Piper PA-28-180 User Manual

PIPER CHEROKEE 180 “C”
SECTION VI
50
Cable tensions for the various controls are as follows:
Rudder: 40 ±5#
Ailerons: 40 ±5# Flap: 10 ±2#
Stabilator: 40 ±5#
Stabilator Trim: 5 ±1#
Flap: 10 ±2#
For extreme cases of wing heaviness, either of the flaps may be adjusted up or
down from the zero position as desired.
SERIAL NUMBER PLATE
The serial number plate is located near the stabilator on the left side of the
airplane. Refer to this number for service or warranty matters.

Piper PA-28-180 Specifications

General

Manufacturer	Piper Aircraft
Model	PA-28-180
Engine	Lycoming O-360-A4A
Horsepower	180 hp
Seating Capacity	4
Wingspan	30 ft (9.1 m)
Height	7 ft 3 in
Service Ceiling	14, 300 ft
Maximum Takeoff Weight	2, 400 lbs
Fuel Capacity	50 US gal (190 L)
Rate of Climb	720 ft/min
Cruise Speed	140 mph