(a) some part of the Commonwealth;

(b) a Contracting State; or

(c) some other country in relation to which there is in force an agreement between Her Majesty's Government in the United Kingdom and the Government of that country which makes provision for the flight over the United Kingdom of aircraft registered in that country.

    (2)

(a) A glider may fly unregistered, and shall be deemed to be registered in the United Kingdom for the purposes of articles 14, 15, 21 and 43 of this Order, on any flight which:


(i) begins and ends in the United Kingdom without passing over any other country, and

(ii) is not for the purpose of public transport or aerial work other than aerial work which consists of the giving of instruction in flying or the conducting of flying tests in a glider owned or operated by a flying club of which the person giving the instruction or conducting the test and the person receiving the instruction or undergoing the test are both members.



(b) Any aircraft may fly unregistered on any flight which:



(i) begins and ends in the United Kingdom without passing over any other country, and

(ii) is in accordance with the 'B Conditions' set forth in Part A of Schedule 3 to this Order.



(c) Paragraph (1) shall not apply to any kite or captive balloon.

(a) The CAA shall grant an air operator's certificate if it is satisfied that the applicant is competent, having regard in particular to his previous conduct and experience, his equipment, organisation, staffing, maintenance and other arrangements, to secure the safe operation of aircraft of the types specified in the certificate on flights of the description and for the purposes so specified.

(b) A certificate may be granted subject to such conditions as the CAA thinks fit and shall, subject to article 81 of this Order, remain in force for the period specified in the certificate.

(a) a glider, if it is not being used for the public transport of passengers or aerial work other than aerial work which consists of the giving of instruction in flying or the conducting of flying tests in a glider owned or operated by a flying club of which the person giving the instruction or conducting the test and the person receiving the instruction or undergoing the test are both members;

(b) a balloon flying on a private flight;

(c) a kite;

(d) an aircraft flying in accordance with the 'A Conditions' or the 'B Conditions' set forth in Part A of Schedule 3 to this Order; or

(e) an aircraft flying in accordance with the conditions of a permit to fly issued by the CAA in respect of that aircraft.

(a) A flying machine registered in the United Kingdom and flying for the purpose of public transport having a maximum total weight authorised exceeding 5700 kg shall carry not less than two pilots as members of the flight crew thereof.

(b)


(i) Subject to sub-paragraphs (ii) and (iii), an aeroplane registered in the United Kingdom and flying for the purpose of public transport in circumstances where the aircraft commander is required to comply with the Instrument Flight Rules and having a maximum total weight authorised of 5700 kg or less and powered by:


(aa) one or more turbine jets;

(bb) one or more turbine propeller engines and provided with a means of pressurising the personnel compartments;

(cc) two or more turbine propeller engines and certificated to carry more than nine passengers;

(dd) two or more turbine propeller engines and certificated to carry fewer than 10 passengers and not provided with a means of pressurising the personnel compartments, unless it is equipped with an autopilot which has been approved by the CAA for the purposes of this article and which is serviceable on take-off; or

(ee) two or more piston engines, unless it is equipped with an autopilot which has been approved by the CAA for the purposes of this article and which is serviceable on take-off;



shall carry not less than two pilots as members of the flight crew thereof.

(ii) An aeroplane described in sub-paragraphs (i)(dd) or (i)(ee) which is equipped with an approved autopilot shall not be required to carry two pilots notwithstanding that before take-off the approved autopilot is found to be unserviceable, if the aeroplane flies in accordance with arrangements approved by the CAA.

(iii) An aeroplane described in sub-paragraphs (i)(cc), (dd) or (ee) which is flying under and in accordance with the terms of a police air operator's certificate shall not be required to carry two pilots.



(c)



(i) Subject to sub-paragraphs (i) and (ii), a helicopter registered in the United Kingdom which has a maximum total weight authorised of 5,700kg or less and a maximum approved seating configuration of 9 or less which is flying for the purpose of public transport in circumstances where the aircraft commander is required to comply with the Instrument Flight Rules or which is flying by night with visual ground reference shall carry not less than two pilots as members of the flight crew thereof unless it is equipped with an autopilot with, at least, altitude hold and heading mode which is serviceable on take off.

(ii) A helicopter described in sub-paragraph (c)(i) which is equipped with an approved autopilot shall not be required to carry two pilots notwithstanding that before take-off the approved autopilot is found to be unserviceable, if the helicopter flies in accordance with arrangements approved by the CAA.

(iii) A helicopter described in sub-paragraph (c)(i) which is flying under and in accordance with the terms of a police air operator's certificate shall not be required to carry two pilots.

