Garmin G500 사용 설명서 - 페이지 7

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2.5.2

Aluminum Foil Tape (non-metallic aircraft only)

Any aluminum foil tape used in the G500/G600 installation (see section 3.1 of this document) must be

inspected every 12 calendar months in accordance with section 8.3.2 of the G500/G600 AML STC

Installation Manual.

GDU 620 – Display Unit

2.5.3

Maintenance of the GDU 620 is 'on condition' only.

GRS 77 – Attitude, Heading Reference System (AHRS)

2.5.4

The GRS 77 utilizes an Earth magnetic field model which is updated once every five years as part of the

Aviation Database maintained by the owner/operator. If the magnetic model is not up to date, the unit will

issue an alert upon startup indicating the model has expired. The model can be updated in accordance

with the database update section of the G500/G600 AML STC Installation Manual.

Otherwise maintenance of the GRS 77 is 'on condition' only.

GMU 44 – Magnetometer

2.5.5

Maintenance of the GMU 44 is 'on condition' only.

GDC 74( ) – Air Data Computer

2.5.6

Test according to Title 14 CFR §§ 91.411 and 91.413 as well as 14 CFR §§ 43 Appendix E. See the

pitot-static checkout procedure in Section 5.8.2 of the G500/G600 AML STC Installation Manual for the

testing procedure.

GTP 59 – OAT Probe

2.5.7

Maintenance of the OAT Probe is 'on condition' only.

GAD 43/43e – Adapter

2.5.8

Maintenance of the GAD 43/43e is 'on condition' only.

2.5.9

Mid-Continent Instruments Attitude Indicator Models 4300-4( ), or 4200-( ) with MD420

If a Mid-Continent Instruments Attitude Indicator is installed as part of the G500/G600 AML STC, the

battery pack must be tested by one of the following means:

1. Manual:

a. Disconnect the battery pack from the Attitude Indicator.

b. Ensure the battery pack is completely charged and at or near room temperature.

c. Connect the battery to a load of 90 ohms (rated for 10 watts) for 60 minutes while

monitoring the battery voltage level.

i. If the battery voltage is at or above 15.0 volts while under load at the end of the

ii. If the battery voltage is below 15.0 volts while under load at the end of the 60

2. Automatic:

a. Use the Mid-Continent Instruments Battery Charger/Tester P/N 36029 to test the

battery.

i. If the time required for discharge is 60 minutes or greater, the battery may be

ii. If the time required for discharge is less than 60 minutes, the battery must be

The battery may be permanently damaged if it is left in a discharged state.

Recharge a discharged battery as soon as possible and

G500/G600 PFD/MFD System

Instructions for Continued Airworthiness

60 minute test, the battery may be recharged in accordance with the

Mid-Continent Instruments Installation Manual and re-installed in the aircraft.

minute test the battery must be replaced.

recharged in accordance with the Mid-Continent Instruments Installation Manual

and re-installed in the aircraft.

replaced.

****WARNING****

maintain with a float charge for maximum battery life.

190-00601-00 Rev. L

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