190-00303-A3
GSB 15 Installation Manual
Rev. 3
Page 1-5
1.3 Certification Statement
The GSB 15 has been shown to meet compliance with the claimed TSO(s) when interfaced with the equipment defined in this installation manual, and installed in
accordance with the requirements and limitations as defined in this installation manual.
The installer must verify that non-Garmin devices to be interfaced meet the installation requirements identified in this manual to assure the installed system will
comply with the Garmin TSO Authorization. Garmin installation requirements will usually specify that the interfaced device has appropriate TSO authorization, and
in some cases, such as for TSO-C144 antennas, may also require that the non-Garmin device meet additional Garmin specifications.
The conditions and tests required for TSO approval of this article are minimum performance standards. Those installing this article either on or within a specific type
or class of aircraft must determine that the aircraft installation conditions are within the TSO standards which include any accepted integrated non-TSO functions.
TSO articles and any accepted integrated non-TSO function(s) must have separate approval for installation in an aircraft. The article may be installed only according
to 14 CFR part 43 or the applicable airworthiness requirements.
In accordance with the Bilateral Oversight Board, Decision 006, for the Agreement Between the United States of America and the European Union on Cooperation
in the Regulation of Civil Aviation Safety, the FAA TSO authorization makes this an approved article within the respective EASA system. This article was tested to
additional standards (see section 1.3.4) that may demonstrate additional airworthiness specification performance standards required by the European Aviation Safety
Agency (EASA).
The Appliance Project Identifier (API) for the GSB 15 is GMN-02201. The API has been used for project identification with the FAA.
1.3.1 GSB 15 TSO Compliance
*The Minimum Performance Standards in this table are the conditions and tests used to achieve FAA TSO authorization. See
for additional standards.
Table 1-12 GSB 15 (011-04937-00, -01) TSO Compliance
TSO/MOPS*
Function Design
Class/Type
System SW
Part Numbers
Boot Block SW
Part Numbers
CLD Part Numbers
TSO-C71
Airborne Static (DC to DC) Electrical Power Converter
N/A
N/A
N/A
N/A