Piper Lance II User Manual

LANCE II SERVICE MANUAL
TABLE VII-II (cont.).
Main Gear Service
Tolerances
Manufacturers Service Service
ig. No. Part No. Nomenclature
Dimension Dimension
Tol. Remarks
17 67926-04 Trunnion Housing .7530 .7530
67926-05 Side Brace Attachment .7550 .7550
18
67026-05 Trunnion Bushing
.499 .498 .004 SEE
NOTE 2
.500 .502
19 NAS-464 Trunnion Side OD .4991
P8A-44
Brace Attaching Bolt
.4982
20 67926-04 Trunnion ID .4410 .4410
67926-05 Housing Torque Link ID .4430 .4440
Attachment
21 6702607 Trunnion .313 .315 SEE NOTES 1, 2 AND 4
Bearing .314
22 67037-06 Strut Assembly .4385 .4395 .0025
.4370 .4370
23 67026-07 Strut Bearing .313 .313 .002 SEE NOTES I AND 4
.314 .315
24 67012-00 Torque Link .313 .314 .002
.312 .312
25 67012-00 Torque
Link .3760
.3770 .0025
.3745 .3745
26 31796-00 Torque Link Bushing
.252 .253 .002 SEE
NOTES I AND 4
.251 .251
NOTES
1. Line ream
to this dimension after installation
of new part.
2. Install bearing
with wet zinc chromate on adjacent
surfaces of bearings and casting.
3. Install using Loctite 601. Rotate part while inserting, if possible, to insure complete coverage.
4. Press fit.
Added: 7/15/81
LANDING GEAR AND BRAKE SYSTEM
1K8

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