Piper Arrow IV Turbo User Manual

CHART 601. LEADING PARTICULARS AND PRINCIPAL DIMENSIONS (cont)
MODEL PA-28RT-201 PA-28RT-201T
FUEL SYSTEM
Fuel Tanks:
Capacity (each) 38.5 gal. 38.5 gal.
Unusable Fuel (each) 2.5 gal. 2.5 gal.
Total Capacity 77 gal. 77 gal.
Total Unusable Fuel (Refer to
Owner’s Handbook, Pilot’s
Information Manual or Flight
Manual for Particular Airplane) 5 gal. 5 gal.
OVERALL
Gross Weight (lbs.) 2750 2900
Wing Loading (lbs/sq. ft.) 16.2 17.0
Length Ft. 24 ft. 8.25 in. 25 ft. 0.23 in.
Width (Span) (Wing Tip to Wing Tip) 35 ft. 5.11 in. 35 ft. 5.11 in.
Height (Static Ground Line) 7 ft. 10.22 in. 7 ft. 10.22 in.
Height, Propeller Hub, Thrust
Line Level 47.64 in. 46.64 in.
Clearance, Propeller Tips, Normal
Static Load 10.40 in. 8.20 in.
Clearance, Propeller Tips, Nose
Strut and Tire Flat 5.47 in. 3.15 in.
6-10-00
Page 6-04
December 1, 1978
1B21
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