Piper Lance II User Manual

LANCE
II SERVICE
MANUAL
COMPONENT
LUBRICANT
FREQUENCY
1. DIAPHRAGM
SHAFT AND
BUSHING
MIL-L-7870
ABOVE
20 F
MIL-C-21567
BELOW
20 F 100 HRS
2. BACK-UP EXTENDER LINKS AND CONTROL ARM
PIVOT POINTS
MIL-L-7870
100 HRS
3. BACK-UP
EXTENDER SPRING
ATTACHMENT
POINTS
MIL-L-7870
100 HRS
4. FUELSELECTOR
LINKAGE
MIL-G-7711
100 HRS
801
873
4 4
SPECIAL
INSTRUCTIONS
1. Diaphragm shaft and bushing - soft film silicon
compound (MIL-C-21567) is recommended for us
when operating
at temperatures
below 20
°
F.
Figure 2-18. Lubrication
Chart (Back-up Extender
& Fuel Selector)
Issued:
1/3/78
HANDLING
AND SERVICING
1D2

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