Piper Lance II User Manual

SECTION II
HANDLING
AND
SERVICING
Aerofiche
Paragraph
Grid No.
2-1.
Introduction
..............................................................
I A 17
2-2.
Dimensions
..................
.............................................
A17
2-3.
Station
Reference
Lines ....................................................
A17
2-4.
W eight and
Balance
Data...................................................
I A 17
2-5.
Serial
Number Plate
.................
......................................
A 17
2-6.
Access
and
Inspection
Provision
.............................................
I
A17
2-7.
Tools
and Test
Equipment
..................................................
I
B
2-8.
Torque
Requirements
......................................................
I B I
2-8a.
Torque
W renches
..........................................................
I B
2-8b.
Identification
of Fluid
Lines ................................................
1B7
2-8c.
Installation
of Flexible
Hose
Assemblies
...................
I.........
........
B7
2-8d.
Support Clamps
...........................................................
B16
2-8e.
Removal
of Cherrylock
Rivets
...............................................
IB18
2-9.
Step. Handhold,
and
W alkways
.............................................
1B21
2-10.
Ground Handling
...................................................
........
IB21
2-
11. General................................................
........
IB21
2-12.
Jacking ..........................................................
IB21
2-13.
W eighing
........................................................
IB22
2-14.
Leveling
.........................................................
B22
2-15.
Mooring........................................................
IB23
2-16.
Locking
Airplane
.................................................
B23
2-17.
Parking
..........................................................
B24
2-18.
Towing
..........................................................
B24
2-19.
Taxiing
......................................
C.......
.........
ICI
2-20.
External
Power Receptacle
..................................................
IC
2-21.
Operation
of External
Power
Receptacle
.............................
IC1
2-22.
Servicing
............
....................................................
I C2
2-23.
General
..........................................................
IC2
2-24.
Fuel
System
...............................................
..............
1C2
2-25.
Servicing
Fuel
System
.............................................
IC2
2-26.
Filling
Fuel
Tanks
...................................
.............
1C2
2-27.
Draining
M
oisture
from Fuel
System
................................
C2
2-27a.
Anti-Icing
Fuel
Additive
..................
...........
..............
1C3
-28.
Draining
Fuel System
........................................
1C3
2-29.
Brake System
.............................................................
C3
2-30.
Servicing
Brake
System ............................................
C3
2-31.
Filling Brake
Cylinder
Reservoir
....................................
1C3
2-32.
Draining
Brake
System
1
1C3
2-32a.
Tires
.....................................................................
C4
2-32b.
Servicing
Tires
...........................................
IC4
2-32c.
Tire
Balance
.............................
. ....................
1C4
2-33.
Hydraulic
System
..........................................................
I C6
2-34.
Servicing
Hydraulic
System
.............................
.
........
1C6
2-35.
Servicing
Hydraulic
Pump
Reservoir
...........................
1C6
2-36.
Landing
Gear System
...................................
........
.........
IC6
2-37.
Servicing
Landing
Gear............................................
IC6
Revised: 10/3/80 1A15
1A15

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