Commission Regulation (EU) No 965/2012Show full title

[F1 SUBPART D INSTRUMENTS, DATA AND EQUIPMENT U.K.

SECTION 1 U.K. Aeroplanes

NCC.IDE.A.100 Instruments and equipment — general U.K.

(a) Instruments and equipment required by this Subpart shall be approved in accordance with the applicable airworthiness requirements if they are: U.K.

(1)

used by the flight crew to control the flight path;

(2)

used to comply with NCC.IDE.A.245;

(3)

used to comply with NCC.IDE.A.250; or

(4)

installed in the aeroplane.

(b) The following items, when required by this Subpart, do not need an equipment approval: U.K.

(1)

spare fuses;

(2)

independent portable lights;

(3)

an accurate time piece;

(4)

chart holder;

(5)

first-aid kits;

(6)

survival and signalling equipment;

(7)

sea anchor and equipment for mooring; and

(8)

child restraint device.

(c) Instruments and equipment not required by this Subpart as well as any other equipment which is not required by other applicable Annexes, but is carried on a flight, shall comply with the following: U.K.

(1)

the information provided by these instruments, equipment or accessories shall not be used by the flight crew to comply with Annex I to Regulation (EC) No 216/2008 or NCC.IDE.A.245 and NCC.IDE.A.250; and

(2)

the instruments and equipment shall not affect the airworthiness of the aeroplane, even in the case of failures or malfunction.

(d) Instruments and equipment shall be readily operable or accessible from the station where the flight crew member that needs to use it is seated. U.K.

(e) Those instruments that are used by a flight crew member shall be so arranged as to permit the flight crew member to see the indications readily from his/her station, with the minimum practicable deviation from the position and line of vision which he/she normally assumes when looking forward along the flight path. U.K.

(f) All required emergency equipment shall be easily accessible for immediate use. U.K.

NCC.IDE.A.105 Minimum equipment for flight U.K.

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:

(a)

the aeroplane is operated in accordance with the operator’s minimum equipment list (MEL);

(b)

the operator is approved by the competent authority to operate the aeroplane within the constraints of the master minimum equipment list (MMEL); or

(c)

the aeroplane is subject to a permit to fly issued in accordance with the applicable airworthiness requirements.

NCC.IDE.A.110 Spare electrical fuses U.K.

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.

NCC.IDE.A.115 Operating lights U.K.

Aeroplanes operated at night shall be equipped with:

(a)

an anti-collision light system;

(b)

navigation/position lights;

(c)

a landing light;

(d)

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;

(e)

lighting supplied from the aeroplane’s electrical system to provide illumination in all passenger compartments;

(f)

an independent portable light for each crew member station; and

(g)

lights to conform with the International Regulations for Preventing Collisions at Sea if the aeroplane is operated as a seaplane.

NCC.IDE.A.120 Operations under VFR — flight and navigational instruments and associated equipment U.K.

(a) Aeroplanes operated under VFR by day shall be equipped with a means of measuring and displaying the following: U.K.

(1)

magnetic-heading;

(2)

time in hours, minutes and seconds;

(3)

pressure altitude;

(4)

indicated airspeed;

(5)

slip; and

(6)

Mach number whenever speed limitations are expressed in terms of Mach number.

(b) Aeroplanes operated under visual meteorological conditions (VMC) over water and out of sight of the land, or under VMC at night, or in conditions where the aeroplane cannot be maintained in a desired flight path without reference to one or more additional instruments, shall be, in addition to (a), equipped with: U.K.

(1)

a means of measuring and displaying the following:

(i)

turn and slip;

(ii)

attitude;

(iii)

vertical speed; and

(iv)

stabilised heading;

(2)

a means of indicating when the supply of power to the gyroscopic instruments is not adequate; and

(3)

a means of preventing malfunction of the airspeed indicating system required in (a)(4) due to condensation or icing.

(c) Whenever two pilots are required for the operation, aeroplanes shall be equipped with an additional separate means of displaying the following: U.K.

(1)

pressure altitude;

(2)

indicated airspeed;

(3)

slip, or turn and slip, as applicable;

(4)

attitude, if applicable;

(5)

vertical speed, if applicable;

(6)

stabilised heading, if applicable; and

(7)

Mach number whenever speed limitations are expressed in terms of Mach number, if applicable.

NCC.IDE.A.125 Operations under IFR — flight and navigational instruments and associated equipment U.K.

Aeroplanes operated under IFR shall be equipped with:

(a)

a means of measuring and displaying the following:

(1)

magnetic heading;

(2)

time in hours, minutes and seconds;

(3)

pressure altitude;

(4)

indicated airspeed;

(5)

vertical speed;

(6)

turn and slip;

(7)

attitude;

(8)

stabilised heading;

(9)

outside air temperature; and

(10)

Mach number whenever speed limitations are expressed in terms of Mach number;

(b)

a means of indicating when the supply of power to the gyroscopic instruments is not adequate;

(c)

whenever two pilots are required for the operation, an additional separate means of displaying for the second pilot:

(1)

pressure altitude;

(2)

indicated airspeed;

(3)

vertical speed;

(4)

turn and slip;

(5)

attitude;

(6)

stabilised heading; and

(7)

Mach number whenever speed limitations are expressed in terms of Mach number, if applicable;

(d)

a means of preventing malfunction of the airspeed indicating systems required in (a)(4) and (c)(2) due to condensation or icing;

(e)

an alternate source of static pressure;

(f)

a chart holder in an easily readable position that can be illuminated for night operations;

(g)

a second independent means of measuring and displaying altitude; and

(h)

an 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 that the attitude indicator is being operated by emergency power.

