- Y Diweddaraf sydd Ar Gael (Diwygiedig)
- Gwreiddiol (Fel y’i mabwysiadwyd gan yr UE)
Commission Regulation (EU) No 965/2012 of 5 October 2012 laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No 216/2008 of the European Parliament and of the Council
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There are outstanding changes not yet made to Commission Regulation (EU) No 965/2012. Any changes that have already been made to the legislation appear in the content and are referenced with annotations.
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used by the flight crew to control the flight path;
used to comply with NCC.IDE.A.245;
used to comply with NCC.IDE.A.250; or
installed in the aeroplane.
spare fuses;
independent portable lights;
an accurate time piece;
chart holder;
first-aid kits;
survival and signalling equipment;
sea anchor and equipment for mooring; and
child restraint device.
the information provided by those instruments, equipment or accessories shall not be used by the flight crew members to comply with Annex II to Regulation (EU) 2018/1139 or points NCC.IDE.A.245 and NCC.IDE.A.250 of this Annex;
the instruments and equipment shall not affect the airworthiness of the aeroplane, even in the case of failures or malfunction.]
Textual Amendments
F2Substituted by Commission Implementing Regulation (EU) 2019/1384 of 24 July 2019 amending Regulations (EU) No 965/2012 and (EU) No 1321/2014 as regards the use of aircraft listed on an air operator certificate for non-commercial operations and specialised operations, the establishment of operational requirements for the conduct of maintenance check flights, the establishment of rules on non-commercial operations with reduced cabin crew on board and introducing editorial updates concerning air operations requirements (Text with EEA relevance).
A flight shall not be commenced when any of the aeroplane’s instruments, items of equipment, or functions, required for the intended flight are inoperative or missing, unless:
the aeroplane is operated in accordance with the operator’s minimum equipment list (MEL);
[F2the operator is approved by the [F3CAA] to operate the aeroplane within the constraints of the master minimum equipment list ( ‘ MMEL ’ ) in accordance with point ORO.MLR.105(j) of Annex III; or]
the aeroplane is subject to a permit to fly issued in accordance with the applicable airworthiness requirements.
Textual Amendments
F3Word in Annex 6 point NCC.IDE.A.105(b) substituted (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 368(4) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)
Aeroplanes shall be equipped with spare electrical fuses, of the ratings required for complete circuit protection, for replacement of those fuses that are allowed to be replaced in flight.
Aeroplanes operated at night shall be equipped with:
an anti-collision light system;
navigation/position lights;
a landing light;
lighting supplied from the aeroplane’s electrical system to provide adequate illumination for all instruments and equipment essential to the safe operation of the aeroplane;
lighting supplied from the aeroplane’s electrical system to provide illumination in all passenger compartments;
an independent portable light for each crew member station; and
lights to conform with the International Regulations for Preventing Collisions at Sea if the aeroplane is operated as a seaplane.
magnetic-heading;
time in hours, minutes and seconds;
[F2barometric altitude;]
indicated airspeed;
slip; and
Mach number whenever speed limitations are expressed in terms of Mach number.
a means of measuring and displaying the following:
turn and slip;
attitude;
vertical speed; and
stabilised heading;
a means of indicating when the supply of power to the gyroscopic instruments is not adequate; and
a means of preventing malfunction of the airspeed indicating system required in (a)(4) due to condensation or icing.
[F2barometric altitude;]
indicated airspeed;
slip, or turn and slip, as applicable;
attitude, if applicable;
vertical speed, if applicable;
stabilised heading, if applicable; and
Mach number whenever speed limitations are expressed in terms of Mach number, if applicable.
Aeroplanes operated under IFR shall be equipped with:
a means of measuring and displaying the following:
magnetic heading;
time in hours, minutes and seconds;
[F2barometric altitude;]
indicated airspeed;
vertical speed;
turn and slip;
attitude;
stabilised heading;
outside air temperature; and
Mach number whenever speed limitations are expressed in terms of Mach number;
a means of indicating when the supply of power to the gyroscopic instruments is not adequate;
whenever two pilots are required for the operation, an additional separate means of displaying for the second pilot:
[F2barometric altitude;]
indicated airspeed;
vertical speed;
turn and slip;
attitude;
stabilised heading; and
Mach number whenever speed limitations are expressed in terms of Mach number, if applicable;
a means of preventing malfunction of the airspeed indicating systems required in (a)(4) and (c)(2) due to condensation or icing;
an alternate source of static pressure;
a chart holder in an easily readable position that can be illuminated for night operations;
a second independent means of measuring and displaying altitude; and
[F2an emergency power supply, independent of the main electrical generating system, for the purpose of operating and illuminating an attitude indicating system for a minimum period of 30 minutes. The emergency power supply shall be automatically operative after the total failure of the main electrical generating system and clear indication shall be given on the instrument or on the instrument panel that the attitude indicator is being operated by emergency power.]
Aeroplanes operated under IFR with a single pilot shall be equipped with an autopilot with at least altitude hold and heading mode.
