Piper Lance II User Manual

1
LANCE
II SERVICE
MANUAL
COMPONENT
1. FLAP
TORQUE
TUBE
BEARING
BLOCKS
2. FLAP
CONTROL
ROD
END
BEARINGS
3.
FLAP
HANDLE
PIVOT
POINT,
LOCK
MECHANISM
AND
TURNBUCKLE
END
4. FLAP
RETURN
AND
TENSION
CHAINS
5.
AILERON
BELLCRANK
PIVOT
POINTS
6.
AILERON
CONTROL
ROD
END
BEARINGS
7. AILERON
BELLCRANK
CABLE
ENDS
875
LUBRICANT
MIL-L-7870
MIL-L-7870
FREQUENCY
100 HRS
100 HRS
100 HRS
500
HRS
100 HRS
100 HRS
100 HRS
MIL-L-7870
MIL-L-787
0
MIL-L7870
MIL-L-7870
MIL-L-7870
863
2
2
4
3
SKETCH
A
SKETCH
B
Figure
2-13.
Lubrication
Chart
(Control
System)
(cont.)
Issued: 1/3/78
1C21
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