4 4
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THIS ELECTRONIC DOCUMENT MAY HAVE BEEN SUPERCEDED.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
ATTITUDE INDICATOR
The attitude indicator is a self-contained
4 - i n c h , D C - p o w e r e d i n s t r u m e n t w h i c h
displays the pitch and roll flight attitude of
the helicopter in relation to the earth's
horizontal plane. A pitch trim knob adjusts
t h e a i r c r a f t s y m b o l v e r t i c a l l y . A n
inclinometer is built in to the instrument face
to provide yaw trim indication. An ATT FAIL
flag is visible when attitude information is
unreliable.
AIRSPEED INDICATOR
The airspeed indicator is a standard 3-inch
pitot -static instrument that indicates the
airspeed in knots on a scale graduated from
0 to 180 knots.
A LTIMETER (BAROMETRIC)
The altimeter, a standard 3-inch instrument,
indicates the altitude of the helicopter from
minus 1000 feet to plus 27,500 feet. The
b a r o m e t r i c p r e s s u r e s c a l e f o r s e t t i n g
reference pressure is shown in inches of
mercury and in millibars.
The magnetic compass is mounted on the central windshield post. A compass card
holder is provided to record the individual helicopter magnetic deviation.
STANDBY MAGNETIC COMPASS
FLIGHT INSTRUMENTS
Summary of Contents for BELL 430
Page 1: ...Product Data ...