Section 917
ASPEN EFD1000/500 System
Page Date: 19. February 2014
917 - 3
Pilot´s Operating Handbook US
EXTRA 330LX
917.1
GENERAL
This Airplane Flight Manual Supplement (AFMS) applies to avionics installations of the following
display combinations:
1. EFD1000 PFD Pilot
2. EFD1000 PFD Pilot and EFD500 MFD
3. EFD1000 PFD Pro
4. EFD1000 PFD Pro and EFD500 MFD
5. EFD1000 PFD Pro and EFD1000 MFD
The Evolution Flight Display System is a multi-display, highly capable Electronic Flight Instrument
System (EFIS) with integral Micro Electromechanical Systems (MEMS)-based Air Data Attitude
and Heading Reference System (ADAHRS) with an internal backup battery. The EFD 1000 PFD
„Pilot“ offers a state-of-the-art Flight Display with attitude indication and slaved Directional Gyro with
mapping. The EFD 1000 PFD „Pro“ offers a HSI/two pointer RMI instead of the Directional Gyro.
When combined with the optional EFD 500 MFD the system offers a multi-panel, Multi-Function-
Display solution that displays high resolution moving maps with Jeppesen© enroute and terminal
data as well as relative terrain depictions. When combined with the optional EFD 1000 MFD an
independent redundant ADAHRS source provides secondary attitude information and a secondary
HSI display at the push of a button. The EFD1000 MFD can instantly revert to a fully-functional flight
display generated from ADAHRS data completely independent of that generated by the PFD.
The EFD1000 Pilot PFD is a Flight Display with Attitude indicator, heading indicator and moving
map. The Pilot PFD cannot be installed with an EFD1000MFD.
The EFD500 is a fully functional MFD with all the capability of the EFD1000 MFD except reversion,
HSI, Remote Sensor Module (RSM), Cross Link information(receive only) and the air data, attitude
and heading features.
The standard internal battery in the EFD1000 or EFD500 is capable of providing 30 or more minutes
of operation at typical cockpit temperatures if aircraft power to the system fails. An Emergency
Backup Battery is not installed.
In the EXTRA 300LT the EFD1000/500 system is used as a secondary (back-up) instrument
system.
CAUTION
Due to the capabilities of the aircraft - especially the extreme agility with high angular
rates - the EFD1000/500 System cannot be operated reliably in acrobatics. Observe flags
and reset EFD1000/500 System if required.
N O T E
Due to the location of the Remote Sensor Module (RSM) the outside air temperature data
are available time-delayed.
The EFD1000/500 System must utilize the software version described below or later approved
versions. The system software version for the Main Application Processor (MAP) and for the Input-
Output Processor (IOP), both of which are contained within the EFD display head, is displayed via
the Main Menu SYSTEM STATUS page.
Summary of Contents for 330lx
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