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190-01277-A3System Maintenance Manual GRA 55/5500 Bell 206 STC
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INFORMATION SUBJECT TO EXPORT CONTROL LAWS
WARNING
CAUTION
NOTE
This document may contain information which is subject to the Export Administration Regulations
(“EAR”) issued by the United States Department of Commerce (15 Code of Federal Regulations (CFR),
Chapter VII, Subchapter C) and which may not be exported, released, or disclosed to foreign nationals
inside or outside of the United States without first obtaining an export license. A violation of the EAR may
be subject to a penalty of up to 10 years imprisonment and a fine of up to $1,000,000 under Section 2410
of the Export Administration Act of 1979. Include this notice with any reproduced portion of this
document.
This information in this document is subject to change without notice. Visit the Garmin web site
(
www.garmin.com) for current updates and supplemental information concerning the operation of
Garmin products.
DEFINITIONS OF WARNINGS, CAUTIONS, AND NOTES
Warnings are used to bring to the installer’s immediate attention that not only
damage to the equipment but personal injury may occur if the instruction is
disregarded.
Cautions are used to alert the individual that damage to equipment may result
if the procedural step is not followed to the letter.
Notes are used to expand and explain the preceding step and provide further
understanding of the reason for the particular operation.
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Table A-3. Weight and Balance Details .............................................................................. A-5
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1INTRODUCTION
1.1Purpose
This document provides Instructions for Continued Airworthiness in compliance with requirements of 14
CFR §27.1529, and Part 27 Appendix A. This ICA is to be used by the agency installing the Garmin GRA
55/5500 radar altimeter system under the GRA 55/5500 STC. This document includes information
required by the operator to adequately maintain the Garmin GRA55/5500 system as installed by this STC.
1.2Scope
This document provides Instructions for Continued Airworthiness for the Bell 206B, 206L, L-1, L-3, and
L-4 rotorcraft, modified by the installation of the Garmin GRA 55/5500 STC.
1.3Document Control
This document is released, archived, and controlled in accordance with the Garmin document control
system.
1.4Permission to Use Certain Documents
Permission is granted to any corporation or person to use GRA 55/5500 STC documents to accomplish the
Instructions for Continued Airworthiness and show compliance with STC engineering data when applying
for approval. 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. ACO:Aircraft Certification Office
2. AEG:Aircraft Evaluation Group
3. AGL:Above Ground Level
4. BIT:Built-In Test
5. CFR:Code of Federal Regulations
6. FAA:Federal Aviation Administration
7. FMCW: Frequency Modulated Continuous Wave
8. FOD:Foreign Object Damage
9. ICA:Instructions for Continued Airworthiness
10. LRU:Line Replaceable Unit
11. NAV:Navigation
12. ODA:Organization Designation Authorization
13. PMI:Principal Maintenance Inspector
14. POI:Principal Operations Inspector
15. RX:Receive
16. STC:Supplemental Type Certificate
17. TSO: Technical Standard Order
18. TX:Transmit
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1.6 Terminology
Except where specifically noted, references made to the ‘GRA’ will equally apply to the GRA 55 and GRA
5500 radar altimeters.
Also, except where specifically noted, references made to the ‘Bell 206L Series’ will apply equally to the
Bell 206L, Bell 206L-1, Bell 206L-3, and Bell 206L-4 models.
1.7 Publications
Content, Scope, Purpose and Arrangement:This document identifies the Instructions for Continued
Airworthiness for the modification of the aircraft by the installation of the Garmin GRA 55/5500 Part 27
STC.
1.7.1Applicability
Applies to aircraft altered by the installation of the Garmin GRA 55/5500 Part 27 STC.
1.7.2Definition of Abbreviations
See Section 1.5 and Section 1.6.
1.7.3Precautions
None.
1.7.4Units of measurement
None.
1.7.5Referenced publications (or their later revisions)
1. Bell Model 206B Maintenance Manual, Bell Document BHT-206B-MM, Revision 12, 1 June
2012
2. Bell Model 206L Maintenance Manual, Bell Document BHT-206L-MM, Revision 36, 1 June 2012
3. Bell Model 206L1 Maintenance Manual, Bell Document BHT-206L1-MM, Revision 33, 1 June
2012
4. Bell Model 206L3 Maintenance Manual, Bell Document BHT-206L3-MM, Revision 19, 1 June
2012
5. Bell Model 206L4 Maintenance Manual, Bell Document BHT-206L4-MM, Revision 16, 1 June
2012
6. Structural Repair Manual for Bell Model 206 Series Helicopters, BHT-206-SRM-1, Revision 1,
April 1995
7. Electrical Standard Practices Manual for all Bell Helicopter Commercial Products, BHT-ELECSPM, Revision 2, July 2012
1.7.6Retention
This document, or the information contained within, will be included in the aircraft’s permanent records.
190-01277-A3System Maintenance Manual GRA 55/5500 Bell 206 STC
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2 SYSTEM DESCRIPTION
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2.1 Description of Alteration
This STC upgrades the existing functionality of the Bell 206B, 206L series aircraft avionics system as
summarized below.
