Garmin GTN 6 series Скачать руководство пользователя страница 18

 

 

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

Page 15 of 21 

190-01007-K9  Rev. 1 

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: 

Table 4. Circuit Breaker Labels 

 

 

GTN INSTALLATION 

LRU

 

POWER INPUT

 

SINGLE

 

DUAL

1

 

GMA 35 

Rotorcraft Power on Connector P3502 

Audio 

GTN 750 

Rotorcraft Power on Connector P1001 

GPS/NAV 

GPS/NAV 1 

Rotorcraft Power on Connector P1004 

GPS/NAV 2 

Rotorcraft Power on Connector P1003 

COM 

COM 1 

COM 2 

GTN 725 

Rotorcraft Power on Connector P1001 

GPS 

GPS 1 

GPS 2 

GTN 650 

Rotorcraft Power on Connector P1001 

GPS/NAV 

GPS/NAV 1 

Rotorcraft Power on Connector P1004 

GPS/NAV 2 

Rotorcraft Power on Connector P1003 

COM 

COM 1 

COM 2 

GTN 635 

Rotorcraft Power on Connector P1001 

GPS 

GPS 1 

GPS 2 

Rotorcraft Power on Connector P1003 

COM 

COM 1 

COM 2 

GTN 625 

Rotorcraft Power on Connector P1001 

GPS 

GPS 1 

GPS 2 

 

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. 

 

 

 

 

 

 

Содержание GTN 6 series

Страница 1: ...EC130 Series as installed in Make and Model Aircraft Reg No ___________ S N __________ Dwg Number 190 01007 K9 Rev 1 Garmin International Inc 1200 E 151st Street Olathe Kansas 66062 USA Record of Revi...

Страница 2: ...ecifications contained herein are the property of Garmin International or its subsidiaries and may not be reproduced or used in whole or in part as the basis for manufacture or sale of products withou...

Страница 3: ...shooting Information 8 2 7 Removal and Replacement Information 8 2 8 Diagrams 18 2 9 Special Inspection Requirements 18 2 10 Application of Protective Treatments 18 2 11 Data Relative to Structural Fa...

Страница 4: ...w 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 Instructions for Continued Airworthiness G...

Страница 5: ...noted references made to the GTN will equally apply to the GTN 625 635 650 725 750 Also GTN 7XX refers specifically to the GTN 725 and GTN 750 and GTN 6XX refers specifically to the GTN 625 GTN 635 an...

Страница 6: ...l for the EC 130 Retention This document or the information contained within will be included in the aircraft s permanent records 2 2 Description of Alteration The GTN navigators are a family of aviat...

Страница 7: ...TN 6XX 7XX PART 27 AML STC SYSTEM MAINTENANCE MANUAL 2 5 Periodic Maintenance The GTN and GMA 35 are designed to detect internal failures A thorough self test is executed automatically upon applicatio...

Страница 8: ...he GMA 35 is installed it must be removed from its rack and the GMA 35 backplate assembly must be removed prior to performing Step 3 When a GMA 35 bonding check is planned perform the GMA 35 bonding c...

Страница 9: ...countersunk fastener heads are in full contact with unit mounting rack holes If a GTN Navigator is installed in the center console inspect the condition of the console and unit install rack around th...

Страница 10: ...dware as follows For antennas that are secured with nuts and bolts clean the fastener hole in the antenna and the underside of the fastener head itself Prep the area underneath the washer on the inner...

Страница 11: ...t skin is not deformed 3 Verify that antenna fasteners are not loose If the aircraft skin is cracked or deformed the internal structure must also be inspected for degradation in the local area Refer t...

Страница 12: ...Instructions for Continued Airworthiness GTN 6XX 7XX Eurocopter EC130 Series Page 9 of 21 190 01007 K9 Rev 1 Figure 1 GTN STC Equipment Fuselage Station Location...

Страница 13: ...on performed in a Eurocopter EC 130T2 Figure 3 depicts a typical installation performed in a Eurocopter EC 130 B4 Figure 4 and Figure 5 show typical circuit breaker installation in EC 130 T2 and EC 13...

Страница 14: ...Instructions for Continued Airworthiness GTN 6XX 7XX Eurocopter EC130 Series Page 11 of 21 190 01007 K9 Rev 1 Figure 2 Typical GTN GMA35 Installation in Eurocopter EC130T2...

Страница 15: ...Instructions for Continued Airworthiness GTN 6XX 7XX Eurocopter EC130 Series Page 12 of 21 190 01007 K9 Rev 1 Figure 3 Typical GTN Installation in Eurocopter EC 130B4...

Страница 16: ...tinued Airworthiness GTN 6XX 7XX Eurocopter EC130 Series Page 13 of 21 190 01007 K9 Rev 1 Figure 4 Circuit Breaker Location in Typical GTN Installation Figure 5 Typical GTN Circuit Breaker Location in...

Страница 17: ...21 190 01007 K9 Rev 1 Figure 6 Typical Circuit Breaker Location in Eurocopter EC130T2 In the EC 130T2 for GTNs mounted in the pedestal the circuit breaker panel is located on top of existing instrumen...

Страница 18: ...orcraft Power on Connector P1001 GPS NAV GPS NAV 1 Rotorcraft Power on Connector P1004 GPS NAV 2 Rotorcraft Power on Connector P1003 COM COM 1 COM 2 GTN 635 Rotorcraft Power on Connector P1001 GPS GPS...

Страница 19: ...Instructions for Continued Airworthiness GTN 6XX 7XX Eurocopter EC130 Series Page 16 of 21 190 01007 K9 Rev 1 Figure 7 EC 130 Series Wire Harness and Coaxial Cable Routing...

Страница 20: ...0 01007 K9 Rev 1 2 7 2 Weight and Balance The weight and moment arm for each piece of equipment for the EC 130 B4 is depicted in Figure 8 The weight and moment arm for each piece of equipment for the...

Страница 21: ...n Requirements If an antenna is replaced under this STC an antenna visual inspection must be performed if there is a suspected lighting strike on the aircraft In the event of a suspected or actual lig...

Страница 22: ...ollow the Garmin ODA Procedures Manual SOP 0055 ACP 0016 for Instructions for Continued Airworthiness The latest revision of this ICA document is available on the Garmin website www flyGarmin com To A...

Страница 23: ......

Страница 24: ...A 1 GTN 6XX 7XX STC Installation Eurocopter EC 130 Series The following diagram must be completed to depict the location of all LRUs and antenna s along with the wire routing for the GTN 6XX 7XX and...

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