Piper SENECA III - Engine Failure with Rear Cabin and Cargo Doors Removed; Electrical Failures

PIPER
AIRCRAFT
CORPORATION SECTION 3
PA-34-220T,
SENECA IH
EMERGENOV
PROCEDURES
Bauert
switch
....
.... . .
.....
OFF
Fuel
selector
..... .. . .
..... ..
,......
OFE
Eauch
down
at
minimum
airspeed.
ENGINE
FAILURE
WITH REAR
CABIN AND CARGO
DOORS3
REMOVED
S.E.
min.
control
speed
of 67
KIAS
for
this configuration.
If airspeed
is
below
67
KlAS
reduce
power
on
operating engine
to
maintain
contro!
ELECTRICAL
FAILURES
ALT
warning
light
illuminated:
Ammeter
Ammeters.......
..
.
...........
check
L & R.check
Electrical
load
,..........
..
..............
reduce
to
minimum
Ahernators..........
.................
OFF.
then
ON
one
at
a
time
ti
alternator
outputs
are
NOT
restored:
Batters
switch
...........
....
..........
OFF
Alternator
switches........
........
OFF,
then
ON
one
at
a
time
li
alternator
outputs
are
NOT
restored:
\\ternator
switches..........
-
, ........
OFF
Baners
switch
..........
...
.....as
required
li
alternator
cannot
be
restored,
reduce
electrical
load
and
land
as
soon as
pracucal.
The
battery
is the
only
remaining
source
of electrical
power.
WARNING
Compass
error may
exceed
10
degrees
with
both alternators
inoperative.
NOTE
If
battery
is depleted,
the landing
gear
must
be
lowered
using
the
emergency
gear
extension
procedure. Gear
position lights
will
be
in-
operative.
ISSCED:
JANUARY
8.
1981
REPORT:
VB-1110
REVISED:
AUGUST 9,
1982
19