Piper Lance II User Manual

LANCE II
SERVICE MANUAL
TABLE
VII-I
(cont.).
Nose
Gear Service
Tolerances
Fig.
No.
Part No.
17 452-477
18 63900-109
19 14976-15
20
14976-16
21 452-445
22 82732-99
23 65003-30
24 95061-136
25 95061-135
26 67026-11
27
35662-02
28 38068-02
29 67050-02
30 20735-05
31
67148-00
32 20735-05
Nomenclature
Sleeve Bearing
Nose Gear
Inner
Bushing
Bushing
Bushing
Steering Cam
Bearing
Nose Gear
Arm
Bushing
Down Lock
Bushing
Bushing
Bushing
Bearing
Bushing, Eccentric
Bearing. Downlock
Lower
Strut
Assembly Torque
Link Fitting
Torque Link
Trunnion
Torque Link Fitting
Torque Link
Manufacturers
Dimension
I.D. .375
I.D. .3125
.3180
I.D. .385
.390
I.D. .260
.265
I.D. .502
I.D. .241
.246
I.D. .193
.195
1.D. .2495
.2505
I.D. .2495
.2505
Service
Dimension
.395
.375
.3235
.3125
.395
.385
.270
.260
.512
.502
.241
.251
.196
.193
.2515
.2495
.2515
.2495
Service
Tol.
.020
.011
.010
.010
.010
.010
.003
.002
.002
Remarks
SEE NOTE 3
SEE
NOTE
I
I.D. .191
.189
I.D. .191
.189
I.D.
.377
.3785
I.D. .4385
.4370
I.D. .312
.313
.189
.193
.189
.193
.377
.3790
.4385
.4370
.312
.314
.004
.004
.002
.0015
.002
Added: 7/15/81
LANDING GEAR AND BRAKE SYSTEM
1J17

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