Piper CHEROKEE CRUISER PA-28-140 Information Manual
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Piper CHEROKEE CRUISER PA-28-140 Information Manual

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  • Page 3 PILOT’S OPERATING MANUAL REFERENCE ONLY THIS ELECTRONIC VERSION OF THE POM/AFM IS NOT APPROVED TO REPLACE ANY OPERATING INFORMATION REQUIRED BY THE REGULATIONS. This manual is incomplete without an APPROPRIATE FAA APPROVED AIRPLANE FLIGHT MANUAL and an APPROPRIATE WEIGHT AND BALANCE REPORT.
  • Page 180 ANEXO I SUPLEMENTO AL MANUAL DE VUELO AI-CDF119-20-115SMV Rev. Org / 2018-03-05 APLICABILIDAD: PIPER CHEROKEE PA-28-140 HK-1791G S/N 28-7625144 ELABORADO POR: OSCAR WILMAN MOSQUERA Inspector de aviónica AIT-CDF119-2229 JUAN SEBASTIAN SANTAMARIA Asistente de Ingeniería REVISADO POR: CARLOS ALBERTO NUÑEZ TAPIERO Ingeniero aeronáutico...
  • Page 181 INSTALACIÓN DE UN TRANSPONDER MODELO GTX335 W/GPS (ADS-B) EN LA AERONAVE HK-1791G OPERADA POR AEROCLUB DE COLOMBIA PILOT OPERATING HANDBOOK SUPLEMENT FOR GARMIN GTX 335 W/GPS (ADS-B) PIPER CHEROKEE PA-28-140 Registration number: HK 1791G Serial number: 28-7625144 This document serves as an PILOT OPERATING HANDBOOK SUPLEMENT when Garmin GTX335 System is installed in Accordance with Technical Data AI-CDF119- 20-HK1791G for the “INSTALACIÓN DE UN TRANSPONDER MODELO GTX335 W/GPS EN...
  • Page 182 DOCUMENT TYPE DOCUMENT No PILOT OPERATING HANDBOOK AI-CDF119-20-115PHO REV. REVISION PAGINA CODIGO. AI-FI-ING-003 2018-03-05 2 de 7 TÍTULO INSTALACIÓN DE UN TRANSPONDER MODELO GTX335 W/GPS (ADS-B) EN LA AERONAVE HK-1791G OPERADA POR AEROCLUB DE COLOMBIA LOG OF REVISIONS Revised Revision Date of Description of revision Number...
  • Page 183 DOCUMENT TYPE DOCUMENT No PILOT OPERATING HANDBOOK AI-CDF119-20-115PHO REV. REVISION PAGINA CODIGO. AI-FI-ING-003 2018-03-05 3 de 7 TÍTULO INSTALACIÓN DE UN TRANSPONDER MODELO GTX335 W/GPS (ADS-B) EN LA AERONAVE HK-1791G OPERADA POR AEROCLUB DE COLOMBIA SECTION 1. GENERAL 1.1 GTX 335 W/GPS ADS-B The Garmin GTX 335 W/GPS ADS-B consists of a Non-Diversity Mode S Transponder and the ES option provides ADS-B extended squitter functionality.
  • Page 184 DOCUMENT TYPE DOCUMENT No PILOT OPERATING HANDBOOK AI-CDF119-20-115PHO REV. REVISION PAGINA CODIGO. AI-FI-ING-003 2018-03-05 4 de 7 TÍTULO INSTALACIÓN DE UN TRANSPONDER MODELO GTX335 W/GPS (ADS-B) EN LA AERONAVE HK-1791G OPERADA POR AEROCLUB DE COLOMBIA 1.2 CAPABILITIES The Garmin GTX 335 W/GPS ADS-B as installed in this aircraft have been shown to meet the equipment requirements of RAC Par 4.2.2.6 ADS-B Out, when operating in accordance with sections 2.1 and 2.2 of this supplement.
