Piper Arrow PA-28R-201 Pilot Operating Handbook page 410

ARROW
PA-28R-201,
7- DESCRIPTION
SECTION
A. PFD
Systems Description (continued)
Engine Instruments
The Entegra PFD provides a display
Oil Pressure (OP), and Fuel Flow (FF) in the upper left hand corner of
(RPM),
the display.
Manifold Pressure
displays engine manifold
Continuously
(In-Hg.). A numeric display below the manifold pressure analog indicator
displays the manifold pressure to the nearest 0.1 In.-Hg. If the manifold
pressure enters the warning
numeric readout will be displayed in the corresponding color.
Tachometer
Continuously displays the current propeller RPM.
analog indicator displays the RPM
the RPM
propeller RPM
numeric readout will be displayed in the corresponding color.
Oil Pressure
Numerically displays oil pressure during engine startin pounds per square
inch (PSI) to the nearest I PSI. The oil pressure indication is removed
minutes afterthe engine oil pressure isoutside the warning (red)range.
Fuel Flow
Continuously displays numeric fuel flow in gallons per
nearest0.1 aPR.
Instruments
Back-up
The Entegra PFD
certain aircraft flight and systems parameters. Back-up
and Attitude instruments are provided to facilitate pilot cross-checking of
PFD
display flightparameters.
heading source.
12, 1995
ISSUED: JULY
MAY
REVISED:
HB-PQY, Page: 9-153-(0)
AND OPERATION
01:
Engine
(red) area, the analog indicator and the
enters the warning (red) area, the analog indicatorand the
system installation includes redundant
The aircraft wet compass
22, 2006
Revision: 18, MAY 22, 2006
SECTION
SUPPLEMENT
(continued)
Pressure, Tachometer
Manifold
pressure in inches of mercury
A numeric display below
to the nearest 10 RPM.
hour (GPH)
means of display of
Altimeter, Airspeed
serves as a back-up
REPORT:
31 of 36,
9
18
If the
3
to the
VB-1612
9-153
9-153