Piper Lance II User Manual

LIST
OF
ILLUSTRATIONS
(cont.)
Aerofiche
Figure
Grid
No.
7-17.
Wheel
Brake
Assembly
...........................
IL5
7-18.
Brake System
Installation .........................
IL7
7-19. Brake
Master Cylinder
(Hand/Parking
Brake) .............
IL8
7-20. Toe
Brake Installation
..........................
ILIO
7-21.
Brake Cylinder (1700)
(Toe Brake)
...................
ILII
7-22.
Brake
Cylinder (10-27)
(Toe Brake)
...................
I II
7-23.
Brake Cylinder
(10-30) (Toe Brake)
....................
IL 14
7-24.
Deleted.
8-1.
Propeller
Installation
............................
2A 1
8-2.
Propeller Blade
Minor
Repair .......................
2A12
8-3.
Propeller
Governor
.............................
2A15
8-4.
Engine Installation
.............................
2A18
8-5. Adjustment
of
Engine Controls
.....................
. 2A20
8-6.
Schematic
Diagram
of RSA Fuel
Injection
System
...........
2A22
8-7.
Fuel
Injector
.................................
2A23
8-8.
Fuel-Air
Bleed
Nozzle
..................
........
. 2B1
8-9.
Height of
Spring in
Distributor
Block
Tower
..............
2B2
8-10.
Contact
Points ..
..............
............
2B3
8-11.
Engine
Timing
Marks
..........................
. 2B3
8-12.
Timing
Light
Connected
to Magneto
...................
2B5
8-13.
Timing
Marks
on Magneto
Rotor
.....................
2B6
8-14.
Painted
Tooth
Centered
in Timing
Window
...............
2B7
8-15.
Timing
Mark
on Rotor
Aligned
With
Pointer
.................
2B7
8-15a.
Timing
Light Connected
to Magneto
and
Breakers.
..........
2B8
8-16.
Cam
End View
of Magneto
.........................
2B 10
8-17.
Removing
Impulse
Coupling
........................
2B
1
8-18.
Checking
Flyweight
to Stop
Pin Clearance
................
2B 11
8-19.
Stop
Pin Installation
Dimension
.
.....................
2B12
8-20.
Checking
Flyweight
Axial Wear
with Drill
Shank
............
2B
13
8-21.
Checking
Flyweight
Radial
Wear
with Gauge
..............
2B 13
8-22.
Points
of Coupling
Body Wear
.......................
2B14
8-23.
Acceptable
and Deformed
Coupling
Springs
...............
2B14
8-24.
Checking
Impulse
Coupling
for
Magnetization
..............
2B15
8-25.
Orientation
of
Springs in
Coupling
Body
.................
2B15
8-26.
Lifting
Inner
End
of Spring
........................
2B16
8-27.
Checking
Harness
Lead
Continuity
....................
2B17
8-28.
Checking
Harness
Lead
Insulation
Resistance
..............
2B
17
8-29.
Modified
Pliers
...............................
2B18
8-30.
Removing
Spring
From Lead
Assembly
.................
2B18
8-31.
Assembly
Tool
................................
2B19
8-32.
Using Assembly
Tool ............................
2B19
8-33. Ferrule
Positioned
Under
Braid ......................
2B19
Revised 6/15/79
1A6

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