3. Insert plug of jumper cable into socket located on aircraft fuselage.
4. Proceed with normal engine starting procedure.
5. Remove jumper cable plug from aircraft.
6. Turn aircraft MASTER SWITCH to ON and check alternator ammeter for indication of output.
—WARNING—
Do not attempt any flight if there is no indication of alternator
output.
—NOTE—
If aircraft battery is weak, charging current will be high. Do not
take off until charging current falls below 20 amperes. Do not
take off with a completely discharged battery because three-volts
are needed to excite the alternator.
ELECTRICAL SYSTEM LOAD DISTRIBUTION
CHART 2406. ELECTRICAL SYSTEM COMPONENT LOADS
Duty Cycle Circuit Load
Cont. Inter. Equipment Breaker (Amps) Optional
X Anti-Collision Light
Grimes 40-010l-XX-l2 10 3.5
Whelen WRML-12 10 3.5
Whelen White Strobe 10 3.8 X
X Position Lights 7.5 5.4
X Landing Lights 10 8.0
X Instrument Light(s) 5 (Max)
Red Flood 5 1.0
Panel 5 2.4
X Reading Light
Dome 5 0.6
X Fuel Pump
Pulsating (Carb) 10 0.5
X Engine Gauges 5 Approx. 1.0
X Elec. Turn & Bank 5 0.5
X Pitot Heat 20 l3.2
X Cigar Lighter 8.0
X Master Solenoid _ 0.8
X Starter Solenoid 15 10.0
X AutoPilot (Avg) 5 0.6
Radio (See Mfg’s Instal-
lation Manual)
—END—
24 - 54 - 00
Page - 24 - 41
Reissued: August 1, 1986
1J16
PIPER AIRCRAFT
PA-28-236
MAINTENANCE MANUAL
To Next Page
Loading...
