BendixKing KFD 840 - Manual (Page 99)

Honeywell Bendix/King KFD 840 Primary Flight Display
KFD 840 PG PN 7450-0840-01 Appendix
Rev C May 28, 2010 12-3
© 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)