Pilot's Operating Handbook
Section 7
Description
Edition 1 - January 15, 2018
Rev. 4
Page 7.3.3
- the airspeed indicator,
- th
e landing gear control unit,
- the flap geared motor,
- the idle position sensor.
Aural warning alerts
According to the airplane configuration, different aural warning alerts sound :
- gear up and idle landing gear / landing gear
- gear up and extended flaps landing gear / landing gear
- stall stall / stall
- gear up, idle and stall stall / landing gear
- gear up, extended flaps and stall
stall / landing gear
- IAS > 269 ± 3 KIAS overspeed / overspeed
Refer to the GARMIN Pilot's Guide for description of the other aural warning alerts.
Cockpit overhead panel - see figure 7.3.2
This panel includes following elements :
- the loud-speaker of GMA,
- the TEST push-button,
- the emergency lighting rheostat.
It is attached to the cabin upper part between frames C6 and C7.
The emergency lighting rheostat is electrically supplied by BATT BUS bar and
protected by PANEL EMER circuit breaker.
The TEST push-button allows to test :
- the autopilot control panel backlighting,
- the MASTER WARNING and MASTER CAUTION indicators,
- the deicing panel led,
- the stick shaker system,
- the fire detection system, if installed,
- the stall aural warning alert,
- the DISPLAY BACKUP push-buttons backlighting,
- the LVL push-button.
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