Garmin G500 Manual de instruções - Página 11

Procurar online ou descarregar pdf Manual de instruções para Ecrã de aviónica Garmin G500. Garmin G500 14 páginas. Primary flight and multifuction display system
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Garmin G500 Manual de instruções

2.13 Additional Instructions

None

2.14 Overhaul Period

The system does not require overhaul at a specific time period. Power on self-test and continuous BIT
will monitor the health of the G500/G600 system. If any LRU indicates an internal failure, the unit may be
removed and replaced. See the troubleshooting section contained in the G500/G600 AML STC
Installation Manual, listed under reference documentation in paragraph 2.1 of this document.

2.15 ICA Revision and Distribution

To revise this ICA, a request must be submitted to the ACO or ODA along with the revised ICA. The
ACO or ODA will obtain AEG acceptance, and approve any revision to the Airworthiness Limitations in
Section 1.4. After FAA acceptance/approval, Garmin will release the revised ICA for customer use, and
provide any required notification of the revision.
The latest revision of this document will be available on the Garmin website (www.garmin.com). A
Garmin Service Bulletin, describing ICA revision, will be sent to dealers if revision is determined to be
significant.

2.16 Assistance

Flight Standards Inspectors or the certificate holder's PMI have the required resources to respond to
questions regarding this ICA. In addition, the customer may refer questions regarding this equipment and
its installation to the manufacturer, Garmin. Garmin customer assistance may be contacted during
normal business hours via telephone 913-397-8200 or email from the Garmin web site at
www.garmin.com.

2.17 Implementation and Record Keeping

Modification of an aircraft by this Supplemental Type Certificate obligates the aircraft operator to include
the maintenance information provided by this document in the operator's aircraft maintenance manual
and/or the operator's aircraft scheduled maintenance program.
G500/G600 PFD/MFD System
190-00601-00 Rev. L
Instructions for Continued Airworthiness
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