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ASPEN EFD1000 EFIS
                                                            

Aspen in flight

Penn Avionics was pleased to be the first shop to install an Aspen EFD1000 system. Penn installed the first Aspen EFD1000 into the AOPA sweepstakes aircraft. The EFD1000 should be an outstanding product available at an extremely reasonable price. The EFD1000 has a built in GPSS converter along with an emergency standby battery to power the unit in the event of an aircraft electrical system failure. If you compare the cost of a standby attitude gyro with battery and external GPSS converter, you have almost purchased the EFD1000 on those two features alone.

We have received many customer inquiries on this system and the following is a short FAQ that we will continue to expand on.

4/2/2008:

Penn Avionics, Inc completes 1st revision of AOPA sweepstakes Archer which includes the Aspen EFD1000 pro. The AOPA archer will be down at Sun&Fun on display, then returning to Penn Avionics for a new one piece metal panel.

Ken and I had a chance to run the EFD1000 pro through it's paces in flight this week. I have to say, that the EFD1000 is everything Aspen said it would be. From start-up, the Aspen EFD1000 was up and running in about the same time it took the GNS-530W to go though it's self test. The knobs and controls on the EFD1000 were intuitive and worked well. In flight the display was bright and clear. There were no viewing angle issues, Ken could read the display from the right seat. The Horizon, HSI, Airspeed, Alt and VSI tapes all operated as advertised without any issues. We believe this truly will be a revolutionary product for the GA owner, and look forward to spending more time behind the EFD1000.

10/1/2008:

Penn Avionics has installed 23 Aspen EFD1000 systems to date. The units have been performing well and customer feedback has been positive. Aspen has released new system software that has added increased autopilot interfaces and improved calibration options. The FAA approved model list continues to grow. The EFD1000 platform is proving itself to be a stable system that offers great advantages at a competitive price.

Aspen in C210 panelAspen in Beech S35 panelAspen in Piper ArrowAspen in Beech A36Aspen in AA5B Tiger

Aspen in A36 PanelAspen in Mooney M20C panelAspen in Arrow panelAspen in Cessna 340 panel

Aspen in AOPA PA28 panelAspen in C210 panelAspen in Barron panelAspen in A36 panelAspen in C182 panel

Beech Sierra with AspenBeech A36 with Aspen Piper PA28-180 AspenBeech A36 1979 Aspen EFD1000

Cirrus SR20 Aspen InstallPiper PA28 Aspen Install TB20 Apsen

8/2009: Flush Mounting Kit

Aspen is now shipping a flush mounting kit for their displays. The flush mounting kit allows the
Aspen display to recess into the instrument panel rather than mounting against it. Add approximately
$690.00 for the flush mount kit (parts + labor). Below are pictures of the kit we installed on a 1979 A36 and
Grumman AG-5B
 
Flush Mount EFD1000 AG-5B

Flush Mount EFD1000 AG5B 2




A36 panel with flush kit

Flush kit side view 

Flush kit side back view 

Below: Cirrus SR20 Aspen Install with Flush Mount kit

Cirrus SR20 Aspen Install 

11/2009: Aspen Software V2.0 now available for EFD1000 systems. This is a field installable upgrade.

Highlights of V2.0:

1.     Added support for optional upgrade for Traffic / WX500 / EWR-50 interface for v2.0 PFDs.

2.     Added RS232 & ARINC429 Airdata outputs.

3.     Added a trend vector display to the altitude tape.

4.     Added high speed ARINC429 inputs.

5.     Added support for internal and bottom mounted RSMs.

6.     Added an “Attitude Ref Symbol Adjust” setting with a range of -5 to +5 to allow fine tuning of the attitude display.

7.     Added Diagnostics:

8.     Improved GPSS mode annunciation and gain adjustment.

9.     Improved AHRS solution robustness with fewer nuisance Cross Check Attitude annunciations.

10.  Improved battery circuit logic to prevent continuous power cycling (screen flashing during initialization or shutdown). This reduces or eliminates the need to disconnect the battery to shut down the EFD.

11.  The AHRS filter’s response to the magnetometer input is also more robust. A “FREE GYRO MODE” has been added to annunciate a condition in which the magnetic observability is below the threshold.

12.  The interfaces to external modules like the RSM and CM are more robust.

13.  The minimum display intensity level has been lowered in “MANUAL” and “AUTO” dimming modes for operators that prefer lower back lighting conditions.

14.  The instrument panel tilt adjustment “Pitch Attitude Trim” has been expanded to allow for pitch adjustments from +20 to -10 degrees.

15.  A Pitot system input monitor has been added.  If the aircraft is configured with a GPS input to the EFD1000, the EFD1000 will compare the GPS groundspeed to the Indicated Airspeed.  If the IAS is less than 30 kts and the GPS groundspeed is greater than 50 kts for 0.5 seconds (or longer), the EFD1000 will display a Red X on the Attitude and Heading while annunciating “CHECK PITOT HEAT”.  If the obstruction is removed, the EFD1000 will perform an AHRS reset, clear the Red Xs and return to the attitude display.

16.  Additional minor enhancements and improvements

1/1/2010:

Aspen is now shipping their MFD display.

EFD1000 Pro General FAQ:

Aspen EFD1000

Aspen EFD1000 on left, Magnetometer top center, configuration module bottom center, (ACU) Analog interface unit on right.

Aspen EDF1000 and Vac Gyros

Aspen EFD1000 and Vac Gyros

Aspen EFD1000 compared to older vacuum gyros.

EFD1000 FAQ:

What aircraft will the EFD1000 be certified in?

