Piper ARCHER II User Manual

ARCHER II
PA-28-181
PILOT’S
OPERATING
HANDBOOK
AND
FAA APPROVED
AIRPLANE FLIGHT MANUAL
FAA APPROVED I N NORMAL AND UTILITY CATEGORIES BASED ON CAR 3. THIS
HANDBOOK INCLUDES THE MATERIAL REQUIRED TO BE FURNISHED TO THE PILOT BY
CAR 3 AND CONSTITUTES THE APPROVED AIRPLANE FLIGHT MANUAL AND MUST BE
CARRIED IN THE AIRPLANE AT ALL TIMES.
AIRPLANE AIRPLANE
SERIAL NO. ________________________ REGIST. NO. _____________________
PA-28-181
REPORT: VB-1120 FAA APPROVED BY: ________________________________
WARD EVANS
D.O.A. NO. SO-1
DATE OF APPROVAL: PIPER AIRCRAFT CORPORATION
JULY 2, 1979 VERO BEACH, FLORIDA
28 - 8390087
OE-KBS
21.04.2018 added AFMS Fuel STC
05.07.2018 added AFMS G5 Instrument
30.04.2019 added GNS430W Upgrade
30.04.2019 added AFMS GFC500 Autopilot

Piper ARCHER II Specifications

General

Manufacturer	Piper Aircraft
Model	Archer II
Engine	Lycoming O-360-A4M
Horsepower	180 hp
Empty Weight	1, 450 lb (658 kg)
Max Takeoff Weight	2, 550 lb (1, 157 kg)
Seating	4
Rate of Climb	720 ft/min (3.7 m/s)
Range	522 miles
Wingspan	35 ft 6 in
Fuel Capacity	50 US gallons (189 liters)