NCC.IDE.A.130 Additional equipment for single-pilot operations under IFR U.K.

Aeroplanes operated under IFR with a single pilot shall be equipped with an autopilot with at least altitude hold and heading mode.

NCC.IDE.A.135 Terrain awareness warning system (TAWS) U.K.

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:

(a)

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

(b)

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 .

NCC.IDE.A.140 Airborne collision avoidance system (ACAS) U.K.

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.

NCC.IDE.A.145 Airborne weather detecting equipment U.K.

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:

(a)

pressurised aeroplanes;

(b)

non-pressurised aeroplanes with an MCTOM of more than 5 700 kg; and

(c)

non-pressurised aeroplanes with an MOPSC of more than nine.

NCC.IDE.A.150 Additional equipment for operations in icing conditions at night U.K.

(a)

Aeroplanes operated in expected or actual icing conditions at night shall be equipped with a means to illuminate or detect the formation of ice.

(b)

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.

NCC.IDE.A.155 Flight crew interphone system U.K.

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.

NCC.IDE.A.160 Cockpit voice recorder U.K.

(a) The following aeroplanes shall be equipped with a CVR: U.K.

(1)

aeroplanes with an MCTOM of more than 27 000 kg and first issued with an individual CofA on or after 1 January 2016 ; and

(2)

aeroplanes with an MCTOM of more than 2 250 kg:

(i)

certified for operation with a minimum crew of at least two pilots;

(ii)

equipped with turbojet engine(s) or more than one turboprop engine; and

(iii)

for which a type certificate is first issued on or after 1 January 2016 .

(b) The CVR shall be capable of retaining data recorded during at least the preceding 2 hours. U.K.

(c) The CVR shall record with reference to a timescale: U.K.

(1)

voice communications transmitted from or received in the flight crew compartment by radio;

(2)

flight crew members’ voice communications using the interphone system and the public address system, if installed;

(3)

the aural environment of the flight crew compartment, including, without interruption, the audio signals received from each boom and mask microphone in use; and

(4)

voice or audio signals identifying navigation or approach aids introduced into a headset or speaker.

(d) The CVR shall start automatically to record prior to the aeroplane moving under its own power and shall continue to record until the termination of the flight when the aeroplane is no longer capable of moving under its own power. U.K.

(e) In addition to (d), depending on the availability of electrical power, the CVR shall start to record as early as possible during the cockpit checks prior to engine start at the beginning of the flight until the cockpit checks immediately following engine shutdown at the end of the flight. U.K.

(f) The CVR shall have a device to assist in locating it in water. U.K.

NCC.IDE.A.165 Flight data recorder U.K.

(a) Aeroplanes with an MCTOM of more than 5 700 kg and first issued with an individual CofA on or after 1 January 2016 shall be equipped with an FDR that uses a digital method of recording and storing data and for which a method of readily retrieving that data from the storage medium is available. U.K.

(b) The FDR shall record the parameters required to determine accurately the aeroplane flight path, speed, attitude, engine power, configuration and operation and be capable of retaining data recorded during at least the preceding 25 hours. U.K.

(c) Data shall be obtained from aeroplane sources that enable accurate correlation with information displayed to the flight crew. U.K.

(d) The FDR shall start automatically to record the data prior to the aeroplane being capable of moving under its own power and shall stop automatically after the aeroplane is incapable of moving under its own power. U.K.

(e) The FDR shall have a device to assist in locating it in water. U.K.

NCC.IDE.A.170 Data link recording U.K.

(a) Aeroplanes first issued with an individual CofA on or after 1 January 2016 that have the capability to operate data link communications and are required to be equipped with a CVR shall record on a recorder, where applicable: U.K.

(1)

data link communication messages related to ATS communications to and from the aeroplane, including messages applying to the following applications:

(i)

data link initiation;

(ii)

controller–pilot communication;

(iii)

addressed surveillance;

(iv)

flight information;

(v)

as far as is practicable, given the architecture of the system, aircraft broadcast surveillance;

(vi)

as far as is practicable, given the architecture of the system, aircraft operational control data; and

(vii)

as far as is practicable, given the architecture of the system, graphics;

(2)

information that enables correlation to any associated records related to data link communications and stored separately from the aeroplane; and

(3)

information on the time and priority of data link communications messages, taking into account the system’s architecture.

(b) The recorder shall use a digital method of recording and storing data and information and a method for readily retrieving that data. The recording method shall allow the data to match the data recorded on the ground. U.K.

