819
Federal Aviation Administration, DOT
§ 91.1415
(3) Have the personnel to perform the
maintenance of program aircraft, in-
cluding airframes, aircraft engines,
propellers, rotors, appliances, emer-
gency equipment and parts, under its
manual and this chapter; or make ar-
rangements with another person for
the performance of maintenance. How-
ever, the program manager must en-
sure that any maintenance, preventive
maintenance, or alteration that is per-
formed by another person is performed
under the program manager’s oper-
ating manual and this chapter.
§ 91.1415
CAMP: Mechanical reliability
reports.
(a) Each program manager who main-
tains program aircraft under a CAMP
must report the occurrence or detec-
tion of each failure, malfunction, or de-
fect in an aircraft concerning—
(1) Fires during flight and whether
the related fire-warning system func-
tioned properly;
(2) Fires during flight not protected
by related fire-warning system;
(3) False fire-warning during flight;
(4) An exhaust system that causes
damage during flight to the engine, ad-
jacent structure, equipment, or compo-
nents;
(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
aircraft structure occurs;
(8) Engine shutdown during flight be-
cause of foreign object ingestion or
icing;
(9) Shutdown of more than one en-
gine during flight;
(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 opening or closing
of landing gear doors during flight;
(13) Brake system components that
result in loss of brake actuating force
when the aircraft 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; and
(16) Aircraft components or systems
that result in taking emergency ac-
tions during flight (except action to
shut down an engine).
(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
program manager must report any
other failure, malfunction, or defect in
an aircraft that occurs or is detected at
any time if, in the manager’s opinion,
the failure, malfunction, or defect has
endangered or may endanger the safe
operation of the aircraft.
(d) Each program manager must send
each report required by this section, in
writing, covering each 24-hour period
beginning at 0900 hours local time of
each day and ending at 0900 hours local
time on the next day to the Flight
Standards District Office that issued
the program manager’s management
specifications. Each report of occur-
rences during a 24-hour period must be
mailed or transmitted to that office
within the next 72 hours. However, a
report that is due on Saturday or Sun-
day may be mailed or transmitted on
the following Monday and one that is
due on a holiday may be mailed or
transmitted on the next workday. For
aircraft operated in areas where mail is
not collected, reports may be mailed or
transmitted within 72 hours after the
aircraft returns to a point where the
mail is collected.
(e) The program manager must trans-
mit the reports required by this section
on a form and in a manner prescribed
by the Administrator, and must in-
clude as much of the following as is
available:
(1) The type and identification num-
ber of the aircraft.
(2) The name of the program man-
ager.
(3) The date.
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