GMA 1347D Installation Manual
Page 1-5
190-00303-21
Revision
C
1.4 Certification
The conditions and tests 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.
1.4.3 TSO/ETSO Compliance
Function TSO/ETSO
Category
Applicable
LRU SW Part
Numbers
(011-01257-00)
Applicable
LRU SW Part
Numbers
(011-01257-20)
Applicable CLD
Part Numbers
(011-01257-00)
Applicable CLD
Part Numbers
(011-01257-20)
Audio Selector
Panels And
Amplifiers
TSO-C50c
ETSO-C50c
All
006-B0203-()
except
006-B0203-00
through
006-B0203-29
All
006-B0203-()
except
006-B0203-00
through
006-B0203-39
006-C0051-20*
006-C0075-00*
006-C0075-01*
006-C0075-03*
006-C0090-()
006-C0091-()
006-C0090-()
006-C0091-()
Airborne Radio
Marker Receiving
Equipment
TSO-C35d
ETSO-2C35d
Class A
All
006-B0203-()
except
006-B0203-00
through
006-B0203-29
All
006-B0203-()
except
006-B0203-00
through
006-B0203-39
006-C0051-20*
006-C0075-00*
006-C0075-01*
006-C0075-03*
006-C0090-()
006-C0091-()
006-C0090-()
006-C0091-()
*Not RTCA/DO-254 Level C Compliant
1.4.4 TSO/ETSO Deviations
TSO Deviation
1. Garmin was granted a deviation from TSO-C35d to use RTCA DO-160D instead of
RTCA DO-138 as the standard for Environmental Conditions and Test Procedures for
Airborne Equipment.
TSO-C35d
2. Garmin was granted a deviation from TSO-C35d to use FAR §21.607(d) instead of FAR
§37.7 as the general rules governing holders of the TSO authorizations.
1. Garmin was granted a deviation from TSO-C50c to use RTCA DO-178B instead of
RTCA DO-178A as the standard for Software Considerations in Airborne Systems and
Equipment Certification.
TSO-C50c
2. Garmin was granted a deviation from TSO-C50c to use RTCA DO-178B instead of
RTCA DO-178A to demonstrate compliance for the verification and validation of the
computer software.
Содержание GMA 1347D-00
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