767
Federal Aviation Administration, DOT
§ 91.413
(2) A schedule for performing the in-
spections that must be performed
under the program expressed in terms
of the time in service, calendar time,
number of system operations, or any
combination of these.
(h)
Changes from one inspection pro-
gram to another.
When an operator
changes from one inspection program
under paragraph (f) of this section to
another, the time in service, calendar
times, or cycles of operation accumu-
lated under the previous program must
be applied in determining inspection
due times under the new program.
(Approved by the Office of Management and
Budget under control number 2120–0005)
[Doc. No. 18334, 54 FR 34311, Aug. 18, 1989;
Amdt. 91–211, 54 FR 41211, Oct. 5, 1989; Amdt.
91–267, 66 FR 21066, Apr. 27, 2001; Amdt. 91–282,
69 FR 44882, July 27, 2004; Docket FAA–2018–
0119, Amdt. 91–350, 83 FR 9171, Mar. 5, 2018]
§ 91.410
[Reserved]
§ 91.411
Altimeter system and altitude
reporting equipment tests and in-
spections.
(a) No person may operate an air-
plane, or helicopter, in controlled air-
space under IFR unless—
(1) Within the preceding 24 calendar
months, each static pressure system,
each altimeter instrument, and each
automatic pressure altitude reporting
system has been tested and inspected
and found to comply with appendices E
and F of part 43 of this chapter;
(2) Except for the use of system drain
and alternate static pressure valves,
following any opening and closing of
the static pressure system, that system
has been tested and inspected and
found to comply with paragraph (a),
appendix E, of part 43 of this chapter;
and
(3) Following installation or mainte-
nance on the automatic pressure alti-
tude reporting system of the ATC
transponder where data correspondence
error could be introduced, the inte-
grated system has been tested, in-
spected, and found to comply with
paragraph (c), appendix E, of part 43 of
this chapter.
(b) The tests required by paragraph
(a) of this section must be conducted
by—
(1) The manufacturer of the airplane,
or helicopter, on which the tests and
inspections are to be performed;
(2) A certificated repair station prop-
erly equipped to perform those func-
tions and holding—
(i) An instrument rating, Class I;
(ii) A limited instrument rating ap-
propriate to the make and model of ap-
pliance to be tested;
(iii) A limited rating appropriate to
the test to be performed;
(iv) An airframe rating appropriate
to the airplane, or helicopter, to be
tested; or
(3) A certificated mechanic with an
airframe rating (static pressure system
tests and inspections only).
(c) Altimeter and altitude reporting
equipment approved under Technical
Standard Orders are considered to be
tested and inspected as of the date of
their manufacture.
(d) No person may operate an air-
plane, or helicopter, in controlled air-
space under IFR at an altitude above
the maximum altitude at which all al-
timeters and the automatic altitude re-
porting system of that airplane, or hel-
icopter, have been tested.
[Doc. No. 18334, 54 FR 34308, Aug. 18, 1989, as
amended by Amdt. 91–269, 66 FR 41116, Aug. 6,
2001; 72 FR 7739, Feb. 20, 2007]
§ 91.413
ATC transponder tests and in-
spections.
(a) No persons may use an ATC trans-
ponder that is specified in 91.215(a),
121.345(c), or § 135.143(c) of this chapter
unless, within the preceding 24 cal-
endar months, the ATC transponder
has been tested and inspected and
found to comply with appendix F of
part 43 of this chapter; and
(b) Following any installation or
maintenance on an ATC transponder
where data correspondence error could
be introduced, the integrated system
has been tested, inspected, and found
to comply with paragraph (c), appendix
E, of part 43 of this chapter.
(c) The tests and inspections speci-
fied in this section must be conducted
by—
(1) A certificated repair station prop-
erly equipped to perform those func-
tions and holding—
(i) A radio rating, Class III;
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