Piper Lance II User Manual

1608
SKETCH
A
LANCE
II
SERVICE
MANUAL
COMPONENT
1.
RUDDER
TUBE
BEARING
BLOCKS
2.
TOE
BRAKE
CYLINDER
ATTACHMENTS
3.
RUDDER
TUBE
CONNECTIONS
4.
BRAKE
ROD
ENDS
5.
STABILATOR
TRIM
SCREW
6.
STABILATOR
SCREW
ROD
ENDS
7.
STABILATOR
HINGE
POINTS
8. RUDDER
TRIM ASSEMBLY
874
LUBRICANT
FLUOROCARBON
RELEASE
AGENT
DRY
LUBRICANT
MS-122
MIL-L-787
0
MIL-L-7870
MIL-L-7870
AERO
LUBRIPLATE
OR
MAG-1,
FISKE
BROS.
RE-
FINING
CO.
MIL-L-7870
MIL-L-7870
MIL-L-7870
FREQUENCY
100 HRS
100
HRS
100 HRS
100 HRS
100 HRS.
100 HRS
100 HRS
100 HRS
863
1810
2
SKETCH
B
SKETCH
C
Figure
2-14.
Lubrication
Chart
(Control
System)
(cont.)
Revised:
7/15/81
1C22
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