Piper Lance II User Manual

FUEL
NOZZLES.
(6)
LANCE II SERVICE MANUAL
INJECTOR
FLOW DIVIDERS (2)
TURBOCHARGER
COMPRESSOR
ENGNE
DRIVEN
FUEL
PUMP
MANIFOLD
PRESSURE
AND FUEL FLOW
GAUGE
ELECTRIC
FUEL PUMP
FUEL SELECTOR
VALVE
FUEL
QUANTITY
GAUGES
Figure
9-2.
Fuel System
(PA-32RT-300T)
Issued:
1/3/78
FUEL
SYSTEM
2D15

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