Digifly FMS50MM, Руководство пользователя

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1.2.2 Mounting ( fmsAT )
1.2.3 Air pressure sensing ( fmsAT )
1.2.4 Electrical supply (fmsAT )
1.2.5 Connection of interface cable fmsAT
The front plate should be perpendicular to ground and also
perpendicular to the airplane main axis. The module should not
receive excessive vibrations from the engine, with peaks not
exceeding 2 G. Front panel mount requires 4 screws brass or stainless
steel, non ferromagnetic.
Connect though a T joint the Static and Dynamic input of fmsAT to the
existing lines. Avoid water entering through the tubing into the
instrument.
The Red (positive) and Black (negative) wires out of the female plug to
fms50 (provided in the installation kit) should be connected to the
same electrical supply of FMS50MM, to switch on simultaneously both
units.
Allow easy accessibility since the same cable is used for downloading
to FMS50MM of the software upgrades.
The system will not provide accurate Pitch and Roll indications with
angles exceeding 60° and in conditions of heavy turbulence or rapid
turns, but will immediately recover proper operation under normal
flight conditions, without any need of re-calibration.
1.2.6 Operative limits ( fmsAT )
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