247
Federal Aviation Administration, DOT
§ 121.703
(b) Each certificate holder shall have
an approved procedure for keeping ade-
quate copies of the record required in
paragraph (a) of this section in the air-
plane in a place readily accessible to
each flight crewmember and shall put
that procedure in the certificate hold-
er’s manual.
§ 121.703 Service difficulty reports.
(a) Each certificate holder shall re-
port the occurrence or detection of
each failure, malfunction, or defect
concerning—
(1) Fires during flight and whether
the related fire-warning system func-
tioned properly;
(2) Fires during flight not protected
by a related fire-warning system;
(3) False fire warning during flight;
(4) An engine exhaust system that
causes damage during flight to the en-
gine, adjacent structure, equipment, or
components;
(5) An aircraft component that
causes accumulation or circulation of
smoke, vapor, or toxic or noxious
fumes in the crew compartment or pas-
senger cabin during flight;
(6) Engine shutdown during flight be-
cause of flameout;
(7) Engine shutdown during flight
when external damage to the engine or
airplane structure occurs;
(8) Engine shutdown during flight due
to foreign object ingestion or icing;
(9) Engine shutdown during flight of
more than one engine;
(10) A propeller feathering system or
ability of the system to control over-
speed during flight;
(11) A fuel or fuel-dumping system
that affects fuel flow or causes haz-
ardous leakage during flight;
(12) An unwanted landing gear exten-
sion or retraction, or an unwanted
opening or closing of landing gear
doors during flight;
(13) Brake system components that
result in loss of brake actuating force
when the airplane is in motion on the
ground;
(14) Aircraft structure that requires
major repair;
(15) Cracks, permanent deformation,
or corrosion of aircraft structures, if
more than the maximum acceptable to
the manufacturer or the FAA;
(16) Aircraft components or systems
that result in taking emergency ac-
tions during flight (except action to
shut down an engine); and
(17) Emergency evacuation systems
or components including all exit doors,
passenger emergency evacuation light-
ing systems, or evacuation equipment
that are found defective, or that fail to
perform the intended functions during
an actual emergency or during train-
ing, testing, maintenance, demonstra-
tions, or inadvertent deployments.
(b) For the purpose of this section
during flight
means the period from the
moment the aircraft leaves the surface
of the earth on takeoff until it touches
down on landing.
(c) In addition to the reports required
by paragraph (a) of this section, each
certificate holder shall report any
other failure, malfunction, or defect in
an aircraft that occurs or is detected at
any time if, in its opinion, that failure,
malfunction, or defect has endangered
or may endanger the safe operation of
an aircraft used by it.
(d) 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 offices 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.
(e) The certificate holder shall sub-
mit the reports required by this section
on a form or in another format accept-
able to the Administrator. The reports
shall include the following informa-
tion:
(1) Type and identification number of
the aircraft.
(2) The name of the operator.
(3) The date, flight number, and stage
during which the incident occurred
(e.g., preflight, takeoff, climb, cruise,
descent landing, and inspection).
(4) The emergency procedure effected
(e.g., unscheduled landing and emer-
gency descent).
248
14 CFR Ch. I (1–1–24 Edition)
§ 121.705
(5) The nature of the failure, mal-
function, or defect.
(6) Identification of the part and sys-
tem involved, including available infor-
mation pertaining to type designation
of the major component and time since
overhaul.
(7) Apparent cause of the failure,
malfunction, or defect (e.g., wear,
crack, design deficiency, or personnel
error).
(8) Whether the part was repaired, re-
placed, sent to the manufacturer, or
other action taken.
(9) Whether the aircraft was ground-
ed.
(10) Other pertinent information nec-
essary for more complete identifica-
tion, determination of seriousness, or
corrective action.
(f) A certificate holder that is also
the holder of a Type Certificate (in-
cluding a Supplemental Type Certifi-
cate), a Parts Manufacturer Approval,
or a Technical Standard Order Author-
ization, or that is the licensee of a type
certificate holder, need not report a
failure, malfunction, or defect under
this section if the failure, malfunction,
or defect has been reported by it under
§ 21.3 of this chapter or under the acci-
dent reporting provisions of 49 CFR
part 830.
(g) No person may withhold a report
required by this section even though
all information required in this section
is not available.
(h) When certificate holder gets addi-
tional information, including informa-
tion from the manufacturer or other
agency, concerning a report required
by this section, it shall expeditiously
submit it as a supplement to the first
report and reference the date and place
of submission of the first report.
[Doc. No. 6258, 29 FR 19226, Dec. 31, 1964, as
amended by Doc. No. 8084, 32 FR 5770, Apr. 11,
1967; Amdt. 121–72, 35 FR 18188, Nov. 28, 1970;
Amdt. 121–143, 43 FR 22642, May 25, 1978;
Amdt. 121–178, 47 FR 13316, Mar. 29, 1982;
Amdt. 121–187, 50 FR 32375, Aug. 9, 1985;
Amdt. 121–195, 53 FR 8728, Mar. 16, 1988;
Amdt. 121–251, 60 FR 65936, Dec. 20, 1995;
Amdt. 121–319, 70 FR 76979, Dec. 29, 2005;
Amdt. 121–387, 87 FR 75846, Dec. 9, 2022]
§ 121.705 Mechanical interruption
summary report.
Each certificate holder shall submit
to the Administrator, before the end of
the 10th day of the following month, a
summary report for the previous
month of:
(a) Each interruption to a flight, un-
scheduled change of aircraft en route,
or unscheduled stop or diversion from a
route, caused by known or suspected
mechanical difficulties or malfunctions
that are not required to be reported
under § 121.703.
(b) The number of engines removed
prematurely because of malfunction,
failure or defect, listed by make and
model and the aircraft type in which it
was installed.
(c) The number of propeller
featherings in flight, listed by type of
propeller and engine and aircraft on
which it was installed. Propeller
featherings for training, demonstra-
tion, or flight check purposes need not
be reported.
[Doc. No. 6258, 29 FR 19226, Dec. 31, 1964, as
amended by Amdt. 121–10, 30 FR 10025, Aug.
12, 1965; Amdt. 121–319, 70 FR 76979, Dec. 29,
2005]
§ 121.707 Alteration and repair re-
ports.
(a) Each certificate holder shall,
promptly upon its completion, prepare
a report of each major alteration or
major repair of an airframe, aircraft
engine, propeller, or appliance of an
aircraft operated by it.
(b) The certificate holder shall sub-
mit a copy of each report of a major al-
teration to, and shall keep a copy of
each report of a major repair available
for inspection by, the representative of
the Administrator who is assigned to
it.
§ 121.709 Airworthiness release or air-
craft log entry.
(a) No certificate holder may operate
an aircraft after maintenance, preven-
tive maintenance or alterations are
performed on the aircraft unless the
certificate holder, or the person with
whom the certificate holder arranges
for the performance of the mainte-
nance, preventive maintenance, or al-
terations, prepares or causes to be pre-
pared—
(1) An airworthiness release; or
(2) An appropriate entry in the air-
craft log.