Garmin Bell 206, Bell 407 Instruction Manual

G500H Flight Display System

Instructions for Continued Airworthiness

Bell 206A/B Series

Reg. No.____________ S/N_______________

STC SR02295LA

Dwg. Number:

190-01150-11 Rev. 2

Garmin International, Inc.

1200 E. 151st Street

Olathe, Kansas 66062 USA

Record of Revision

Rev. Date Description of Change

1 02/11/10 Initial Release 2 04/12/10 Update to latest installation data revisions; changed VFR placard text;

updated equipment station locations.

INTRODUCTION ................................................................................................................... 3

1.1 Purpose ................................................................................................................. 3

1.2 Scope .................................................................................................................... 3

1.3 Document Control ................................................................................................. 3

1.4 Permission to Use Certain Documents ................................................................. 3

1.5 Definitions ............................................................................................................. 3

2. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS .................................................... 4

2.1 Introduction ........................................................................................................... 4

2.2 Description of Alteration ........................................................................................ 5

2.3 Control, Operating Information ............................................................................. 8

2.4 Servicing Information ............................................................................................ 8

2.5 Periodic Maintenance Instructions ........................................................................ 8

2.6 Troubleshooting Information ................................................................................. 9

2.7 Removal and Installation Information ................................................................... 13

2.8 Diagrams ............................................................................................................... 18

2.9 Special Inspection Requirements ......................................................................... 18

2.10 Application of Protective Treatments .................................................................... 18

2.11 Data Relative to Structural Fasteners ................................................................... 18

2.12 Special Tools ........................................................................................................ 18

2.13 Additional Instructions ........................................................................................... 19

2.14 Overhaul Period .................................................................................................... 19

2.15 ICA Revision and Distribution ............................................................................... 19

2.16 Assistance............................................................................................................. 19

2.17 Implementation and Record Keeping ................................................................... 19

3. AIRWORTHINESS LIMITATIONS ........................................................................................ 19

G500H Flight Display System 190-01150-11 Rev. 2 Instructions for Continued Airworthiness Bell 206A/B Series Page 2 of 19

1. INTRODUCTION

1.1 Purpose

This document is designed for use by the installing agency of the Garmin G500H PFD/MFD System as Instructions for Continued Airworthiness in response to Title 14 CFR Part 27.1529, Part 27 Appendix A.. This ICA includes information required by the operator to adequately maintain the Garmin G500H system installed under STC SR02295LA.

1.2 Scope

This document identifies the Instruction for Continued Airworthiness for the modification of the rotorcraft for installation of the Garmin G500H PFD/MFD System installed under STC SR02295LA.

1.3 Document 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 2.15 for information on how to gain FAA acceptance or approval and how to notify customers of changes.

1.4 Permission to Use Certain Documents

Permission is granted to any corporation or person applying for approval of a Garmin G500H system 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 con strue suitability of the documents. It is the responsibility of the applicant to determine the suitability of the documents for the ICA.

1.5 Definitions

The following terminology is used within this document:

1) ACO: Aircraft Certification Office

2) ADC: Air Data Computer

3) AEG: Aircraft Evaluation Group

4) AHRS: Attitude Heading Reference System

5) CFR: Code of Federal Regulations

6) FAA: Federal Aviation Administration

7) ICA: Instructions for Continued Airworthiness

8) MFD: Multi-Function Display

9) PFD: Primary Flight Display

10) PMI: Principle Maintenance Inspector

11) STC: Supplemental Type Certificate

G500H Flight Display System 190-01150-11 Rev. 2 Instructions for Continued Airworthiness Bell 206A/B Series Page 3 of 19

2. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS

2.1 Introduction

Content, Scope, Purpose and Arrangement: This document identifies the Instructions for

Continued Airworthiness for the modification of the rotorcraft by installation of the Garmin G500H PFD/MFD System.

