EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
DOCUMENT # 900-00041-001
PAGE 150-226
REVISION D
© Copyright 2019 Aspen Avionics Inc.
Vs:
No Flap Stall speed (bottom of green band)
Vso: Full Flap Stall speed (bottom of white band) - set to Vso= Vs on aircraft with
no flaps
Vyse: Single Engine best rate of climb (blue marker) on multi engine aircraft – set to
zero “0” on single engine aircraft.
Vmc: Single Engine minimum control speed (red marker) on multi engine aircraft –
set to zero “0” on single engine aircraft.
Initial Flap Extension Speed – set to zero “0” on aircraft without a published
initial flap extension speed. For aircraft that have a published speed at which
the first notch of flap may be deployed, set to that published value.
IAS UNITS: Set to Knots or MPH as defined in the AFM
TAPES:
UNLOCKED = Must only be set when Airspeed and Altimeter are still in basic T
configuration. With this setting the pilot can turn airspeed and
altitude tapes on or off via menu.
LOCK OFF
*
= Must be used if the airspeed tape on the EFD cannot be
configured to look exactly like the mechanical indicator. Tapes
are turned off and cannot be turned on by pilot.
LOCK ON = Tapes are always enabled and cannot be turned off by pilot.
*
NOTE: Tapes cannot be locked off unless the airspeed indicator and altimeter are located in the
original basic “T” configuration.
VSPD EDIT:
UNLOCKED = Pilot can modify value of VSPEED textual markers in the Main
Menu.
LOCKED =
Pilot cannot modify the values of the VSPEED textual
markers in the Main Menu.
10.4.7.2
PANEL TILT PITCH ADJ
This setting is used to compensate for aircraft instrument panels that are inclined with
respect to the aircraft leveling indices. The EFD1000 AHRS performance and the RSM
calibration depend on the AHRS sensor orientation to the aircraft waterline using the
aircraft leveling indices.
CAUTION: Do not use the “PANEL TILT PITCH ADJ” adjustment to align the Aircraft Reference Symbol
to a zero pitch mark for level flight. Though such an adjustment appears to be a natural
step, incorrect adjustment may result in incorrect pitch, roll and heading values. For
non-tilted panel installations, the EFD1000 AHRS must show zero degrees pitch when
the aircraft is leveled using the aircraft leveling indices. Adjustment of the PANEL TILT
