Piper Lance II User Manual

LANCE
II SERVICE
MANUAL
-CA
UTION
-
Do
not lubricate control wheel
shaft or bushing. Clean only
using
alcohol or other
suitable solvent.
COMPONENT
LUBRICANT
FREQUENCY
1. AILERON
HINGE PINS
MIL-L-7870*
100 HRS
2. FLAP HINGE BEARINGS
MIL-L-7870 100 HRS
3. STABILATOR
HINGE PINS
MIL-L-7870 100
HRS
4. RUDDOER HINGE BEARINGS
MIL-L-7870
100 HRS
5. CONTROL CABLE PULLEYS
MIL-L-7870
100 HRS
6. TRIM CONTROL WHEEL
MIL-L-7870
100 HRS
7. O-RING, CONTROL SHAFT BUSHING PARKER O-RING
LUBRICANT
AS REQUIRED
8.
TEE BAR PIVOT POINT
MIL-L-7870
100 HRS
9. CONTROL
COLUMN CHAIN
MIL-L-7870
500 HRS
10. CONTROL COLUMN FLEX. JOINTS
AND SPROCKET MIL-L-7870
100 HRS
11. STABILATOR CONTROL
MIL-L-7870
100 HRS
877
10
3
SPECIAL INSTRUCTIONS
Figure 2-12. Lubrication Chart (Control System)
6
SPECIAL INSTRUCTIONS
Aileron
hinges should first be cleaned
with a dry type solvent
then lubrcated with MIL-L-7870.
Figure 2-12.
Lubrication
Chart
(Control
System)
Interim Revision:
July 30, 1986
1C20
HANDLING
AND SERVICING

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