Garmin Part 23 AML STC User Manual

Browse online or download User Manual for Unknown Garmin Part 23 AML STC. Garmin Part 23 AML STC Airplane Flight Manual Supplement

  • Download
  • Add to my manuals
  • Print
  • Page
    / 13
  • Table of contents
  • BOOKMARKS
  • Rated. / 5. Based on customer reviews
Page view 0
G500 PFD/MFD System
Instructions for Continued Airworthiness
as installed in
_____________________________
(Make and Model Airplane)
Reg. No.____________ S/N_______________
Dwg. Number:
190-01102-00 Rev. 5
Garmin International, Inc.
1200 E. 151st Street
Olathe, Kansas 66062 USA
Record of Revision
Rev.
Date
Description of Change
1
06/30/09
Initial Release
2
11/30/09
Add replacement instructions for OAT bond strap
3
02/08/11
Update referenced publications. Clarified periodic maintenance
instructions. Foil check annual. Added new special inspection
requirements and periodic bonding test.
4
08/15/11
Remove “FAA Approved” language. Update IM rev. Add additional
instructions for Mid-Continent standby attitude indicator installations.
5
12/11/12
Added information regarding GAD 43e. Added additional Control,
Operating Information and deleted Pilot’s Guide reference. Incorporated
GDC 74 testing procedural information from Installation Manual. Revised
lightning strike inspection.
Page view 0
1 2 3 4 5 6 ... 12 13

Summary of Contents

Page 1 - G500 PFD/MFD System

G500 PFD/MFD System Instructions for Continued Airworthiness as installed in _____________________________ (Make and Model Airplane) Reg. No.______

Page 2

G500 PFD/MFD System 190-01102-00 Rev. 5 Instructions for Continued Airworthiness Page 10 of 13 2.13 Additional Instructions None 2.14 Overhaul Per

Page 3

G500 PFD/MFD System 190-01102-00 Rev. 5 Instructions for Continued Airworthiness Page 11 of 13 3. APPENDIX A 3.1 LRU Locations The following table

Page 4 - 2.1 Introduction

G500 PFD/MFD System 190-01102-00 Rev. 5 Instructions for Continued Airworthiness Page 12 of 13 3.2 Wire Routing – Single-Engine The following diag

Page 5 - 2.4 Servicing Information

G500 PFD/MFD System 190-01102-00 Rev. 5 Instructions for Continued Airworthiness Page 13 of 13 3.3 Wire Routing – Twin-Engine The following diagra

Page 6

G500 PFD/MFD System 190-01102-00 Rev. 5 Instructions for Continued Airworthiness Page 2 of 13 1. INTRODUCTION ...

Page 7

G500 PFD/MFD System 190-01102-00 Rev. 5 Instructions for Continued Airworthiness Page 3 of 13 1. INTRODUCTION 1.1 Purpose This document is designe

Page 8

G500 PFD/MFD System 190-01102-00 Rev. 5 Instructions for Continued Airworthiness Page 4 of 13 2. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 2.1 Intr

Page 9

G500 PFD/MFD System 190-01102-00 Rev. 5 Instructions for Continued Airworthiness Page 5 of 13 data on each screen. The function of the soft keys a

Page 10 - 2.16 Assistance

G500 PFD/MFD System 190-01102-00 Rev. 5 Instructions for Continued Airworthiness Page 6 of 13 2.5 Periodic Maintenance Instructions All G500 syste

Page 11 - Description of Location

G500 PFD/MFD System 190-01102-00 Rev. 5 Instructions for Continued Airworthiness Page 7 of 13 2.5.9 Mid Continent Instruments Attitude Indicator M

Page 12

G500 PFD/MFD System 190-01102-00 Rev. 5 Instructions for Continued Airworthiness Page 8 of 13 2.5.10 Electrical Bonding Test G500 LRU electrical

Page 13

G500 PFD/MFD System 190-01102-00 Rev. 5 Instructions for Continued Airworthiness Page 9 of 13 If any work has been done on the aircraft that could

Comments to this Manuals

No comments