Applicability: Applies to Bell models 206A, 206A-1 and 206B

rotorcraft altered by installation of the Garmin

G500H PFD/MFD System. Definition of Abbreviations: See Section 1.5 Precautions: None Units of measurement: None Referenced publications:

Additional Maintenance Data: Garmin 190-01150-41 Rev. 2 “INSTALLATION,

Garmin 190-01150-06 Rev. 1 “G500H Rotorcraft

STC Installation Manual” or later FAA Approved

Revisions

Garmin 190-01150-40 Rev. 1 “GENERAL

ARRANGEMENT, G500H SYSTEM, BELL 206 A/B

ROTORCRAFT” or later FAA Approved Revisions

G500H SYSTEM, BELL 206A/B ROTORCRAFT” or

later FAA Approved Revisions

Garmin 005-W0222-00 Rev. 3 “G500H MAIN

WIRE HARNESS ASSEMBLY” or later FAA

Approved Revisions

Garmin 005-W0222-01 Rev. 1 “G500H NAV 1

HARNESS ASSEMBLY” or later FAA Approved

Revisions

Garmin 005-W0222-02 Rev. 1 “G500H GPS 2

HARNESS ASSEMBLY” or later FAA Approved

Revisions

Garmin 005-W0222-03 Rev. 1 “G500H NAV 2

HARNESS ASSEMBLY” or later FAA Approved

Revisions

Garmin 005-W0222-04 Rev. 1 “G500H WX

DATALINK HARNESS ASSEMBLY” or later FAA

Approved Revisions

Garmin 005-W0222-05 Rev. 1 “G500H IRIDIUM

DATALINK HARNESS ASSEMBLY” or later FAA

Approved Revisions

Garmin 005-W0222-06 Rev. 1 “G500H VIDEO

G500H Flight Display System 190-01150-11 Rev. 2 Instructions for Continued Airworthiness Bell 206A/B Series Page 4 of 19

HARNESS ASSEMBLY” or later FAA Approved

Revisions

Garmin 005-W0222-07 Rev. 2 “G500H SERIAL

ALTITUDE HARNESS ASSEMBLY” or later FAA

Approved Revisions

Garmin 005-W0222-08 Rev. 1 “G500H TRAFFIC

HARNESS ASSEMBLY” or later FAA Approved

Revisions Retention: This document, or the information contained within,

will be included in the rotorcraft’s permanent

records.

2.2 Description of Alteration

This STC upgrades existing avionics for the Bell 206A/B rotorcraft as summarized below. The Garmin G500H Flight Display System consists of an instrument panel mounted GDU 620 display

and remote mounted LRUs which provide data to the display. The GDU 620 provides controls for the G500H system and a PFD and MFD in the pilot’s primary field of view. The remote mounted LRUs include one GRS 77H AHRS, one GMU 44 Magnetometer, one GDC 74H ADC, and one GTP 59 OAT probe.

Rotorcraft modified under this G500H STC are restricted to VFR only, including rotorcraft that may not have previously been restricted to VFR. To clarify this operation limitation, a placard with the text, “APPROVED FOR DAY/NIGHT VFR” is required to be in the pilot’s view.

All installed G500H equipment is connected to a power bus that receives power as soon as the battery master switch is turned on.

G500H Flight Display System 190-01150-11 Rev. 2 Instructions for Continued Airworthiness Bell 206A/B Series Page 5 of 19

Separate circuit breakers have been installed in the overhead circuit breaker panel for each for the GDU 620 (PFD), GRS 77H + GMU 44 (AHRS), and GDC 74H (ADC) as circled belo w:

COPILOT

HEADSET

PILOT

HEADSET

FLOATS

XPNDR COMNAV

TURNCABLEHOIST

INDCUTPOWER

OFF

PWR

ADCAHRSPFD

MKR

HAND

AUDIO/

MIKE

CARGO HTR HTR

HOOK CONT PWR

LDG INST PIT

LT LT LT

FUELBOOST

COCK

FUEL

SAS

CONT

INVTR

CAUTIONLTTOT

IND

ENG

FUEL

XMSN

AFT FWD

HYD GOV IGN

BOOST CONT ENG

OFF

POS LT

HTR

START

DIR

GYRO PITOT DEFOG

& ATT HEAT BLOWER

IND

QTY

INST LT

OFF BRT

HEAT

VENT

GEN

OFF

FIELD

OFF

BATOGEN

VALVE

START

ENG

TEMP

INDPRESS

ENG

HEAT

OFF

ANTI

COLL LT

GEN

RESET

OFF

F F

G500H Flight Display System 190-01150-11 Rev. 2 Instructions for Continued Airworthiness Bell 206A/B Series Page 6 of 19

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