Garmin B4- Manuals

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 5 of 82 CHAPTER 4 Section 04-00-00 Airworthiness Limitations There are no additional Airworthiness Limitations as defined in 14 CFR Part 27, Appendix A. A27.4 that result from this ...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 6 of 82 CHAPTER 5 Section 05-00-00 Continued Airworthiness Inspections 1. General This chapter contains time limit intervals for the Component Overhaul Schedule and Scheduled Inspec...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 7 of 82 The G500H Installation has a Post-Lightning Strike Inspection that must be performed in the event of a suspected or actual lightning strike to the aircraft. The Post-Lightni...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 8 of 82 OAT- Outside Air Temperature GTP- Garmin Temperature Probe ADC- Air Data Computer STC- Supplemental Type Certificate AHRS- Attitude Heading Reference System 05-00-00

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 9 of 82 Section 05-20-10 Continued Airworthiness Scheduled Inspections 1. General This section contains requirements for scheduled inspections. Also included is a list of special to...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 10 of 82 discrepancies are not missed. It is important to have adequate lighting for all phases of the inspection . The special tools necessary for the G500H inspection are listed a...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 11 of 82 Table 5-02 -1 year (Annual) Inspection Registration No. Serial No. Helicopter Total Hours 1 Year (Annual) Scheduled Inspection • The 1 Year inspection shall be accomplished...

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...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 13 of 82 GTP 59 OAT Probe Installation 1. Access GTP 59 OAT Probe (reference Section 6-00-00- Dimensions and Access). Inspect GTP 59 OAT and mount for physical damage cracks, and co...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 15 of 82 Table 5-04 -10 Year/2000 Flight Hour Inspection Registration No. Serial No. Helicopter Total Hours 10 Year/ 2000 Flight Hour Scheduled Inspection • The 10 Year/ 2000 Flight...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 16 of 82 GDC 74H ADC 7. Access GDC 74H, (Reference Section 6-00-00 Dimensions and Access) and disconnect all harness connectors. 8. Measure the resistance between the GDC 74H and a ...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 17 of 82 Section 05-20-20 Continued Airworthiness Special Inspections 1. General This section contains requirements for special inspections. Also included is a list of special tools...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 19 of 82 CHAPTER 6 Section 06-00-00 Dimensions and Access 1. Access Methods For removal and installation of specific components, reference Section 31-00-00 Instruments, Removal and ...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 20 of 82 b) GDC 74H, Air Data Computer GDC 74H is located underneath the cabin floor between station 2249 and 2737 on the left side of the aircraft. (Figure 6-02) Access Methods i. ...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 22 of 82 d) Shelf Installation The shelf installation is located underneath the cabin floor between station 2249 and 2737 on the left side of the aircraft. (Figure 6-04) Access Meth...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 25 of 82 g) GDU 620 Installation The GDU 620 is located in the left hand side of the instrument panel (Reference Section 31-00-00 Instruments, Figures 31-08 through 31-11 for specif...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 26 of 82 h) Cooling Fan Installation (If option is installed) The Cooling Fan is located on the forward side of the flight control pedestal (Figure 6-08) Access Methods i. Unlatch a...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 27 of 82 CHAPTER 8 Section 8-00-00 Weight and Balance Information Installation # Description Weight CG Location 190-01527-07 GTP 59 OAT Probe 0.08 lbs STA 2208, WL -2547, BL 7.2 190...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 28 of 82 CHAPTER 11 Section 11-00-00 Placards and Markings 1. Placards and Decals Shelf Installation The Shelf Installation requires one (1) placard that is mounted to the upper sur...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 29 of 82 E.F.I.S. Circuit Breaker Installation Circuit Breaker Installation requires one (1) placard that is mounted to the top of the lower pedestal with three .50 in diameter hole...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 30 of 82 CHAPTER 12 Section 12-00-00 Servicing Maintenance Practices This chapter includes Return-to-Service Practices and Calibration Practices to be used with the G500H Flight Dis...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 31 of 82 Section 12-10-00 Return-to-Service Practices 1. General a) GMU 44 Magnetometer 1. Power up the G500H system with the GDU 620 in normal mode. 2. Verify that the GDU displays...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 32 of 82 Section 12-20-00 Calibration Requirements Condition Calibrations Required GRS 77H Pitch/Roll Offset See Section 5 of the G500H STC Installation Manual GRS/GMU Magnetic Cali...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 34 of 82 Section 20-10-00 Torques Maintenance Practices 1. Torque Wrenches a) Torque Wrench Accuracy Torque wrenches must be of good quality and calibrated at least once a year. Any...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 38 of 82 Section 20-30-00 Painting Maintenance Practices The following procedures should be used to touch-up paint flaking, scratches, nicks, and gouges. Warning: Cleaning solvents ...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 39 of 82 Section 20-40-00 Corrosion Control Maintenance Practices 1. Corrosion Control The G500H mounting components are fabricated primarily of aluminum. All components should be i...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 41 of 82 b) If damage is through the paint surface prepare area for paint touch-up using following methods. Note: On high strength steel, do not use power tools other than a flap br...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 42 of 82 Section 20-90-00 Dye Penetrant Inspection Methods Warning: solvents can cause burns and irritation when it contacts skin; proper gloves should be worn. Vapors are harmful a...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 43 of 82 CHAPTER 31 Section 31-00-00 Instruments 1. Description and Operation The Garmin G500H Flight Display System consists of an instrument panel mounted GDU 620 display and remo...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 44 of 82 a) GMU 44 Magnetometer i Removal 1. Access the GMU 44 magnetometer (reference Section 6-00-00 Dimensions and Access). 2. Unscrew the three screws that hold the GMU 44 to it...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 45 of 82 4. Carefully remove the unit from its mounting location. ii Installation 1. Position the unit and fasten using the four (4) screws. 2. Connect the pitot/static plumbing. 3....

