LIMITATIONS
FAA
AIRPLANE
O
PERATIONS
MANUAL
1-01-10
Page
8
Code
01
REVISION 41
Copyright © by Embraer. Refer to cover page for details.
MANEUVERING FLIGHT LOAD FACTORS
These corresponding accelerations limit the bank angle during turns
and limit the pull-up maneuvers.
LOAD FACTOR LIMIT FLAPS UP
FLAPS DOWN
(9°,18°, 22° and 45°)
Positive 2.50 g 2.00 g
Negative -1.00 g 0 g
RUNWAY
Runway Slope...............................................................-2% TO +2%
Runway Surface Type...................................................PAVED
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