Piper Lance II User Manual

1.
LANCE
II SERVICE
MANUAL
COMPONENT
LUBRICANT
FREQUENCY
1. MAIN GEAR PIVOT POINTS
2. MAIN GEAR DOOR HINGE
3. MAIN
GEAR TORQUE
LINKS
4.
EXPOSED OLEO
STRUT MAIN
5. MAIN
GEAR WHEEL
BEARINGS
6. MAIN GEAR
DOOR CONTROL ROD
ENDS
7. MAIN
GEAR
SIDE BRACE
LINK ASSEMBLY
8. UPPER SIDE
BRACESWIVEL
FITTING
9. MAIN
GEAR DOWNLOCK
ASSEMBLY
RETRACTION
FITTING
AND CYLINDER
ATTACHMENT
POINTS
10.
OLEO STRUT
FILLER
POINT (MAIN
GEAR)
11. HYDRAULIC PUMP RESERVOIR
12.
BRAKE RESERVOIR
MIL-G-23827
MIL-L-787
0
MIL-L-7870
FLUOROCARBON
RELEASE
AGENT DRY LUBRICANT
MS-122
TEXACO MARFAX ALL
PURPOSE GREASE OR
MOBIL
GREASE
77
(OR MOBIL
EP2
GREASE)
MIL-L-7870
MIL-G-23827
MIL-G-23827
MIL-L-7870
MIL-H-5606
MIL-H-5606
MIL-H-5606
100 HRS
100 HRS
100 HRS
100
HRS
100
HRS
100 HRS
100 HRS
100 HRS
100 HRS
AS REQUIRED
100 HRS
100 HRS
.10 9
6
4
843
SPECIAL
INSTRUCTIONS
1. Main wheel bearings
- Disassemble and
clean with a dry
type solvent.
Ascertain
that grease
is packed
between
the
roller and
cone. Do
not pack
grease in
wheel
housing. Whee
bearings
require cleaning
and
repacking
after
exposure
to an abnormal
quantity
of
water.
2. Oleo struts,
hydraulic pump
reservoir and brake
reservoir
- Fill per
Instructions
on unit or
container or
refer to service manual.
Figure
2-10. Lubrication
Chart (Landing Gear,
Main)
HANDLING
AND
SERVICING
1C18
Issued:
1/3/78

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