(a)
No person may operate an airplane, or helicopter, in controlled airspace
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 Appendix
E 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), appendices E and F, of part 43 of this chapter; and
(3) Following
installation or maintenance on the automatic pressure altitude reporting
system of the 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.
(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 properly equipped to perform those functions and
holding--
(i) An
instrument rating, Class I;
(ii) A limited instrument rating appropriate to the make and model
of appliance 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
[(v) deleted]
(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 airplane, or helicopter, in controlled airspace under
IFR at an altitude above the maximum altitude at which all altimeters
and the automatic altitude reporting system of that airplane, or helicopter,
have been tested.
Amdt. 91-269, Eff. 4/6/2003