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船舶用GPSシステム Garmin GNS 530WのPDF 取扱説明書をオンラインで閲覧またはダウンロードできます。Garmin GNS 530W 23 ページ。 For continued airworthiness bell 206b
Garmin GNS 530W にも：パイロット・マニュアル補遺 (24 ページ), パイロット・マニュアル補遺 (50 ページ), パイロット・マニュアル補遺 (50 ページ), パイロット・マニュアル補遺 (24 ページ), 補足マニュアル (12 ページ), クイック・リファレンス (23 ページ), クイック・リファレンス (25 ページ)

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[3] The lateral arm is measured in terms of the butt line (BL). The centerline of the helicopter is BL0.00.

The moment arms to the left side (looking forward) are negative (-) and the moment arms to the right

side are positive (+).

[4] Location of the 500W Series unit and GPS antenna may vary slightly depending whether or not a

dual navigator system is installed.

2.3 Control, Operating Information

See the Pilot's Guides or the 500W Rotorcraft STC Installation Manual for system operation and self-test

information. The 500W Rotorcraft STC Installation Manual is listed under the reference documentation in

paragraph 2.1 of this document, and the Pilot's Guides are listed in the related documents section of the

500W Rotorcraft STC Installation Manual.

2.4 Servicing Information

None. In the event of system failure, troubleshoot the 500W Series unit in accordance with Section 2.6.

2.5 Periodic Maintenance Instructions

The 500W Series units are designed to detect internal failure. A thorough self-test is executed

automatically upon application of power to the units, and built-in test is continuously executed. Detected

errors are indicated on the equipment via failure annunciations.

Maintenance of the components installed by this STC is on condition, except as noted in the following

table.

Item

Interval

500W Series

12 Months

Unit

500W Series

12 Months

Mounting Rack

500W Series

Instructions for Continued Airworthiness Bell 206B

Table 1 Periodic Maintenance Inspections

Description/Procedure

Conduct a visual inspection (look for signs of wear, deterioration,

or damage to wires, backshells, or connectors) of the 500W

Series unit and wiring harnesses to ensure installation integrity:

1. Inspect the unit for security of attachment.

2. Inspect all knobs and buttons for legibility.

3. Inspect condition of wiring, routing and

attachment/clamping.

4. Inspect related antennas for proper sealing and attachment.

5. Inspect integrity of shield terminations.

6. Inspect for signs of corrosion on equipment, racks and it's

backplates and rack mounting.

Inspect the mounting rack for any signs of excessive wear,

corrosion, or damage. Check mounting rack corners for cracks.

Check integrity of connector plate attachment to the back of

mounting rack. Check the tightness of fasteners attaching

mounting rack to rotorcraft structure and re-torque 12 to 15 in-lbs

if required.

Replace unit mounting rack if any damage has been found.

190-01226-03 Rev. 5

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