Piper Lance II User Manual

LANCE II
SERVICE MANUAL
A307
906
O 0
0
0 o t
BOLT NAS1104-17
WASHER AN960-416L
(UNDER
HEAD)
WASHER
AN960416 (UNDER
NUT)
NUT MS210454
SKETCH A
0
0
0
0
0
A
TORQUE TO
80-90 IN.
LBS.
SECTION A-A
NOTE
MAXIMUM
NUMBER OF WASHERS BETWEEN
FORWARD FACE OF WING AND AFT
FACE OF
FUSELAGE FITTING IS (1)
AN960-16L AND (1) AN960616. IT
IS ALSO ACCEPTABLE TO
HAVE THE FACES OF THE FITTINGS AGAINST EACH OTHER, IN WHICH CASE THE
AN960-616 L WASHER SHOULD BE USED UNDER THE BOLT HEAD. THE AN960-616 MAY BE
ADDED
UNDER THE NUT WHEN
NOT USED AS A SHIM.
SEE
NOTE
A-A
A NS960-6 SKETCH B
AN960-616
Figure
4-2. Wing
Installation
Revised:
9/2/78
STRUCTURE
1E3

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