Piper Arrow PA-28R-201 Pilot Operating Handbook page 351

ARROW
PA-28R.201,
SECTION 1 GENERAL
The MFD is intended to be a supplemental display of situational and navigation
information to the pilot. Its primary function is to provide a moving map display
to the pilot for increased situational awareness. The MFD
data from a variety of GPS
thunderstorm detection unit, Engine Sensor Unit, and either the L3 Skywatch
Traffic Advisory
System
Collision Alert Device (TCAD)
groupings of information presented on "Pages".
Figure 2 EX5000
provides the display of the following
The MFD
• Manifold Pressure
•
Engine RPM
•
Engine Oil Temperature
• Engine Oil Pressure
EGT
12, 1995
ISSUED:
JULY
REVISED:
JANUARY
HB-PQY, Page: 9-93-(0)
(continued)
sensors, the BFG
(TAS), Bendix/King
system. The unit is organized around logical
2JO RPN
EGT
11
Iii
I
series 700-00004-OXX-(
9, 2006
Revision: 16, JANUARY 9, 2006
SECTION
SUPPLEMENT
is capable of accepting
WX-500
Stormscope
or the Ryan
TAS,
60 PSI
Electrical
[]
Fuel Quanti
1 R
riri
FW1
Fuel
USEDI
I
Multi-Function Display
)
aircraft parameters:
•
Cylinder Head Temperature
• Aircraft ElectricalStatus
•
Outside Air Temperature
•
Fuel Quantity
Fuel Usage Data
•
REPORT:
3 of 30,
9
16
passive
Traffic and
VB1612
I
9-93
9-93