Garmin | GTX 335 | Garmin GTX 335 AFMS-EASA Garmin GTX 33X and GTX 3X5 Transponders for ADSB

Garmin GTX 335 AFMS-EASA Garmin GTX 33X and GTX 3X5 Transponders for ADSB
GARMIN Ltd. or its subsidiaries
c/o GARMIN International, Inc.
1200 E. 151st Street
Olathe, Kansas 66062 U.S.A.
EASA Approved AIRPLANE FLIGHT MANUAL
SUPPLEMENT
GTX 33X and GTX 3X5 Transponders for ADS-B
Dwg. Number: 190-00734-16 Rev. 1
This Supplement is Applicable to the Following Manuals:
190-00734-15
This Supplement must be attached to the FAA Approved STC Airplane
Flight Manual Supplement when the GARMIN GTX 33X or GTX 3X5
transponder is installed in accordance with STC SA01714WI. The
information contained herein supplements the information of the STC
Airplane Flight Manual Supplement. For Limitations, Procedures, and
Performance information not contained in this Supplement consult the basic
Pilot’s Operating Handbook, FAA Approved Airplane Flight Manual and
the FAA Approved STC Airplane Flight Manual Supplement.
Airplane Serial Number: ______________________________________
Airplane Registration Number: _________________________________
Signed By: ______
__________________________
For Manager, Seattle Aircraft Certification Office
Federal Aviation Administration
Date: ___02/08/2017______________
EASA Approval No. 10060873
EASA AFMS,
GTX 33X and GTX 3X5 XPDR for ADS-B
190-00734-16 Rev.1
Page 1
© Copyright 2016-2017
GARMIN Ltd. or its subsidiaries
All Rights Reserved
Except as expressly provided herein, no part of this manual may be reproduced,
copied, transmitted, disseminated, downloaded or stored in any storage medium,
for any purpose without the express prior written consent of GARMIN.
GARMIN hereby grants permission to download a single copy of this manual
and of any revision to this manual onto a hard drive or other electronic storage
medium to be viewed and to print one copy of this manual or of any revision
hereto, provided that such electronic or printed copy of this manual or revision
must contain the complete text of this copyright notice and provided further that
any unauthorized commercial distribution of this manual or any revision hereto
is strictly prohibited.
GARMIN International, Inc.
1200 E. 151st Street
Olathe, KS 66062 USA
Telephone: 913-397-8200
www.garmin.com
EASA AFMS,
GTX 33X and GTX 3X5 XPDR for ADS-B
190-00734-16 Rev.1
Page 2
GARMIN International, Inc
Log of Revisions
EASA Approved AIRPLANE FLIGHT MANUAL
SUPPLEMENT
GTX 33X and GTX 3X5 Transponders for ADS-B
REV
NO.
PAGE
NO(S)
1
ALL
DESCRIPTION
Original Issue
EASA AFMS,
GTX 33X and GTX 3X5 XPDR for ADS-B
DATE OF
APPROVAL
EASA APPROVED
02.08.2017
EASA Approval
No 10060873
Signed by Ed Kolano
Seattle ACO
190-00734-16 Rev.1
Page 3
This page intentionally left blank.
EASA AFMS,
GTX 33X and GTX 3X5 XPDR for ADS-B
190-00734-16 Rev.1
Page 4
Table of Contents
Section 1. - General
Section 2. - Limitations
Section 3. – Emergency Procedures
Section 4. – Normal Procedures
Section 5. - Performance
Section 6. – Weight and Balance
Section 7. – Systems Description
EASA AFMS,
GTX 33X and GTX 3X5 XPDR for ADS-B
6
6
6
6
6
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190-00734-16 Rev.1
Page 5
Section 1. - General
The information in this supplement is EASA-approved material and must be
attached to the FAA Approved STC Airplane Flight Manual Supplement, (P/N:
190-00734-15) when the airplane has been modified by installation of the
GARMIN GTX 33X or GTX 3X5 Transponder in accordance with STC
SA01714WI.
This EASA approved Airplane Flight Manual Supplement is required in addition
to the FAA approved Airplane Flight Manual Supplement, (P/N: 190-00734-15).
The GTX 33X (GTX 33/330/33D/330D) meets the requirements in CS-ACNS
for ADS-B (Automatic Dependent Surveillance-Broadcast) and ELS.
The GTX 3X5 (GTX 335/335R/345/345R) meets the requirements in CS-ACNS
for ADS-B (Automatic Dependent Surveillance-Broadcast) and ELS.
Section 2. - Limitations
2.1 Portable Electronic Devices
Bluetooth functionality in Class IV aircraft is not approved under this STC and
must be disabled. Additional approval is required to enable Bluetooth
functionality for this class of aircraft.
The Connext interface and data provided by the GTX to a PED is not approved
to replace required aircraft equipment. The data presented on the PED may not
have the required integrity to be used as the sole source of information to base
tactical or strategic decision making.
Use of the Connext interface during critical phases of flight by the pilot flying is
prohibited.
Section 3. – Emergency Procedures
No Change
Section 4. – Normal Procedures
No Change
Section 5. - Performance
No Change
Section 6. – Weight and Balance
No Change
Section 7. – Systems Description
No Change
EASA AFMS,
GTX 33X and GTX 3X5 XPDR for ADS-B
190-00734-16 Rev.1
Page 6
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