Piper SENECA III - Stalls

SECTION
4
PIPER
AIRCRAFT
CORPORATION
NORMAL
PROCEDURES
PA-34-220T,
SENECA
Ill
4.59
STALLS
The
loss
of altitude
during
a
power
off
stall
with
the
gear
and
flaps
retracted
may
be
as
much
as
400
feet.
The
loss
of
altitude
with
the
gear
down
and
40°
of
flaps
may
also be
as
much
as
400
feet.
A
power
on
stall
may
result
in
as
much
as
150 feet
of altitude
loss.
The
stall
warning
system
is
inoperative
with
the battery
switch
OFF.
REPORT:
VB-III0
ISSUED:
AUGUST 17, 1981
4-38