Mooney M20TN S type, Руководство по эксплуатации для пилотов

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MOONEY
M20TN - MODEL TYPE-S
SECTION VII
AIRPLANE AND SYSTEM DESCRIPTION
7 -- 5
AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE -- 04-02-2008
Instrument panel lighting is provided by post lights, overhead panel lights and the internally
lighted G1000 Integrated Cockpit System. Optimum cockpit panel lighting for night flying is
achieved by using a combination of panel lights and overhead map lights.
NOTE:
The illustrations depict a standard panel configuration. The location of instru-
ments, switches, and avionics may be relocated in each aircraft, dependant upon
the optional equipment selected by the customer and available panel space.
GARMIN G1000
The GARMIN G1000 Integrated Avionics System consists of a Primary Flight Display (PFD), a
Multi--Function Display (MFD), an Audio Panel, and Attitude and Heading Reference System
(AHRS), an Air Data Computer (ADC), and the sensors and computers to process flight and en-
gine information for display to the pilot. The system contains dual GPS receivers, dual VOR/ILS
receivers, dual VHF communications transceivers, a transponder, and an integrated annunci-
ation system to alert the pilot of certain abnormal conditions.
The Primary Flight Display (PFD) typically displays airspeed, attitude, altitude, and heading in-
formation in a traditional format. Slip information is shown as a trapezoid under the bank pointer.
One width of the trapezoid is equal to a one ball width slip. Rate of turn information is shown on
the scale above the compass rose; full scale deflection is equal to a standard rate turn. The fol-
lowing controls are available on the PFD (clockwise from top right):
S
Communications frequency volume and squelch knob
S
Communications frequency set knobs
S
Communications frequency transfer button
S
Altimeter setting knob (baro/QNH set)
S
Course knob
S
Map range knob and cursor control
S
FMS control buttons and knob
S
PFD softkey buttons, including master warning/caution acknowledgement
S
Altitude reference set knob
S
Heading bug control
S
Navigation frequency transfer button
S
Navigation frequency set knobs
S
Navigation frequency volume and Identifier knob
The PFD displays the crew alerting (annunciator) system. When an alert message is received,
an aural tone will be heard. Selecting the Alert button will allow the flight crew to see additional
information regarding the alert message.
Trend vectors are shown on the airspeed and altimeter displays as a magenta line predicting 6
seconds at the current rate. The turn rate indicator also functions as a trend indicator on the com-
pass scale.
The PFD can be displayed in a composite format for emergency use by pressing the DISPLAY
BACKUP button on the audio panel. In the composite mode, the crew alerting function remains
operative, but no map functions are available.
The Multi--Function Display (MFD) typically displays engine data, maps, terrain, traffic and to-
pography displays, and flight planning and progress information. The display unit is identical to
the PFD and contains the same controls as previously listed.
The audio panel contains traditional transmitter and receiver selectors, as well as an integral
intercom and marker beacon system. The marker beacon lights appear on the PFD. In addition,
a clearance recorder records the last 2
½ minutes of received audio. Lights above the selections
indicate what selections are active. Pressing the red DISPLAY BACKUP button on the audio
panel causes both the PFD and MFD to display a composite mode.