Garmin SR02232LA Bedienerhandbuch

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400W Series Rotorcraft
Instructions for Continued Airworthiness
as installed in
_____________________________
(Make and Model Rotorcraft)
Reg. No.____________ S/N_______________
STC SR02232LA
Document Number
190-00356-21 Rev. C
Garmin Ltd. Or its subsidiaries
c/o Garmin International, Inc.
1200 E. 151st Street
Olathe, Kansas 66062 USA
Record of Revision
Rev. Date Description of Change
A 10/24/08 Initial Release
B 1/28/09 Added table for list of interfaced equipment, STC number, and changed
document title.
C 4/24/09 Added STC number and changed revision levels in section 2.1
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1 2 3 4 5 6 ... 14 15

Inhaltsverzeichnis

Seite 1 - 400W Series Rotorcraft

400W Series Rotorcraft Instructions for Continued Airworthiness as installed in _____________________________ (Make and Model Rotorcraft) Reg. No._

Seite 2

400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 10 of 15 2.8 Diagrams Refer to the 400W Series Installatio

Seite 3

400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 11 of 15 Table 3: Unit Location Information Part and Mode

Seite 4

400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 12 of 15 Table 4: 400W Series Power Input 14 VDC 28 VDC I

Seite 5

400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 13 of 15 Table 5: Circuit Breaker Size and Placard Unit Po

Seite 6

400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 14 of 15 2.14 Additional Instructions None 2.15 Overhaul

Seite 7

400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 15 of 15 APPENDIX A 3.1 Wire Routing The following diagram

Seite 8 - 2.4 Servicing Information

400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 2 of 15 This page intentionally left blank

Seite 9 - 2.7.1 400W Series Unit

400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 3 of 15 1. INTRODUCTION...

Seite 10 - 2.8 Diagrams

400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 4 of 15 1. INTRODUCTION 1.1 PURPOSE This document is desi

Seite 11

400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 5 of 15 14) TSO: Technical Standard Order 15) BIT: Built

Seite 12

400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 6 of 15 2.2 Description of Alteration The Garmin Model 4

Seite 13 - 2.13 Special Tools

400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 7 of 15 Table 1: Interfaced Equipment to 400W Series Unit

Seite 14

400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 8 of 15 2.3 Control, Operating Information See the 400W S

Seite 15 - 3.1 Wire Routing

400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 9 of 15 2.6 Troubleshooting Information If error indicatio

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