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Section 91.409

14 CFR Ch. I (1-1-19 Edition)

type certificate data sheets, airworthiness directives, and other approved
data. If the progressive inspection is
discontinued, the owner or operator
shall immediately notify the responsible Flight Standards office, in writing, of the discontinuance. After the
discontinuance, the first annual inspection under Section 91.409(a)(1) is due within 12
calendar months after the last complete inspection of the aircraft under
the progressive inspection. The 100hour inspection under Section 91.409(b) is due
within 100 hours after that complete
inspection. A complete inspection of
the aircraft, for the purpose of determining when the annual and 100-hour
inspections are due, requires a detailed
inspection of the aircraft and all its
components in accordance with the
progressive inspection. A routine inspection of the aircraft and a detailed
inspection of several components is not
considered to be a complete inspection.
(e) Large airplanes (to which part 125 is
not applicable), turbojet multiengine airplanes, turbopropeller-powered multiengine airplanes, and turbine-powered
rotorcraft. No person may operate a
large airplane, turbojet multiengine
airplane, turbopropeller-powered multiengine airplane, or turbine-powered
rotorcraft unless the replacement
times for life-limited parts specified in
the aircraft specifications, type data
sheets, or other documents approved by
the Administrator are complied with
and the airplane or turbine-powered
rotorcraft, including the airframe, engines, propellers, rotors, appliances,
survival equipment, and emergency
equipment, is inspected in accordance
with an inspection program selected
under the provisions of paragraph (f) of
this section, except that, the owner or
operator of a turbine-powered rotorcraft may elect to use the inspection
provisions of Section 91.409(a), (b), (c), or (d) in
lieu of an inspection option of
Section 91.409(f).
(f) Selection of inspection program
under paragraph (e) of this section. The
registered owner or operator of each
airplane or turbine-powered rotorcraft
described in paragraph (e) of this section must select, identify in the aircraft maintenance records, and use one
of the following programs for the inspection of the aircraft:

(1) A continuous airworthiness inspection program that is part of a continuous airworthiness maintenance
program currently in use by a person
holding an air carrier operating certificate or an operating certificate issued
under part 121 or 135 of this chapter and
operating that make and model aircraft under part 121 of this chapter or
operating that make and model under
part 135 of this chapter and maintaining it under Section 135.411(a)(2) of this chapter.
(2) An approved aircraft inspection
program approved under Section 135.419 of this
chapter and currently in use by a person holding an operating certificate
issued under part 135 of this chapter.
(3) A current inspection program recommended by the manufacturer.
(4) Any other inspection program established by the registered owner or
operator of that airplane or turbinepowered rotorcraft and approved by the
Administrator under paragraph (g) of
this section. However, the Administrator may require revision of this inspection program in accordance with
the provisions of Section 91.415.
Each operator shall include in the selected program the name and address
of the person responsible for scheduling
the inspections required by the program and make a copy of that program
available to the person performing inspections on the aircraft and, upon request, to the Administrator.
(g) Inspection program approved under
paragraph (e) of this section. Each operator of an airplane or turbine-powered
rotorcraft desiring to establish or
change an approved inspection program
under paragraph (f)(4) of this section
must submit the program for approval
to the responsible Flight Standards office. The program must be in writing
and include at least the following information:
(1) Instructions and procedures for
the conduct of inspections for the particular make and model airplane or
turbine-powered rotorcraft, including
necessary tests and checks. The instructions and procedures must set
forth in detail the parts and areas of
the airframe, engines, propellers, rotors, and appliances, including survival
and emergency equipment required to
be inspected.

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