(c) The recorder shall be capable of retaining data recorded for at least the same duration as set out for CVRs in NCC.IDE.A.160. U.K.

(d) The recorder shall have a device to assist in locating it in water. U.K.

(e) The requirements applicable to the start and stop logic of the recorder are the same as the requirements applicable to the start and stop logic of the CVR contained in NCC.IDE.A.160(d) and (e). U.K.

NCC.IDE.A.175 Flight data and cockpit voice combination recorder U.K.

Compliance with CVR requirements and FDR requirements may be achieved by:

(a)

one flight data and cockpit voice combination recorder if the aeroplane has to be equipped with a CVR or an FDR; or

(b)

two flight data and cockpit voice combination recorders if the aeroplane has to be equipped with a CVR and an FDR.

NCC.IDE.A.180 Seats, seat safety belts, restraint systems and child restraint devices U.K.

(a) Aeroplanes shall be equipped with: U.K.

(1)

a seat or berth for each person on board who is aged 24 months or more;

(2)

a seat belt on each passenger seat and restraining belts for each berth;

(3)

a child restraint device (CRD) for each person on board younger than 24 months;

(4)

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:

(i)

on each flight crew seat and on any seat alongside a pilot’s seat; and

(ii)

on each observer’s seat located in the flight crew compartment;

and

(5)

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 .

(b) A seat belt with upper torso restraint system shall: U.K.

(1)

have a single point release; and

(2)

on flight crew seats, on any seat alongside a pilot’s seat and on the seats for the minimum required cabin crew, include two shoulder straps and a seat belt that may be used independently.

NCC.IDE.A.185 Fasten seat belt and no smoking signs U.K.

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.

NCC.IDE.A.190 First-aid kit U.K.

(a) Aeroplanes shall be equipped with first-aid kits in accordance with Table 1. U.K.

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

(b) First-aid kits shall be: U.K.

(1)

readily accessible for use; and

(2)

kept up-to-date.

NCC.IDE.A.195 Supplemental oxygen — pressurised aeroplanes U.K.

(a) Pressurised aeroplanes operated at flight altitudes for which the oxygen supply is required in accordance with (b) shall be equipped with oxygen storage and dispensing apparatus capable of storing and dispensing the required oxygen supplies. U.K.

(b) Pressurised aeroplanes operated above flight altitudes at which the pressure altitude in the passenger compartments is above 10 000 ft shall carry enough breathing oxygen to supply: U.K.

(1)

all crew members and:

(i)

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;

(ii)

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

(iii)

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;

(2)

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.

(c) Pressurised aeroplanes operated at flight altitudes above 25 000 ft shall, in addition, be equipped with: U.K.

(1)

a device to provide a warning indication to the flight crew of any loss of pressurisation; and

(2)

quick donning masks for flight crew members.

NCC.IDE.A.200 Supplemental oxygen — non-pressurised aeroplanes U.K.

(a) Non-pressurised aeroplanes operated at flight altitudes when the oxygen supply is required in accordance with (b) shall be equipped with oxygen storage and dispensing apparatus capable of storing and dispensing the required oxygen supplies. U.K.

(b) Non-pressurised aeroplanes operated above flight altitudes at which the pressure altitude in the passenger compartments is above 10 000 ft shall carry enough breathing oxygen to supply: U.K.

(1)

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

(2)

all crew members and passengers for any period that the pressure altitude in the passenger compartments will be above 13 000 ft.

NCC.IDE.A.205 Hand fire extinguishers U.K.

(a) Aeroplanes shall be equipped with at least one hand fire extinguisher: U.K.

(1)

in the flight crew compartment; and

(2)

in each passenger compartment that is separate from the flight crew compartment, except if the compartment is readily accessible to the flight crew.

(b) The type and quantity of extinguishing agent for the required fire extinguishers shall be suitable for the type of fire likely to occur in the compartment where the extinguisher is intended to be used and to minimise the hazard of toxic gas concentration in compartments occupied by persons. U.K.

NCC.IDE.A.206 Crash axe and crowbar U.K.

(a) Aeroplanes with an MCTOM of more than 5 700 kg or with an MOPSC of more than nine shall be equipped with at least one crash axe or crowbar located in the flight crew compartment. U.K.

(b) In the case of aeroplanes with an MOPSC of more than 200, an additional crash axe or crowbar shall be installed in or near the rearmost galley area. U.K.

(c) Crash axes and crowbars located in the passenger compartment shall not be visible to passengers. U.K.

NCC.IDE.A.210 Marking of break-in points U.K.

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.

Figure 1

Marking of break-in points

NCC.IDE.A.215 Emergency locator transmitter (ELT) U.K.

(a) Aeroplanes shall be equipped with: U.K.

(1)

an ELT of any type when first issued with an individual CofA on or before 1 July 2008 ;

(2)

an automatic ELT when first issued with an individual CofA after 1 July 2008 .

(b) ELTs of any type shall be capable of transmitting simultaneously on 121,5 MHz and 406 MHz. U.K.

