Honeywell BENDIXKing APEX EDGE Series - AIRCRAFT CONFIGURATION

Honeywell Bendix/King KFD 840 Primary Flight Display
KFD 840 PG PN 7450-0840-01 Appendix
Rev C May 28, 2010 11-3
© Honeywell International Inc. Do not copy without express permission of Honeywell
AIRCRAFT CONFIGURATION
This section is provided as a reference to the pilot for a record of the
configuration of the KFD 840 as it is installed in the aircraft
ITEM
RESOL-
UTION
INPUT
VALUE
RANGE
UNITS
CONFIGURATION
Roll
Adjust
0.1
0-180.0
DEG
Pitch
Adjust
0.1
0-90.0
DEG
S/R
Pointer
--
SKY,
ROLL
--
V
S0
1.0
0-240
(276)
Kts /
(MPH)
V
S1
1.0
0-240
(276)
Kts /
(MPH)
V
FE
1.0
0-240
(276)
Kts /
(MPH)
V
NO
1.0
0-240
(276)
Kts /
(MPH)
V
NE
1.0
0-240
(276)
Kts /
(MPH)
V
MCA
1.0
0-240
(276)
Kts /
(MPH)
V
YSE
1.0
0-240
(276)
Kts /
(MPH)