Piper TURBO ARROW III User 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 TURBO ARROW III Specifications

General

Manufacturer	Piper Aircraft
Model	Turbo Arrow III
Horsepower	200 hp
Max Takeoff Weight	2, 900 lbs
Fuel Capacity	72 gallons
Service Ceiling	20, 000 ft
Seating Capacity	4
Type	Single-engine piston
Propeller	Constant-speed
Landing Distance	1, 200 ft