Landing; Engine Driven Fuel Pump Failure - Piper SENECA III Pilot's Information Manual

PIPER AIRCRAFT
CORPORATION
SECTION
3
PA-34-220T, SENECA Ill
EMERGENCV
PROCEDURES
Fuel
selector
inop. engme
. . . . .
OFF
Aux.
'uel
pumps
. ..
.'.
OFF
When
using
fuel from
tank on the side opposite the operating engine.
Fuel
selector
operating
engine
........... ...........
CROSSFEED
Fuel
selector
inop. engine
...........
...........
OFF
Aut
fuel pumps.............
..........
OFF
Use
crossfeed
in level
cruise flight only.
NOTE
Do
not crossfeed with full fuel
on same
side as
operating engine
since
vapor
return
fuel flow
will
be
lost
through the vent system
LANDlNG
Fuel
selector
operating engine
. . . . . . .
.
.
. . , ,
.
..
.
.
.
,
ON
Fuel
selector inop,
engme
............. . ...........
OFF
ENGINE DRIVEN FUEL PUMP FAILURE
Throttle
.........
...........
retard
Aux
fuel
pump...........
.
.........unlatch,
on
HI
Throttle
.........
...........reset (7596
power
or below)
CAUTION
If
normal
engine operation and fuel
flow is
not
immediately
re-established,
the
auxiliary
fuel
pump
should
be
turned
off.
The
lack of
a
fuel
flow indication while
on the
Hl
auxiliary
fuel
pump position
could indicate
a leak in the
fuel
system,
or
fuel
exhaustion.
ISSUED:
JANUARY 8, 1981
REPORT: VB-Ill0
REVISED:
APRIL 9, 1982
3-7