Initially the EFD1000 will be certified in aircraft 6000lbs and less. The STC approved model list should cover most popular general aviation aircraft (no helicopters at this time). In our opinion, it would be very difficult to obtain a field approval to install the EFD1000 into an aircraft not listed on the Aspen STC approved model list.

What instruments can I remove to make room for the EFD1000 (and still be legal for IFR)?

This will vary by aircraft, but in general an existing DG and/or VSI can be removed. The turn coordinator gyro can also be removed if the autopilot in not interfaced to it.

STEC autopilots, Cessna 200 and 300 autopilots, and King KAP140 autopilots are interfaced to the turn coordinator and therefore it cannot be removed. In these cases the turn coordinator could be relocated to the co-pilot side or "blind" mounted if necessary.

Aspen VSI layput

What back-up instruments are required with an EFD1000 installation?

FAR 23.1311 (a)(5) requires that independent secondary instruments be installed for Attitude, Airspeed, Magnetic direction indicator (whisky compass is OK). These must be within the pilots center field of view (see fig 5.2 below). In most cases the existing instruments can be re-located to meet this requirement.

The backup Gyro Horizon must be a vacuum driven unit. If the backup Horizon Gyro is electric, it must be interfaced to a standby battery or to an independent DC bus being driven by an alternator independent of the Aspen EFD1000.

Standby Inst Locations

Aspen Layout Piper

 

Will the Aspen interface to my autopilot?

Most popular GA autopilots will interface with the Aspen. The Aspen will not be able to replace the autopilots position reference source (i.e. Horizon gyro or Turn Coordinator gyro). The Aspen will be able to provide a  heading input, GPSS input, and nav input to the autopilot.

Note: The initial EFD1000 units will not interface with Century or Cessna autopilots only STEC and King. This limitation will be removed in the next software release.

If your autopilot has a DC Flight Director output, the Aspen will display Flight Director command bars. (If you have an existing King KI-256 flight director, you have DC flight director outputs). If your autopilot does not have an existing DC Flight Director output, the Aspen will not display Flight Director command bars.

King KFC200, KFC150 and KFC225 autopilots will be able to provide DC flight director outputs for the Aspen. STEC SYS-55(X) and 60-2 autopilots will be able to provide DC flight director outputs to the Aspen as long as the STEC ST-645 or ST-670 flight director interface is installed.

Will the Aspen have a GPSS converter?

Yes. The Aspen has an internal GPSS converter and will provide GPSS functionality between your GPS and autopilot. Some existing GPS units will not be compatible, ask for details. (Note: all Garmin 400/500 series units are compatible)

Does the Aspen have a backup battery?

Yes. The EFD1000 has an internal emergency battery. This internal battery will continue to power the unit for 30 minutes in the event of an aircraft DC bus failure.

Will the Aspen display data link weather?

The initial release of the EFD1000 will not have the weather interface. The weather interface will be available as an optional interface in the future. The Aspen will interface with the Heads-up XM data-link (the Heads-up XM link is also compatible with the Avidyne EX500/5000 MFD). The Garmin GDL-69 is not compatible with the Aspen EFD1000.

Will The Aspen display traffic information?

The initial release of the EFD1000 will not have the traffic interface. The traffic interface will be available as an optional interface in the future.

What is the nature of the standby GPS in the Aspen EFD1000?

The Aspen standby GPS is built into the Magnetometer antenna. This is a VFR only GPS and is intended to allow the EFD1000 to continue to provide navigation information to the last GPS waypoint in the event of a failure of the panel mounted GPS that is driving the EFD1000. The pilot can not enter a waypoint into the EFD1000, and only the last waypoint or route will be the current waypoint.

Will The Aspen EFD1000 display the 7 required Garmin WAAS annunciations?

Yes. The Aspen will display the 7 required Garmin WAAS annunciations (VLOC, GPS, TERM, APR, WPT, MSG,INTG). (This is only relevant for customers whose Garmin is mounted outside the pilot's field of view such as pre 1984 Beech A36, all F33 aircraft, Grumman AA5, etc).

Will I need two Aspen ACU units?

The Aspen EFD1000 standard package comes with one ACU (Analog control unit). For customers with dual Garmin 400/500 units and one autopilot this is all you will need. For customers with older analog nav-coms (i.e. King KX155) and / or GPS units that use an RS232 output rather than ARINC 429, a second ACU may be required.

What is the issue with heading bootstrap compatibility?

This will only be an issue for some installations. The heading bootstrap is an electronic interface that allows the aircraft's HSI or DG to electrically transmit the heading information to another avionics system. Examples of avionics systems that may require a bootstrap from the HSI or DG would be; Sky watch (TAS) traffic systems, Air Data computers, WX500 storm scopes, Argus maps, Avidyne EX500/5000 MFD that have radar interface, RMI systems, Sandel/King EHSI's.

Most GA bootstraps were accomplished using an older analog XYZ 26 volt 400 hz syncro format. The Aspen EFD1000 does not support this format. The Aspen EFD1000 supports low speed ARINC 429 label 320 digital bootstrap format. This can substitute for the legacy analog bootstrap in some configurations (such as the L-3 Sky watch system which can accept XYZ analog, or 429 digital heading input). There are external heading converters that can take the Aspen 429 digital heading output and convert it to the legacy analog XYZ format, but these are in the $4000.00 range and generaly cost prohibitive. For customers that have legacy equipment that must have an analog bootstrap input, we would recommend retaining the legacy HSI/DG and re-locating it to the co-pilot (or other) location.

Penn Avionics can evaluate the customer's aircraft and provide a written quote for the Aspen EFD1000. Please use our on line quote request form.


Copyright 2006 Penn Avionics, Inc. All rights reserved rev 3/22/2010

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