Piper SENECA III - Page 307

PIPER
AIRCRAFT
CORPORATION
SECTlON 9
PA-34-220T,
SENECA
III
SUPPLEMENT
7
OFF
or
if there
is
an
electrical
system
failure,
the
slave engine will
return to
the
controlled
selected
RPM plus
approximately
25
RPM
"out
of
syn-
chronization"
regardless
of
the
position of
the synchrophaser switch.
SECTION 5
-
PERFORMANCE
No
changes
to
the
basic
perforrnance
provided
by
Section
5
of this
Pilot's Operating
Handbook
are
necessary
for
this
supplement.
ISSUED:
JANUARY 8,
1981
REPORT:
VB-1110
3
of
4,
9-57