GARMIN Ltd. or its subsidiaries c/o GARMIN International, Inc E. 151st Street Olathe, Kansas U.S.A.

Similar documents
INSTRUCTIONS FOR USING THIS SAMPLE FLIGHT MANUAL SUPPLEMENT

TAS Probe User manual Document version 1.0

Instructions for Continued Airworthiness GDL 84/88 Part 23 AML STC as installed in. (Make and Model Airplane)

AOA System Owner s Manual

GTX 330/330D. Mode S Transponder. Pilot s Guide

SERVICE LETTER TITLE EQUIPMENT/FURNISHINGS - AMSAFE AIRPLANE FLIGHT MANUAL SUPPLEMENT

6275-S1 PNEUMATIC DRILL OPERATING MANUAL ORIGINAL INSTRUCTIONS. P/N November 2014 Revision 1

SUPPLEMENT 9 EASA CERTIFIED AIRPLANES

The FAA published Federal Regulation 14 CFR and 111 cm in May The final rule dictates that effective January 1, 2020, aircraft

Revisions to this AML must be coordinated between the STC holder and the responsible Aircraft Certification Office (ACO), and require FAA approval.

Section 7 Supplements. Miodel 400A SUPPLEMENTS

SERVICE BULLETIN TITLE NAVIGATION - GARMIN G1000 ENHANCED SEARCH AND RESCUE ENABLEMENT

Hawker 900XP. FAA Approved Airplane Flight Manual Supplement Pack

Copyright 2016 GARMIN Ltd. or its subsidiaries All Rights Reserved

skybeacon TM STC Instructions for Continued Airworthiness and Maintenance Manual

AIRCRAFT SERVICE CHANGE

SERVICE BULLETIN. The airplanes that follow that are equipped with the Garmin G1000 Nav III Avionics Option and the WAAS installed with SB

SERVICE BULLETIN. SERIAL NUMBERS thru B0001 thru 208B5178

OPERATIONAL BULLETIN

Hawker 850XP. Supplement Pack

CESSNA MODEL 208B 867 SHP - GARMIN G1000 Serials 208B2197 and 208B5000 and On

AIRCRAFT SERVICE CHANGE

SERVICE BULLETIN. The equivalent of this service bulletin has been incorporated on production airplanes and On.

Certification Memorandum. Guidance to Certify an Aircraft as PED tolerant

Registry Publication 17

AIRCRAFT SERVICE CHANGE

GAR-AERO WHEEL ADAPTERS & TIRES

A V I A T I O N BI 2008/45 C I V I L E

FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT

SUPERSEDED. [Docket No. FAA ; Directorate Identifier 2005-CE-08-AD; Amendment ; AD ]

CIVIL AVIATION PUBLICATION CAP 00 GENERAL

SERVICE BULLETIN TITLE NAVIGATION - ENHANCED SURVEILLANCE TRANSPONDER STRAPPING MODIFICATION

SERVICE BULLETIN. EFFECTIVITY SERIAL NUMBERS 525 (CJ1+) thru with GPS-4000S installed

GTN 625/635/650/725/750 and GMA 35 Instructions for Continued Airworthiness as installed in

TRANSMITTAL SHEET. Concurrent Requirement Added G450 Customer Bulletin Number 141 (aircraft that have previously incorporated ASC 016)

Terms of Reference for a rulemaking task. Portable Electronic Devices (PEDs)

Portable electronic devices

Subject: Automatic Dependent Surveillance-Broadcast (ADS-B) Operations and Operational Authorization

SERVICE LETTER TITLE AIR CONDITIONING - TRANSMIT KELLY AEROSPACE SERVICE BULLETIN KATS-SB

GTX 345 Transponder & ICAO IFR Filing. Charlotte County Composite Squadron FL Feb 2017 Maj Dick Morrell, Lt Tom Britton

RECOMMENDED FIELD APPROVAL APPLICATION Portland Flight Standards District Office

Garrecht TRX 1500 Traffic-Sensor

TABLE OF CONTENTS 1.0 INTRODUCTION...

NUMBER 904 RECORDING / INDICATING SYSTEMS (ATA 31) PLANEVIEW MASTER OPERATING SYSTEM SOFTWARE UPDATE

NUMBER 008 PLACARDS AND MARKINGS (ATA 11) MAXIMUM ZERO FUEL GROSS WEIGHT - 48,000 POUNDS PLACARD INSTALLATION

ATTACHMENT. Company Name: Initial Shipping Address (if different from the Revision

SERVICE ADVISORY. NO.: 0608 Revision A. All Garmin Aviation Service Centers

BEFORE THE FEDERAL AVIATION ADMINISTRATION WASHINGTON D.C. Docket FAA PETITION OF DELTA AIR LINES, INC. FOR AN EXEMPTION December 21, 2012

CIVIL AVIATION PUBLICATION CAP 08 CERTIFICATE OF AIRWORTHINESS

SERVICE BULLETIN SB

SERVICE BULLETIN. NOTE: SL should be accomplished in conjunction with this service bulletin.

