Piper TURBO ARROW III User Manual

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TABLE XI-V. ELECTRICAL SYSTEM TROUBLESHOOTING (cont)
Outlet indicated on Faulty voltage regulator. Start engine, turn on load
ammeter does not (Ref. alternator test
meet minimum values procedure), set throttle
specified in alternator at 2300 rpm. Check
system test procedure. voltage at buss bar
(convenient check point,
remove cigar lighter and
check from center contact
(+) to ground (-). Voltage
should be 13.5 volts
minimum. If voltage is
below this value, replace
regulator.
High resistance Check visually for loose
connections in field binding posts at the
or output circuit. various junction points
in system, alternator
battery post, lugs on
ammeter, connection at
voltage regulator, circuit
breaker, etc., (see wiring
schematic). (Examine
crimped terminal ends
for signs of deterioration
at crimp or strands of
broken wire at crimp.
Tighten any loose binding
posts or replace bad wire
terminals.)
Trouble Cause Remedy
Revised: 2/13/89
CHEROKEE ARROW III SERVICE MANUAL
ELECTRICAL SYSTEM
ALTERNATOR (cont)

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