    (4)

(a) An aircraft registered in the United Kingdom engaged on a flight for the purpose of public transport shall carry:


(i) a flight navigator as a member of the flight crew; or

(ii) navigational equipment suitable for the route to be flown;



if on the route or any diversion therefrom, being a route or diversion planned before take-off, the aircraft is intended to be more than 500 nautical miles from the point of take-off measured along the route to be flown, and to pass over part of an area specified in Schedule 7 to this Order.

(b) The flight navigator carried in compliance with this article shall be carried in addition to any person who is carried in accordance with this article to perform other duties.

    (5) An aircraft registered in the United Kingdom which is required by the provisions of article 15 of this Order to be equipped with radio communciations apparatus shall carry a flight radiotelephony operator as a member of the flight crew.

    (6) The CAA may, in the interests of safety, direct the operator of an aircraft registered in the United Kingdom that all or any aircraft operated by him, when flying in circumstances specified in the direction, shall carry, in addition to the flight crew required to be carried by the provisions of this article, such additional persons as members of the flight crew as it may specify in the direction.

    (7)

(a) This paragraph applies to any flight for the purpose of public transport by an aircraft registered in the United Kingdom:


(i) on which is carried 20 or more passengers; or

(ii) which may in accordance with its certificate of airworthiness carry more than 35 passengers and on which at least one passenger is carried.



(b) The crew of an aircraft on a flight to which this paragraph applies shall include cabin attendants carried for the purposes of performing in the interests of the safety of passengers, duties to be assigned by the operator or the commander of the aircraft but who shall not act as members of the flight crew.

(c)



(i) Subject to sub-paragraph (ii), on a flight to which this paragraph applies, there shall be carried not less than one cabin attendant for every 50 or fraction of 50 passenger seats installed in the aircraft.

(ii) The number of cabin attendants calculated in accordance with sub-paragraph (i) need not be carried if the CAA has granted written permission to the operator to carry a lesser number on that flight and the operator carries the number specified in that permission and complies with any other terms and conditions subject to which such permission is granted.

(a) Subject to sub-paragraph (b), this article shall apply to public transport aircraft registered in the United Kingdom except aircraft used for the time being solely for flights not intended to exceed 60 minutes in duration, which are either:


(i) flights solely for training persons to perform duties in an aircraft; or

(ii) flights intended to begin and end at the same aerodrome.



(b) This article shall not apply to an aircraft flying, or intended by the operator of the aircraft to fly solely under and in accordance with the terms of a police air operator's certificate.

    (2)

(a) The operator of every aircraft to which this article applies shall:


(i) make available to each member of his operating staff an operations manual;

(ii) ensure that each copy of the operations manual is kept up to date; and

(iii) ensure that on each flight every member of the crew has access to a copy of every part of the operations manual which is relevant to his duties on the flight.



(b)



(i) Subject to sub-paragraph (ii), each operations manual shall contain all such information and instructions as may be necessary to enable the operating staff to perform their duties as such including in particular information and instructions relating to the matters specified in Part A of Schedule 10 to this Order.

(ii) The operations manual shall not be required to contain any information or instructions available in a flight manual accessible to the persons by whom the information or instructions may be required.

    (3)

(a) An aircraft to which this article applies shall not fly unless, not less than 30 days prior to such flight, the operator of the aircraft has furnished to the CAA a copy of the whole of the operations manual for the time being in effect in respect of the aircraft.

(b) Subject to sub-paragraph (c), any amendments or additions to the operations manual shall be furnished to the CAA by the operator before or immediately after they come into effect.

(c) Where an amendment or addition relates to the operation of an aircraft to which the operations manual did not previously relate, that aircraft shall not fly for the purpose of public transport until the amendment or addition has been furnished to the CAA.

(d) Without prejudice to the foregoing sub-paragraphs, the operator shall make such amendments or additions to the operations manual as the CAA may require for the purpose of ensuring the safety of the aircraft or of persons or property carried therein or the safety, efficiency or regularity of air navigation.

(a) Subject to sub-paragraph (b), articles 72 and 73 of this Order apply in relation to any aircraft registered in the United Kingdom which is either:


(i) engaged on a flight for the purpose of public transport; or

(ii) operated by an air transport undertaking.



(b) Articles 72 and 73 of this Order shall not apply in relation to a flight made only for the purpose of instruction in flying given by or on behalf of a flying club or flying school, or a person who is not an air transport undertaking.

