Piper Arrow PA-28R-201 Pilot Operating Handbook page 399

SECTION 9
SUPPLEMENT 18
SECTION 3- EMERGENCY
Aircraft Engine Power
During an engine failure the pilot may electto attempt an engine restart. During
thistime large voltage drops may cause the PFD
During this initialization process the PFD
alignment during flight and therefore the pilot may
attitude and aircraft control using the standby instruments.
• Refer to the
Emergency
• If the PFD
is able to perform fast alignment, when
• Maintain
straight and level flight
• If
engine does not restart, m aintain wings level and appropriate aircraft
speed.
• Press the fasterect button.
• Ifthe PFD
was not able to perform fast alignment, maintain aircraft control
with reference to the standby instruments for aircraft attitudeinformation.
In case of engine failure, minimize
and turn off all non-essential electrical equipment
preserve battery capacity.
If standby
when primary alternator is OFF.
Loss of Fuel Flow
ElectricFuel Pump
Fuel Selector
Engine Driven Fuel Pump
Throttle
ElectricFuel Pump
Throttle
If normal engine operation and fuel flow is not immediately
re-established, the electric fuel pump
The lack of fuel flow indication while the electric pump
on could
exhaustion. If fuel system
selectorto OFF.
REPORT: VB-1612
20 of 36
9-142,
HB-PQY, Page: 9-142-(0)
PROCEDURES
Loss
Section of the Pilot's Operating Handbook.
OR
CAUTION
NOTE
alternator is installed, select it to OFF
Failure
CAUTION
indicate a leak in the fuel system
leak is verified, switch fuel
Revision: 18, MAY 22, 2006
PA-28R-201,
(continued)
to lose power and reinitialize.
not be able to complete a fast
may
have to obtain aircraft
prompted
the use of the starter
Check on tank containing usable fuel
RESET
should be turned OFF.
or fuel
ISSUED:
REVISED:
ARROW
by the PFD:
to
ON
RETARD
ON
as required
is
JULY 12, 1995
MAY 22, 2006
9-142