SECTION
2
PIPER
AIRCRAFT
CORPORATION
LIMITATIONS
PA-28R-201T,
CHEROKEE
TURBO
ARROW III
2.5 AIRSPEED
INDICATOR
MARKINGS
MARKING
IAS
Red Radial Line
(Never
Exceed)
183
KTS
Yellow Arc
(Caution Range
-
Smooth Air Only)
146 KTS
to
183 KTS
Green Arc (Normal Operating Range)
63 KTS
to
146 KTS
White Arc
(Flap Down)
56 KTS
to
103 KTS
2.7 POWER PLANT LIMITATIONS
(a)
Number
of
Engines
1
(b)
Engine Manufacturer
Teledyne Continental
(c)
Engine Model No.
TSIO-360-F
(d)
Engine Operating Limits
(1)
Maximum Horsepower
200
(2)
Maximum
Rotation Speed
(RPM)
2575
(3)
Maximum Manifold
Pressure
(In. Mercury)
41
(4)
Maximum
Oil Temperature
240°F
(e)
Oil
Pressure
Minimum
(red
line)
10 PSI
Maximum
(red
line)
100
PSI
(f)
Fuel
Pressure
Maximum
(red
line)
19
PSI
(g)
Fuel
Grade
(niittinium
octane)
100LL
-
Blue or
100/130
-
Green
(h)
Number
of
Propellers
1
(i)
Propeller
Manufacturer
Hartzell
(j)
Propeller
Hub
and Blade Model
BHC-C2YF-lBF/F8459A-8R
(k)
Propeller
Diameter
Minimum
76
IN.
Maximum
75
IN.
(1)
Blade
Angle Limits
Low Pitch Stop
14.2
±
.2°
High
Pitch
Stop
29 ± 1°
REPORT:
VB-800
ISSUED: DECEMBER
20,
1976
2-2
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