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

Page 8 of 21 

190-01007-K9  Rev. 1 

Visual Inspection 
(Only if antenna is 
installed by this STC) 

Visual inspection on the antenna 

1.  Clean the antenna with water and mild soap. 
2.  Verify there are no cracks on the antenna and around 

attachment fasteners. 

3.  Verify that all sealing fillets around the antenna are in 

good condition. 

 
If the antenna is broken, cracked, or dented it must be 
replaced. 
 
In the event attachment is not secure, re-attach antenna and 
complete the Electrical Bonding Test. 
 
In the event the antenna seal shows signs of damage, 
complete the Electrical Bonding Test and re-seal the antenna. 
 
Visual inspection of the rotorcraft exterior skin around installed 
antenna - 

1.  Clean the exterior of the aircraft skin within a 10 inch 

radius of the antenna with water and mild soap.   

2.  Inspect aircraft skin around the antenna footprint to verify 

there are no cracks and aircraft 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 to approved method defined in the Standard 
Practices Manual (MTC 20-03-06-407) - Repair of metal 
structures.

 

To be performed 
coincident with 
the Eurocopter 
EC 130 600 flight 
hour inspection 
or every 24 
months, 
whichever 
comes first. 

Perform visual 
inspection in 
event of 
suspected 
lighting strike. 

 

2.6  Troubleshooting Information 

If error indications are displayed on the GTN 6XX or 7XX, consult Section 4, Troubleshooting of the GTN 
6XX/7XX PART 27 AML STC SYSTEM MAINTENANCE MANUAL. Refer to the GTN System 
Configuration and Checkout Log retained in the aircraft permanent records for a list of the interfaced 
equipment and system configuration data. 

2.7  Removal and Replacement Information 

For removal and replacement instructions, refer to the 

GTN 6XX/7XX PART 27 AML STC SYSTEM 

MAINTENANCE MANUAL

 Section 5, Equipment Removal and Replacement. 

2.7.1  Equipment Location and Access 

Figure 2 depicts the typical location for the GTN 6XX/7XX and optional GMA 35. 

 

 

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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