MAIN GEAR (Cont.)
CLEANING, INSPECTION AND REPAIR OF MAIN GEAR OLEO
1. Clean all parts with a suitable dry type cleaning solvent.
2. Inspect landing gear oleo assembly components for following:
a. Bearings and bushings for excess wear, corrosion, scratches and overall damage.
b. Retaining pins for wear and damage.
c. Lock rings for cracks, burrs, etc.
d. Cylinder and orifice tube for corrosion, scratches, nicks and excess wear.
e. Orifice plate for hole restriction.
f.
Fork tube for corrosion, scratches, nicks, dents and misalignment.
g. Air valve general condition.
3. Repair of oleo is limited to smoothing out minor scratches, nicks and dents and replacement of parts.
ASSEMBLY OF MAIN GEAR OLEO
1. Determine that all parts are cleaned and inspected.
2. To install piston tube plug, first lubricate plug o-ring with hydraulic fluid (MIL-H-5606A) and install it
on plug. Lubricate inside wall of tube. Insert plug into top of tube and push it to fork end. Align the
bolt holes of fork, tube and plug, and install bolt assembly.
3. If desired, cement a cork in hole in bottom of fork body to prevent dirt from entering between fork and
tube.
4. To assemble components of orifice tube, insert orifice plate into bottom of tube and secure with snap
ring.
5. To install tube in oleo housing, insert tube up through housing. With end of tube exposed through top
of housing, install o-ring, retainer, washer, and locknut. Tighten locknut only finger tight at this time.
6. Assemble components of piston tube on tube by placing, in order, snap ring, washer, lower bearing
with outer and inner o-ring and upper bearing. Align two .125 diameter holes and lock pin holes with
corresponding holes in piston tube and install pins.
7. Lubricate wall of cylinder oleo housing and tube, and carefully insert tube assembly into housing,
guiding orifice tube into piston tube. Install wiper strip, slide washer into position and secure assembly
with snap ring.
8. Tighten locknut at top of housing.
9. Ascertain that bushings are installed in upper and lower torque links and then install links. Torque link
bolt assemblies should be lubricated and installed with flat of bolt head hex adjacent to milled stop of
wide end of link. (Use same thickness of spacer washers between two links as those removed to maintain
correct wheel alignment.) Tighten bolts only tight enough to allow no side play in links, yet be free
enough to rotate.
– NOTE –
Instructions contained in step 10 pertain to left oleo strut
assemblies only.
10. Assemble squat switch actuator bracket on bolt assembly. Insert a rivet through hole provided in
bracket into upper link and install nut. Install squat switch bracket immediately above actuator bracket.
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
32-10-00
Page 32-16
Reissued: July 1, 1993
3B9
Summary of Contents for PA-32R-301T SARATOGA S
Page 26: ...CHAPTER 4 AIRWORTHINESS LIMITATIONS 1C1 ...
Page 29: ...CHAPTER 5 TIME LIMITS MAINTENANCE CHECKS 1C4 ...
Page 53: ...CHAPTER 6 DIMENSIONS AND AREAS 1D6 ...
Page 64: ...CHAPTER 7 LIFTING AND SHORING 1D21 ...
Page 68: ...CHAPTER 8 LEVELING AND WEIGHING 1E1 ...
Page 72: ...CHAPTER 9 TOWING AND TAXIING 1E5 ...
Page 76: ...CHAPTER 10 PARKING AND MOORING 1E9 ...
Page 80: ...CHAPTER 11 REQUIRED PLACARDS 1E13 ...
Page 92: ...CHAPTER 12 SERVICING 1F1 ...
Page 126: ...CHAPTER 20 STANDARD PRACTICES AIRFRAME 1G17 ...
Page 127: ...THIS PAGE INTENTIONALLY LEFT BLANK ...
Page 139: ...CHAPTER 21 ENVIRONMENTAL SYSTEMS 1H5 ...
Page 188: ...CHAPTER 22 AUTOFLIGHT 1J7 ...
Page 193: ...CHAPTER 23 COMMUNICATIONS 1J12 ...
Page 203: ...CHAPTER 24 ELECTRICAL POWER 1J22 ...
Page 263: ...CHAPTER 25 EQUIPMENT FURNISHINGS 2A13 ...
Page 269: ...CHAPTER 27 FLIGHT CONTROLS 2A20 ...
Page 332: ...CHAPTER 28 FUEL 2D11 ...
Page 363: ...CHAPTER 29 HYDRAULIC POWER 2E18 ...
Page 404: ...CHAPTER 30 ICE AND RAIN PROTECTION 2G16 ...
Page 470: ...CHAPTER 32 LANDING GEAR 3A13 ...
Page 550: ...CHAPTER 33 LIGHTS 3D24 ...
Page 562: ...CHAPTER 34 NAVIGATION AND PITOT STATIC 3E12 ...
Page 582: ...CHAPTER 35 OXYGEN 3F8 ...
Page 604: ...CHAPTER 37 VACUUM 3G6 ...
Page 616: ...CHAPTER 39 3G18 ELECTRIC ELECTRONIC PANELS MULTIPURPOSE PARTS ...
Page 620: ...CHAPTER 51 STRUCTURES 3G22 ...
Page 636: ...CHAPTER 52 DOORS 3H14 ...
Page 650: ...CHAPTER 55 STABILIZERS 3I4 ...
Page 662: ...CHAPTER 56 WINDOWS 3I16 ...
Page 670: ...CHAPTER 57 WINGS 3I24 ...
Page 688: ...CHAPTER 61 PROPELLER 3J18 ...
Page 704: ...CHAPTER 70 STANDARD PRACTICES ENGINES 3K10 ...
Page 708: ...CHAPTER 71 POWER PLANT 3K14 ...
Page 737: ...CHAPTER 73 ENGINE FUEL SYSTEM 4A13 ...
Page 749: ...CHAPTER 74 IGNITION 4B1 ...
Page 783: ...CHAPTER 77 ENGINE INDICATING 4C11 ...
Page 793: ...CHAPTER 78 EXHAUST 4C21 ...
Page 801: ...CHAPTER 79 OIL 4D5 ...
Page 805: ...CHAPTER 80 STARTING 4D9 ...
Page 819: ...CHAPTER 81 TURBINES 4D23 ...
Page 833: ...CHAPTER 91 CHARTS WIRING DIAGRAMS 4E13 ...