Piper Lance II User Manual

LANCE II
SERVICE MANUAL
c. Rinse the battery
and box with clean
water and dry.
d. Place
the cap over the
battery box drain.
e. Reinstall the battery.
TABLE XI-II.
ELECTRICAL
SYSTEM
COMPONENT
LOADS
DUTY CYCLE
CON'T. INMT.
LOAD
(AMPS)
EQUIPMENT
X
Anti-Collision Light
X
X
X
X
X
X
X
Whelen White Strobe
Position Lights
X Landing Lights
Instrument Lights
Red Flood
Panel
X Reading Light
Passenger
X Fuel Pump
Rotary (Fuel Inj't)
Engine Gages
Elec.
Turn
& Bank
Pitot Heat
Pitot and Pressure Mast
Heat
X Cigar Lighter
Master Solenoid
X Starter Solenoid
Radio (See Mfg's Installation
Manual)
X Baggage Comp't Light
X
Landing
Gear
Pump
(Circuit
Breaker)
Solenoid
X
Gear
Down
Lights
2H13
4.4
5.4
8.0
(Max.)
OPT
OPT
OPT
1.0
OPT
1.5
OPT
1.0
OPT
6.0
Approx 1.0
0.5
13.2
20.5
8.0
0.8
10.0
0.6
25.0
0.8
Total 0.3
X
X
OPT
OPT
OPT
OPT
X
X
OPT
X
X
X
Issued:
1/3/78
ELECTRICAL SYSTEM

Piper Lance II Specifications

General

Manufacturer	Piper Aircraft
Max Takeoff Weight	3, 600 lb (1, 633 kg)
Crew	1
Horsepower	300 hp
Seats	6
Length	27 ft 7 in (8.41 m)
Capacity	5 passengers