    (2) For the purposes of this Order:

(a) 'flight time', in relation to any person, means all time spent by that person in:


(i) a civil aircraft whether or not registered in the United Kingdom (other than such an aircraft of which the maximum total weight authorised does not exceed 1600 kg and which is not flying for the purpose of public transport or aerial work); or

(ii) a military aircraft (other than such an aircraft of which the maximum total weight authorised does not exceed 1600 kg and which is flying on a military air experience flight),



while it is in flight and he is carried therein as a member of the crew thereof;

(b) 'day' means a continuous period of 24 hours beginning at midnight Co-ordinated Universal Time;

(c) a helicopter shall be deemed to be in flight from the moment the helicopter first moves under its own power for the purpose of taking off until the rotors are next stopped; and

(d) a military air experience flight is a flight by a military aircraft operated under the auspices of the Royal Air Force Air Cadet Organisation for the purpose of providing air experience to its cadets.

(a) Subject to sub-paragraph (b), an aircraft registered in the United Kingdom shall, when in flight, carry documents in accordance with Schedule 11 to this Order.

(b) If the flight is intended to begin and end at the same aerodrome and does not include passage over the territory of any country other than the United Kingdom, the documents may be kept at that aerodrome instead of being carried in the aircraft.

(a) the manner in which aircraft may move or fly including in particular provision for requiring aircraft to give way to military aircraft;

(b) the lights and other signals to be shown or made by aircraft or persons;

(c) the lighting and marking of aerodromes; and

(d) any other provisions for securing the safety of aircraft in flight and in movement and the safety of persons and property on the surface.

    (2) Subject to the provisions of paragraph (3), it shall be an offence to contravene, to permit the contravention of, or to fail to comply with, the Rules of the Air.

    (3) It shall be lawful for the Rules of the Air to be departed from to the extent necessary:

(a) for avoiding immediate danger;

(b) for complying with the law of any country other than the United Kingdom within which the aircraft then is; or

(c) for complying with Military Flying Regulations (Joint Service Publication 318) or Flying Orders to Contractors (Aviation Publication 67) issued by the Secretary of State in relation to an aircraft of which the commander is acting as such in the course of his duty as a member of any of Her Majesty's naval, military or air forces.

(a) the service is provided in accordance with the standards and procedures specified in a manual of air traffic services in respect of that place;

(b) the manual is produced to the CAA within a reasonable time after a request for its production is made by the CAA; and

(c) such amendments or additions have been made to the manual as the CAA may from time to time require.

(a) an aerodrome licensed under this Order for the take-off and landing of such aircraft; or

(b) a Government aerodrome, or an aerodrome owned or managed by the CAA, notified as available for the take-off and landing of such aircraft, or in respect of which the person in charge of the aerodrome has given his permission for the particular aircraft to take off or land as the case may be;

and in accordance with any conditions subject to which the aerodrome may have been licensed or notified, or subject to which such permission may have been given.

    (2) Subject to paragraph (3), paragraph (1) applies to:

(a) aeroplanes of which the maximum total weight authorised exceeds 2730 kg and which are flying:


(i) for the purpose of the public transport of passengers;

(ii) for the purpose of instruction in flying given to any person for the purpose of becoming qualified for the grant of a pilot's licence or the inclusion of an aircraft rating, a night rating or a night qualification in a licence; or

(iii) for the purpose of carrying out flying tests in respect of the grant of a pilot's licence or the inclusion of an aircraft rating or a night rating in a licence;



(b) aeroplanes of which the maximum total weight authorised does not exceed 2730 kg engaged on either:



(i) scheduled journeys for the purpose of the public transport of passengers;

(ii) flights for the purpose of the public transport of passengers beginning and ending at the same aerodrome;

(iii) flights for the purpose of:


(aa) instruction in flying given to any person for the purpose of becoming qualified for the grant of a pilot's licence or the inclusion of an aircraft rating, a night rating or a night qualification in a licence; or

(bb) a flying test in respect of the grant of a pilot's licence or the inclusion of an aircraft rating, a night rating or a night qualification in a licence; or



(iv) flights for the purpose of the public transport of passengers at night;



(c) helicopters and gyroplanes engaged on such flights as are specified in sub-paragraphs (b)(i) and (iii); and

(d) gliders (other than gliders being flown under arrangements made by a flying club and carrying no person other than a member of the club) which are flying for the purpose of the public transport of passengers or for the purpose of instruction in flying.

    (3) Nothing in paragraph (1) shall apply to or in relation to an aircraft flying under and in accordance with the terms of a police air operator's certificate.

