Garmin GTX 33 Installation Manual - Page 67

GTX 33 Installation Manual, Rev. F, B-15

Get Garmin GTX 33 PDF manuals and user guides View all Garmin GTX 33 manuals
Add to My Manuals
Save this manual to your list of manuals

Page 67 highlights

Item # 66. 67. Table B-1. Version 1 ADS-B Field Approval Compliance Matrix AMC Section # 8.5.4 8.6 AMC Item Compliance Summary In case more stringent barometric altimetry requirements are applicable in line with airspace requirements (e.g. RVSM) or other function requirements (e.g. ACAS II), then these requirements and their related regulation take precedence. Aircraft Identification Identification needs to be provided to the ADS-B transmit system so that the information is identical to the filed ICAO flight plan. This information may be provided from: [General information, no compliance statement req'd] [General information, no compliance statement req'd] A flight management Flight ID is programmed as part 68. 8.6.1 system; or A pilot control panel; or of the transponder configuration, and may also be For aircraft, which always operate manually configured by the pilot. with the same flight identification (e.g. using registration as the flight identification) it may be programmed into equipment at installation. In case no ICAO flight plan is filed, the Flight ID is programmed as part 69. 8.6.2 Aircraft Registration needs to be pro- of the transponder vided to the ADS-B transmit system. configuration. Special Position Identification (SPI) For ATC transponder-based The IDENT key is available to ADS-B transmit systems, the SPI the pilot on the GTX 33 control and 70. 8.7 capability needs to be provided. The display device, or a SPI capability should remote mounted IDENT button be integrated into the transponder may also be installed. functionality and should be controlled from the transponder con- trol panel. 71. 8.8 Emergency Status/Emergency Indica- [Section heading, no tor compliance statement req'd] 190-00906-00 Rev. F GTX 33 Installation Manual Page B-15

  • 1
  • 2
  • 3
  • 4
  • 5
  • 6
  • 7
  • 8
  • 9
  • 10
  • 11
  • 12
  • 13
  • 14
  • 15
  • 16
  • 17
  • 18
  • 19
  • 20
  • 21
  • 22
  • 23
  • 24
  • 25
  • 26
  • 27
  • 28
  • 29
  • 30
  • 31
  • 32
  • 33
  • 34
  • 35
  • 36
  • 37
  • 38
  • 39
  • 40
  • 41
  • 42
  • 43
  • 44
  • 45
  • 46
  • 47
  • 48
  • 49
  • 50
  • 51
  • 52
  • 53
  • 54
  • 55
  • 56
  • 57
  • 58
  • 59
  • 60
  • 61
  • 62
  • 63
  • 64
  • 65
  • 66
  • 67
  • 68
  • 69
  • 70
  • 71
  • 72
  • 73
  • 74
  • 75
  • 76
  • 77
  • 78
  • 79
  • 80
  • 81
  • 82
  • 83
190-00906-00
GTX 33 Installation Manual
Rev. F
Page B-15
66.
8.5.4
In case more stringent barometric
altimetry requirements are
applicable in line with
airspace requirements (e.g. RVSM) or
other function
requirements (e.g. ACAS II),
then these requirements and their
related regulation take
precedence.
[General information, no
compliance statement req’d]
67.
8.6
Aircraft Identification
[General information, no
compliance statement req’d]
68.
8.6.1
Identification needs to be provided to
the ADS-B transmit system so that
the information is identical to the filed
ICAO flight plan. This information may
be provided from:
A flight management
system; or
A pilot control panel; or
For aircraft, which always operate
with the same flight identification (e.g.
using
registration as the flight
identification) it may be
programmed into
equipment at installation.
Flight ID is programmed as part
of the transponder
configuration, and may also be
manually configured by the pilot.
69.
8.6.2
In case no ICAO flight plan is filed, the
Aircraft Registration needs to be pro-
vided to the ADS-B transmit system.
Flight ID is programmed as part
of the transponder
configuration.
70.
8.7
Special Position Identification (SPI)
For ATC transponder-based
ADS-B transmit systems, the SPI
capability needs to be provided. The
SPI capability should
be integrated into the transponder
functionality and should be
controlled from the transponder con-
trol panel.
The IDENT key is available to
the pilot on the GTX 33 control and
display device, or a
remote mounted IDENT button
may also be installed.
71.
8.8
Emergency Status/Emergency Indica-
tor
[Section heading, no
compliance statement req’d]
Table B-1.
Version 1 ADS-B Field Approval Compliance Matrix
Item #
AMC
Section #
AMC Item
Compliance Summary