Garmin GNS 480, Инструкция по установке

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Limitations
5-2 560-0982-01 Rev L GNS 480 (CNX80) Installation Manual
d) When flight planning an LNAV/VNAV or LPV approach, operators should use the Garmin
Prediction Program part number 006-A0154-02 (with the
<insert installed antenna model
number/part number> antenna selected) in addition to any NOTAMs issued for the approach.
5.3 Installation
The conditions and test required for TSO approval of this article are minimum performance standards. It is
the responsibility of those installing this article either on or within a specific type or class of aircraft to
determine that the aircraft installation conditions are within the TSO standards. TSO articles must have
separate approval for installation in an aircraft. The article may be installed only if performed under 14
CFR part 43 or the applicable airworthiness requirements.
The GNS 480 WAAS/GPS receiver is compatible on aircraft equipped with SATCOM when installed with
an appropriate antenna. See table notes in Section 1.3.10 for more information on compatible antennas.
5.3.1 GPS Antenna
The WAAS/GPS receiver is compatible with the GPS antennas listed in Section 1.3.10. Antenna selection
may affect operational limitations.
5.3.2 Antenna Installation – General
GNS 480 interfaces to GPS antennas other than those identified in this installation manual are outside the
scope of this manual and may require further evaluation for certification and/or other FAA airworthiness
approval.
5.3.3 Equipment Interfaced to the GNS 480
GNS 480 interfaces to aircraft systems other than those shown in this installation manual are outside the
scope of this manual and may require further evaluation and/or certification approval.
All equipment interfaced to the GNS 480 must be previously or concurrently approved.
5.3.4 Preservation of Previous Systems
It is the installer’s responsibility to preserve the essential characteristic of the aircraft being modified by
this manual to be in accordance with the aircraft manufacturer’s original design. This includes the
preservation of multiple power buses, which reduce the probability of interrupting power to essential
instruments and avionics. For Aircraft on the AML certified under 14 CFR Part 23 post amendment 41,
use of the GNS 480 for IFR operations requires a functional redundant electrical power system.
5.3.5 Aircraft Radio Station License
An aircraft radio station license is not required when operating in U.S. airspace, but may be required when
operating internationally.