Here's the textbook answer from Part 43, Appendix A...
(c) Preventive maintenance. Preventive maintenance is limited to the
following work, provided it does not involve complex assembly operations:
(1) Removal, installation, and repair of landing gear tires.
(2) Replacing elastic shock absorber cords on landing gear.
(3) Servicing landing gear shock struts by adding oil, air, or both.
(4) Servicing landing gear wheel bearings, such as cleaning and greasing.
(5) Replacing defective safety wiring or cotter keys.
(6) Lubrication not requiring disassembly other than removal of
nonstructural items such as cover plates, cowlings, and fairings.
(7) Making simple fabric patches not requiring rib stitching or the removal
of structural parts or control surfaces. In the case of balloons, the making
of small fabric repairs to envelopes (as defined in, and in accordance with,
the balloon manufacturers' instructions) not requiring load tape repair or
replacement.
(8) Replenishing hydraulic fluid in the hydraulic reservoir.
(9) Refinishing decorative coating of fuselage, balloon baskets, wings tail
group surfaces (excluding balanced control surfaces), fairings, cowlings,
landing gear, cabin, or cockpit interior when removal or disassembly of any
primary structure or operating system is not required.
(10) Applying preservative or protective material to components where no
disassembly of any primary structure or operating system is involved and
where such coating is not prohibited or is not contrary to good practices.
(11) Repairing upholstery and decorative furnishings of the cabin, cockpit,
or balloon basket interior when the repairing does not require disassembly of
any primary structure or operating system or interfere with an operating
system or affect the primary structure of the aircraft.
(12) Making small simple repairs to fairings, nonstructural cover plates,
cowlings, and small patches and reinforcements not changing the contour so as
to interfere with proper air flow.
(13) Replacing side windows where that work does not interfere with the
structure or any operating system such as controls, electrical equipment,
etc.
(14) Replacing safety belts.
(15) Replacing seats or seat parts with replacement parts approved for the
aircraft, not involving disassembly of any primary structure or operating
system.
(16) Trouble shooting and repairing broken circuits in landing light wiring
circuits.
(17) Replacing bulbs, reflectors, and lenses of position and landing
lights.
(18) Replacing wheels and skis where no weight and balance computation is
involved.
(19) Replacing any cowling not requiring removal of the propeller or
disconnection of flight controls.
(20) Replacing or cleaning spark plugs and setting of spark plug gap
clearance.
(21) Replacing any hose connection except hydraulic connections.
(22) Replacing prefabricated fuel lines.
(23) Cleaning or replacing fuel and oil strainers or filter elements.
(24) Replacing and servicing batteries.
(25) Cleaning of balloon burner pilot and main nozzles in accordance with
the balloon manufacturer's instructions.
(26) Replacement or adjustment of nonstructural standard fasteners
incidental to operations.
(27) The interchange of balloon baskets and burners on envelopes when the
basket or burner is designated as interchangeable in the balloon type
certificate data and the baskets and burners are specifically designed for
quick removal and installation.
(28) The installations of anti-misfueling devices to reduce the diameter of
fuel tank filler openings provided the specific device has been made a part
of the aircraft type certificiate data by the aircraft manufacturer, the
aircraft manufacturer has provided FAA-approved instructions for installation
of the specific device, and installation does not involve the disassembly of
the existing tank filler opening.
(29) Removing, checking, and replacing magnetic chip detectors.
(30) The inspection and maintenance tasks prescribed and specifically
identified as preventive maintenance in a primary category aircraft type
certificate or supplemental type certificate holder's approved special
inspection and preventive maintenance program when accomplished on a primary
category aircraft provided:
(i) They are performed by the holder of at least a private pilot
certificate issued under part 61 who is the registered owner (including co-
owners) of the affected aircraft and who holds a certificate of competency
for the affected aircraft (1) issued by a school approved under Sec.
147.21(e) of this chapter; (2) issued by the holder of the production
certificate for that primary category aircraft that has a special training
program approved under Sec. 21.24 of this subchapter; or (3) issued by
another entity that has a course approved by the Administrator; and
(ii) The inspections and maintenance tasks are performed in accordance with
instructions contained by the special inspection and preventive maintenance
program approved as part of the aircraft's type design or supplemental type
design.
(31) Removing and replacing self-contained, front instrument panel-mounted
navigation and communication devices that employ tray-mounted connectors that
connect the unit when the unit is installed into the instrument panel,
(excluding automatic flight control systems, transponders, and microwave
frequency distance measuring equipment (DME)). The approved unit must be
designed to be readily and repeatedly removed and replaced, and pertinent
instructions must be provided. Prior to the unit's intended use, and
operational check must be performed in accordance with the applicable
sections of part 91 of this chapter.
(32) Updating self-contained, front instrument panel-mounted Air Traffic
Control (ATC) navigational software data bases (excluding those of automatic
flight control systems, transponders, and microwave frequency distance
measuring equipment (DME)) provided no disassembly of the unit is required
and pertinent instructions are provided. Prior to the unit's intended use, an
operational check must be performed in accordance with applicable sections of
part 91 of this chapter.