Turbine-powered aeroplanes with a maximum certified take-off mass (MCTOM) of more than 5 700 kg or a maximum operational passenger seating configuration (MOPSC) of more than nine shall be equipped with a TAWS that meets the requirements for:
class A equipment, as specified in an acceptable standard, in the case of aeroplanes for which the individual certificate of airworthiness (CofA) was first issued after 1 January 2011 ; or
class B equipment, as specified in an acceptable standard, in the case of aeroplanes for which the individual CofA was first issued on or before 1 January 2011 .
Unless otherwise provided for by Regulation (EU) No 1332/2011, turbine-powered aeroplanes with an MCTOM of more than 5 700 kg or an MOPSC of more than 19 shall be equipped with ACAS II.
The following aeroplanes shall be equipped with airborne weather detecting equipment when operated at night or in IMC in areas where thunderstorms or other potentially hazardous weather conditions, regarded as detectable with airborne weather detecting equipment, may be expected to exist along the route:
pressurised aeroplanes;
non-pressurised aeroplanes with an MCTOM of more than 5 700 kg; and
non-pressurised aeroplanes with an MOPSC of more than nine.
Aeroplanes operated in expected or actual icing conditions at night shall be equipped with a means to illuminate or detect the formation of ice.
The means to illuminate the formation of ice shall not cause glare or reflection that would handicap flight crew members in the performance of their duties.
Aeroplanes operated by more than one flight crew member shall be equipped with a flight crew interphone system, including headsets and microphones for use by all flight crew members.
aeroplanes with an MCTOM of more than 27 000 kg and first issued with an individual CofA on or after 1 January 2016 ; and
aeroplanes with an MCTOM of more than 2 250 kg:
certified for operation with a minimum crew of at least two pilots;
equipped with turbojet engine(s) or more than one turboprop engine; and
for which a type certificate is first issued on or after 1 January 2016 .
[F5the preceding 25 hours for aeroplanes with an MCTOM of more than 27 000 kg and first issued with an individual CofA on or after 1 January 2022 ; or]
the preceding 2 hours in all other cases.]
Textual Amendments
Textual Amendments
voice communications transmitted from or received in the flight crew compartment by radio;
flight crew members’ voice communications using the interphone system and the public address system, if installed;
the aural environment of the flight crew compartment, including, without interruption, the audio signals received from each boom and mask microphone in use; and
voice or audio signals identifying navigation or approach aids introduced into a headset or speaker.
data link communication messages related to ATS communications to and from the aeroplane, including messages applying to the following applications:
data link initiation;
controller–pilot communication;
addressed surveillance;
flight information;
as far as is practicable, given the architecture of the system, aircraft broadcast surveillance;
as far as is practicable, given the architecture of the system, aircraft operational control data; and
as far as is practicable, given the architecture of the system, graphics;
information that enables correlation to any associated records related to data link communications and stored separately from the aeroplane; and
information on the time and priority of data link communications messages, taking into account the system’s architecture.
Compliance with CVR requirements and FDR requirements may be achieved by:
one flight data and cockpit voice combination recorder if the aeroplane has to be equipped with a CVR or an FDR; or
two flight data and cockpit voice combination recorders if the aeroplane has to be equipped with a CVR and an FDR.
a seat or berth for each person on board who is aged 24 months or more;
a seat belt on each passenger seat and restraining belts for each berth;
a child restraint device (CRD) for each person on board younger than 24 months;
a seat belt with upper torso restraint system incorporating a device that will automatically restrain the occupant’s torso in the event of rapid deceleration:
on each flight crew seat and on any seat alongside a pilot’s seat; and
on each observer’s seat located in the flight crew compartment;
and
a seat belt with upper torso restraint system on the seats for the minimum required cabin crew, in the case of aeroplanes first issued with an individual CofA after 31 December 1980 .
a single point release;
on the seats for the minimum number of required cabin crew members, two shoulder straps and a seat belt that may be used independently;
on flight crew members seats and on any seat alongside a pilot's seat, either of the following:
two shoulder straps and a seat belt that may be used independently;
a diagonal shoulder strap and a seat belt that may be used independently for the following aeroplanes:
aeroplanes with an MCTOM of 5 700 kg or less and with an MOPSC of nine or less that are compliant with the emergency landing dynamic conditions defined in the applicable certification specification;
aeroplanes with an MCTOM of 5 700 kg or less and with an MOPSC of nine or less that are not compliant with the emergency landing dynamic conditions defined in the applicable certification specification and having an individual CofA first issued before 25 August 2016 .]
Aeroplanes in which not all passenger seats are visible from the flight crew seat(s) shall be equipped with a means of indicating to all passengers and cabin crew when seat belts shall be fastened and when smoking is not allowed.
