Mooney M20TN S type Скачать руководство пользователя

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MOONEY

M20TN - MODEL TYPE-S

SECTION VII

AIRPLANE AND SYSTEM DESCRIPTION

7 -- 6

AIRPLANE FLIGHT MANUAL

ORIGINAL ISSUE -- 04-02-2008

The Attitude and Heading Reference System (AHRS) uses GPS, rate sensors, air data, and

magnetic variation to determine pitch and roll attitude, sideslip and heading. Operation is pos-

sible in a degraded mode if the system loses any of these inputs, but the AHRS must have at

least the ADC or GPS input to function. Status messages alert the crew of the loss of any of these

inputs. The AHRS will align while the aircraft is in motion, but will align quicker if the wings are

kept level during the alignment process.
The Air Data Computer (ADC) provides airspeed, altitude, vertical speed, and air temperature to

the display system. In addition to the primary displays, this information is used by the FMS and

TIS systems.
Engine instruments are displayed on the MFD. Discrete engine sensor information is processed

by the GARMIN Engine Airframe (GEA) sub--system. When an engine sensor indicates a value

outside the normal operating range, the legend will turn yellow for caution range, and turn red

and flash for warning range.
The G1000 also interfaces to the S--TEC 55x or GFC700 (if equipped) autopilot and repeats the

autopilot mode annunciators on the G1000 PFD. This provides easy viewing of the autopilot op-

erating mode and status, but remains a supplemental display of autopilot operating modes.
The GDL 69A is a remote sensor that receives broadcast weather data from a service of XM

Satellite Radio and delivers the data to to the G--1000 MFD. Highly reliable, near real--time

weather information is transmitted to the aircraft via XM Satellite Radio. XM WX Satellite Weath-

er service operate in the S--band frequency to provide continuous uplink capabilities at any alti-

tude throughout North America. Also available with the GDL--69A is XM’s digital audio entertain-

ment, which provides 130--plus channels of music, news, talk, sports and information. For

detailed operating instructions, see Garmin G--1000 Cockpit Reference Guide for the Mooney

M20TN.
The TSO’d KN 63, if installed, is a complete 100 watt, 200--channel remote DME system. Dis-

tances up to 389 nm (at line--of--sight altitude), groundspeeds up to 999 knots and time--to--sta-

tion up to 99 minutes are computed digitally and displayed on the G--1000 PFD and controlled by

the G--1000 interface controls. Distance lock--on is virtually instantaneous (usually within one

second) with accurate groundspeed and time--to--station readouts following in less than a min-

ute. For detailed operating instructions, see Garmin G--1000 Cockpit Reference Guide for the

Mooney M20TN.
The TSO’d Becker ADF 3502--(2) Automatic Direction Finder system, if installed, provides accu-

rate bearing--to--station in the 200 kHz to 1799 kHz frequency range, complete with ADF, ANT

and BFO tuning modes, plus audio output for station identification and monitoring AM broad-

casts. It is displayed on the G--1000 PFD and controlled by the PFD interface controls. For de-

tailed operating instructions, see Garmin G--1000 Cockpit Reference Guide for the Mooney

M20TN.
Traffic data detected by the L--3 Communications Goodrich SKYWATCH

Traffic Advisory Sys-

tem (TAS), if installed, will appear on the MFD and traffic display pages of the G--1000. For de-
tailed operating instructions regarding the interface of the G--1000 with the SKYWATCH

refer

to the Pilot’s Guide for the SKYWATCH

and the Garmin G--1000 Cockpit Reference Guide for

the Mooney M20TN.
Refer to the GARMIN G1000 Cockpit Reference Guide for the M20TN MODEL aircraft, GARMIN

P/N 00--00450--03, Rev. A or later FAA approved, for complete descriptions of the G1000 system

and operating procedures.

Revision B -- 11-21-2014