Piper cherokee WARRIOR Pilots Operating Manual page 30

CHEROKEE WARRIOR
SECTION I
LIMITATIONS
The following limitations must be observed in the operation of this airplane:
A. ENGINE
Lycoming O-320-E3D
ENGINE LIMITS
For all operations 2700 RPM, 150 HP
B. FUEL
80187 octane aviation fuel minimum grade
C.
PROPELLER
Sensenich 74DM6, maximum diameter 74 inches. Minimum diameter 72 inches. Static
RPM at maximum permissible throttle setting: Not over 2375, not under 2275. No
additional tollerance permitted.
McCauley lcl60/EGM7653, maximum diameter 76 inches. Minimum diameter 74.5
inches. Static RPM at maximum permissible throttle setting: Not over 2400, not under
2300. No additional tollerance permitted.
D. POWER INSTRUMENTS
OIL TEMPERATURE
FAA APPROVED JULY 25,1973
REVISED: APRIL 16.1976
Green Arc (Normal Operating Range)
Red Line (Maximum)
OIL PRESSURE
Green Arc (Normal Operating Range)
Yellow Arc (Caution Range)
R c d L i n e ( M i n i n r u m )
l ( c : t l l . i n c ( M i r x i r n u r r r )
FUEL PRESSURE
Green Arc (NormalOperating Range)
Red Line (Minimum)
Red Line (Maximum)
TACHOMETER
Green Arc (NormalOperating R*g.)
Red Line (Maximum Continuous Power)
7 5 ' F t o 2 4 5 ' F
245"F
60 PSI tO 90 PSI
25 PSI to 60 PSI
2 5 P S I
( ) 0 I ' s l
.5 PSI to 8 PSI
.5 PSI
8 PSI
500 to 2700 RPM
27OO RPM
REPORT: VB-573 PAGE 3-l
MODEL: PA-28-151