Bedienungsanleitung Garmin GTN 625 (Seite 25 von 412) (Englisch)

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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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