Instruction Manual

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 Replacement
a) GMU 44, Magnetometer
Magnetometer is located in the tail boom between TB 868 and 1578. (Figure 6-01)
Access Methods
i. Removal
1. Un-latch and open the battery door on the left side of the aircraft.
2. If a battery is installed it may be necessary to remove the battery to gain access to
the magnetometer. Consult the manufacturers Installation and removal
instructions for proper removal of unit.
ii. Installation
1. Re-install battery if removed to gain access to the magnetometer. Consult the
manufacturers Installation and Removal instructions for proper installation of unit.
2. Close the battery access door and latch it.
Caution: Use of power tools during removal or installation of
panels and attaching hardware may damage nut plates or
deform holes in composite doors, covers, panels, and fairings.
06-00-00
Figure 6-01
GMU 44
TB
868
REF
TB
1578
REF