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カーナビゲーションシステム Garmin GTN 6 series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 GTN 6 series 24 ページ。 Instructions for continued airworthiness for md 369e; md 369f; md 369ff
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panel, the circuit breaker panel is located in the cargo area and tail boom, as shown in Figure 6. In the EC

130 B4, the circuit breakers for the GTN 6XX are located on top of instrument panel support, or the right

hand side of the pedestal as shown in Figure 5.

Equipment circuit breaker placards are labeled as follows:

LRU

GMA 35

GTN 750

GTN 725

GTN 650

GTN 635

GTN 625

1. Dual installation labeling applies to GTN LRUs only

The GTN and optional GMA 35 wiring harness power and switch connections are routed as shown in

Figure 4. Since the GTNs may be interfaced with preexisting GPS antennas, coaxial wire routing may

differ slightly from the depicted figure. Refer to the aircraft wire routing worksheets and equipment

location forms that were filled out during initial GTN/GMA 35 installation for additional details.

GTN/GMA 35 installation racks, back plates, and wiring harnesses may be accessed by removing the

GTN LRUs as specified in GTN 6XX/7XX PART 27 AML STC SYSTEM MAINTENANCE MANUAL

Section 5, Equipment Removal and Replacement.

Instructions for Continued Airworthiness GTN 6XX/7XX - Eurocopter EC130 Series

Page 15 of 21

Table 4. Circuit Breaker Labels

POWER INPUT

Rotorcraft Power on Connector P3502

Rotorcraft Power on Connector P1001

Rotorcraft Power on Connector P1004

Rotorcraft Power on Connector P1003

Rotorcraft Power on Connector P1001

Rotorcraft Power on Connector P1004

Rotorcraft Power on Connector P1003

Rotorcraft Power on Connector P1001

Rotorcraft Power on Connector P1003

Rotorcraft Power on Connector P1001

GTN INSTALLATION

SINGLE

DUAL

Audio

GPS/NAV 1

GPS/NAV

GPS/NAV 2

COM 1

COM

COM 2

GPS 1

GPS

GPS 2

GPS/NAV 1

GPS/NAV

GPS/NAV 2

COM 1

COM

COM 2

GPS 1

GPS

GPS 2

COM 1

COM

COM 2

GPS 1

GPS

GPS 2

190-01007-K9 Rev. 1