Table 1 | |
Number of first-aid kits required | |
Number of passenger seats installed | Number of first-aid kits required |
---|---|
0 – 100 | 1 |
101 – 200 | 2 |
201 – 300 | 3 |
301 – 400 | 4 |
401 – 500 | 5 |
501 or more | 6 |
readily accessible for use; and
kept up-to-date.
all crew members and:
100 % of the passengers for any period when the cabin pressure altitude exceeds 15 000 ft, but in no case less than 10 minutes’ supply;
at least 30 % of the passengers, for any period when, in the event of loss of pressurisation and taking into account the circumstances of the flight, the pressure altitude in the passenger compartment will be between 14 000 ft and 15 000 ft; and
at least 10 % of the passengers for any period in excess of 30 minutes when the pressure altitude in the passenger compartment will be between 10 000 ft and 14 000 ft;
all the occupants of the passenger compartment for no less than 10 minutes, in the case of aeroplanes operated at pressure altitudes above 25 000 ft, or operated below that altitude, but under conditions that will not allow them to descend safely to a pressure altitude of 13 000 ft within 4 minutes.
a device to provide a warning indication to the flight crew of any loss of pressurisation; and
quick donning masks for flight crew members.
all crew members and at least 10 % of the passengers for any period in excess of 30 minutes when the pressure altitude in the passenger compartment will be between 10 000 ft and 13 000 ft; and
all crew members and passengers for any period that the pressure altitude in the passenger compartments will be above 13 000 ft.
in the flight crew compartment; and
in each passenger compartment that is separate from the flight crew compartment, except if the compartment is readily accessible to the flight crew.
If areas of the aeroplane’s fuselage suitable for break-in by rescue crews in an emergency are marked, such areas shall be marked as shown in Figure 1.
an ELT of any type or an aircraft localisation means meeting the requirement of Annex IV (Part CAT), CAT.GEN.MPA.210, to Regulation (EU) No 965/2012, when first issued with an individual CofA on or before 1 July 2008 ;
an automatic ELT or an aircraft localisation means meeting the requirement of Annex IV (Part CAT), CAT.GEN.MPA.210, to Regulation (EU) No 965/2012, when first issued with an individual CofA after 1 July 2008 .]
landplanes operated over water at a distance of more than 50 NM from land or taking off or landing at an aerodrome or operating site where, in the opinion of the pilot-in-command, the take-off or approach path is so disposed over water that there would be a likelihood of a ditching; and
seaplanes operated over water.
a sea anchor and other equipment necessary to facilitate mooring, anchoring or manoeuvring the aeroplane on water, appropriate to its size, weight and handling characteristics; and
equipment for making the sound signals as prescribed in the International Regulations for Preventing Collisions at Sea, where applicable.
equipment for making the distress signals;
life-rafts in sufficient numbers to carry all persons on board, stowed so as to facilitate their ready use in emergency; and
life-saving equipment to provide the means of sustaining life, as appropriate to the flight to be undertaken.
signalling equipment to make the distress signals;
at least one survival ELT(S); and
additional survival equipment for the route to be flown taking account of the number of persons on board.
remains within a distance from an area where search and rescue is not especially difficult corresponding to:
120 minutes at one-engine-inoperative (OEI) cruising speed for aeroplanes capable of continuing the flight to an aerodrome with the critical engine(s) becoming inoperative at any point along the route or planned diversion routes; or
30 minutes at cruising speed for all other aeroplanes;
or
remains within a distance no greater than that corresponding to 90 minutes at cruising speed from an area suitable for making an emergency landing, for aeroplanes certified in accordance with the applicable airworthiness standard.
conducting two-way communication for aerodrome control purposes;
receiving meteorological information at any time during flight;
conducting two-way communication at any time during flight with those aeronautical stations and on those frequencies prescribed by the appropriate authority; and
providing for communication on the aeronautical emergency frequency 121,5 MHz.
the ATS flight plan, if applicable; and
the applicable airspace requirements.
Textual Amendments
Textual Amendments
F7Inserted by Commission Implementing Regulation (EU) 2019/1384 of 24 July 2019 amending Regulations (EU) No 965/2012 and (EU) No 1321/2014 as regards the use of aircraft listed on an air operator certificate for non-commercial operations and specialised operations, the establishment of operational requirements for the conduct of maintenance check flights, the establishment of rules on non-commercial operations with reduced cabin crew on board and introducing editorial updates concerning air operations requirements (Text with EEA relevance).
Aeroplanes shall be equipped with a pressure altitude reporting secondary surveillance radar (SSR) transponder and any other SSR transponder capability required for the route being flown.
Aeronautical databases used on certified aircraft system applications shall meet data quality requirements that are adequate for the intended use of the data.
The operator shall ensure the timely distribution and insertion of current and unaltered aeronautical databases to all aircraft that require them.
Notwithstanding any other occurrence reporting requirements as defined in Regulation (EU) No 376/2014, the operator shall report to the database provider instances of erroneous, inconsistent or missing data that might be reasonably expected to constitute a hazard to flight.
In such cases, the operator shall inform flight crew and other personnel concerned, and shall ensure that the affected data is not used.]]
Textual Amendments
Textual Amendments
F1Inserted by Commission Regulation (EU) No 800/2013 of 14 August 2013 amending Regulation (EU) No 965/2012 laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No 216/2008 of the European Parliament and of the Council (Text with EEA relevance).
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