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Piper Lance II User Manual

Piper Lance II
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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

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Piper Lance II Specifications

General IconGeneral
ManufacturerPiper Aircraft
Max Takeoff Weight3, 600 lb (1, 633 kg)
Crew1
Horsepower300 hp
Seats6
Length27 ft 7 in (8.41 m)
Capacity5 passengers

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