Garmin GAD 43 Installation Manual - Page 15

Certification, 5.1 TSO Compliance - tso number

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1.5 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 in compliance under 14 CFR Part 43 or the applicable airworthiness requirements. The Appliance Project Identifier for the for the GAD 43 is GMN-00724. Documents submitted to the FAA or other regulatory agencies on behalf of this project will be filed under and referred to by this number. 1.5.1 TSO Compliance Function Turn and Slip Instrument Bank and Pitch Instruments Direction (Heading) Instrument, Magnetic Automatic Pilots TSO/SAE/RTCA/EURO CAE TSO-C3e SAE AS8004 Incomplete System [1] TSO-C4c SAE AS8001 Incomplete System [1] TSO-C6e SAE AS8013A Incomplete System [1] TSO-C9c SAE AS402A Incomplete System [1] Category Type II Turn Error, Category A Applicable LRU SW P/Ns 006-B0876-00 through 006-B0876-( ) 006-B0876-00 through 006-B0876-( ) 006-B0876-00 through 006-B0876-( ) 006-B0876-00 through 006-B0876-( ) Applicable Custom Logic Device P/Ns N/A N/A N/A N/A Notes: [1] The TSOs identified in the table above are for an incomplete system and requires the GAD 43 to be installed and checked out according to this installation manual. GAD 43 Installation Manual 190-00899-00 Page 1-5 Rev. B

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GAD 43 Installation Manual
Page 1-5
190-00899-00
Rev. B
1.5 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 in compliance under 14
CFR Part 43 or the applicable airworthiness requirements. The Appliance Project Identifier for the
for the GAD 43 is GMN-00724. Documents submitted to the FAA or other regulatory agencies on behalf
of this project will be filed under and referred to by this number.
1.5.1 TSO Compliance
Function
TSO/SAE/RTCA/EURO
CAE
Category
Applicable
LRU SW P/Ns
Applicable
Custom Logic
Device P/Ns
Turn and Slip Instrument
TSO-C3e
SAE AS8004
Incomplete System [1]
Type II
006-B0876-00
through
006-B0876-( )
N/A
Bank and Pitch Instruments
TSO-C4c
SAE AS8001
Incomplete System [1]
Turn Error,
Category A
006-B0876-00
through
006-B0876-( )
N/A
Direction (Heading)
Instrument, Magnetic
TSO-C6e
SAE AS8013A
Incomplete System [1]
006-B0876-00
through
006-B0876-( )
N/A
Automatic Pilots
TSO-C9c
SAE AS402A
Incomplete System [1]
006-B0876-00
through
006-B0876-( )
N/A
Notes:
[1] The TSOs identified in the table above are for an incomplete system and requires the GAD 43 to
be installed and checked out according to this installation manual.