    (4)

(a) Subject to sub-paragraph (c), the person in charge of any area in the United Kingdom intended to be used for the taking off or landing of helicopters at night other than such a place as is specified in paragraph (1) shall cause to be in operation, whenever a helicopter flying for the purpose of the public transport of passengers is taking off or landing at that area by night, such lighting as will enable the pilot of the helicopter:


(i) in the case of landing, to identify the landing area in flight, to determine the landing direction and to make a safe approach and landing; and

(ii) in the case of taking off, to make a safe take-off.



(b) Subject to sub-paragraph (c), a helicopter flying for the purpose of the public transport of passengers at night shall not take off or land at a place to which sub-paragraph (a) applies unless there is in operation such lighting.

(c) Nothing in this paragraph shall apply to or in relation to an aircraft flying under and in accordance with the terms of a police air operator's certificate.

(a) the price to be charged for the carriage of passengers, baggage or cargo on flights to which a permission granted under article 113(1) of this Order relates;

(b) any additional goods, services or other benefits to be provided in connection with such carriage;

(c) the prices, if any, to be charged for any such additional goods, services or benefits; and

(d) the commission, or rates of commission, to be paid in relation to the carriage of passengers, baggage or cargo;

(a) in the case of a microlight aeroplane, either in accordance with sub-paragraph (c) or on the wing;

(b) in the case of a balloon, on the basket or envelope; or

(c) in the case of any other aircraft on the fuselage or car as the case may be.

    (5) The nationality and registration marks shall be painted on the aircraft or shall be affixed thereto by any other means ensuring a similar degree of permanence in the manner specified in paragraphs 2 and 3 of this Part.

     2 Position and size of marks


    (1) The position and size of marks on heavier than air aircraft (excluding kites) shall be as follows:

(a) on the horizontal surfaces of the wings:


(i) on aircraft having a fixed wing surface, the marks shall appear on the lower surface of the wing structure and shall be on the port wing unless they extend across the whole surface of both wings. So far as is possible the marks shall be located equidistant from the leading and trailing edges of the wings. The tops of the letters shall be towards the leading edge of the wing;

(ii) the height of the letters shall be:


(aa) subject to sub-paragraph (bb), at least 50 centimetres;

(bb) if the wings are not large enough for the marks to be 50 centimetres in height, marks of the greatest height practicable in the circumstances;



(b) on the fuselage (or equivalent structure) and vertical tail surfaces:



(i) the marks shall also appear either:


(aa) on each side of the fuselage (or equivalent structure), and shall, in the case of fixed wing aircraft be located between the wings and the horizontal tail surface; or

(bb) on the vertical tail surfaces;



(ii) when located on a single vertical tail surface, the marks shall appear on both sides. When located on multi-vertical tail surfaces, the marks shall appear on the outboard sides of the outer-surfaces. Subject to sub-paragraphs (iv) and (v), the height of the letters constituting each group of marks shall be at least 30 centimetres;

(iii) if one of the surfaces authorised for displaying the required marks is large enough for those marks to be 30 centimetres in height (whilst complying with sub-paragraph (v)) and the other is not, marks of 30 centimetres in height shall be placed on the largest authorised surface;

(iv) if neither authorised surface is large enough for marks of 30 centimetres in height (whilst complying with sub-paragraph (v)), marks of the greatest height practicable in the circumstances shall be displayed on the larger of the two authorised surfaces;

(v) the marks on the vertical tail surfaces shall be such as to leave a margin of at least 5 centimetres along each side of the vertical tail surface;

(vi) on rotary wing aircraft where owing to the structure of the aircraft the greatest height practicable for the marks on the side of the fuselage (or equivalent structure) is less than 30 centimetres, the marks shall also appear on the lower surface of the fuselage as close to the line of symmetry as is practicable and shall be placed with the tops of the letters towards the nose. The height of the letters constituting each group of marks shall be:



(aa) subject to sub-paragraph (bb), at least 50 centimetres; or

(bb) if the lower surface of the fuselage is not large enough for the marks to be of 50 centimetres in height, marks of the greatest height practicable in the circumstances;



(c) wherever in this paragraph marks of the greatest height practicable in the circumstances are required, that height shall be such as is consistent with compliance with paragraph 3 of this Part.

    (2) The position and size of marks on airships and free balloons shall be as follows:

(a) in the case of airships the marks shall be placed on each side of the airship. They shall be placed horizontally either on the hull near the maximum cross-section of the airship or on the lower vertical stabiliser;

(b) in the case of free balloons, the marks shall be in two places on diametrically opposite sides of the balloon;

(c) in the case of both airships and free balloons the side marks shall be so placed as to be visible from the sides and from the ground. The height of the letters shall be at least 50 centimetres.

