203
THIS IS AN UNCONTROLLED DOCUMENT.
THIS ELECTRONIC DOCUMENT MAY HAVE BEEN SUPERCEDED.
THE MOST CURRENT DOCUMENT INFORMATION IS AVAILABLE
FROM YOUR BELL HELICOPTER TEXTRON REPRESENTATIVE.
PRODUCT DATA
JANUARY 2003
T h e B a s i c D u a l P i l o t I F R f a c t o r y
configuration consists of a digital , three-
axis (pitch, roll, and yaw), dual electronic
channel flight control system, with yaw
d a m p e r . S y s t e m c o m p o n e n t s a n d
architecture are shown in the block diagram
below. Detailed system description and
operational information may be found in
the attached document;
link(KFC500PG-
single.PDF.)
DUAL PILOT IFR with BASIC SCAS/ATT
with E/M Instruments -No 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
Iron Gyros - Electromechanical Instruments
Operating Parameters:
3-Axis: Pitch, Roll and Yaw
SCAS Engage on ground
Autopilot engage above 50 knots
Modes: Attitude Hold
Summary of Contents for BELL 430
Page 1: ...Product Data ...
