Piper ARROW III Service Manual

TABLE IX-I. FUEL SENDER LOCATIONS
Piper P/N: Piper P/N:
550 504 550 503
Rochester P/N: Rochester P/N:
774041 7740-40
See Note
PA-28R-201
S/N: 28R-7737002 to 28R-7737161 inclusive
PA-28R-201T Inboard Outboard
S/N: 28R-7703001 to 28R-7703380 inclusive
PA-28R-201
S/N: 28R-7737162 and up
PA-28R-201T Outboard Inboard
S/N: 28R-7703381 and up
Note:
Fuel quantity sender Piper P/N: 550 504 requires fiber washer insulators. Refer to Figure 9-3, View B-B.
Figure 9-4. Engine Primer System Placard (PA-28R-201T)
Revised: 2/13/89
2E16
CHEROKEE ARROW III SERVICE MANUAL
FUEL SYSTEM

Piper ARROW III Specifications

General

Manufacturer	Piper Aircraft
Model	ARROW III
Engine	Lycoming IO-360-C1C6
Horsepower	200 hp
Maximum Takeoff Weight	2, 750 lb (1, 247 kg)
Seating Capacity	4
Propeller	2-blade, constant speed
Length	24 ft 7 in (7.49 m)