Garmin G600 Manual de instrucciones - Página 11

Navegue en línea o descargue pdf Manual de instrucciones para Pantalla de aviónica Garmin G600. Garmin G600 14 páginas.

2.13 Additional Instructions

None

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.

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.

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.

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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