Piper SENECA III - Gear-Up Emergency Landing; Engine Failure with Rear Cabin and Cargo Doors Removed; Electrical Failure

SECTION 3
PIPER
AIRCRAFT
CORPORATION
EMERGENOV
PROCEDURES
PA-34-220T,
SENECA
DI
To
execnic
a
manual
extension
of
the
landing
gear,
power
should
be
reduced
to
maintain airspeed
below
85 KlAS.
Place
the
landing
gear
selector
switch
in
the GEAR
DOWN
position
and
pull
the
emergency
gear
exterision
knob.
Check
for 3
green
indicator
lights.
WARNING
ff
the
emergency
gear
extension
knob has
been
pulled
out
to
lower
the
gear
due
to
a
gear
system
malfunction.
lease
the
control
in its
extended
position
until
the
airplane
has
been
put
on
jacks
to
check the
proper
function
of
the
landing
gears
hydraulic
and
electrical
systems.
3.19
GEAR-UP
EMERGENCY
LANDING
An
approach
should
be made
with
power
at
a
normal
airspeed with the
flap
position
to
be
used
at
the
pilot's
discretion. Flaps
up
will reduce
wing
flap
damage.
Close
the throttles
just
before
touchdown.
Turn
OFF
the
battery
and
ignition
switches
and
move
the
fuel
selector
valve
controls
to
OFF.
Contact
to
the
surface should
be
made
at
a
minimum
airspeed.
3.21
ENGINE
FAILURE WITH
REAR
CABIN
AND CARGO DOORS
REMOVED
The
minimum
smgle
engine
control
speed
for
this configuration
is
67
KlAS
If
engine
failure
occurs
at
an
airspeed
below
67
KIAS.
reduce
power
as
necessary
on
the
operating
engine
and apply
rudder
to
maintain
direc-
tional
controL
3.23
ELECTRlCAL
FAILURES
SN
344
I
3300 I
THRU
34-8233205
If
an
ALT
annunciator
light
illuminates,
observe the
ammeters
to
determine
which alternator
is
inoperative.
If
both
ammeters
show
zero
output.
reduce
electrical
loads
to
the
minimum.
Turn OFF
both
abernator
switches
and
then
turn
them
momentarily
ON
one
at
a
time
while
obsen
ing
the
ammeters.
The
alternator
showing the
LEAST
(but
not
Jero)
current
should be
turned
ON
The
other
alternator
should
be left OFF.
Electrical
REPORT:
VB-1110
ISSUED:
JANUARY
8. 1981
3-20
REVISED:
AUGUST
4,
1982