     3 Width, spacing and thickness of marks


    (1) For the purposes of this paragraph:

(a) 'standard letter' shall mean any letter other than the letters I, M and W;

(b) the width of each standard letter and the length of the hyphen between the nationality mark and the registration mark shall be two thirds of the height of a letter;

(c) the width of the letters M and W shall be neither less than two thirds of their height nor more than their height; and

(d) the width of the letter I shall be one sixth of the height of the letter.

    (2) The thickness of the lines comprising each letter and hyphen shall be one sixth of the height of the letters forming the marks.

    (3) Each letter and hyphen shall be separated from the letter or hyphen which it immediately precedes or follows by a space equal to either one quarter or one half of the width of a standard letter. Each such space shall be equal to every other such space within the marks.

(a) testing the aircraft;

(b) demonstrating the aircraft with a view to the sale of that aircraft or of other similar aircraft;

(c) proceeding to or from a place at which the aircraft is to be tested or demonstrated as aforesaid, or overhauled, repaired or modified;

(d) delivering the aircraft to a person who has agreed to buy, lease or sell it; or

(e) proceeding to or from a place for the purpose of storage.

    (3) Without prejudice to article 43 of this Order the operator of the aircraft shall satisfy himself before the aircraft takes off that the aircraft is in every way fit for the intended flight.

    (4) The aircraft shall fly only within the United Kingdom.

(a) it does not have a certificate of airworthiness duly issued or rendered valid under the law of the United Kingdom; or

(b) the certificate of airworthiness or certificate of validation issued in respect of the aircraft has ceased to be in force by virtue of any of the matters specified in Article 9(7) of this Order.

    (2)

(a) In the case of an aircraft falling within paragraph (1)(a) the aircraft shall fly only for the purpose of enabling it to:


(i) qualify for the issue or renewal of a certificate of airworthiness or the validation thereof after an application has been made for such issue, renewal or validation as the case may be, or carry out a functional check of a previously approved modification of the aircraft (and for the purpose of this Schedule 'a previously approved modification' shall mean a modification which has previously been approved by the CAA in respect of that aircraft or another aircraft of the same type);

(ii) proceed to or from a place at which any inspection, repair, modification, maintenance, approval, test or weighing of, or the installation of equipment in, the aircraft is to take place or has taken place for a purpose referred to in sub-paragraph (a), after any relevant application has been made, or at which the installation of furnishings in, or the painting of, the aircraft is to be undertaken; or

(iii) proceed to or from a place at which the aircraft is to be or has been stored.



(b) In the case of an aircraft falling within paragraph (1)(b), it shall fly only for the purpose of enabling it to:



(i) proceed to a place at which any inspection or maintenance required by virtue of Article 9(7)(b)(ii) of this Order is to take place; or

(ii) proceed to a place at which any inspection, maintenance or modification required by virtue of Article 9(7)(b)(i) or (c) of this Order is to take place and in respect of which flight the CAA has given permission in writing; or

(iii) carry out a functional check, test or in-flight adjustment in connection with the carrying out in a manner approved by the CAA of any overhaul, repair, previously approved modification, inspection or maintenance required by virtue of Article 9(7) of this Order.

    (3) The aircraft shall be:

(a) an aircraft in respect of which a certificate of airworthiness or validation has previously been in force under this Order and has not subsequently had any modification which requires approval unless that modification is a previously approved modification which has been granted such an approval under the law of the country in which the aircraft was registered at that time; or

(b) an aircraft identical in design (including any modifications) with an aircraft in respect of which such a certificate is or has been in force.

    (4) The aircraft and its engines shall be certified as fit for flight by the holder of an aircraft maintenance engineer's licence granted under this Order, being a licence which entitles him to issue that certificate or by a person approved by the CAA for the purpose of issuing certificates under this condition, and in accordance with that approval.

    (5) The aircraft shall carry the minimum flight crew specified in any certificate of airworthiness or validation which has previously been in force under the Order in respect of the aircraft, or is or has previously been in force in respect of any other aircraft of identical design.

    (6) The aircraft shall not carry any persons or cargo except persons performing duties in the aircraft in connection with the flight or persons who are carried in the aircraft to perform duties in connection with a purpose referred to in paragraph (2).

    (7) The aircraft shall not fly over any congested area of a city, town or settlement except to the extent that it is necessary to do so in order to take off or land.