  • Page 185 DOCUMENT TYPE DOCUMENT No PILOT OPERATING HANDBOOK AI-CDF119-20-115PHO REV. REVISION PAGINA CODIGO. AI-FI-ING-003 2018-03-05 5 de 7 TÍTULO INSTALACIÓN DE UN TRANSPONDER MODELO GTX335 W/GPS (ADS-B) EN LA AERONAVE HK-1791G OPERADA POR AEROCLUB DE COLOMBIA SECTION 2. LIMITATIONS 2.1 Minimum Equipment The GTX 335 W/GPS (ADS-B) must have the following system interfaces fully functional in order to be compliant with the requirements for RAC Par 4.2.2.6 ADS-B Out operations: Interfaced Equipment...
  • Page 186 DOCUMENT TYPE DOCUMENT No PILOT OPERATING HANDBOOK AI-CDF119-20-115PHO REV. REVISION PAGINA CODIGO. AI-FI-ING-003 2018-03-05 6 de 7 TÍTULO INSTALACIÓN DE UN TRANSPONDER MODELO GTX335 W/GPS (ADS-B) EN LA AERONAVE HK-1791G OPERADA POR AEROCLUB DE COLOMBIA Transponder and ADS-B Out functions will no longer be available. NOTE This guidance is supplementary to any guidance provided in the POH or AFM for the installed aircraft for loss of power generation.
  • Page 187 DOCUMENT TYPE DOCUMENT No PILOT OPERATING HANDBOOK AI-CDF119-20-115PHO REV. REVISION PAGINA CODIGO. AI-FI-ING-003 2018-03-05 7 de 7 TÍTULO INSTALACIÓN DE UN TRANSPONDER MODELO GTX335 W/GPS (ADS-B) EN LA AERONAVE HK-1791G OPERADA POR AEROCLUB DE COLOMBIA 1090ES TX CTL................VERIFY ON NO 1090ES TX................
  • Page 189 Piper - PA-28-140 HK-1791-G 28-7625144...
  • Page 190 © Copyright 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...
  • Page 191 Garmin International, Inc Log of Revisions FAA Approved AIRPLANE FLIGHT MANUAL SUPPLEMENT SUPPLEMENTAL AIRPLANE FLIGHT MANUAL GARMIN G5 ELECTRONIC FLIGHT INSTRUMENT DATE OF PAGE NO(S) DESCRIPTION FAA APPROVED APPROVAL Robert Murray Original Issue 7/22/2016 ODA STC Unit Administrator Robert Murray Added information regarding...
  • Page 192 This page intentionally left blank. AFMS, Garmin G5 AML STC 190-01112-13 Rev. 5 Page ii...
  • Page 193 Table of Contents Section 1 – General ....................1-1 Abbreviations and Terminology ......................1-2 Section 2 – Limitations ....................2-1 System Software Requirements ......................2-1 Use of Secondary Instruments ......................2-1 Kinds of Operations ..........................2-1 Section 3 – Emergency Procedures ................. 3-1 G5 Failure Indications ..........................
  • Page 194 This page intentionally left blank. AFMS, Garmin G5 AML STC 190-01112-13 Rev. 5 Page iv...

