265
Federal Aviation Administration, DOT
§ 25.621
that are pressure tested as parts of hy-
draulic 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 appli-
cable casting factor.
(c)
Critical castings.
Each casting
whose failure could preclude continued
safe flight and landing of the airplane
or could result in serious injury to oc-
cupants is a critical casting. Each crit-
ical casting must have a factor associ-
ated with it for showing compliance
with strength and deformation require-
ments of § 25.305, and must comply with
the following criteria associated with
that factor:
(1) A casting factor of 1.0 or greater
may be used, provided that—
(i) It is demonstrated, in the form of
process qualification, proof of product,
and process monitoring that, for each
casting design and part number, the
castings produced by each foundry and
process combination have coefficients
of variation of the material properties
that are equivalent to those of wrought
alloy products of similar composition.
Process monitoring must include test-
ing of coupons cut from the prolonga-
tions of each casting (or each set of
castings, if produced from a single pour
into a single mold in a runner system)
and, on a sampling basis, coupons cut
from critical areas of production cast-
ings. The acceptance criteria for the
process monitoring inspections and
tests must be established and included
in the process specifications to ensure
the properties of the production cast-
ings are controlled to within levels
used in design.
(ii) Each casting receives:
(A) Inspection of 100 percent of its
surface, using visual inspection and liq-
uid penetrant or equivalent inspection
methods; and
(B) Inspection of structurally signifi-
cant internal areas and areas where de-
fects are likely to occur, using radio-
graphic or equivalent inspection meth-
ods.
(iii) One casting undergoes a static
test and is shown to meet the strength
and deformation requirements of
§ 25.305(a) and (b).
(2) A casting factor of 1.25 or greater
may be used, provided that—
(i) Each casting receives:
(A) Inspection of 100 percent of its
surface, using visual inspection and liq-
uid penetrant or equivalent inspection
methods; and
(B) Inspection of structurally signifi-
cant internal areas and areas where de-
fects are likely to occur, using radio-
graphic or equivalent inspection meth-
ods.
(ii) Three castings undergo static
tests and are shown to meet:
(A) The strength requirements of
§ 25.305(b) at an ultimate load cor-
responding to a casting factor of 1.25;
and
(B) The deformation requirements of
§ 25.305(a) at a load of 1.15 times the
limit load.
(3) A casting factor of 1.50 or greater
may be used, provided that—
(i) Each casting receives:
(A) Inspection of 100 percent of its
surface, using visual inspection and liq-
uid penetrant or equivalent inspection
methods; and
(B) Inspection of structurally signifi-
cant internal areas and areas where de-
fects are likely to occur, using radio-
graphic or equivalent inspection meth-
ods.
(ii) One casting undergoes a static
test and is shown to meet:
(A) The strength requirements of
§ 25.305(b) at an ultimate load cor-
responding to a casting factor of 1.50;
and
(B) The deformation requirements of
§ 25.305(a) at a load of 1.15 times the
limit load.
(d)
Non-critical castings.
For each
casting other than critical castings, as
specified in paragraph (c) of this sec-
tion, the following apply:
(1) A casting factor of 1.0 or greater
may be used, provided that the require-
ments of (c)(1) of this section are met,
or all of the following conditions are
met:
(i) Castings are manufactured to ap-
proved specifications that specify the
minimum mechanical properties of the
material in the casting and provides
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