Piper Lance II User Manual

TABLE XI-l.
INDEX -
ELECTRICAL
SYSTEM SCHEMATICS
Aerofiche
Subject
Figure
Grid
No.
Air Blower ...........................................................
Alternator
and Starter
(PA-32RT-300T)
..................................
Alternator
and
Starter
(PA-32RT-300)
...................................
Anti-Collision
Lights ..................................................
Avionics .............................................................
Engine Instruments
(PA-32RT-300T)
...................................
Engine
Instruments (PA-32RT-300)
.....................................
Forward
Baggage
Light
and Cigar
Lighter
................................
Forward
Baggage
Light
and
Cigar Lighter
................................
Fuel
Pump (PA-32RT-300T)
............................................
Fuel
Pump
(PA-32RT-300).............................................
Instruments.
Navigation
and Radio
Lights................................
Landing
Gear
(PA-32RT-300)
...........................................
Landing Gear
(PA-32RT-300T)
.........................................
Landing
Light
........................................................
Passenger
Reading
Lights ..............................................
Pitch
Trim ...........................................................
Pitot
Heat............................................................
Stall
Warning
.........................................................
Turn
and Bank
.......................................................
11-60
11-44
11-45
11-58
11-52
11-49
11-50
11-61
11-63
11-53
11-54
11-48
11-46
11-47
11-59
11-51
11-55
11-57
11-62
11-56
2118
2110
2111
2118
2116
2115
2115
2119
2119
2117
2117
2114
2112
2113
2118
2116
2117
2118
2119
2117
Revised:
10/3/80
2F14

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