  • Page 195: Section 1 - General

    SECTION 1 – GENERAL The G5 Electronic Flight Instrument can display the following information to the pilot depending on the installation and location of the G5 instrument. • Primary attitude • Primary slip and turn rate information • Primary heading •...

  • Page 196: Abbreviations And Terminology

    Abbreviations and Terminology The following glossary is applicable within the airplane flight manual supplement Attitude Direction Indicator AFMS Airplane Flight Manual Supplement Attitude Course Deviation Indicator Directional Gyro Dead Reckoning Federal Aviation Administration Global Positioning System GPSS GPS Roll Steering Heading Horizontal Situation Indicator Instrument Landing System...

  • Page 197: Section 2 - Limitations

    SECTION 2 – LIMITATIONS System Software Requirements The G5 must utilize the following or later FAA approved software versions for this AFMS revision to be applicable: Component Software Version G5 Electronic Flight Instrument 5.00 Use of Secondary Instruments The original type design approved instruments for airspeed, altitude and vertical speed remain the primary indications for these parameters.
  • Page 198 This page intentionally left blank. AFMS, Garmin G5 AML STC 190-01112-13 Rev. 5 Page 2–2...

  • Page 199: Section 3 - Emergency Procedures

    SECTION 3 – EMERGENCY PROCEDURES G5 Failure Indications If a G5 function fails, a large red ‘X’ is typically displayed over the instrument(s) or data experiencing the failure. Upon G5 power-up, certain instruments remain invalid as equipment begins to initialize. All instruments should be operational within one minute of power-up.

  • Page 200: Gps Failure

    GPS Failure If GPS navigation receivers and/or navigation information are not available or invalid, the G5 will display Dead Reckoning mode (DR) or Loss of Integrity mode (LOI) on the HSI in the lower left corner. If Alternate Navigation Sources (ILS, LOC, VOR) Are Available: 1.

  • Page 201: Loss Of Electrical Power To The Gad 29B (If Installed)

    Loss of Electrical Power to the GAD 29B (If Installed) In the event of a loss of aircraft electrical power to the optional GAD 29B, the heading and course datum will be unavailable to the autopilot and the autopilot may deviate from the intended path or may disconnect. GPS flight plan course information may be displayed on the HSI and VFR will be displayed in amber text on the HSI.
  • Page 202 This page intentionally left blank. AFMS, Garmin G5 AML STC 190-01112-13 Rev. 5 Page 3–4...

  • Page 203: Section 4 - Normal Procedures

    SECTION 4 – NORMAL PROCEDURES G5 Power Button and Knob The G5 display will power on with the application of aircraft power. The G5 power button is used to turn the display on and off. Press and hold the power button to turn the display off. The knob performs the following functions: Press to access the Menu.

  • Page 204: Autopilot Operations With The G5 Hsi

    Autopilot Operations with the G5 HSI The G5 and optional GAD 29B offer various integration capabilities dependent upon the type of autopilot installed in a particular aircraft. The G5 Electronic Flight Instrument installation in this aircraft provides the following autopilot functions (appropriate boxes will be checked): ...
  • Page 205 navigator. If the GPSS data is invalid (for example, if there is no active GPS leg) or the selected HSI source on the G5 HSI is not GPS, the annunciated GPSS text will be yellow and a zero turn command will be sent to the autopilot.
  • Page 206 This page intentionally left blank. AFMS, Garmin G5 AML STC 190-01112-13 Rev. 5 Page 4–4...

  • Page 207: Section 5 - Performance

    SECTION 5 – PERFORMANCE No change. 190-01112-13 Rev. 5 AFMS, Garmin G5 AML STC Page 5–1...
  • Page 208 This page intentionally left blank. AFMS, Garmin G5 AML STC 190-01112-13 Rev. 5 Page 5–2...

  • Page 209: Section 6 - Weight And Balance

    SECTION 6 – WEIGHT AND BALANCE See current weight and balance data. 190-01112-13 Rev. 5 AFMS, Garmin G5 AML STC Page 6–1...
  • Page 210 This page intentionally left blank. AFMS, Garmin G5 AML STC 190-01112-13 Rev. 5 Page 6–2...

  • Page 211: Section 7 - System Description

    SECTION 7 – SYSTEM DESCRIPTION Refer to Garmin G5 Electronic Flight Instrument Pilot’s Guide for Certified Aircraft, part number 190-01112-12 Rev A (or later approved revisions), for a description of the G5 electronic flight instrument. This reference material is not required to be on board the aircraft but does contain a more in depth description of all the functions and capabilities of the G5.
  • Page 212 The following table shows the meaning of each message. System messages are displayed in white text. Message Meaning External Power Lost Aircraft power has been removed from the G5. Critical battery fault! Battery has critical fault condition and the unit is about to power off to avoid Powering off damage to the battery.

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