Piper Arrow IV Turbo User Manual

STATION REFERENCE LINES.
In order to facilitate the location of various components of the airplane which require maintenance and
servicing, a method utilizing fuselage station (Sta.) wing station or buttock line (BL), and water line (WL)
designations is frequently employed in this manual. (Refer to Figure 6-3.) Fuselage stations, buttock and water
lines are reference points measured by inches in the vertical or horizontal direction from a given reference line
which indicates station locations of structural members of the airplane. Station O of the fuselage is 44.5 inches
ahead of the lower edge of the firewall; station O (BL) of the wing and stabilator is the centerline of the
airplane; and station O (WL) of the fuselage vertical stabilizer and rudder is 20.5 inches below the cabin floor
as measured at the rear wing spar with the airplane level.
THIS SPACE INTENTIONALLY LEFT BLANK
6-20-00
Page 6-07
December 1, 1978
1B24
PIPER AIRCRAFT
PA-28RT-201 / 201T
* MAINTENANCE MANUAL

Piper Arrow IV Turbo Specifications

General

Manufacturer	Piper Aircraft
Model	Arrow IV Turbo
Horsepower	200 hp
Seating Capacity	4
Landing Gear	Retractable tricycle
Range	773 nautical miles
Service Ceiling	20, 000 ft
Fuel Capacity	72 gallons
Propeller	2-blade constant speed
Max Takeoff Weight	2, 900 lb (1, 315 kg)
Stall Speed (Flaps Down)	55 knots
Rate of Climb	1, 000 ft/min