Piper Arrow IV Turbo Maintenance Manual page 45

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