Federal Aviation Administration, DOT

Pt. 125, App. A

(2) Deactivate or remove an IMM or
FRM once installed unless it is replaced by a means that complies with
paragraph (d) of this section.
(g) Inspection Program Revisions. No
person may operate an airplane for
which airworthiness limitations have
been approved by the responsible Aircraft Certification Service office in accordance with SectionSection 26.33, 26.35, or 26.37 of
this chapter after the airplane is modified in accordance with paragraph (d)
of this section unless the inspection
program for that airplane is revised to
include those applicable airworthiness
limitations.
(h) After the inspection program is
revised as required by paragraph (g) of
this section, before returning an airplane to service after any alteration
for which airworthiness limitations are
required by SectionSection 25.981, 26.33, 26.35, or 26.37
of this chapter, the person must revise
the inspection program for the airplane
to include those airworthiness limitations.
(i) The inspection program changes
identified in paragraphs (g) and (h) of
this section must be submitted to the
operator-s assigned Flight Standards
office responsible for review and approval prior to incorporation.
(j) The requirements of paragraph (d)
of this section do not apply to airplanes operated in all-cargo service,
but those airplanes are subject to paragraph (f) of this section.
(k) After the date by which any person is required by this section to modify 100 percent of the affected fleet, no
person may operate in passenger service any airplane model specified in
Table 2 of this section unless the airplane has been modified to comply
with Section 26.33(c) of this chapter.
TABLE 2
Model - Boeing
747
737
777
767
757

Series ..................
Series ..................
Series ..................
Series.
Series.

Model - Airbus
A318, A319, A320, A321 Series.
A300, A310 Series.
A330, A340 Series.

(l) No person may operate any airplane on which an auxiliary fuel tank
is installed after December 26, 2017 unless the FAA has certified the tank as

compliant with Section 25.981 of this chapter,
in effect on December 26, 2008.
(m) Exclusions. The requirements of
this section do not apply to the following airplane models:
(1) Convair CV-240, 340, 440, including
turbine powered conversions.
(2) Lockheed L-188 Electra.
(3) Vickers VC-10.
(4) Douglas DC-3, including turbine
powered conversions.
(5) Bombardier CL-44.
(6) Mitsubishi YS-11.
(7) BAC 1-11.
(8) Concorde.
(9) deHavilland D.H. 106 Comet 4C.
(10) VFW - Vereinigte Flugtechnische
VFW-614.
(11) Illyushin Aviation IL 96T.
(12) Bristol Aircraft Britannia 305.
(13) Handley Page Herald Type 300.
(14) Avions Marcel Dassault - Breguet
Aviation Mercure 100C.
(15) Airbus Caravelle.
(16) Fokker F-27/Fairchild Hiller FH-
227.
(17) Lockheed L-300.
[Doc. No. FAA-2005-22997, 73 FR 42502, July
21, 2008, as amended by Amdt. 125-57, 74 FR
31619, July 2, 2009; Docket FAA-2018-0119,
Amdt. 125-68, 83 FR 9174, Mar. 5, 2018]

APPENDIX A TO PART 125 - ADDITIONAL
EMERGENCY EQUIPMENT
(a) Means for emergency evacuation. Each
passenger-carrying landplane emergency exit
(other than over-the-wing) that is more that
6 feet from the ground with the airplane on
the ground and the landing gear extended
must have an approved means to assist the
occupants in descending to the ground. The
assisting means for a floor level emergency
exit must meet the requirements of
Section 25.809(f)(1) of this chapter in effect on April
30, 1972, except that, for any airplane for
which the application for the type certificate
was filed after that date, it must meet the
requirements under which the airplane was
type certificated. An assisting means that
deploys automatically must be armed during
taxiing, takeoffs, and landings. However, if
the Administrator finds that the design of
the exit makes compliance impractical, the
Administrator may grant a deviation from
the requirement of automatic deployment if
the assisting means automatically erects
upon deployment and, with respect to required emergency exits, if an emergency
evacuation demonstration is conducted in

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