Garmin GAD 43e Installation Manual - Page 43

LIMITATIONS, 1 Operation, 2 Installation, 2.1 Equipment Interfaced to the GAD 43

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7. LIMITATIONS 7.1 Operation There are no Part 23 aircraft type limitations. All functions of the GAD 43 meet the appropriate design assurance qualifications for a secondary system for aircraft in Class I, Class II, and Class III in accordance with AC 23.1309-1C, Figure 2. The TSO authorizations with the RTCA/DO178B software levels by function are listed in Section 1.5. 7.2 Installation Installation of the GAD 43 is restricted to locations in the aircraft that are consistent with the DO-160E categories defined in the GAD 43 Environmental Qualification Form (EQF), P/N 005-00496-07. The conditions and tests required for TSO authorization 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. 7.2.1 Equipment Interfaced to the GAD 43 GAD 43 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. GAD 43 Installation Manual 190-00899-00 Page 7-1 Rev. B

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GAD 43 Installation Manual
Page 7-1
190-00899-00
Rev. B
7.
LIMITATIONS
7.1 Operation
There are no Part 23 aircraft type limitations. All functions of the GAD 43 meet the appropriate design
assurance qualifications for a secondary system for aircraft in Class I, Class II, and Class III in
accordance with AC 23.1309-1C, Figure 2. The TSO authorizations with the RTCA/DO178B software
levels by function are listed in Section 1.5.
7.2 Installation
Installation of the GAD 43 is restricted to locations in the aircraft that are consistent with the
DO-160E categories defined in the GAD 43 Environmental Qualification Form (EQF),
P/N 005-00496-07.
The conditions and tests required for TSO authorization 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.
7.2.1 Equipment Interfaced to the GAD 43
GAD 43 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.