SERVICE BULLETIN SERIAL NUMBERS

GTX 330/330D. Mode S Transponder. Pilot s Guide. software version 8 and up

R1 CESSNA AIRCRAFT COMPANY

2017 PILOT TRAINING CATALOG

Revision Transmittal. June 11, Cessna Distributors and Authorized Service Facilities and CPC's

SERVICE LETTER REVISION

Garmin GNC 420 GPS Navigator with VHF COM

Revo, Incorporated: Amendment ; Docket No. FAA ; Directorate Identifier 2012-CE-013-AD.

COCKPIT USB POWER INTEGRATION

TDR Mode S and ADS-B Transponders

SR22T Pilot s Operating Handbook (POH) Temporary Change

INSTRUCTIONS FOR COMPLETING THE FIELD APPROVAL CHECKLIST. AC A APPENDIX A, dated 08/17/2016

NUMBER 903 RECORDING / INDICATING SYSTEMS (ATA 31) PLANEVIEW MASTER OPERATING SYSTEM SOFTWARE UPDATE

SUPPLEMENT A33 TO THE AIRPLANE FLIGHT MANUAL DA 40 NG. Integrated Avionics System Garmin G1000,

EASA Safety Information Bulletin. SIB No.: Issued: 09 December 2013

REPUBLIC of SAN MARINO CIVIL AVIATION AUTHORITY

Directorate General of Civil Aviation Application for Type Certificate (TC)/ Restricted Type Certificate (RTC)

The following airplanes equipped with the Garmin G1000 Avionics system:

R2 CESSNA AIRCRAFT COMPANY

HAWKER BEECHCRAFT CORPORATION MODELS B300 AND B300C (C-12W) AIRPLANES

SERVICE BULLETIN EQUIPMENT/FURNISHINGS - PILOT AND COPILOT SHOULDER HARNESS GUIDE RETAINING WASHER INSPECTION AND/OR REPLACEMENT SYNOPSIS OF CHANGE

ADS-B (Automatic Dependent Surveillance Broadcast)

INSTRUCTIONS FOR CONTINUED AIRWORTHINESS

SUPPLEMENT A33 TO THE AIRPLANE FLIGHT MANUAL DA 62. Integrated Avionics System Garmin G1000 and. G1000 NXi, SBAS and P-RNAV Operation

Aai Manual Of Air Traffic Services Part 2

Private Pilot Ground School Syllabus

BGA GMP Sailplane and Self Sustaining Sailplane Maintenance Programme

Part 135 Recurrency (B)

Certificate of Airworthiness

Type Acceptance Report

GCAA GUYANA CIVIL AVIATION AUTHORITY

CIVIL AVIATION REGULATIONS PART 10 COMMERCIAL AIR TRANSPORT BY FOREIGN AIR OPERATORS WITHIN FEDERATED STATES OF MICRONESIA

Piper Arrow Pa t Maintenance Manual

IMPLEMENTATION PROCEDURES AIRWORTHINESS

[Docket No. FAA ; Directorate Identifier 2016-CE-015-AD; Amendment. Airworthiness Directives; PILATUS AIRCRAFT LTD.

GARMIN CONNEXT WIRELESS CONNECTIVITY SOLUTIONS

SUPPLEMENT AUGUST CITATION PERFORMANCE CALCULATOR (CPCalc) MODEL THRU FM-S51-00 S51-1 U.S.

United States News & Regulatory Updates

SERVICE BULLETIN. Single Engine SEB TITLE FLIGHT CONTROLS - LOWER RUDDER HINGE HARDWARE INSPECTION

Development of EFB. Electronic Flight Bag. a message for Flight Examiners

SERVICE ADVISORY NO.: 1506 Rev A

SUPPLEMENT 3 11 APRIL CITATION PERFORMANCE CALCULATOR (CPCalc) MODEL AND ON 510FM-S3-00 S3-1 U.S.

AEROSPACE RECOMMENDED PRACTICE

Revision 2 03/15/2017. North Coast Flight School Inc.

FILE FAA APPROVED ROTORCRAFT FLIGHT MANUAL SUPPLEMENT EUROCOPTER

Pilot's Operating Handbook Supplement AS-09

Piper Mirage Pa p Poh Flight Manual

Electrical system, HIRF and Lightning

Beech Baron 58 Poh Sdocuments2

Transcription:

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 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. 151 st Street Olathe, KS 66062 USA Telephone: 913-397-8200 www.garmin.com 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) DESCRIPTION DATE OF APPROVAL EASA APPROVED 1 ALL Original Issue 02.08.2017 EASA Approval No 10060873 Signed by Ed Kolano Seattle ACO Page 3

This page intentionally left blank. Page 4

Table of Contents Section 1. - General 6 Section 2. - Limitations 6 Section 3. Emergency Procedures 6 Section 4. Normal Procedures 6 Section 5. - Performance 6 Section 6. Weight and Balance 6 Section 7. Systems Description 6 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 Section 4. Normal Procedures Section 5. - Performance Section 6. Weight and Balance Section 7. Systems Description Page 6