    (8) Without prejudice to the provisions of article 20(2) of this Order, the aircraft shall carry such flight crew as may be necessary to ensure the safety of the aircraft.

B Conditions


    (1) An aircraft may fly for a purpose set out in paragraph (2) subject to the conditions set out in paragraphs (3) to (8) whether or not it is registered in accordance with article 3(1) of this Order and when there is not in force in respect thereof:

(a) in the case of an aircraft which is so registered, a certificate of airworthiness duly issued or rendered valid under the law of the country in which the aircraft is registered or,

(b) in the case of an aircraft which is not so registered, either a certificate of airworthiness duly issued or rendered valid under the law of the United Kingdom or a permit to fly issued by the CAA in respect of that aircraft.

    (2) The aircraft shall fly only for the purpose of:

(a) experimenting with or testing the aircraft (including any engines installed thereon) or any equipment installed or carried in the aircraft;

(b) enabling it to qualify for the issue of a certificate of airworthiness or the validation thereof or the approval of a modification of the aircraft or the issue of a permit to fly;

(c) demonstrating and displaying the aircraft, any engines installed thereon or any equipment installed or carried in the aircraft with a view to the sale thereof or of other similar aircraft, engines or equipment;

(d) demonstrating and displaying the aircraft to employees of the operator;

(e) the giving of flying training to or the testing of flight crew employed by the operator or the training or testing of other persons employed by the operator and who are carried or are intended to be carried pursuant to paragraph (7)(a); or

(f) proceeding to or from a place at which any experiment, inspection, repair, modification, maintenance, approval, test or weighing of the aircraft, the installation of equipment in the aircraft, demonstration, display or training is to take place for a purpose referred to in sub-paragraphs (a), (b), (c), (d) or (e) or at which installation of furnishings in, or the painting of, the aircraft is to be undertaken.

    (3) The flight shall be operated by a person approved by the CAA for the purposes of these Conditions and subject to any additional conditions which may be specified in such an approval.

    (4) If not registered in the United Kingdom the aircraft shall be marked in a manner approved by the CAA for the purposes of these Conditions, and articles 15, 17, 43, 46, 76 and 78 of this Order shall be complied with in relation to the aircraft as if it was registered in the United Kingdom.

    (5) Without prejudice to article 20(2) of this Order, the aircraft shall carry such flight crew as may be necessary to ensure the safety of the aircraft.

    (6) No person shall act as pilot in command of the aircraft except a person approved for the purpose by the CAA.

    (7) The aircraft shall not carry any cargo, or any persons other than the flight crew except the following:

(a) persons employed by the operator who during the flight carry out duties or are tested or receive training in connection with a purpose specified in paragraph (2);

(b) persons acting on behalf of the manufacturers of component parts of the aircraft (including its engines) or of equipment installed in or carried in the aircraft for carrying out during the flight duties in connection with a purpose so specified;

(c) persons approved by the CAA under article 133 of this Order as qualified to furnish reports for the purposes of article 9 of this Order;

(d) persons other than those carried under the preceding provisions of this sub-paragraph who are carried in the aircraft in order to carry out a technical evaluation of the aircraft or its operation;

(e) cargo which comprises equipment carried in connection with a purpose specified in paragraph (2)(f); or

(f) persons employed by the operator or persons acting on behalf of the manufacturers of component parts of the aircraft (including its engines) or of equipment installed in or carried in the aircraft in connection with a purpose specified in paragraph (2)(f) which persons have duties in connection with that purpose.

    (8) The aircraft shall not fly, except in accordance with procedures which have been approved by the CAA in relation to that flight, over any congested area of a city, town or settlement.

(a) Every aircraft of a description specified in the first column of the Table set forth in paragraph 4 of this Schedule and which is registered in the United Kingdom shall be provided, when flying in the circumstances specified in the second column of the said Table, with adequate equipment, and for the purpose of this paragraph the expression 'adequate equipment' shall mean, subject to sub-paragraph (b), the scales of equipment respectively indicated in that Table.

(b) If the aircraft is flying in a combination of such circumstances, the scales of equipment shall not on that account be required to be duplicated.

     2 The equipment carried in an aircraft as being necessary for the airworthiness of the aircraft shall be taken into account in determining whether this Schedule is complied with in respect of that aircraft.

     3 The following items of equipment shall not be required to be of a type approved by the CAA:

(a) The equipment referred to in Scale A (ii).

(b) First aid equipment and handbook, referred to in Scale A.

(c) Time-pieces, referred to in Scale F.