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 46 of 82 3. Visually inspect the connectors to ensure there are no bent or damaged pins. Repair any damage. 4. Connect the connector to the GRS 77H, ensuring that each slidelock is ...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 47 of 82 2. Connect the rear connectors, ensuring that each slidelock is secured on both sides. 3. Set the GDU 620 into place. 4. Install the six mounting screws into the bezel of t...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 48 of 82 3. Disconnect the connectors. 4. Remove the cooling fan. ii Installation 1. Connect the connectors. 2. Set the cooling fan into place. 3. Install the three mounting screws ...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 49 of 82 Figure 31-01 GMU 44 MAGNETOMETER INSTALLATION, EXPLODED VIEW (Reference Table 31-01) 31-00-00

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 51 of 82 Figure 31-02 SHELF INSTALLATION, EXPLODED VIEW (Reference Table 31-02) 31-00-00

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 57 of 82 Figure 31-07 INSTRUMENT PANEL INSTALLATION (Reference Table 31-07) 31-00-00

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 59 of 82 Figure 31-08 INSTRUMENT PANEL ASSEMBLY (Reference Table 31-08) 31-00-00

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 61 of 82 Table 31-10 List of Consumable Materials DESCRIPTION P/N VENDOR/SPECIFICATION THREAD LOCK 242 LOCTITE ADHESIVE 1300L 3M Cleaning cloth, Low-Lint -- Commercial Mineral Spiri...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 62 of 82 4. Troubleshooting guide If error indications are displayed on the GDU 620 display unit, consult the Troubleshooting section contained in Table 31-11. The G500H will displa...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 63 of 82 Problem Cause Solution (valid data is being received on the 429 input port as shown on the GDU 620 PORT MONITORING page) Wrong device is connected to port on GDU 620. Use c...

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 65 of 82 Alert Text Cause Solution FAN 2 FAIL Fan 2 has reported 0 RPM when it was powered with a PW M duty cycle higher than or equal to 10% Inspect the GDU fan for an obstruction....

Instructions for Continued Airworthiness 190-01527-15 Rev 1 for the Garmin G500H Installation in Eurocopter EC130 Page 67 of 82 Alert Text Cause Solution TRAFFIC FAIL The traffic information system has failed. The GDU 620 is not receiving traffic information from the traffic sensor. Verify wiring be...