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Tecnam P92-JS - GENERATOR LIGHT; VOLT-AMMETER; OIL AND CYLINDER HEADS TEMP. - OIL PRESSURE; O.A.T. INDICATOR

Tecnam P92-JS
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FLIGHT MANUAL
Date: Issue 3: 25
th
May 2010
7-9
P92-JS
S E C T I O N 7
SYSTEMS
GENERATOR LIGHT
Generator light (red) illuminates for the following conditions:
Generator failure
Failure of regulator/rectifier, with consequent overvoltage sensor set off.
The battery can support energy requirements for 26 min (see page 3-8)
VOLT-AMMETER
The voltmeter indicates voltage on bus bar; a positive value of the ammeter
indicates the generator is charging the battery, a negative value indicates the
battery's discharge rate.
OIL AND CYLINDER HEADS TEMP. - OIL PRESSURE
These instruments are connected in series with their respective sensors. The same
breaker protects all temperature instruments while a second breaker protects oil
pressure indicator and other instruments.
O.A.T. INDICATOR
A digital Outside Air Temperature indicator (°C) is located on the upper left side
of the instrument panel. The sensor is placed on cabin top.
STALL WARNING SYSTEM
The aircraft is equipped with a stall warning system consisting of a sensor located
on the right wing leading edge connected to a warning noisemaker located on the
instrument panel.
AVIONICS
The central part of the instrument panel holds room for avionics equipment. The
manufacturer of each individual system furnishes features for each system.
EXTERNAL POWER SUPPLY
On the right side of the tail cone, an external power is present. Using this device
it is possible to feed the electric system by an external power source. It should be
used at the engine start-up in cold weather condition.

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