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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THIS ELECTRONIC DOCUMENT MAY HAVE BEEN SUPERCEDED.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
The Electronic Flight Instrument System [EFIS], provides easy visualization of aircraft
attitude and navigation information and permits a modular approach to aircraft systems
integration. The EFIS consists of two (or four) programmable, self-contained 5 inch
color Active Matrix Liquid Crystal Display [AMLCD] indicators, the Electronic Attitude
Director Indicator (EADI) and the Electronic Horizontal Situation Indicator (EHSI). These
AMLCD indicators are configured as one EHSI and one EADI or two EHISs and two
EADIs. They display aircraft heading and attitude along with navigational and AFCS
information. The EADI and EHSI have the same bezel configuration. Each bezel is split
in two sections, a vertical section and a horizontal section. The bezel vertical section
contains four softkeys (“C”, “
▲
”, “
●
” and “
◆
”) and a rotary/push-button switch (“DIM”).
The bezel horizontal section contains two rotary push-button switches (“CRS SEL” and
“DH/HDG SEL”) and an inclinometer. The inclinometer on the EHSI is covered by a
blanking plate.
EADI DISPLAY AND CONTROLS LEGEND
ELECTRONIC FLIGHT INSTRUMENT SYSTEM
ROGERSON KRATOS NEOAV 500H
NOTE: DETAILED SYSTEM INFORMATION MAY BE FOUND IN THE
ATTACHED DOCUMENT;
LINK (RK-EFIS-PHB10-97.PDF)
Содержание BELL 430
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