Piper Lance II User Manual

LANCE
II SERVICE
MANUAL
FUEL
INLET
FUEL
STRAINER
SECTION
- AA
IDLE
VALVE
LEVER
CONNECTED
TO
THROTTLE
LEVER
MANUAL
LINKAGE
CONTROL
CUT-OFF
CONSTANT HEAD
IDLE
SPRING
CONSTANT EFFO
SPRING
AIR DIAPHRAGM
NOZZLE
(ONE
PER CYLINDER)
FLOW DIVIDER
THROTTLE
VALVE
THROTTLE
LEVER
IDLE
SPEED
ADJUSTMENT
FUEL
CT TUBE
FUEL
DIAPHRAGM
BALL SERVO VALVE
AIR
Figure
8A-6.
Schematic
Diagram
of RSA-Fuel
Injection
System
POWER
PLANT
- TURBO

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