Instructions for Continued Airworthiness GTN 6XX/7XX - Eurocopter EC130 Series
Page 19 of 21 190-01007-K9 Rev. 1
2.11 Data Relative to Structural Fasteners
Refer to Garmin P/N 190-01007-B1, GTN 6XX/7XX PART 27 AML STC SYSTEM MAINTENANCE
MANUAL Section 5 for fastener information.
2.12 Special Tools
A milliohm meter with an accuracy of +/- 0.1 milliohms ohms (or better) is required to measure the
electrical bonding between the GTN/GMA system components and aircraft ground.
2.13 Additional Instructions
None. N/A
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 GTN system. If any LRU indicates an internal failure, the unit may be removed
and replaced (Refer to Section 5 of the GTN 6XX/7XX PART 27 AML STC SYSTEM MAINTENANCE
MANUAL for Removal and Reinstallation instructions). See GTN 6XX/7XX PART 27 AML STC SYSTEM
MAINTENANCE MANUAL, Section 4 for Troubleshooting information.
2.15 ICA Revision and Distribution
To revise this ICA, Garmin will follow the Garmin ODA Procedures Manual SOP-0055/ACP-0016 for
Instructions for Continued Airworthiness. The latest revision of this ICA document is available on the
Garmin website (
www.flyGarmin.com). To Access Aviation Manuals, select the ‘Support’ tab and then
select ‘Manuals’. You may also contact Garmin General Aviation Product Support at 866-739-5687 (US
toll free) 913-397-8200 or
avionics@garmin.com. A Garmin Service Bulletin describing ICA revision will
be sent to Garmin dealers if a 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 contact Garmin with questions regarding this
equipment and its installation. Garmin Customer Support may be contacted during normal business hours
via telephone 913-397-8200 or from the Garmin web site at
www.flyGarmin.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 rotorcraft scheduled maintenance program.
To Next Page
Loading...
Need help?
General