(d) Torches, referred to in Scales G, H, K and Z.

(e) Whistles, referred to in Scale H.

(f) Sea anchors, referred to in Scales J and K.

(g) Rocket signals, referred to in Scale J.

(h) Equipment for mooring, anchoring or manoeuvring aircraft on the water, referred to in Scale J.

(i) Paddles, referred to in Scale K.

(j) Food and water, referred to in Scales K, U and V.

(k) First aid equipment, referred to in Scales K, U and V.

(l) Stoves, cooking utensils, snow shovels, ice saws, sleeping bags and Arctic suits, referred to in Scale V.

(m) Megaphones, referred to in Scale Y.

     4 Table

Description of aircraft	Circumstances of flight	Scale of equipment required
(1) Gliders	(a) flying for purposes other than public transport or aerial work; and when flying by night	A (ii)
	(b) flying for the purpose of public transport or aerial work; and	A, B(i) and (ii), D and F(i)
	(i) when flying by night	C and G
	(ii) when carrying out aerobatic manoeuvres	B (iii)
(2) Aeroplanes	(a) flying for purposes other than public transport; and	A (i) and (ii) and B (i)
	(i) when flying by night	C and D
	(ii) when flying under Instrument Flight Rules: (aa) outside controlled airspace	D
	(bb) within Class A, B or C airspace	E with E (iv) duplicated and F
	(cc) within Class D and E airspace	E and F
	(iii) when carrying out aerobatic manoeuvres	B (iii)
	(b) flying for the purpose of public transport; and	A, B (i) and (ii), D and F (i)
	(i) when flying under Instrument Flight Rules except flights outside controlled airspace in the case of aeroplanes having a maximum total weight authorised not exceeding 1150 kg	E with E (iv) duplicated and F
	(ii) when flying by night; and in the case of aeroplanes of which the maximum total weight authorised exceeds 1150 kg	C and G, E with E (iv) duplicated and F
	(iii) when flying over water beyond gliding distance from land	H
	(iv) on all flights on which in the event of any emergency occurring during the take-off or during the landing at the intended destination or any likely alternate destination it is reasonably possible that the aeroplane would be forced to land onto water	H
	(v) when flying over water: (aa) in the case of an aeroplane: (aaa) classified in its certificate of airworthiness as being of performance group A, C or X; or (bbb) having no performance group classification in its certificate of airworthiness and of such a weight and performance that with any one of its power units inoperative and the remaining power unit or units operating within the maximum continuous power conditions specified in the certificate of airworthiness, performance schedule or flight manual relating to the aeroplane issued or rendered valid by the CCA it is capable of a gradient of climb of at least 1 in 200 at an altitude of 5000 ft in the International Standard Atmosphere specified in or ascertainable by reference to the certificate of airworthiness in force in respect of that aircraft;
	when either more than 400 nautical miles or more than 90 minutes flying time*[30] from the nearest aerodrome at which an emergency landing can be made	H and K
	(bb) in the case of all other aeroplanes, when more than 30 minutes flying time*[31] from such an aerodrome	H and K
	(vi) on all flights which involve manoeuvres on water	H, J and K
	(vii) when flying at a height of 10 000 ft or more above mean sea level: (aa) having a certificate of airworthiness first issued (whether in the United Kingdom or elsewhere) before 1st January 1989	L1 or L2
	(bb) having a certificate of airworthiness first issued (whether in the United Kingdom or elsewhere) on or after 1st January 1989	L2
	(viii) on flights when the weather reports or forecasts available at the aerodrome at the time of departure indicate that conditions favouring ice formation are likely to be met	M
	(ix) when carrying out aerobatic manoeuvres	B (iii)
	(x) on all flights on which the aircraft carries a flight crew of more than one person	N
	(xi) on all flights for the purpose of the public transport of passengers	Q and Y(i), (ii) and (iii)
	(xii) on all flights by a pressurised aircraft	R
	(xiii) when flying over substantially uninhabited land areas where, in the event of an emergency landing, tropical conditions are likely to be met	U
	(xiv) when flying over substantially uninhabited land or other areas where, in the event of an emergency landing, polar conditions are likely to be met	V
	(xv) when flying at an altitude of more than 49 000 ft	W
(3) Turbine-jet aeroplanes having a maximum total weight authorised exceeding 5700 kg or pressurised aircraft having a maximum total weight authorised exceeding 11 400 kg	when flying for the purpose of public transport	O
(4) Turbine-engined aeroplanes having a maximum total weight authorised exceeding 5700 kg and piston-engined aeroplanes having a maximum total weight authorised exceeding 27 000 kg except for such aeroplanes falling within paragraphs (5) or (6): (a) which are operated by an air transport undertaking under a certificate of airworthiness in the Transport Category (Passenger) or the Transport Category (Cargo); or	when flying on any flight	P