NCC.IDE.A.220 Flight over water U.K.

(a) The following aeroplanes shall be equipped with a life-jacket for each person on board or equivalent individual floatation device for each person on board younger than 24 months, stowed in a position that is readily accessible from the seat or berth of the person for whose use it is provided: U.K.

(1)

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

(2)

seaplanes operated over water.

(b) Each life-jacket or equivalent individual flotation device shall be equipped with a means of electric illumination for the purpose of facilitating the location of persons. U.K.

(c) Seaplanes operated over water shall be equipped with: U.K.

(1)

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

(2)

equipment for making the sound signals as prescribed in the International Regulations for Preventing Collisions at Sea, where applicable.

(d) The pilot-in-command of an aeroplane operated at a distance away from land where an emergency landing is possible greater than that corresponding to 30 minutes at normal cruising speed or 50 NM, whichever is the lesser, shall determine the risks to survival of the occupants of the aeroplane in the event of a ditching, based on which he/she shall determine the carriage of: U.K.

(1)

equipment for making the distress signals;

(2)

life-rafts in sufficient numbers to carry all persons on board, stowed so as to facilitate their ready use in emergency; and

(3)

life-saving equipment to provide the means of sustaining life, as appropriate to the flight to be undertaken.

NCC.IDE.A.230 Survival equipment U.K.

(a) Aeroplanes operated over areas in which search and rescue would be especially difficult shall be equipped with: U.K.

(1)

signalling equipment to make the distress signals;

(2)

at least one survival ELT(S); and

(3)

additional survival equipment for the route to be flown taking account of the number of persons on board.

(b) The additional survival equipment specified in (a)(3) does not need to be carried when the aeroplane: U.K.

(1)

remains within a distance from an area where search and rescue is not especially difficult corresponding to:

(i)

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

(ii)

30 minutes at cruising speed for all other aeroplanes;

or

(2)

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.

NCC.IDE.A.240 Headset U.K.

(a) Aeroplanes shall be equipped with a headset with a boom microphone or equivalent for each flight crew member at their assigned station in the flight crew compartment. U.K.

(b) Aeroplanes operated under IFR or at night shall be equipped with a transmit button on the manual pitch and roll control for each required flight crew member. U.K.

NCC.IDE.A.245 Radio communication equipment U.K.

(a) Aeroplanes operated under IFR or at night, or when required by the applicable airspace requirements, shall be equipped with radio communication equipment that, under normal radio propagating conditions, shall be capable of: U.K.

(1)

conducting two-way communication for aerodrome control purposes;

(2)

receiving meteorological information at any time during flight;

(3)

conducting two-way communication at any time during flight with those aeronautical stations and on those frequencies prescribed by the appropriate authority; and

(4)

providing for communication on the aeronautical emergency frequency 121,5 MHz.

(b) When more than one communication equipment unit is required, each shall be independent of the other or others to the extent that a failure in any one will not result in failure of any other. U.K.

NCC.IDE.A.250 Navigation equipment U.K.

(a) Aeroplanes shall be equipped with navigation equipment that will enable them to proceed in accordance with: U.K.

(1)

the ATS flight plan, if applicable; and

(2)

the applicable airspace requirements.

(b) Aeroplanes shall have sufficient navigation equipment to ensure that, in the event of the failure of one item of equipment at any stage of the flight, the remaining equipment shall allow safe navigation in accordance with (a), or an appropriate contingency action, to be completed safely. U.K.

(c) Aeroplanes operated on flights in which it is intended to land in IMC shall be equipped with suitable equipment capable of providing guidance to a point from which a visual landing can be performed. This equipment shall be capable of providing such guidance for each aerodrome at which it is intended to land in IMC and for any designated alternate aerodromes. U.K.

NCC.IDE.A.255 Transponder U.K.

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.

NCC.IDE.A.260 Electronic navigation data management U.K.

(a) The operator shall only use electronic navigation data products that support a navigation application meeting standards of integrity that are adequate for the intended use of the data. U.K.

(b) When the electronic navigation data products support a navigation application needed for an operation for which Annex V (Part-SPA) to Regulation (EU) No 965/2012 requires an approval, the operator shall demonstrate to the competent authority that the process applied and the delivered products meet standards of integrity that are adequate for the intended use of the data. U.K.

(c) The operator shall continuously monitor both the process and the products, either directly or by monitoring the compliance of third party providers. U.K.

(d) The operator shall ensure the timely distribution and insertion of current and unaltered electronic navigation data to all aeroplanes that require it. U.K.

SECTION 2 U.K. Helicopters

NCC.IDE.H.100 Instruments and equipment — general U.K.

(a) Instruments and equipment required by this Subpart shall be approved in accordance with the applicable airworthiness requirements if they are: U.K.

(1)

used by the flight crew to control the flight path;

(2)

used to comply with NCC.IDE.H.245;

(3)

used to comply with NCC.IDE.H.250; or

(4)

installed in the helicopter.

(b) The following items, when required by this Subpart, do not need an equipment approval: U.K.

