Garmin Software Version 0857.09 Manual de Instruções Página 59

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G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 6-5
190-01180-02 Revision 3
6.6 GMU 44 REMOVAL & REPLACEMENT
Removal:
1. Make sure all airplane electrical power is disconnected.
2. For airplanes with long range fuel tanks -Remove the left wing tip by unscrewing
the phillips screws. For airplanes with standard fuel tanks - Remove the square
access panel (left wing top).
3. Unscrew the three screws that hold the GMU 44 to its mounting rack.
4. Carefully lift the GMU 44 from its mounting rack.
5. Disconnect the airplane harness connector from the GMU 44 electrical connector.
6. Place protective caps on the GMU 44 connector and on the harness connector.
7. Remove the unit from the airplane.
Reinstallation:
1. Remove the protective caps from the GMU 44 electrical connector and its associated
airplane harness connector. Visually inspect the electrical connectors to make sure there
are no bent or damaged pins. Repair any damage.
2. Connect the airplane harness connector to the GMU 44 electrical connector.
3. Lower the GMU 44 into the locator pins on the mounting rack. Make sure the GMU 44
direction arrow aligns with the mounting rack direction arrow.
CAUTION
It is recommended that new screws are used to secure the GMU 44 to
the mounting rack. If the original screws must be re-used, coat the screw
threads with Loctite 242 (blue) thread locking compound to restore their
anti-rotational properties.
Securing screws MUST be non-magnetic.
4. Secure the GMU 44 to the mounting rack with three phillips screws.
5. Make sure the location of the electrical connector and the routing of the associated
electrical wire harness are as noted in the removal process.
6. Make sure all tools and equipment are removed from the area.
7. For airplanes with long range fuel tanks -Install the left wing tip. For airplanes with
standard fuel tanks - Install the square access panel (left wing top).
8. Proceed to Section 8 for checkout.
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