EFD1000 E5 Dual Electronic Flight Instrument (EFI) Install Manual
DOCUMENT # 900-00041-001
PAGE 186-226
REVISION D
© Copyright 2019 Aspen Avionics Inc.
Aircraft Type:
______________________________________________________
Date:
________________________
Aircraft Serial Number:
_____________________________________
Tail Number:
____________________________
The following five pages must be printed and used during checkout. The Section number refers to the
section in the manual where the test is performed. This form must be included in document package to
be included in aircraft maintenance records.
Complete by performing test of Section 10.5.4
Calibrated
Heading
Source
Tolerance
Actual EFD
Heading
Calibrated
Heading
Source
Tolerance
Actual EFD
Heading
30
+/- 4
210
+/- 4
60
+/- 4
240
+/- 4
90
+/- 4
270
+/- 4
120
+/- 4
300
+/- 4
150
+/- 4
330
+/- 4
180
+/- 4
360
+/- 4
Complete by performing test of Section 10.6.1
IAS Setting
Band Color
Band
Range
Description
Pass
Vne =
Red
>Vne
Red arc displayed at all speeds above Vne
Vno =
Yellow
Vno - Vne
Yellow arc extending from Vno to Vne
Vs =
Green
Vs - Vno
Green arc extending from Vs to Vno
Vfe =
White
Vso - Vfe
Top of White arc
Vso =
White
Bottom of White Arc
Vyse =
Blue Marker
= Vyse
Blue Marker at Vyse
Vmc =
Red Marker
= Vmc
Red Marker at Vmc
=
Triangle (White) =
White triangle at initial flap extension airspeed
Aircraft with Vmo/Mmo Airspeed Indicator
Test
Description
Pass
Barber Pole or Redline
Position
Verify the Barber Pole or Redline appears at the correct airspeeds
as shown in Table 10-1.
NOTE
Single engine aircraft and aircraft with no flaps will not use all parameters above.