(1)

independent portable light;

(2)

an accurate time piece;

(3)

chart holder;

(4)

first-aid kit;

(5)

survival and signalling equipment;

(6)

sea anchor and equipment for mooring; and

(7)

child restraint device.

(c) Instruments and equipment not required by this Subpart as well as any other equipment which is not required by other applicable Annexes, but is carried on a flight, shall comply with the following: U.K.

(1)

the information provided by these instruments, equipment or accessories shall not be used by the flight crew to comply with Annex I to Regulation (EC) No 216/2008 or NCC.IDE.H.245 and NCC.IDE.H.250; and

(2)

the instruments and equipment shall not affect the airworthiness of the helicopter, even in the case of failures or malfunction.

(d) Instruments and equipment shall be readily operable or accessible from the station where the flight crew member that needs to use it is seated. U.K.

(e) Those instruments that are used by a flight crew member shall be so arranged as to permit the flight crew member to see the indications readily from his/her station, with the minimum practicable deviation from the position and line of vision which he/she normally assumes when looking forward along the flight path. U.K.

(f) All required emergency equipment shall be easily accessible for immediate use. U.K.

NCC.IDE.H.105 Minimum equipment for flight U.K.

A flight shall not be commenced when any of the helicopter’s instruments, items of equipment or functions required for the intended flight are inoperative or missing, unless:

(a)

the helicopter is operated in accordance with the operator’s minimum equipment list (MEL);

(b)

the operator is approved by the competent authority to operate the helicopter within the constraints of the master minimum equipment list (MMEL); or

(c)

the helicopter is subject to a permit to fly issued in accordance with the applicable airworthiness requirements.

NCC.IDE.H.115 Operating lights U.K.

Helicopters operated at night shall be equipped with:

(a)

an anti-collision light system;

(b)

navigation/position lights;

(c)

a landing light;

(d)

lighting supplied from the helicopter’s electrical system to provide adequate illumination for all instruments and equipment essential to the safe operation of the helicopter;

(e)

lighting supplied from the helicopter’s electrical system to provide illumination in all passenger compartments;

(f)

an independent portable light for each crew member station; and

(g)

lights to conform with the International Regulations for Preventing Collisions at Sea if the helicopter is amphibious.

NCC.IDE.H.120 Operations under VFR — flight and navigational instruments and associated equipment U.K.

(a) Helicopters operated under VFR by day shall be equipped with a means of measuring and displaying the following: U.K.

(1)

magnetic heading;

(2)

time in hours, minutes and seconds;

(3)

pressure altitude;

(4)

indicated airspeed; and

(5)

slip.

(b) Helicopters operated under VMC over water and out of sight of the land, or under VMC at night, or when the visibility is less than 1 500 m, or in conditions where the helicopter cannot be maintained in a desired flight path without reference to one or more additional instruments, shall be equipped, in addition to (a), with: U.K.

(1)

a means of measuring and displaying the following:

(i)

attitude;

(ii)

vertical speed; and

(iii)

stabilised heading;

(2)

a means of indicating when the supply of power to the gyroscopic instruments is not adequate; and

(3)

a means of preventing malfunction of the airspeed indicating system required in (a)(4) due to condensation or icing.

(c) Whenever two pilots are required for the operation, helicopters shall be equipped with an additional separate means of displaying the following: U.K.

(1)

pressure altitude;

(2)

indicated airspeed;

(3)

slip;

(4)

attitude, if applicable;

(5)

vertical speed, if applicable; and

(6)

stabilised heading, if applicable.

NCC.IDE.H.125 Operations under IFR — flight and navigational instruments and associated equipment U.K.

Helicopters operated under IFR shall be equipped with:

(a)

a means of measuring and displaying the following:

(1)

magnetic heading;

(2)

time in hours, minutes and seconds;

(3)

pressure altitude;

(4)

indicated airspeed;

(5)

vertical speed;

(6)

slip;

(7)

attitude;

(8)

stabilised heading; and

(9)

outside air temperature;

(b)

a means of indicating when the supply of power to the gyroscopic instruments is not adequate;

(c)

whenever two pilots are required for the operation, an additional separate means of displaying the following:

(1)

pressure altitude;

(2)

indicated airspeed;

(3)

vertical speed;

(4)

slip;

(5)

attitude; and

(6)

stabilised heading;

(d)

a means of preventing malfunction of the airspeed indicating systems required in (a)(4) and (c)(2) due to condensation or icing;

(e)

an alternate source of static pressure;

(f)

a chart holder in an easily readable position that can be illuminated for night operations; and

(g)

an additional means of measuring and displaying attitude as a standby instrument.

NCC.IDE.H.130 Additional equipment for single-pilot operations under IFR U.K.

Helicopters operated under IFR with a single pilot shall be equipped with an autopilot with at least altitude hold and heading mode.

NCC.IDE.H.145 Airborne weather detecting equipment U.K.

Helicopters with an MOPSC of more than nine and operated under IFR or at night shall be equipped with airborne weather detecting equipment when current weather reports indicate that thunderstorms or other potentially hazardous weather conditions, regarded as detectable with airborne weather detecting equipment, may be expected to exist along the route to be flown.

