400W Series Rotorcraft 190-00356-21 Rev. C
Instructions for Continued Airworthiness Page 14 of 15
2.14 Additional Instructions
None
2.15 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 400W Series unit. If the unit indicates an internal failure, the unit may be
removed and replaced. See troubleshooting section contained in the 400W Series Installation Manual,
listed under reference documentation in paragraph 2.1 of this document.
2.16 ICA Revision and Distribution
To revise this ICA, a letter must be submitted to the ACO along with the revised ICA. The ACO will
obtain AEG acceptance, and approve any revision to the Airworthiness Limitations Section 3. 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.
2.17 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.
2.18 Implementation and Record Keeping
Modification of a rotorcraft by this Supplemental Type Certificate obligates the rotorcraft operator to
include the maintenance information provided by this document in the operator’s rotorcraft maintenance
manual and/or the operator’s rotorcraft scheduled maintenance program.
3. AIRWORTHINESS LIMITATIONS SECTION
There are no additional Airworthiness Limitations as defined in 14 CFR § 27, Appendix A. A27.4 that
result from this modification. The Airworthiness Limitations section is FAA approved and specifies
maintenance required under §§43.16 and 91.403 of the Federal Aviation Regulations unless an
alternative program has been FAA approved.
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