Piper SENECA III - Landing Gear Unsafe Warnings; Manual Extension of Landing Gear; Gear up Landing

SECTION 3
PIPER
AIRCRAFT
CORPORATION
EMERGENCY
PROCEDURES
PA-34-220T, SENECA Ill
CAUTION
Actuate
the auxiliary
fuel
pumps
if
vapor
suppression
is
required
(LO
position)
or
the
engine
driven
fuel
pump
fails
(H1 position).
The
auxiliary
fuel
pumps
have
no
standby
function.
Actuation
of
the
Hl
switch
position
when
the
engine
fuel injection
system
is func-
tioning
normally
may cause
engine roughness
due
to
excessively
rich
fuel
air mixture.
LANDING
GEAR
UNSAFE
WARNINGS
Red
light
indicates
gear
in
transit.
Recycle
gear
if
indication continues.
Light
will
illuminate
when
gear
warning
horn
sounds
at
low
throttle settings.
MANUAL
EXTENSION
OF
LANDING
GEAR
Check
following
before
extending
gear
manually:
Circuit
breakers
- -
- - - - -
-
- - - - - - . . .
.
.
.
. . .
.
. . . .
,
check
Battery
switch
..........
..........
ON
Alternators..........
.
...........check
Navigation
lights
. . . , , , .
. . . . . . . . . .
.
. .
OFF
(daytime)
To
extend.
reposition clip
downward
clear
of
knob
and
proceed
as
follows:
Airspeed
........... .
..........
reduce
(85
KIAS
max.)
Gear
selector
..........
.........
GEAR
DOWN
LOCKED
position
Emerg.
gear
extend knob
...........
...........,
pu]\
Indicator
lights
..............
.... ... ..........
3
green
Leave
emergency
gear
extension
knob
out.
GEAR UP
LANDING
Approach
...........
..........
Normal
Flaps...........
..........
as
desired
Throttles.........
...........closed
prior
to
touchdown
REPORT:
VB-Il10
ISSUED:
JANUARY
8,
1981
3-8
REVISED:
APRIL 9, 1982