Power Plant Limitations - Arrow PA-28R-201 Pilot's Operating Handbook And Faa Approved Airplane Flight Manual

PIPER AIRCRAFT CORPORATION
PA-28R-201, ARROW
2.7 POWER PLANT LIMITATIONS
(a) Number of Engines
(b) Engine Manufacturer
(c) Engine Model No.
(d) Engine Operating Limits
(1) Maximum Horsepower
(2) Maximum Rotation Speed (RPM)
(3) Maximum Oil Temperature
(e) Oil Pressure
Minimum (red line)
Maximum (red line)
(t) Fuel Flow/Pressure
Maximum (red line)
(g) Fuel Grade (minimum octane)
(h) Number of Propellers
(i) Propeller Manufacturer
(j) 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 Propeller Only)
ISSUED: SEPTEMBER 15, 1988
SECTION 2
LIMITATIONS
1
Lycoming
IO-360-CIC6
200
2700
245°F
25 PSI
100 PSI
21.4 GPHl12 PSI
100 or 100LL
Aviation Grade
1
McCauley or Hartzell
B2D34C213/90DHA-16
HC-C2YK-l(
)FI
F7666A-2R
73
74
72
74
12.5 + 0.2°
27.5 + 0.5°
14.0
+
0.2°
29.0+ 2.0°
Avoid continuous
operation between
1500 and 1950 rpm
below 15 inches
manifold pressure.
REPORT: VB-1365
2-3