400W Series Rotorcraft Instructions for Continued Airworthiness as installed in _____________________________ (Make and Model Rotorcraft) Reg. No._
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
400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 11 of 15 Table 3: Unit Location Information Part and Mode
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
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
400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 14 of 15 2.14 Additional Instructions None 2.15 Overhaul
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
400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 2 of 15 This page intentionally left blank
400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 3 of 15 1. INTRODUCTION...
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
400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 5 of 15 14) TSO: Technical Standard Order 15) BIT: Built
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
400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 7 of 15 Table 1: Interfaced Equipment to 400W Series Unit
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
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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