NCC.IDE.H.150 Additional equipment for operations in icing conditions at night U.K.

(a) Helicopters operated in expected or actual icing conditions at night shall be equipped with a means to illuminate or detect the formation of ice. U.K.

(b) 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. U.K.

NCC.IDE.H.155 Flight crew interphone system U.K.

Helicopters 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.

NCC.IDE.H.160 Cockpit voice recorder U.K.

(a) Helicopters with an MCTOM of more than 7 000 kg and first issued with an individual CofA on or after 1 January 2016 shall be equipped with a CVR. U.K.

(b) The CVR shall be capable of retaining data recorded during at least the preceding 2 hours. U.K.

(c) The CVR shall record with reference to a timescale: U.K.

(1)

voice communications transmitted from or received in the flight crew compartment by radio;

(2)

flight crew members’ voice communications using the interphone system and the public address system, if installed;

(3)

the aural environment of the cockpit, including, without interruption, the audio signals received from each crew microphone; and

(4)

voice or audio signals identifying navigation or approach aids introduced into a headset or speaker.

(d) The CVR shall start automatically to record prior to the helicopter moving under its own power and shall continue to record until the termination of the flight when the helicopter is no longer capable of moving under its own power. U.K.

(e) In addition to (d), depending on the availability of electrical power, the CVR shall start to record as early as possible during the cockpit checks prior to engine start at the beginning of the flight until the cockpit checks immediately following engine shutdown at the end of the flight. U.K.

(f) The CVR shall have a device to assist in locating it in water. U.K.

NCC.IDE.H.165 Flight data recorder U.K.

(a) Helicopters with an MCTOM of more than 3 175 kg and first issued with an individual CofA on or after 1 January 2016 shall be equipped with an FDR that uses a digital method of recording and storing data and for which a method of readily retrieving that data from the storage medium is available. U.K.

(b) The FDR shall record the parameters required to determine accurately the helicopter flight path, speed, attitude, engine power, configuration and operation and be capable of retaining data recorded during at least the preceding 10 hours. U.K.

(c) Data shall be obtained from helicopter sources that enable accurate correlation with information displayed to the flight crew. U.K.

(d) The FDR shall start automatically to record the data prior to the helicopter being capable of moving under its own power and shall stop automatically after the helicopter is incapable of moving under its own power. U.K.

(e) The FDR shall have a device to assist in locating it in water. U.K.

NCC.IDE.H.170 Data link recording U.K.

(a) Helicopters first issued with an individual CofA on or after 1 January 2016 that have the capability to operate data link communications and are required to be equipped with a CVR shall record on a recorder, where applicable: U.K.

(1)

data link communication messages related to ATS communications to and from the helicopter, including messages applying to the following applications:

(i)

data link initiation;

(ii)

controller–pilot communication;

(iii)

addressed surveillance;

(iv)

flight information;

(v)

as far as is practicable, given the architecture of the system, aircraft broadcast surveillance;

(vi)

as far as is practicable, given the architecture of the system, aircraft operational control data; and

(vii)

as far as is practicable, given the architecture of the system, graphics;

(2)

information that enables correlation to any associated records related to data link communications and stored separately from the helicopter; and

(3)

information on the time and priority of data link communications messages, taking into account the system’s architecture.

(b) The recorder shall use a digital method of recording and storing data and information and a method for readily retrieving that data. The recording method shall allow the data to match the data recorded on the ground. U.K.

(c) The recorder shall be capable of retaining data recorded for at least the same duration as set out for CVRs in NCC.IDE.H.160. U.K.

(d) The recorder shall have a device to assist in locating it in water. U.K.

(e) The requirements applicable to the start and stop logic of the recorder are the same as the requirements applicable to the start and stop logic of the CVR contained in NCC.IDE.H.160(d) and (e). U.K.

NCC.IDE.H.175 Flight data and cockpit voice combination recorder U.K.

Compliance with CVR and FDR requirements may be achieved by one flight data and cockpit voice combination recorder.

NCC.IDE.H.180 Seats, seat safety belts, restraint systems and child restraint devices U.K.

(a) Helicopters shall be equipped with: U.K.

(1)

a seat or berth for each person on board who is aged 24 months or more;

(2)

a seat belt on each passenger seat and restraining belts for each berth;

(3)

for helicopters first issued with an individual CofA after 31 December 2012 , a seat belt with an upper torso restraint system for each passenger who is aged 24 months or more;

(4)

a child restraint device (CRD) for each person on board younger than 24 months;

(5)

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

(6)

a seat belt with upper torso restraint system on the seats for the minimum required cabin crew, in the case of helicopters first issued with an individual CofA after 31 December 1980 .

(b) A seat belt with upper torso restraint system shall: U.K.

(1)

have a single point release; and

(2)

on flight crew seats, on any seat alongside a pilot’s seat and on the seats for the minimum required cabin crew, include two shoulder straps and a seat belt that may be used independently.

