menu Page - Nav Setup a142
- Installation Menu Page - Nav Setup B142
- Installation Menu Page - Nav Setup C143
- Installation Menu Page - Rs-232 Config a143
- Installation Menu Page - Rs-232 Config B144
- Installation Menu Page - Rs-232 Config C144
- Installation Menu Page - Acu Config a144
- Installation Menu Page - Acu Config B145
- Installation Menu Page - Misc Config a145
- Installation Menu Page - Misc Config B145
- Installation Menu Page - Misc Config C146
- Installation Menu Page - Misc Config D146
- Installation Menu Page - Rsm Calibration146
- Installation Menu Page - Accel Bias Cal148
- Installation Menu Page - Wx-500148
- Installation Menu Page - Dfc A/P Config148
- Installation Menu Page - Aoa Config148
- Installation Menu Page - Network Page148
- Installation Menu Page - Diagnostics149
- Configuration Definitions149
- Ias Configurations149
- Figure 10-3: Notional Diagnostics Page149
- Panel Tilt Pitch Adj150
- Figure 10-4: Illustration of Aircraft 2º Nose High151
- Figure 10-5: Illustration of Zero Degree Pitch Adjustment151
- Panel Roll Adj152
- Attitude Ref Symbol Adj152
- Nav Setup Configuration152
- Gps/Nav#1 (ID#1)152
- Composite Phase (Vor1, Vor2)152
- Acu Configuration152
- Acu Hsi Type152
- Figure 10-6: GPS/NAV Example152
- Acu Datum153
- Exiting / Saving Data153
- Rsm Calibration153
- Calibration Overview153
- Figure 10-7: HSI Type Example153
- Second Phase Rsm Location Evaluation154
- Table 10-2: Vertical Component Evaluation Table154
- Figure 10-8: Nt Example155
- Figure 10-9: EFD1000 Diagnostic Page Magnetometer Row Example155
- Conventional Gear Rsm Calibration Procedure156
- Figure 10-10: RSM Calibration Graphic157
- Rsm Calibration Procedure158
- Figure 10-11: RSM Calibration Page158
- Figure 10-12: Calibration in Process159
- Figure 10-13: Aircraft Turning159
- Figure 10-14: Accept/Reject Results159
- Heading Offset Adjustment160
- Figure 10-15: Results Accepted160
- Figure 10-16: Results Rejected160
- Figure 10-17: Calibration Heading before Adjustment160
- Heading Accuracy Test161
- Heading Interference Test161
- Figure 10-18: Calibrated Heading after Adjustment161
- Ground Test Procedure162
- Indicated Airspeed Display162
- Altitude Display163
- System Leak Test163
- Ahrs Sensor Test163
- GPS1 Sensor Test (Labeled as GPS1)163
- All Gps Interfaces163
- Analog Gps Interfaces163
- NAV Receiver Sensor Test (Label as VLOC1)164
- Backup Navigation Indicator164
- Autopilot Sensor Test164
- Ancillary Equipment Heading Check165
- Ancillary Equipment Air Data Check165
- Internal Battery Tests165
- Tapes Configuration Check165
- Emi Test166
- Flight Control Interference Check169
- Obs Mode Check169
- Ea100 Adapter Testing170
11 Post Installation Flight Check171
- Attitude Display Flight Checks171
- Heading Card Flight Checks171
- Ils Flight Checks171
- Autopilot Flight Checks (if Installed)172
- Document Operational Check172
12 Operating Instructions173
- Pilot Controls173
- Overview173
- Power Control173
Environmental Qualification Forms175
Table 13-1: EFD1000 E5 Environmental Qualification Form175
Table 13-2: RSM Environmental Qualification Form176
Table 13-3: ACU Environmental Qualification Form177
Appendix A : Troubleshooting179
Appendix B : Installation Final Check Sheet185
- Appendix D : Component Maintenance Manual (CMM)193
- Appendix C : Sample of Afms Section 1.2 (Installed Equipment Configuration Matrix)195
Appendix E : Ea100 Adapter195
E1 General Limitations196
E2 Ea100 Specifications197
Figure E1: EA100 Outline Drawing (Inches) and Center of Gravity198
Figure E2: EA100 Block Diagram (Bendix King Autopilots)198
Figure E3: EA100 Block Diagram (Century Autopilots)198
E3 Outline Drawing198
E4 Ea100 System Architecture198
E5 Ea100 Installation199
E5.1 Equipment Location Documentation199
E5.2 Weight and Balance199
E5.3 Mechanical Installation199
Figure E4: EA100 Mounting200
E5.4 Electrical Installation201
Figure E5: A/P AHRS FAIL Annunciator Location202
Figure E6: MS25041-4 Dimmable "Catseye203
E5.5 Fabrication of Tr1 or Tr2 Transformer Isolation Box (Century Autopilots Only)203203
E5.6 Electrical Connection204
E5.7 Wiring Diagrams205
Figure E8: EA100 Main Wiring Connections(King and Century)206
Figure E9: EA100 to KAP100/KAP150/KFC150 Attitude Source W/Disc207
Figure E10: EA100 to KAP/KFC200 Attitude Source W/Disc208
Figure E11: EA100 to KFC225 Attitude Source W/Disc209
Figure E12: EA100 to KFC250 (with KA141) Attitude Source W/Disc210
Figure E13: EA100 to KFC250 (Without KA141) Attitude Source W/Disc211
Figure E14: Reserved211
Figure E15: EA100 to Century IIB Attitude Source W/Disc212
Figure E16: EA100 to Century III Attitude Source W/Disc213
Figure E17: EA100 to Century IV Attitude Source W/Disc214
Figure E18: EA100 to Century 21 Attitude Source W/Disc215
Figure E19: EA100 to Century 31 Attitude Source W/Disc216
Figure E20: EA100 to Century 41 Attitude Source W/Disc217
Figure E21: EA100 to Century 2000 Attitude Source W/Disc218
Figure E22: EA100 to Century 4000 Attitude Source W/Disc219
E5.8 Configuration220
E5.9 Ea100 Ground Test Procedure220
E5.9 Autopilot Gyro Alignment222
E5.10 Ground Emi Test222

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Aspen Avionics EFD1000 E5 Specifications

General

Display Type	Active Matrix LCD
Resolution	1024 x 768 pixels
Weight	3.3 lbs (1.5 kg)
Operating Temperature	-15°C to +55°C
Display Size	6.25 in. diagonal
Interfaces	RS-232, ARINC 429

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