AIRPLANE
FLIGHT
LIMITATIONS
ANAC APPROVED 2-10
REVISION 15 code 03 Page 3
Copyright © by Embraer. Refer to cover page for details.
MANEUVERING SPEED (V
A
)
EM170AOM020014D.DGN
45000
40000
35000
30000
25000
20000
15000
10000
5000
0
ALTITUDE − ft
200 210 220 230 240 250 260 270 280 290 300
AIRSPEED − KIAS
M
MO
= 0.82
V
A
NOTE: Maneuvers that involve angle of attack near the stall or full
application of rudder, elevator, and aileron controls should be
confined to speeds below V
A
. In addition, the maneuvering
flight load factor limits, presented in this Section, should not be
exceeded.
CAUTION: RAPID AND LARGE ALTERNATING CONTROL INPUTS,
ESPECIALLY IN COMBINATION WITH LARGE
CHANGES IN PITCH, ROLL, OR YAW (E.G. LARGE SIDE
SLIP ANGLES) MAY RESULT IN STRUCTURAL
FAILURES AT ANY SPEED, EVEN BELOW V
A
.