NCC.IDE.H.185 Fasten seat belt and no smoking signs U.K.

Helicopters 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.

NCC.IDE.H.190 First-aid kit U.K.

(a) Helicopters shall be equipped with at least one first-aid kit. U.K.

(b) The first-aid kit(s) shall be: U.K.

(1)

readily accessible for use; and

(2)

kept up-to-date.

NCC.IDE.H.200 Supplemental oxygen — non-pressurised helicopters U.K.

(a) Non-pressurised helicopters operated at flight altitudes when the oxygen supply is required in accordance with (b) shall be equipped with oxygen storage and dispensing apparatus capable of storing and dispensing the required oxygen supplies. U.K.

(b) Non-pressurised helicopters operated above flight altitudes at which the pressure altitude in the passenger compartments is above 10 000 ft shall carry enough breathing oxygen to supply: U.K.

(1)

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

(2)

all crew members and passengers for any period that the pressure altitude in the passenger compartment will be above 13 000 ft.

NCC.IDE.H.205 Hand fire extinguishers U.K.

(a) Helicopters shall be equipped with at least one hand fire extinguisher: U.K.

(1)

in the flight crew compartment; and

(2)

in each passenger compartment that is separate from the flight crew compartment, except if the compartment is readily accessible to the flight crew.

(b) The type and quantity of extinguishing agent for the required fire extinguishers shall be suitable for the type of fire likely to occur in the compartment where the extinguisher is intended to be used and to minimise the hazard of toxic gas concentration in compartments occupied by persons. U.K.

NCC.IDE.H.210 Marking of break-in points U.K.

If areas of the helicopter’s fuselage suitable for break-in by rescue crews in an emergency are marked, such areas shall be marked as shown in Figure 1.

Figure 1

Marking of break-in points

NCC.IDE.H.215 Emergency locator transmitter (ELT) U.K.

(a) Helicopters shall be equipped with at least one automatic ELT. U.K.

(b) Helicopters operating on a flight over water in support of offshore operations in a hostile environment and at a distance from land corresponding to more than 10 minutes flying time at normal cruising speed, where in the case of the critical engine failure, the helicopter is able to sustain level flight, shall be equipped with an automatically deployable ELT (ELT(AD)). U.K.

(c) An ELT of any type shall be capable of transmitting simultaneously on 121,5 MHz and 406 MHz. U.K.

NCC.IDE.H.225 Life-jackets U.K.

(a) Helicopters shall be equipped with a life-jacket for each person on board or equivalent individual floatation device for each person on board younger than 24 months, which shall be worn or stowed in a position that is readily accessible from the seat or berth of the person for whose use it is provided, when: U.K.

(1)

operated on a flight over water at a distance from land corresponding to more than 10 minutes flying time at normal cruising speed, where in the case of the critical engine failure, the helicopter is able to sustain level flight;

(2)

operated on a flight over water beyond autorotational distance from the land, where in the case of critical engine failure, the helicopter is not able to sustain level flight; or

(3)

taking off or landing at an aerodrome or operating site where the take-off or approach path is over water.

(b) Each life-jacket or equivalent individual flotation device shall be equipped with a means of electric illumination for the purpose of facilitating the location of persons. U.K.

NCC.IDE.H.226 Crew survival suits U.K.

Each crew member shall wear a survival suit when:

(a)

operating on a flight over water in support of offshore operations, at a distance from land corresponding to more than 10 minutes flying time at normal cruising speed, where in the case of the critical engine failure, the helicopter is able to sustain level flight and when:

(1)

the weather report or forecasts available to the pilot-in-command indicate that the sea temperature will be less than plus 10 °C during the flight; or

(2)

the estimated rescue time exceeds the estimated survival time;

or

(b)

so determined by the pilot-in-command based on a risk assessment taking into account the following conditions:

(1)

flights over water beyond autorotational distance or safe forced landing distance from land, where in the case of the critical engine failure, the helicopter is not able to sustain level flight; and

(2)

the weather report or forecasts available to the pilot-in-command indicate that the sea temperature will be less than plus 10 °C during the flight.

NCC.IDE.H.227 Life-rafts, survival ELTs and survival equipment on extended overwater flights U.K.

Helicopters operated:

(a)

on a flight over water at a distance from land corresponding to more than 10 minutes flying time at normal cruising speed, where in the case of the critical engine failure, the helicopter is able to sustain level flight; or

(b)

on a flight over water at a distance corresponding to more than 3 minutes flying time at normal cruising speed, where in the case of the critical engine failure, the helicopter is not able to sustain level flight, and if so determined by the pilot-in-command by means of a risk assessment;

shall be equipped with:

(1)

in the case of a helicopter carrying less than 12 persons, at least one life-raft with a rated capacity of not less than the maximum number of persons on board, stowed so as to facilitate their ready use in emergency;

(2)

in the case of a helicopter carrying more than 11 persons, at least two life-rafts, stowed so as to facilitate their ready use in an emergency, sufficient together to accommodate all persons capable of being carried on board and, if one is lost the remaining life-raft(s) having the overload capacity sufficient to accommodate all persons on the helicopter;

(3)

at least one survival ELT (ELT(S)) for each required life-raft; and

(4)

life-saving equipment, including means of sustaining life, as appropriate to the flight to be undertaken.

