Instructions for Continued Airworthiness 190-01527-15 Rev 1
for the Garmin G500H Installation in Eurocopter EC130 Page 12 of 82
2. Conduct visual inspection of wires, backshells, and connectors looking for signs of wear,
deterioration or damage. Replace as required.
3. Inspect harness connections in back of unit. Secure any loose connections and support
unsecure wiring harness with additional clamping and / or tie rap supports if required.
4. Inspect unit for security of attachment. Replace the damaged or corroded hardware.
Replace any missing hardware. Torque all screws in accordance with Section 20-10-00
Torques Maintenance Practice.
GMU 44 Magnetometer Installation
1. Access GMU 44 (reference Section 6-00-00- Dimensions and Access). Inspect GMU 44
and mount for physical damage cracks, and corrosion. Treat and repair corrosion as
required in Section 20-40-00 Corrosion Control Maintenance Practices.
2. Conduct visual inspection of wires, backshells, and connectors looking for signs of wear,
deterioration or damage. Replace as required.
3. Inspect hardware. Replace the damaged or corroded hardware. Replace any missing
hardware. Torque all screws in accordance with Section 20-10-00 Torques Maintenance
Practice.
4. Inspect harness connections in back of unit. Secure any loose connections and support
unsecure wiring harness with additional clamping and / or tie rap supports if required.
Shelf Installation
1. Access Shelf Installation (reference Section 6-00-00- Dimensions and Access). Inspect for
physical damage cracks, and corrosion. Treat and repair corrosion as required in Section 20-
40-00 Corrosion Control Maintenance Practices
2. Inspect hardware. Replace the damaged or corroded hardware. Replace any missing
hardware. Torque all screws in accordance with Section 20-10-00 Torques Maintenance
Practice.
GDC 74H ADC Installation
1. Access GDC 74H (reference Section 6-00-00- Dimensions and Access). Inspect GDC 74H
and mount for physical damage cracks, and corrosion. Treat and repair corrosion as
required in Section 20-40-00 Corrosion Control Maintenance Practices.
2. Inspect unit for security of attachment. Replace the damaged or corroded hardware.
Replace any missing hardware. Torque all screws in accordance with Section 20-10-00
Torques Maintenance Practice.
3. Conduct visual inspection of wires, backshells, and connectors looking for signs of wear,
deterioration or damage. Replace as required.
4. Inspect harness connections in back of unit. Secure any loose connections and support
unsecure wiring harness with additional clamping and / or tie rap supports if required.
5. Inspect Pitot-Static System for damage. Replace parts as needed. Complete the 90 Day
Inspection found in Table 5-01.
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