Engine Failure With Rear Cabin And Cargo Doors Removed; Electrical Failures - Piper SENECA III Pilot's Information Manual

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