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ML.A.305 Aircraft continuing-airworthiness record system

Available versions for ERULES-1963177438-14276

Regulation (EU) 2019/1383 found in: Balloon Rule Book - Part-BOP Part-BFCL Part-ML CS-31GB CS-31HB CS-31TGB (Sep 2020)

Version Text

ML.A.305
Aircraft continuing-airworthiness record system

Regulation
(EU) 2019/1383

(a)     At the completion of any maintenance, the
certificate of release to service (CRS) required by point [ML.A.801](#_DxCrossRefBm1924813375)
shall be entered in the aircraft continuing airworthiness record system. Each
entry shall be made as soon as possible but not later than 30 days after the
day of the completion of the maintenance task.

(b)     The aircraft continuing airworthiness
records shall consist of an aircraft logbook, engine logbook(s) or engine
module log cards, propeller logbook(s) and log cards, for any
service-life-limited component, as appropriate.

(c)      The aircraft type and registration mark,
the date together with the total flight time and flight cycles and landings,
shall be entered in the aircraft logbooks.

(d)     The aircraft continuing airworthiness
records shall contain:

(1)     the current status of ADs and measures
mandated by the competent authority in immediate reaction to a safety problem;

(2)     the current status of modifications,
repairs and other DAH maintenance recommendations;

(3)     the current status of compliance with the
AMP;

(4)     the current status of service-life-limited
components;

(5)     the current mass and balance report;

(6)     the current list of deferred maintenance.

(e)     In addition to the authorised release
document, EASA Form 1, as set out in Appendix II of Annex I
(Part-M), or equivalent, the following information relevant to any component
installed, such as engine, propeller, engine module or service-life-limited
component, shall be entered in the appropriate engine or propeller logbook,
engine module or service-life-limited component log card:

(1)     the identification of the component;

(2)     the type, serial number and registration,
as appropriate, of the aircraft, engine, propeller, engine module or
service-life-limited component to which the particular component has been
fitted, along with the reference to the installation and removal of the
component;

(3)     the date together with the component’s
accumulated total flight time, flight cycles, landings and calendar time, as
relevant to the particular component;

(4)     the current information referred to in
point (d), applicable to the component.

(f)      The person or organisation responsible
for the management of continuing airworthiness and tasks pursuant to point [ML.A.201](#_DxCrossRefBm1924813371),
shall control the records as detailed in point [ML.A.305](#_DxCrossRefBm1924813386)
and present the records to the competent authority upon request.

(g)     All entries made in the aircraft
continuing airworthiness records shall be clear and accurate. When it is
necessary to correct an entry, the correction shall be made in a manner that
clearly shows the original entry.

(h)     An owner shall ensure that a system has
been established to keep the following records for the periods specified:

(1)     all detailed maintenance records in
respect of the aircraft and any service-life-limited component fitted thereto,
until such time as the information contained therein is superseded by new
information equivalent in scope and detail but no less than 36 months
after the aircraft or component has been released to service;

(2)     the total time in service, this is to say
hours, calendar time, cycles and landings, of the aircraft and all
service-life-limited components, for at least 12 months after the
aircraft or component has been permanently withdrawn from service;

(3)     the time in service, this is to say hours,
calendar time, cycles and landings, as appropriate, since the last scheduled
maintenance of the component subjected to a service life limit, at least until
the component scheduled maintenance has been superseded by another scheduled
maintenance of equivalent work scope and detail;

(4)     the current status of compliance with the
AMP at least until the scheduled maintenance of the aircraft or component has
been superseded by another scheduled maintenance of equivalent work scope and
detail;

(5)     the current status of ADs applicable to
the aircraft and components, at least 12 months after the aircraft or
component has been permanently withdrawn from service;

(6)     details of current modifications and
repairs to the aircraft, engine(s), propeller(s) and any other component vital
to flight safety, at least 12 months after they have been permanently
withdrawn from service.