Piper PA-28-161 Maintenance Manual

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

Piper PA-28-161 Specifications

General

Manufacturer	Piper Aircraft
Model	PA-28-161 Warrior II
Engine	Lycoming O-320-D3G
Horsepower	160 hp
Seating Capacity	4
Wingspan	35 ft (10.7 m)
Length	24 ft 0 in
Maximum Speed	127 knots
Cruise Speed	122 knots
Maximum Takeoff Weight	2, 325 lb (1, 055 kg)
Fuel Capacity	48 US gallons (182 L)