Section 125.411

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

a form and manner prescribed by the
Administrator.
(b) Each certificate holder shall submit each report required by this section, covering each 24-hour period beginning at 0900 local time of each day
and ending at 0900 local time on the
next day, to the FAA office in Oklahoma City, Oklahoma. Each report of
occurrences during a 24-hour period
shall be submitted to the collection
point within the next 96 hours. However, a report due on Saturday or Sunday may be submitted on the following
Monday, and a report due on a holiday
may be submitted on the next work
day.

(c) When an airworthiness release
form is prepared, the certificate holder
must give a copy to the pilot in command and keep a record of it for at
least 60 days.
(d) Instead of restating each of the
conditions of the certification required
by paragraph (b) of this section, the
certificate holder may state in its
manual that the signature of a person
authorized in part 43 of this chapter
constitutes that certification.

[Doc. No. 19779, 45 FR 67235, Oct. 9, 1980, as
amended by Amdt. 125-49, 70 FR 76979, Dec.
29, 2005]

SOURCE: Amdt. 125-53, 72 FR 63412, Nov. 8,
2007, unless otherwise noted.

Section 125.411 Airworthiness
release
maintenance record entry.

or

(a) No certificate holder may operate
an airplane after maintenance, preventive maintenance, or alteration is performed on the airplane unless the person performing that maintenance, preventive maintenance, or alteration prepares or causes to be prepared - 
(1) An airworthiness release; or
(2) An entry in the aircraft maintenance records in accordance with the
certificate holder-s manual.
(b) The airworthiness release or
maintenance record entry required by
paragraph (a) of this section must - 
(1) Be prepared in accordance with
the procedures set forth in the certificate holder-s manual;
(2) Include a certification that - 
(i) The work was performed in accordance with the requirements of the
certificate holder-s manual;
(ii) All items required to be inspected
were inspected by an authorized person
who determined that the work was satisfactorily completed;
(iii) No known condition exists that
would make the airplane unairworthy;
and
(iv) So far as the work performed is
concerned, the airplane is in condition
for safe operation; and
(3) Be signed by a person authorized
in part 43 of this chapter to perform
maintenance, preventive maintenance,
and alteration.

Subpart M - Continued Airworthiness and Safety Improvements

Section 125.501 Purpose and definition.
(a) This subpart requires operators to
support the continued airworthiness of
each airplane. These requirements may
include, but are not limited to, revising
the inspection program, incorporating
design changes, and incorporating revisions to Instructions for Continued
Airworthiness.
(b) [Reserved]
[Amdt. 125-53, 72 FR 63412, Nov. 8, 2007, as
amended by Docket FAA-2018-0119, Amdt.
125-68, 83 FR 9174, Mar. 5, 2018]

Section 125.503

[Reserved]

Section 125.505 Repairs assessment for pressurized fuselages.
(a) No person may operate an Airbus
Model A300 (excluding the -600 series),
British Aerospace Model BAC 1-11, Boeing Model 707, 720, 727, 737 or 747,
McDonnell Douglas Model DC-8, DC-9/
MD-80 or DC-10, Fokker Model F28, or
Lockheed Model L-1011 beyond the applicable flight cycle implementation
time specified below, or May 25, 2001,
whichever occurs later, unless operations specifications have been issued
to reference repair assessment guidelines applicable to the fuselage pressure boundary (fuselage skin, door
skin, and bulkhead webs), and those
guidelines are incorporated in its
maintenance program. The repair assessment guidelines must be approved
by the responsible Aircraft Certification Service office for the type certificate for the affected airplane.

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