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Garmin GTN 650 Manual

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190-01007-A3 GTN 6XX/7XX AML STC Installation Manual
Rev. 4 Page 1-3
1.3.1 Approved Aircraft with Systems Not Covered by the STC
Aircraft identified on the Approved Model List have been determined to meet a minimum required
configuration for applicability of the STC. However, since some of these aircraft may have been modified
over the years or may have been manufactured with systems which are not identified or approved in this
manual for integration with the GTN, it may be difficult to use the data herein to completely substantiate
the installation in compliance with the STC. It is the installer’s responsibility to make the final
determination of applicability for each aircraft. Use this manual to assess each installation prior to
modifying any Type Certified aircraft to ensure the applicability of the GTN AML STC.
It is possible/permissible for installers and other appropriately certificated persons to seek FAA approval
for installation and operational use of the GTN equipment with systems not identified in this manual, such
as for aircraft certificated under 14 CFR parts 25, 27, or 29, by means of a field approval, STC, or TC.
Refer to FAA Advisory Circular (AC) 20-138( ) and other applicable guidance when applying for
installation and operational approval. AC 21-40 provides guidance for the STC approval process and
AC 43-210 provides guidance for the field approval process. If the field approval process is used, it is
advisable to consider the conditions and stipulations in FAA Flight Standards Information Bulletin for
Airworthiness (FSAW), 94-32c, “Guidance for Performing Field Approvals of Installation and
Operational Use of Global Positioning Systems (GPS) or GPS with Wide Area Augmentation Systems
(GPS/SBAS), Referred to as Global Navigation Satellite Systems (GNSS) Equipment”, as revised.
1.3.2 Part 23 Aircraft Not Identified on the AML
Aircraft identified in AC 23.1309-1D as Class I, II, III, or IV airplanes which are not identified on the
GTN AML STC may be valid candidates for installation of the GTN/GMA 35. Installers should contact
Garmin Tech Support with detailed drawings of the aircraft’s proposed installation. Engineering analysis
may allow for the inclusion of these aircraft in a future revision of the FAA Approved Model List. Also,
data provided in this manual may be used to perform the alteration but additional FAA approval is
required.
1.3.3 Other Aircraft Not Covered by the AML
Transport Category Aircraft (Part 25), and Rotorcraft (Part 27/29) are not part of this GTN AML STC.
However, these aircraft may be valid candidates for installation of this system. Installers may contact
Garmin for possible additional information that may support an installation of this type. Data provided in
this manual may be used to perform the alteration but additional FAA approval is required.
1.3.4 Required Documentation for All Installations
Regardless of applicability of the AML STC or alternative field approval application for installation and
operational approval, the aircraft must be returned to service in a means acceptable to the cognizant
aviation authority. An example would be submission of an FAA Form 337; “Major Repair and Alteration
Airframe, Powerplant, Propeller, or Appliance” to the appropriate FAA Flight Standards District Office
describing the work accomplished. The FAA Form 337 must detail the equipment and systems to which
the respective GTN System is interfaced and reflect appropriately approved or acceptable data for which
any follow-on FAA Field Approval is being sought. See AC 43.9-1F for instructions for completing the
FAA Form 337. In addition, the Configuration and Checkout Log must be completed and attached with
the Instructions for Continued Airworthiness such that any aircraft with the modifications detailed in this
manual may be properly maintained.
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