Piper SENECA III - Page 299

PIPER
AIRCRAFT
CORPORATION
SECTION
9
PA,34-220T,
SENECA
III
SUPPLEMENT 6
SECTION 3
-
EMERGENCY
PROCEDURES
The
malfunction
of
any
required
deice
equipment requires
immediate
action
to
avoid
icing
conditions,
ENGINE
FAILURE
IN
IClNG CONDITIONS
Select
alternate
air
and
attempt
restart,
If unable
to
restart
engme.
Inop.
prop
.......-----.
.
............feather
Airspeed..........
.
....
....
...........
..atorabove92KIAS
Descend
if
necessary
to
maintain
airspeed.
Electrical
load
............. .
.......
. . ...........
reduce
Avoid
further
icing
conditions
if possible.
Land
as
soon
as
practical
Maintain
at
least
89
KIAS
on
finaL
Do
not
extend
gear
or
lower
flaps
until
certain
of making
field.
Flaps...........
.
. . .
...........25°
ALTERNATOR
FAILURE IN
ICING
CONDITIONS
Alternator
switches....
--... .... . . .
--..........
OFF
then ON
Circuit breakers.
. . . .
.
.
.
.
.
.
. .
. . . . .
.
. .
.
.
.
. .
. .
.
check
and
reset
lf
unable
to
restore
alternator:
Avionics
..................
............
all
off
except
Nav Comm
and
Transp.
Electric
wipdshield
..............
............
OFF
to
maintain
65A
load
If
icing
continues,
terminate
flight
as
soon
as
practical.
Prior
to
landing:
Electric
windshield
.
. . . .
. . . .
. . .
.
.
. . . .
.
. . . . . .
.
ON
if
necessary
Gear
may
require
free
fall
extension.
WING-TAIL
DEICER
PANEL
LIGHT
If
light
is
illuminated
more
than
20
seconds
pull
surface
deice
circuit
breaker.
ISSUED:
JANUARY
8,
1981
REPORT:
VB-1110
REVISED:
AUGUST 17,
1981
7
of 10, 9-51