Piper Lance II User Manual

2
3
4
LANCE
II SERVICE
MANUAL
12
TORQUE SUPPORT BRACKET
NOTES
1. IT MAY
HAVE BEEN
NECESSARY TO
USE SPECIAL
LANDING GEAR
ATTACHMENT
HARDWARE
DURING
ASSEMBLY
OF THE
AIRCRAFT
DUE TO
MANUFACTURING
TOLERANCES.
THEREFORE,
SPECIAL
ATTENTION
SHOULD
BE GIVEN
WHEN REMOVING
HARDWARE
TO INSPECT
AND INSURE
THE SAME
DIAMETER
HARDWARE
IS USED UPON
REASSEMBLY.
STANDARD
AN4
OR AN5
BOLTS ARE
REPLACED
BY ALTERNATE
OVERSIZED
BOLTS
NAS3004
OR NAS3005
RESPECTIVELY,
WHEN OVERSIZED
HARDWARE
IS REQUIRED.
2. WHEN
NEW BUSHINGS,
P/N 14843-16,
ARE INSTALLED
LINE REAM
I.D. TO .376/.375.
BUSHINGS
TO BE PRESS
FIT AND IF LOOSE ON INSTALLATION,
INSTALL WITH
LOCTITE 601.
7/15/81
LANDING
GEAR
AND BRAKE
SYSTEM
1K3
Revise

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