362
14 CFR Ch. I (1–1–19 Edition)
§ 125.411
a form and manner prescribed by the
Administrator.
(b) Each certificate holder shall sub-
mit each report required by this sec-
tion, covering each 24-hour period be-
ginning at 0900 local time of each day
and ending at 0900 local time on the
next day, to the FAA office in Okla-
homa City, Oklahoma. Each report of
occurrences during a 24-hour period
shall be submitted to the collection
point within the next 96 hours. How-
ever, a report due on Saturday or Sun-
day may be submitted on the following
Monday, and a report due on a holiday
may be submitted on the next work
day.
[Doc. No. 19779, 45 FR 67235, Oct. 9, 1980, as
amended by Amdt. 125–49, 70 FR 76979, Dec.
29, 2005]
§ 125.411
Airworthiness release or
maintenance record entry.
(a) No certificate holder may operate
an airplane after maintenance, preven-
tive maintenance, or alteration is per-
formed on the airplane unless the per-
son performing that maintenance, pre-
ventive maintenance, or alteration pre-
pares or causes to be prepared—
(1) An airworthiness release; or
(2) An entry in the aircraft mainte-
nance 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 certifi-
cate holder’s manual;
(2) Include a certification that—
(i) The work was performed in ac-
cordance 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 sat-
isfactorily 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.
(c) When an airworthiness release
form is prepared, the certificate holder
must give a copy to the pilot in com-
mand 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.
Subpart M—Continued Airworthi-
ness and Safety Improve-
ments
S
OURCE
: Amdt. 125–53, 72 FR 63412, Nov. 8,
2007, unless otherwise noted.
§ 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 revi-
sions 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]
§ 125.503
[Reserved]
§ 125.505
Repairs assessment for pres-
surized fuselages.
(a) No person may operate an Airbus
Model A300 (excluding the –600 series),
British Aerospace Model BAC 1–11, Boe-
ing 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 ap-
plicable flight cycle implementation
time specified below, or May 25, 2001,
whichever occurs later, unless oper-
ations specifications have been issued
to reference repair assessment guide-
lines applicable to the fuselage pres-
sure boundary (fuselage skin, door
skin, and bulkhead webs), and those
guidelines are incorporated in its
maintenance program. The repair as-
sessment guidelines must be approved
by the responsible Aircraft Certifi-
cation Service office for the type cer-
tificate for the affected airplane.
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