Aspen Avionics EFD1000 E5 - Page 6

EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
DOCUMENT # 900-00041-001 PAGE 6-226 REVISION D
© Copyright 2019 Aspen Avionics Inc.
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
3 SYSTEM 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
4 STC 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
5 PRE-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