Piper SENECA II User Manual

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PIPER SENECA II SERVICE MANUAL
11-40. STARTING MOTOR SERVICE TEST SPECIFICATIONS. Prestolite specifications for 12-volt
cranking motors installed as standard equipment on the PA-34-200T are as follows:
TABLE XI-Ill. STARTING MOTOR SPECIFICATIONS
Motor Model
MCL-6501
Min. Brush Tension
32 oz. (With New
Max. Brush Tension
40 oz. Brushes)
No-Load Test (75°F):
Volt
5
;:::
Max. Amps
65
"'
Min. RPM
4900
~
:;;
'-
Stall Torque:
Cl)
w
Max. Amps
410
...
::l
0
Min.Torque, Ft.-Lbs.
8
...
Cl)
Approx. Volts
2
w
a:
Q.
11-41. BATTERY.
11-42. SERVICING BATTERY. The battery is located in the left forward portion of the nose section. It is
enclosed in a fiberglass box with a vent system and a drain. The vents allow fresh air to enter the box and
draw off fumes that may accumulate due to the charging process of the battery. The drain is clamped off
from the bottom of the fuselage and should be opened occasionally to drain any accumulation of liquid or
during cleaning of the box. The battery should be checked for fluid level but must not be filled above the
baffle plates. A hydrometer check should be performed to determine the percent of charge in the battery.
All connections must be clean and tight.
NOTE
Refer to note under paragraph 11-29 "Maintenance" when replacing
cables in battery circuit.
11-43. REMOVAL OF BATTERY.
a. Remove the access cover over nose wheel and battery in the nose baggage compartment.
b. Disconnect the battery cables.
NOTE
Always remove the ground cable first and install last to prevent
accidental short circuiting or arcing.
c. Lift the battery from the box.
Revised: 12/08/83
2G21
ELECTRICAL SYSTEM

Piper SENECA II Specifications

General

Brand	Piper
Model	SENECA II
Category	Aircrafts
Language	English