Piper Lance II User Manual

A
maximum
of
(3)
AN96066
washers
can
used
to
permit
a maximum
of
2.5
threads
exposd
on
the
bolt
Torque
to
230/240
Inch-pounds.
1. SPINNER
2.
PROPELLER
3. FUEL
FLOW
DIVIDER
4. OIL FILLER
5.
OIL
COOLER,
RIGHT
6. OIL
COOLER,
LEFT
7. VENT
TUBE
8. STARTER
9. GOVERNOR
10.
FUEL NOZZLE
11.
ENGINE
MOUNT
12. VALVE, OIL DRAIN
13. AIR FILTER
14. COVER,
FILTER
15.
FILTER
CAP
16.
BOLT, NUT,
WASHER
17. SANDWICH
(J-3049-38)
1. SPACER
(J-12333-2)
19. ENGINE MOUNT
20. PLUG
21.
SANDWICH
(J-3049-35)
22.
ENGINE
23. MOUNTING
KIT
(J-3804-31)
LANCE
II SERVICE MANUAL
133
Section A-A
21
B34
TORQUE TO
140-160
IN.LBS.
A
21
11
1t
Figure
8-4. Engine
Installation
POWER
PLANT
Issued:
1/3/78
2A18

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