Garmin G500 Посібник - Сторінка 9

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Section 1. GENERAL

1.1

Garmin G500 Primary Flight / Multi-Function Display System

The G500 PFD/MFD System consists of a Primary Flight Display (PFD) and

Multi-Function Display (MFD) housed in a single Garmin Display Unit (GDU),

plus an Air Data Computer (ADC) and Attitude and Heading Reference System

(AHRS). The G500 interfaces with other installed systems in the aircraft,

including Garmin GPS/SBAS navigators, VHF navigation radios, Garmin GDL

69 data link radios, Garmin GSR 56 Iridum transceivers, and various weather

radars, audio panels, video sources, radar altimeters, traffic systems and ADF

navigators.

The primary function of the PFD is to provide attitude, heading, air data and

navigation information to the pilot. The primary function of the MFD is to

provide mapping, terrain, and flight plan information.

The standby instruments (altimeter, airspeed, attitude, and magnetic compass)

are completely independent from the PFD and will continue to operate in the

event the PFD is not usable. These standby instruments should be included in

the pilot's normal instrument scan and may be referenced if the PFD data is in

question. A second G500 system installed on the co-pilot's side does not require

additional standby instruments.

1.2

System Power Sources

The G500 system depends on electrical power to maintain proper operation. The

Garmin Display Unit (GDU), Attitude and Heading Reference System (AHRS),

and Air Data Computer (ADC) are directly tied to the aircraft's main or essential

bus and energized when the aircraft master switch is turned on. Other systems,

like the navigation equipment, weather datalink, autopilot and Adapter (GAD)

are typically located on the avionics bus and may not be operable during engine

start.

The major components of the G500 are circuit breaker protected with resettable

type breakers available to the pilot. These breakers are located at the main or

essential bus circuit breaker panel and labeled as follows:

PFD

AHRS -

ADC

GAD

STBY ATT- Electric Standby Attitude Gyro

In dual installations the pilot side equipment is suffixed with the number 1 and

the copilot side equipment is suffixed with the number 2. For example: PFD 1

and PFD 2.

AFMS, GARMIN G500 PFD/MFD SYSTEM

FAA APPROVED

Garmin Display Unit (PFD/MFD), GDU 620

Attitude and Heading Reference System, GRS 77

Air Data Computer, GDC 74A

Garmin Adapter, GAD 43/43e (optional)

190-01102-01 Rev. 9

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