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
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Record of Revision |
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Rev. |
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Description of Change |
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10/24/08 |
Initial Release |
B |
1/28/09 |
Added table for list of interfaced equipment, STC number, and changed |
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document title. |
C |
4/24/09 |
Added STC number and changed revision levels in section 2.1 |
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400W Series Rotorcraft |
190-00356-21 |
Rev. C |
Instructions for Continued Airworthiness |
Page |
2 of 15 |
1. |
INTRODUCTION................................................................................................................... |
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1.1 |
PURPOSE ............................................................................................................ |
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1.2 |
Scope .................................................................................................................... |
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1.3 |
Document Control ................................................................................................. |
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1.4 |
Permission to Use Certain Documents ................................................................. |
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1.5 |
Definitions ............................................................................................................. |
4 |
2. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS .................................................... |
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2.1 |
Introduction ........................................................................................................... |
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2.2 |
Description of Alteration ........................................................................................ |
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2.3 |
Control, Operating Information ............................................................................. |
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2.4 |
Servicing Information ............................................................................................ |
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2.5 |
Periodic Maintenance Instructions ........................................................................ |
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2.6 |
Troubleshooting Information ................................................................................. |
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2.7 |
Removal and Replacement Information ............................................................... |
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2.8 |
Diagrams ............................................................................................................... |
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2.9 |
General Procedural Instructions ........................................................................... |
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2.10 |
Special Inspection Requirements ......................................................................... |
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2.11 |
Application of Protective Treatments .................................................................... |
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2.12 |
Data Relative to Structural Fasteners ................................................................... |
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2.13 |
Special Tools ........................................................................................................ |
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2.14 |
Additional Instructions ........................................................................................... |
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2.15 |
Overhaul Period .................................................................................................... |
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2.16 |
ICA Revision and Distribution ............................................................................... |
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2.17 |
Assistance ............................................................................................................. |
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2.18 |
Implementation and Record Keeping ................................................................... |
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3. |
AIRWORTHINESS LIMITATIONS SECTION....................................................................... |
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APPENDIX A |
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3.1 ......................................................................................................... |
Wire Routing |
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Figure 1: 400W ....................................................................Series Control and Display Layout |
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Table 1: Interfaced ...................................................................Equipment to 400W Series Unit |
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Table 2: Unit Weight .................................................................................................Information |
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Table 3: Unit Location ..............................................................................................Information |
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Table 4: 400W ..............................................................................................Series Power Input |
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Table 5: Circuit ..................................................................................Breaker Size and Placard |
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400W Series Rotorcraft |
190-00356-21 |
Rev. C |
Instructions for Continued Airworthiness |
Page |
3 of 15 |
1. INTRODUCTION
1.1PURPOSE
This document is designed for use by the installing agency of the Garmin Model 400W series GPS/WAAS Nav/Com as Instructions for Continued Airworthiness in response to Federal Aviation regulation (FAR) Part 27.1529, Part 27 Appendix A. The ICA includes information required by the operator to adequately maintain the Garmin Models 400W series installed under Rotorcraft Approved Model List (AML) STC SR02232LA.
1.2Scope
This document identifies the Instruction for Continued Airworthiness for the modification of the rotorcraft for installation of the Garmin Models 400W series GPS/WAAS Nav/Com installed under Rotorcraft Approved Model List (AML) STC SR02232LA.
1.3Document Control
This document shall be released, archived, and controlled in accordance with the Garmin document control system. When this document is revised, refer to Section 2.16 for information on how to gain FAA acceptance or approval and how to notify customers of changes.
1.4Permission to Use Certain Documents
Permission is granted to any corporation or person applying for approval of a Garmin Model 400W series to use and reference appropriate STC documents to accomplish the Instructions for Continued Airworthiness and show compliance with STC engineering data. This permission does not construe suitability of the documents. It is the responsibility of the applicant to determine the suitability of the documents for the ICA.
1.5Definitions
The following terminology is used within this document:
1)AC: Advisory Circular
2)ACO: Aircraft Certification Office
3)AEG: Aircraft Evaluation Group
4)CFR: Code of Federal Regulations
5)DER: Designated Engineering Representative
6)FAA: Federal Aviation Administration
7)IAW: In Accordance With
8)ICA: Instructions for Continued Airworthiness
9)MFD: Multi-Function Display unit
10)PMI: Primary Manufacturing Inspector
11)POI: Primary Operations Inspector
12)STC: Supplemental Type Certificate
13)TC: Type Certification or Type Certificate
400W Series Rotorcraft |
190-00356-21 |
Rev. C |
Instructions for Continued Airworthiness |
Page |
4 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 and Arrangement: |
This document identifies the Instructions for |
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Continued Airworthiness for the modification of the |
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rotorcraft by installation of the Garmin Models |
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400W Series GPS/WAAS Nav/Com. |
Applicability: |
Applies to rotorcraft altered by installation of the |
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Garmin Model 400W Series GPS/WAAS Nav/Com. |
Definition of Abbreviations: |
See Section 1.5 |
Precautions: |
None |
Units of measurement: |
None |
Referenced publications: |
190-00357-22 Rev. C STC Rotorcraft Installation |
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Supplement for 400W/500W Series |
(or later FAA approved revisions) |
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190-00356-02 Rev. G 400W Series Installation |
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Manual |
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005-C0221-02 Rev. 4 400W Series Rotorcraft AML |
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STC Installation Master Data List |
Retention: |
This document, or the information contained within, |
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will be included in the rotorcraft’s permanent |
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records. |
400W Series Rotorcraft |
190-00356-21 |
Rev. C |
Instructions for Continued Airworthiness |
Page |
5 of 15 |
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