(a) General. The factors, tests, and inspections specified in
paragraphs (b) and (c) of this section must be applied in addition to
those necessary to establish foundry quality control. The inspections must
meet approved specifications. Paragraphs (c) and (d) of this section apply
to structural castings except castings that are pressure tested as parts
of hydraulic or other fluid systems and do not support structural loads.
(b) Bearing stresses and surfaces. The casting factors specified
in paragraphs (c) and (d) of this section --
(1) Need not exceed 1.25 with respect to bearing stresses regardless of
the method of inspection used; and
(2) Need not be used with respect to the bearing surfaces of a part
whose bearing factor is larger than the applicable casting factor.
(c) Critical castings. For each casting whose failure would
preclude continued safe flight and landing of the rotorcraft or result in
serious injury to any occupant, the following apply:
(1) Each critical casting must --
(i) Have a casting factor of not less than 1.25; and
(ii) Receive 100 percent inspection by visual, radiographic, and
magnetic particle (for ferromagnetic materials) or penetrant (for
nonferromagnetic materials) inspection methods or approved equivalent
inspection methods.
(2) For each critical casting with a casting factor less than 1.50,
three sample castings must be static tested and shown to meet --
(i) The strength requirements of §29.305 at an ultimate load
corresponding to a casting factor of 1.25; and
(ii) The deformation requirements of §29.305 at a load of 1.15 times
the limit load.
(d) Noncritical castings. For each casting other than those
specified in paragraph (c) of this section, the following apply:
(1) Except as provided in paragraphs (d)(2) and (3) of this section,
the casting factors and corresponding inspections must meet the following
table: