Piper Lance II User Manual

5862
PITCH
TRIM
5 AMP
LANCE
II
SERVICE
MANUAL
FUEL
Figure
11-53.
Fuel Pump
(PA-32RT-300T)
2601
Figure
11-54.
Fuel Pump
(PA-32RT-300)
PA-32
RT-300T
AND
PA-32
RT-300
Figure 11-55.
Pitch
Trim
Figure
11-56.
Turn
and
Bank
Revised:
9/2/78
ELECTRICAL
SYSTEM
2117

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