Piper Lance II User Manual

I
LANCE
I
SERVICE
MANUAL
2327
I l
/
"
_
1.
BRAKE
RESERVOIR
2.
RIGHT
BRAKE
AND
RUDDR
PEEAL
3.
LEFT
BRAKE
AND
UDDER
PEDAL
4.
RIGHT
BRAKE
CYLINDER
5.
LEFT
RBAKE
CYLINDER
6.
BRAKE
HANDLE
7.
HANDLE
RELEASE
BUTTON
8.
MASTER
CYLINDER
ASSEMBLY
9.
TOROUE
TUBE
10.
RUDDER
PEDAL
PADS
11.
BOLT
ASSEMLY
12.
CLEVIS
PIN
13.
LINE,
INLET
Figure
7-18.
Brake
System
Installation
Revised:
9/2/78
LANDING
GEAR
AND
BRAKE
SYSTEM
1L7

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