Pilot's Operating Handbook
Section 7
Description
Edition 0 - March 05, 2019
Rev. 1
Page 7.9.20
Emergency lighting
Emergency lighting consists of two swiveling floodlights located on both sides of the
cockpit overhead panel above front seats. It illuminates instrument panel assembly in
case of visor lighting tubes and / or instrument integrated lighting failure.
A rheostat located on the cockpit overhead panel controls emergency lighting
operation and intensity. Forward rotation of control knob allows changing from OFF
position to minimum lighting then increasing lighting to maximum brightness.
Figure 7.9.7 (1/2) - Internal lighting controls
1)
Instrument panel lighting switch (rheostat)
2)
DIMMER switch
3)
Cabin lighting switch (rear seats reading light)
4)
Access door, baggage compartment and FWD dome light
(delayed breaker) push-button
5)
Emergency lighting switch
6)
Breaker panel lighting switch
PIM - DO NOT USE FOR FLIGHT OPERATIONS