Garmin SR02232LA- Manuals

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

Page 5 - INSTRUCTIONS FOR CONTINUED AIRWORTHINESS; STC Rotorcraft Installation

400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 5 of 15 14) TSO: Technical Standard Order 15) BIT: Built In Test 16) TCDS: Type Certificate Data Sheet 17) N/A: Not Applicable 2. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 2.1 Introduction Content, Scope, Purpose...

Page 6 - Description of Alteration

400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 6 of 15 2.2 Description of Alteration The Garmin Model 400W Series GPS/WAAS Nav/Com unit is a 6 ¼ inch wide panel mounted unit with all the interface connections behind the instrument panel. The 400W Series unit...

Page 7 - Table 1: Interfaced Equipment to 400W Series Unit

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 Unit Model ____________________ 400W Series unit P/N ____________________ Manufacturer / Model Location Main NAV Indicator VOR/ILS NAV Indica...

Page 8 - Information

400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 8 of 15 2.3 Control, Operating Information See the 400W Series Installation Manual (P/N 190-00356-02), listed under the reference documentation in paragraph 2.1 of this document, for system operation and self-te...

Page 10 - General Procedural Instructions; GPS 400W Weight (Installed with rack and back plate)

400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 10 of 15 2.8 Diagrams Refer to the 400W Series Installation Manual, P/N 190-00356-02 and STC Rotorcraft Installation Supplement for 400W/500W Series, P/N 190-00357-22 (listed under reference documentation in sec...

Page 11 - Table 3: Unit Location Information; Part and Model

400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 11 of 15 Table 3: Unit Location Information Part and Model Number C.G. Station (inches) Installed Location Description 400W Series Unit GPS Antenna Procedures and data required for wiring maintenance are describ...

Page 12 - Table 4: 400W Series Power Input; Input

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 Input Connector Mode Typical Max Typical Max GPS 400W Main power P4001 -- 760mA 1.4A 410mA 700mA GNC 420W Main power P4001 -- 1.12A 2.5A 560mA 1.2A COM pow...

Page 13 - Table 5: Circuit Breaker Size and Placard; Unit Power; Special Inspection Requirements

400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 13 of 15 Table 5: Circuit Breaker Size and Placard Unit Power Input Placard(s) 14 VDC Breaker Size 28 VDC Breaker Size GPS 400W (P/N 011-01057-00, -10, -40, -50) Main (P4001) 5 A 5 A Main (P4001) 5 A 5 A GNC 420...

Page 14 - Additional Instructions; None; Overhaul Period

400W Series Rotorcraft 190-00356-21 Rev. C Instructions for Continued Airworthiness Page 14 of 15 2.14 Additional Instructions None 2.15 Overhaul Period The system does not require overhaul at a specific time period. Power on self-test and continuous BIT will monitor the health of the 400W Series un...

Page 15 - APPENDIX A

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 depicts the wire harness and coax cable routing for the 400W Series unit(s) and antenna(s) throughout the rotorcraft structure: