EasyManua.ls Logo

Embraer 190 - Page 333

Embraer 190
484 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
PERFORMANCE
AIRPLANE
FLIGHT
MANUAL
5-01
CTA APPROVED
Page 18 code 01
ORIGINAL
AFM-1912
TAKEOFF MAXIMUM STOPPING MARGIN
The use of minimum V
1
has long been understood to be a valuable aid
in the prevention of rejected takeoff (RTO) overrun accidents. The
minimum V
1
provided by the CAFM will be the lowest V
1
for the
RTOW. As such, it will provide the greatest margin between the
accelerate-stop distance available and the accelerate-stop distance
required. For airplanes with relatively low ground minimum control
speeds, the lowest permissible V
1
may be as such as 40 knots below
the rotation speed, V
R
. This puts the pilot into a position of having to
continue a takeoff following an engine failure at a very low speed.
The input parameters provided in boxes “Maximum stopping margin”
and “Maximum difference between V
1
and V
R
” are intended to allow
the airline user to take advantage of the benefits provided by the use
of minimum V
1
while at the same time reducing the exposure time
between V
1
and V
R
to suit his needs.
As actual takeoff weight is reduced below the field length limited
weight (FLLW) there is a range of V
1
speeds defined by V
1
MIN and V
1
MAX. The greatest stopping margin is provided when V
1
= V
1
MIN. At
relatively low actual takeoff weights the stopping margin provided by
V
1
MIN may be much greater than the required to provide reasonable
protection for an RTO overrun. There is a corresponding large
exposure time between V
1
and V
R
where a takeoff would have to be
continued following an engine failure.
Maximum difference between V
1
and V
R
(!V) allows the user to limit
the calculation of V
1
MIN as follows: as actual takeoff weight is
reduced below the FLLW the calculation of V
1
MIN proceeds normally;
at the point where V
1
MIN is equal to V
R
!V, then the calculation of
V
1
MIN is governed by the specified speed difference.
Maximum stopping margin allows the user to limit the calculation of
V
1
MIN as follows: as actual takeoff weight is reduced below the
FLLW, the calculation of V
1
MIN proceeds normally; at the point where
the specified stopping margin is reached, the calculation of V
1
MIN is
governed by the stopping margin, i.e., V
1
MIN is increased in order to
keep the stopping margin. V
1
MIN will not be allowed to be greater
than V
1
MAX (V
R
or V
MBE
).

Table of Contents

Related product manuals