Piper Warrior III - Page 849

STATIC RPM WORKSHEET
Aircraft Model: _____________________
Aircraft S/N: _____________________
Date: _____________________
OAT: _____________________
Relative Humidity (Temp
) (Dew PT ) ___________________%
Wind above 10 Knots
Tested
Static RPM: ________________ Average
Oil Temp: __________________
Rpm: ______________ (See Chart 3)
Delta rpm (subtract) ______________ (See Chart 4)
BASELINE Static rpm ______________
Tested ______________
Static rpm: ______________
Result to be within tolerance __
± 50 rpm__ (See “Allowable Tolerance,” in text.)
PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 9
Nov 30/06
4J7
71-00-00