Piper Arrow PA-28R-201 Pilot Operating Handbook page 34

ARROW
PA-28R-201,
2.7
POWER PLANT
(a) Number of Engines
(b) Engine Manufacturer
(c) Engine Model No.
(d) Engine Operating Limits
(1) Maximum
(2) Maximum
(3) Maximum
(e) Oil Pressure
Minimum
(red line)
Maximum
(f) Fuel Flow/Pressure
Maximum
(g) Fuel Grade (minimum
of Propellers
(h) Number
(I) Propeller Manufacturer
Propeller Hub and Blade Model
)
(1) McCauley
(2) Hartzell
(k) Propeller Diameter
(1) McCauley
Minimum
Maximum
(2) Hartzell
Minimum
Maximum
(1) Blade Angle Limits
(1) McCauley
Low Pitch Stop
High Pitch Stop
(2) Hartzell
Low Pitch Stop
High Pitch Stop
(m) RPM Restriction
(McCauley
ISSUED: JULY
12,1995
HB-PQY, Page: 2-3-(0)
LIMITATIONS
Horsepower
Rotation Speed (RPM)
Oil Temperature
(redline)
(red line)
octane)
Propeller Only)
LIMITATIONS
21.4 GPHII2
Aviation Grade
McCauley
B2L)34C213190DHA-16
HC-C2YK-1(
Avoid continuous
operation between
1500 and 1950 rpm
below 15 inches
manifold pressure.
REPORT:
Issued: JULY 12, 1995
SECTION 2
Lycoming
10-360-C 1C6
200
2700
245°F
25 PSI
100 PSI
PSI
100 or IOOLL
I
or Hartzell
)F/
F7666A-2R
73
74
72
74
12.5 + 0.2°
27.5 0.5°
+
14.0 02°
+
29.0 ÷ 2.0°
VE-1612
2.3
2-3