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PRODUCT DATA
JANUARY 2003
T h e D u a l P i l o t I F R w i t h S i n g l e A F C S /
K F C 5 0 0 c o n f i g u r a t i o n c o n s i s t s o f a
completely integrated, digital , three-axis
(p i t c h , r o l l, a n d y a w ) d u a l e l e c t r o n i c
channel flight control system, with yaw
damper, coupled Flight Director, and a four
tube Electronic Flight Instrument System
( E F I S ) . T h e S i n g l e A F C S i n s t a l l a t i o n
replaces the Attitude Indicator and HSI with
four four inch EFS-40 displays, and then
adds the KFC-500 Flight Control System.
System components and architecture are
shown in the block diagram below. Detailed
s y s t e m d e s c r i p t i o n a n d o p e r a t i o n a l
information may be found in the attached
document;
link(KFC500PG-single.PDF.)
DUAL PILOT IFR with Single AFCS/KFC500
EFS-40 (FOUR TUBE) with Flight Director
System Components
KFC 500 Flight Controls
KCP 520 Flight Computer
KLA 575 Linear Actuators
KSA 572 Trim Actuators
KRG 333 Accelerometer/Rate Gyro
Position Transducers
KAD 480 Air Data System
Iron Gyros - 4 Tube EFIS
Operating Parameters:
3-Axis: Pitch, Roll and Yaw
SCAS Engage on ground
Autopilot engage above 50 knots
Modes: HDG, NAV, APR, ALT HOLD/SELECT,
VS, IAS, VNAV
Summary of Contents for BELL 430
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