FAA-H-8083-25C · Source PDF page 241
Flight Manuals and Other Documents
Preventive Maintenance · PHAK page 9-11
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is limited to work that does not involve complex assembly • Cleaning or replacing fuel and oil strainers or filter
operations including the following: elements; servicing batteries, cleaning balloon burner
pilot and main nozzles in accordance with the balloon
• Removal, installation, and repair of landing gear
manufacturer’s instructions.
tires and shock cords; servicing landing gear shock
struts by adding oil, air, or both; servicing gear wheel • The interchange of balloon baskets and burners on
bearings; replacing defective safety wiring or cotter envelopes when the basket or burner is designated as
keys; lubrication not requiring disassembly other than interchangeable in the balloon type certificate data
removal of nonstructural items, such as cover plates, and the baskets and burners are specifically designed
cowlings, and fairings; making simple fabric patches for quick removal and installation; adjustment
not requiring rib stitching or the removal of structural of nonstructural standard fasteners incidental to
parts or control surfaces. In the case of balloons, operations.
the making of small fabric repairs to envelopes
• The installations of anti-misfueling devices to reduce
(as defined in, and in accordance with, the balloon
the diameter of fuel tank filler openings only if the
manufacturer’s instructions) not requiring load tape
specific device has been made a part of the aircraft type
repair or replacement.
certificate data by the aircraft manufacturer, the aircraft
• Replenishing hydraulic fluid in the hydraulic manufacturer has provided FAA-approved instructions
reservoir; refinishing decorative coating of fuselage, for installation of the specific device, and installation
balloon baskets, wings, tail group surfaces (excluding does not involve the disassembly of the existing tank
balanced control surfaces), fairings, cowlings, filler opening; troubleshooting and repairing broken
landing gear, cabin, or flight deck interior when circuits in landing light wiring circuits.
removal or disassembly of any primary structure
• Removing and replacing self-contained, front
or operating system is not required; applying
instrument panel-mounted navigation and
preservative or protective material to components
communication devices that employ tray-mounted
where no disassembly of any primary structure or
connectors which connect the unit when the unit
operating system is involved and where such coating
is installed into the instrument panel (excluding
is not prohibited or is not contrary to good practices;
automatic flight control systems, transponders, and
repairing upholstery and decorative furnishings of the
microwave frequency distance measuring equipment
cabin, flight deck, or balloon basket interior when the
(DME)). The approved unit must be designed to be
repair does not require disassembly of any primary
readily and repeatedly removed and replaced, and
structure or operating system or interfere with an
pertinent instructions must be provided. Prior to the
operating system or affect the primary structure of
unit’s intended use, an operational check must be
the aircraft; making small, simple repairs to fairings,
performed in accordance with the applicable sections
nonstructural cover plates, cowlings, and small
of 14 CFR part 91 on checking, removing, and
patches and reinforcements not changing the contour
replacing magnetic chip detectors.
to interfere with proper air flow; replacing side
• Inspection and maintenance tasks prescribed and
windows where that work does not interfere with the
specifically identified as preventive maintenance in
structure or any operating system, such as controls,
a primary category aircraft type certificate or STC
electrical equipment, etc.
holder’s approved special inspection and preventive
• Replacing safety belts, seats or seat parts with
maintenance program when accomplished on a
replacement parts approved for the aircraft, not
primary category aircraft.
involving disassembly of any primary structure or
• Updating self-contained, front instrument panel-
operating system, bulbs, reflectors, and lenses of
mounted air traffic control (ATC) navigational
position and landing lights.
software databases (excluding those of automatic
• Replacing wheels and skis where no weight-and-
flight control systems, transponders, and microwave
balance computation is involved; replacing any
frequency DME), only if no disassembly of the unit is
cowling not requiring removal of the propeller or
required and pertinent instructions are provided; prior
disconnection of flight controls; replacing or cleaning
to the unit’s intended use, an operational check must
spark plugs and setting of spark plug gap clearance;
be performed in accordance with applicable sections
replacing any hose connection, except hydraulic
of 14 CFR part 91.
connections; however, prefabricated fuel lines may
be replaced.
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