The GRA 55/5500 radar altimeter system features: two antenna architecture for transmitting and receiving
radio waves for altitude quantities, remote mounted LRU transceiver for quantifying Above Ground Level
(AGL) altitude information, and interface capabilities to the existing aircraft G500H Flight Deck System
(FDS) for pilot display of aircraft altitude and system degraded warnings. The GRA 55/5500 radar
altimeter may also integrate with an installed Garmin GTN 6XX/7XX for the purpose of providing the
optional 50 ft callout as part of optional HTAWS functionality.
The GRA 55/5500 LRU which is 3.99"x3.02"x11.62" mounted, is located on the supplied mounting rack
that is electrically bonded to the avionics shelf. The two approved radar altimeter antennas are optimally
located on the underside of the tailboom, separated by a minimum distance of 20" on center using
approved antenna mounts installed via STC SR09598RC, STC SR02162LA or other mounting provisions
that are compatible with the approved radar altimeter antennas. The system requires a 5 Amp minimum
circuit breaker installed on the overhead panel to supply power.
2.2 Block Diagram
Figure 2-1. GRA 55/5500 Block Diagram
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3 GRA 55/5500 CONTROL AND OPERATION
NOTE
3.1 Control, Operating, and Testing Information
The GRA 55/5500 is a fully automated, remote-mounted LRU which requires no user controls or inputs.
The GRA 55/5500 displays the radar altitude height above ground level on compatible display systems.
Radar altitudes will be displayed ranging from ground level to 2550ft AGL.
The GRA 55/5500 has a built-in self-test (BIST/BITE) and fault logging functionality which includes
automated self-test and fault detection monitoring of the entire internal TX and RX circuitry. This feature
occurs every time the unit power is cycled and subsequently every minute during normal operation at
calculated altitudes ranging from 250ft to 2550ft AGL and during “No Computed Data” (NCD) conditions.
The GRA 55/5500 will encounter NCD conditions; at actual altitudes above 2550ft AGL, during excess
pitch or roll maneuvering, or anytime the ground reflection is poor.
3.2 Downloading and Installing the GRA 55/5500 Retrofit Installation Tool
GRA 55/5500 configuration, calibration, diagnostics, and software upgrades are performed using a
personal computer (installed with Microsoft Windows XP Service Pack 3 or later) and the GRA 55/5500
Retrofit Installation Tool, Garmin part number 006-A0451-00. The tool is available for download from the
Dealer Resource Center portion of the Garmin website (www.garmin.com). See the accompanying
“readme” file in the tool’s installation directory for the latest instructions.
A standard USB-A plug to USB-B plug commercial cable (not provided) is required to
interface between a personal computer USB-A receptacle and the GRA 55/5500 USB-B
receptacle installed in the wiring harness. This dongle cable is required to use the GRA
55/5500 Retrofit Installation Tool.
Installation
1. Once downloaded, launch the installation file from the directory in which it is stored (or use the
web browser’s download shortcuts).
2. The GRA 55/5500 Retrofit Installation Tool Setup Wizard will begin.
3. Click “Next” as prompted by the setup wizard, and adjust any settings (e.g. installation directory)
as needed.
4. The last screen of the setup wizard will show “Installation Complete.” Click the “Close” button to
close the setup wizard.
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3.3 Using the GRA 55/5500 Retrofit Installation T ool
Once the GRA 55/5500 Retrofit Installation Tool has been installed:
1. Connect the PC to the GRA 55/5500
2. Start the GRA 55/5500 Retrofit Installation Tool from the provided “Start Menu” shortcut, or
launch the application from its program folder
3. Power-up the GRA 55/5500 by applying aircraft power
4. The connection status in the lower, right-hand corner of the GRA 55/5500 Retrofit Installation
Tool will transition from “Not Connected,” to “Connected.”
5. If the GRA 55/5500 Retrofit Installation Tool does not display “Connected” in the lower, righthand corner, check the installation and make sure the GRA 55/5500 has been powered-up and that
the USB cable is properly connected to the PC.
If the PC displays a “Found New Hardware” wizard, the GRA 55/5500 Retrofit Installation Tool was not
able to automatically install the device driver. It may be necessary to manually install the device drivers.
Copies of the drivers’ “.inf” and “.dll” files are located in the target installation directory selected during
installation. Consult the PC’s operating system documentation on manually installing drivers.
3.4 Installation Tool Pages
The Installation Tool contains five tabbed pages, all of which can be useful in troubleshooting a problem.
The pages are: Status, Configuration, Software, Diagnostics, and Utilities (See Figure 3-1).
Figure 3-1. Installation Tool Page Tabs
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3.4.1Status Page
The status page (Figure 3-2) is displayed by selecting the Status tab. This page provides the basic fault
status of the unit. During normal operation, the status of each fault should indicate “normal.” If the unit
indicates a fault, the fault’s entry on the list is displayed in a bold, red font. The status also updates to show
the specific failure under that fault. Table 5-1 identifies the various unit faults that can be encountered
during normal operation of the GRA 55/5500. Use Table 5-1 as a reference to determine the proper actions
to take after a fault has been identified.
Figure 3-2. Status Page
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