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english - Anac

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EMBRAER 30 March 2012 EA-2005T13-16 Sheet 21/30<br />

DATA PERTINENT TO ALL MODELS 190-200<br />

DATUM A perpendicular plane to the fuselage centerline, located at<br />

15 256 mm ahead of the wing stub front spar. This spar is<br />

located 414 mm ahead of the wing jack point.<br />

LEVELING MEANS Plumb line between the points P1 to P2 located inside the<br />

landing gear compartment on the left side, as illustrated below.

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