Piper Arrow PA-28R-201 Pilot Operating Handbook page 56

SECTION 3
EMERGENCY PROCEDURES
.ii ENGINE POWER
If engine failure was caused
regained after switching fuel tanks untilthe empty fuellines are filled. This
may requireup to ten seconds.
If power is not regained, proceed with the Power Off Landing procedure
(refer to the emergency checklist and paragraph 3.15).
3.13 ENGINE
POWER
Complete engine power loss is usually caused by fuel flow interruption
and power will be restored shortly afterfuel flow is restored. If power
occurs at a low altitude, the first step isto prepare for an emergency landing
(refer to paragraph
maintained.
If altitude permits, switch. the fuel selector to another tank containing
fueL and turn the electricfuel pump
RICH and the alternate air to OPEN.
indication of the cause of the power
indicated, check
containing fuel.
When power is restored move
and turnOFF the electric fuel pump.
If the preceding steps do not restore power, prepare for an emergency
landing.
If time permits, turn the ignition switch to L, then to R, then back to
BOTH. Move the throttleand mixture control levers to different settings.
This may restore power ifthe problem is too rich or too lean a mixture or if
there isa partial fuel system restriction. Try the other fueltank. Water in the
fuel could take some time to be used up, and allowing the
restore power.
may
indicationswillbe normal.
REPORT: VB-1612
342
HB-PQY, Page: 3-12-(0)
DURING
LOSS
by fuel exhaustion, power
IN FLIGUT
LOSS
3.15). An airspeed of at least 79 KIAS
to ON.
the tank selector position to be sure it is on a tank
the alternate air to the CLOSED
If power loss is due to water, fuel flow/pressure
PA-28R-201,
TAKEOPF
(35b) (continued)
(3.Sc)
Move the mixture control to
Check the engine gauges
loss. If no fuel flow/pressure
engine to windmill
ISSUED:
JULY
Issued: JULY 12, 1995
ARROW
will not be
loss
should be
for an
is
position
12, 1995
3-12