Appendix A to Part 43 - Major Alterations, Major Repairs, and Preventive Maintenance
14:188.8.131.52.22.0.283.14.45 : Appendix A
Appendix A to Part 43 - Major Alterations, Major Repairs, and
(a) Major alterations - (1) Airframe major
alterations. Alterations of the following parts and alterations
of the following types, when not listed in the aircraft
specifications issued by the FAA, are airframe major
(ii) Tail surfaces.
(iv) Engine mounts.
(v) Control system.
(vi) Landing gear.
(vii) Hull or floats.
(viii) Elements of an airframe including spars, ribs, fittings,
shock absorbers, bracing, cowling, fairings, and balance
(ix) Hydraulic and electrical actuating system of
(x) Rotor blades.
(xi) Changes to the empty weight or empty balance which result
in an increase in the maximum certificated weight or center of
gravity limits of the aircraft.
(xii) Changes to the basic design of the fuel, oil, cooling,
heating, cabin pressurization, electrical, hydraulic, de-icing, or
(xiii) Changes to the wing or to fixed or movable control
surfaces which affect flutter and vibration characteristics.
(2) Powerplant major alterations. The following
alterations of a powerplant when not listed in the engine
specifications issued by the FAA, are powerplant major
(i) Conversion of an aircraft engine from one approved model to
another, involving any changes in compression ratio, propeller
reduction gear, impeller gear ratios or the substitution of major
engine parts which requires extensive rework and testing of the
(ii) Changes to the engine by replacing aircraft engine
structural parts with parts not supplied by the original
manufacturer or parts not specifically approved by the
(iii) Installation of an accessory which is not approved for the
(iv) Removal of accessories that are listed as required
equipment on the aircraft or engine specification.
(v) Installation of structural parts other than the type of
parts approved for the installation.
(vi) Conversions of any sort for the purpose of using fuel of a
rating or grade other than that listed in the engine
(3) Propeller major alterations. The following
alterations of a propeller when not authorized in the propeller
specifications issued by the FAA are propeller major
(i) Changes in blade design.
(ii) Changes in hub design.
(iii) Changes in the governor or control design.
(iv) Installation of a propeller governor or feathering
(v) Installation of propeller de-icing system.
(vi) Installation of parts not approved for the propeller.
(4) Appliance major alterations. Alterations of the basic
design not made in accordance with recommendations of the appliance
manufacturer or in accordance with an FAA Airworthiness Directive
are appliance major alterations. In addition, changes in the basic
design of radio communication and navigation equipment approved
under type certification or a Technical Standard Order that have an
effect on frequency stability, noise level, sensitivity,
selectivity, distortion, spurious radiation, AVC characteristics,
or ability to meet environmental test conditions and other changes
that have an effect on the performance of the equipment are also
(b) Major repairs - (1) Airframe major repairs.
Repairs to the following parts of an airframe and repairs of the
following types, involving the strengthening, reinforcing,
splicing, and manufacturing of primary structural members or their
replacement, when replacement is by fabrication such as riveting or
welding, are airframe major repairs.
(i) Box beams.
(ii) Monocoque or semimonocoque wings or control surfaces.
(iii) Wing stringers or chord members.
(v) Spar flanges.
(vi) Members of truss-type beams.
(vii) Thin sheet webs of beams.
(viii) Keel and chine members of boat hulls or floats.
(ix) Corrugated sheet compression members which act as flange
material of wings or tail surfaces.
(x) Wing main ribs and compression members.
(xi) Wing or tail surface brace struts.
(xii) Engine mounts.
(xiii) Fuselage longerons.
(xiv) Members of the side truss, horizontal truss, or
(xv) Main seat support braces and brackets.
(xvi) Landing gear brace struts.
(xix) Skis, and ski pedestals.
(xx) Parts of the control system such as control columns,
pedals, shafts, brackets, or horns.
(xxi) Repairs involving the substitution of material.
(xxii) The repair of damaged areas in metal or plywood stressed
covering exceeding six inches in any direction.
(xxiii) The repair of portions of skin sheets by making
(xxiv) The splicing of skin sheets.
(xxv) The repair of three or more adjacent wing or control
surface ribs or the leading edge of wings and control surfaces,
between such adjacent ribs.
(xxvi) Repair of fabric covering involving an area greater than
that required to repair two adjacent ribs.
(xxvii) Replacement of fabric on fabric covered parts such as
wings, fuselages, stabilizers, and control surfaces.
(xxviii) Repairing, including rebottoming, of removable or
integral fuel tanks and oil tanks.
(2) Powerplant major repairs. Repairs of the following
parts of an engine and repairs of the following types, are
powerplant major repairs:
(i) Separation or disassembly of a crankcase or crankshaft of a
reciprocating engine equipped with an integral supercharger.
(ii) Separation or disassembly of a crankcase or crankshaft of a
reciprocating engine equipped with other than spur-type propeller
(iii) Special repairs to structural engine parts by welding,
plating, metalizing, or other methods.
(3) Propeller major repairs. Repairs of the following
types to a propeller are propeller major repairs:
(i) Any repairs to, or straightening of steel blades.
(ii) Repairing or machining of steel hubs.
(iii) Shortening of blades.
(iv) Retipping of wood propellers.
(v) Replacement of outer laminations on fixed pitch wood
(vi) Repairing elongated bolt holes in the hub of fixed pitch
(vii) Inlay work on wood blades.
(viii) Repairs to composition blades.
(ix) Replacement of tip fabric.
(x) Replacement of plastic covering.
(xi) Repair of propeller governors.
(xii) Overhaul of controllable pitch propellers.
(xiii) Repairs to deep dents, cuts, scars, nicks, etc., and
straightening of aluminum blades.
(xiv) The repair or replacement of internal elements of
(4) Appliance major repairs. Repairs of the following
types to appliances are appliance major repairs:
(i) Calibration and repair of instruments.
(ii) Calibration of radio equipment.
(iii) Rewinding the field coil of an electrical accessory.
(iv) Complete disassembly of complex hydraulic power valves.
(v) Overhaul of pressure type carburetors, and pressure type
fuel, oil and hydraulic pumps.
(c) Preventive maintenance. Preventive maintenance is
limited to the following work, provided it does not involve complex
(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
(4) Servicing landing gear wheel bearings, such as cleaning and
(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
(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
(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
(21) Replacing any hose connection except hydraulic
(22) Replacing prefabricated fuel lines.
(23) Cleaning or replacing fuel and oil strainers or filter
(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
(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
(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 § 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 § 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.
(Secs. 313, 601 through 610, and 1102, Federal Aviation Act of 1958
as amended (49 U.S.C. 1354, 1421 through 1430 and 1502); (49 U.S.C.
106(g) (Revised Pub. L. 97-449, Jan. 21, 1983); and 14 CFR 11.45)
[Doc. No. 1993, 29 FR 5451, Apr. 23, 1964, as amended by Amdt.
43-14, 37 FR 14291, June 19, 1972; Amdt. 43-23, 47 FR 41086, Sept.
16, 1982; Amdt. 43-24, 49 FR 44602, Nov. 7, 1984; Amdt. 43-25, 51
FR 40703, Nov. 7, 1986; Amdt. 43-27, 52 FR 17277, May 6, 1987;
Amdt. 43-34, 57 FR 41369, Sept. 9, 1992; Amdt. 43-36, 61 FR 19501,
May 1, 1996; Amdt. 43-45, 77 FR 71096, Nov. 29, 2012]