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BELL HELICOPTER BELL 430 - SINGLE PILOT & DUAL PILOT IFR with Dual AFCS;KFC500; SINGLE PILOT & DUAL PILOT IFR with Dual AFCS;KFC50

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205
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THIS ELECTRONIC DOCUMENT MAY HAVE BEEN SUPERCEDED.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
SINGLE PILOT & DUAL PILOT IFR with Dual AFCS/KFC500
with EFS-40 (FOUR TUBE) with Flight Director
System Components
KFC 500 Flight Controls
Two KCP 520 Flight Computers
KLA 575 Linear Actuators
KSA 572 Trim Actuators
Two KRG 333 Accelerometer/Rate Gyros
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
The Single & Dual Pilot IFR with Dual AFCS/
KFC500 configuration consists of a two
completely integrated, digital, three-axis
(pitch, roll, and yaw) dual electronic
channel flight control systems, with yaw
damper,
coupled Flight Director(System
1 only), and a four tube Electronic Flight
Instrument System (EFIS). The Dual AFCS
installation replaces the Attitude Indicator
and HSI with four four inch EFS-40
displays, and then
adds the KFC-500 Flight
Control Systems. System components and
architecture are shown in the block diagram
below. Detailed system description and
operational information may be found in
the attached document; link(KFC500PG-
dual.PDF.)

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