Piper Lance II User Manual

SECTION VI
HYDRAULIC
SYSTEM
Aerofiche
Paragraph
Grid
No.
6-1.
Introduction
..................................
. IH 14
6-2.
Description
....................................
. H 14
6-3. Troubleshooting
..............
....................
IH
18
6-4.
Hydraulic
Pump ...................
..............
H 19
6-5.
Removal of
Hydraulic Pump
.....................
H 19
6-6. Disassembly
of Hydraulic
Pump ...................
IH 19
6-7. Cleaning, Inspection
and Repairs of Hydraulic Pump
....... IH 19
6-8.
Assembly
of Hydraulic Pump
....................
1H20
6-9.
Test and Adjustment
of Hydraulic
Pump ..............
H 21
6-10. Installation
of Hydraulic Pump ...................
III
6-11. Gear Back-Up Extender
Actuator Assembly ..................
1I1
6-12. Removal of Gear Back-Up
Extender Actuator Assembly
..... 1I1
6-13. Installation of Gear Back-Up Extender Actuator Assembly . . 112
6-14.
Check and Adjustment of Gear Back-Up
Extender Actuator . . .
114
6-14a.
Operational Check of Retractable
Landing Gear System .....
116
6-15.
Nose Gear
Actuating Cylinder
. ...................
117
6-16. Removal of Nose Gear Actuating Cylinder ............. 117
6-17. Disassembly of Nose Gear Actuating Cylinder .......... 118
6-18.
Cleaning, Inspection and Repair
of Nose Gear Actuating Cylinder
119
6-19. Assembly of Nose Gear
Actuating Cylinder ............
119
6-20.
Installation of Nose Gear Actuating
Cylinder ..........
119
6-21.
Main Gear Actuating Cylinder
...... ....................
. 119
6-22. Removal of Main Gear Actuating Cylinder ............. 119
6-23. Disassembly of Main Gear Actuating Cylinder .......... 1111
6-24. Cleaning, Inspection and Repair of Main Gear Actuating Cylinder 1111
6-25. Assembly of Main Gear Actuating Cylinder ............ 1I11
6-26. Installation of Main Gear Actuating Cylinder ........... 1112
6-27. Hydraulic
Lines ...................
....... . 1112
6-28.
Removal and Installation of Hydraulic
Lines ............ 1112
6-29. Testing
Hydraulic System
..........................
. 1112
6-30. Servicing
Hydraulic Pump/Reservoir
......................
1113
Revised: 9/2/78
1H13

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