NCC.IDE.H.230 Survival equipment U.K.

Helicopters operated over areas in which search and rescue would be especially difficult shall be equipped with:

(a)

signalling equipment to make distress signals;

(b)

at least one survival ELT (ELT(S)); and

(c)

additional survival equipment for the route to be flown taking account of the number of persons on board.

NCC.IDE.H.231 Additional requirements for helicopters conducting offshore operations in a hostile sea area U.K.

Helicopters operated in offshore operations in a hostile sea area, at a distance from land corresponding to more than 10 minutes flying time at normal cruising speed, shall comply with the following:

(a)

When the weather report or forecasts available to the pilot-in-command indicate that the sea temperature will be less than plus 10 °C during the flight, or when the estimated rescue time exceeds the calculated survival time, or the flight is planned to be conducted at night, all persons on board are wearing a survival suit.

(b)

All life-rafts carried in accordance with NCC.IDE.H.227 shall be installed so as to be usable in the sea conditions in which the helicopter’s ditching, flotation and trim characteristics were evaluated in order to comply with the ditching requirements for certification.

(c)

The helicopter shall be equipped with an emergency lighting system with an independent power supply to provide a source of general cabin illumination to facilitate the evacuation of the helicopter.

(d)

All emergency exits, including crew emergency exits, and the means of opening them shall be conspicuously marked for the guidance of occupants using the exits in daylight or in the dark. Such markings shall be designed to remain visible if the helicopter is capsized and the cabin is submerged.

(e)

All non-jettisonable doors that are designated as ditching emergency exits shall have a means of securing them in the open position so that they do not interfere with occupants’ egress in all sea conditions up to the maximum required to be evaluated for ditching and flotation.

(f)

All doors, windows or other openings in the passenger compartment intended to be used for the purpose of underwater escape shall be equipped so as to be operable in an emergency.

(g)

Life-jackets shall be worn at all times, unless the passenger or crew member is wearing an integrated survival suit that meets the combined requirement of the survival suit and life-jacket.

NCC.IDE.H.232 Helicopters certified for operating on water — miscellaneous equipment U.K.

Helicopters certified for operating on water shall be equipped with:

(a)

a sea anchor and other equipment necessary to facilitate mooring, anchoring or manoeuvring the helicopter on water, appropriate to its size, weight and handling characteristics; and

(b)

equipment for making the sound signals prescribed in the International Regulations for Preventing Collisions at Sea, where applicable.

NCC.IDE.H.235 All helicopters on flights over water — ditching U.K.

Helicopters shall be designed for landing on water or certified for ditching in accordance with the relevant airworthiness code or fitted with emergency flotation equipment when operated on a flight over water in a hostile environment at a distance from land corresponding to more than 10 minutes flying time at normal cruising speed.

NCC.IDE.H.240 Headset U.K.

Whenever a radio communication and/or radio navigation system is required, helicopters shall be equipped with a headset with boom microphone or equivalent and a transmit button on the flight controls for each required pilot and/or crew member at his/her assigned station.

NCC.IDE.H.245 Radio communication equipment U.K.

(a) Helicopters operated under IFR or at night, or when required by the applicable airspace requirements, shall be equipped with radio communication equipment that, under normal radio propagating conditions, shall be capable of: U.K.

(1)

conducting two-way communication for aerodrome control purposes;

(2)

receiving meteorological information;

(3)

conducting two-way communication at any time during flight with those aeronautical stations and on those frequencies prescribed by the appropriate authority; and

(4)

providing for communication on the aeronautical emergency frequency 121,5 MHz.

(b) When more than one communications equipment unit is required, each shall be independent of the other or others to the extent that a failure in any one will not result in failure of any other. U.K.

(c) When a radio communication system is required, and in addition to the flight crew interphone system required in NCC.IDE.H.155, helicopters shall be equipped with a transmit button on the flight controls for each required pilot and crew member at his/her assigned station. U.K.

NCC.IDE.H.250 Navigation equipment U.K.

(a) Helicopters shall be equipped with navigation equipment that will enable them to proceed in accordance with: U.K.

(1)

the ATS flight plan, if applicable; and

(2)

the applicable airspace requirements.

(b) Helicopters shall have sufficient navigation equipment to ensure that, in the event of the failure of one item of equipment at any stage of the flight, the remaining equipment shall allow safe navigation in accordance with (a), or an appropriate contingency action, to be completed safely. U.K.

(c) Helicopters operated on flights in which it is intended to land in IMC shall be equipped with navigation equipment capable of providing guidance to a point from which a visual landing can be performed. This equipment shall be capable of providing such guidance for each aerodrome at which it is intended to land in IMC and for any designated alternate aerodromes. U.K.

NCC.IDE.H.255 Transponder U.K.

Helicopters 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.]

Textual Amendments

F1 Inserted 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).