Airspeed Indicator Markings; Power Plant Limitations - Piper CHEROKEE WARRIOR II Information Manual

SECTION 2
LTh1ITATIONS
25
AIRSPEED INDICATOR MARKINGS
MARKING
Red Radial Line (Never Exceed)
Yellow Arc (Caution Range - Smooth Air Only)
Green Arc (N onnal Operating Range)
White Arc (Flap Down)
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)
(f) Fuel Pressure
Minimum (red line)
Maximum (red line)
(g) Fuel (minimum grade)
(h)
Number of Propellers
(i) Propeller Manufacturer
(j)
Propeller Model
(k) Propeller Diameter
Minimum
Maximum
'(l) 74DM6-0-60 Propeller Tolerance
(static rpm at maximum permissible
throttle·setting, Sea Level, ISA)
NOTE
PIPER AIRCRAFT CORPORATION
PA-28-161, CHEROKEE WARRIOR II
IAS
160 KTS
126 KTS to 160 KTS
50 KTS to 126 KTS
44 KTS to 103 KTS
1
Lycoming
0-320-D2A or 0-320-D3G
160
2700
245°F
25 PSI
100 PSI
5 PSI
8
PSI
100 or lOOLL Aviation Grade
1
Sensenich
74DM6-0-60 or
74DM6-0-58
72 IN.
74 IN.
Not above 2430 RPM
Not below 2330 RPM
Refer to the airplane maintenance manual for test procedure to
determine approved static rpm under non standard conditions.
(m) 74DM6-0-58 Propeller Tolerance
(static RPM at maximum pennissible
throttle setting, Sea Level, ISA)
NOTE
Not above 2465 RPM
Not below 2365 RPM
Refer to the airplane maintenance manual for test procedure to
determine approved static rpm under non standard conditions.
REPORT: VB-880
2-2
ISSUED: DECEMBER 16 1976
REVISED: SEPTEMBER 13, 1990