(b) in respect of which application has been made and not withdrawn or refused for such a certificate, and which fly under the 'A Conditions' or under a certificate of airworthiness in the Special Category	when flying on any flight	P
(5) Aeroplanes in respect of which there is in force a certificate of airworthiness in the Transport Category (Passenger) or Transport Category (Cargo) and aeroplanes in respect of which application has been made, and not withdrawn or refused, for such a certificate of airworthiness and which fly under the 'A Conditions' or in respect of which there is in force a certificate of airworthiness in the Special Category except for such aeroplanes falling within paragraph(6): (a) which conform to a type first issued with a type certificate (whether in the United Kingdom or elsewhere) on or after 1st April 1971 and which have a maximum total weight authorised exceeding 5700 kg but not exceeding 11 400 kg; or	when flying on any flight	S(i)
(b) which conform to a type first issued with a type certificate (whether in the United Kingdom or elsewhere) on or after 1st April 1971 and which have a maximum total weight authorised exceeding 11 400 kg but not exceeding 27 000 kg; or	when flying on any flight	S(ii)
(c) which conform to a type first issued with a type certificate (whether in the United Kingdom or elsewhere) on or after 1st April 1971 and which have a maximum total weight authorised exceeding 27 000 kg but not exceeding 230 000 kg; or	when flying on any flight	S(iii)
(d) which conform to a type first issued with a type certificate in the United Kingdom on or after 1st January 1970 and which have a maximum total weight authorised exceeding 230 000 kg;	when flying on any flight	S(iii)
(6) Aeroplanes in respect of which there is in force a certificate of airworthiness in the Transport Category (Passenger) or Transport Category (Cargo) and aeroplanes in respect of which application has been made, and not withdrawn or refused, for such a certificate of airworthiness and which fly under 'A Conditions' or in respect of which there is in force a certificate of airworthiness in the Special Category: (a) for which an individual certificate of airworthiness was first issued (whether in the United Kingdom or elsewhere) on or after 1st June 1990 and which have a maximum total weight authorised not exceeding 5700 kg, are powered by 2 or more turbine engines and are certified to carry more than 9 passengers; or	when flying on any flight	S(iv)
(b) for which an individual certificate of airworthiness was first issued (whether in the United Kingdom or elsewhere) on or after 1st June 1990 and which have a maximum total weight authorised exceeding 5700 kg but not exceeding 27 000 kg; or	when flying on any flight	S(v)
(c) for which an individual certificate of airworthiness was first issued (whether in the United Kingdom or elsewhere) on or after 1st June 1990 and which have a maximum total weight authorised exceeding 27 000 kg.	when flying on any flight	S(vi)
(7) Aeroplanes in respect of which there is in force a certificate of airworthiness in the Aerial Work or Private Category and for which an individual certificate of airworthiness was first issued (whether in the United Kingdom or elsewhere) on or after 1 June 1990 and which have a maximum total weight authorised exceeding 27 000 kg.	when flying on any flight	S(vi)
(8) Aeroplanes: (a) which conform to a type first issued with a type certificate (whether in the United Kingdom or elsewhere) on or after 1st April 1971 and having a maximum total weight authorised exceeding 27 000 kg and in respect of which there is in force a certificate of airworthiness in the Transport Category (Passenger) or the Transport Category (Cargo); or	when flying on any flight	T
(b) which conform to a type first issued with a type certificate in the United Kingdom on or after 1st January 1970 and which have a maximum total weight authorised exceeding 230 000 kg and in respect of which there is in force such a certificate of airworthiness; or	when flying on any flight	T
(c) having a maximum total weight authorised exceeding 27 000 kg which conform to a type first issued with a type certificate on or after 1st April 1971 (or 1st January 1970 in the case of an aeroplane having a maximum total weight authorised exceeding 230 000 kg) in respect of which an application has been made, and not withdrawn or refused for such a certificate of airworthiness and which fly under the 'A Conditions' or in respect of which there is in force a certificate of airworthiness in the Special Category.	when flying on any flight	T
(9) Aeroplanes powered by one or more turbine jets or one or more turbine propeller engines and which have a maximum total weight authorised exceeding 15,000 kg or which in accordance with the certificate of airworthiness in force in respect thereof may carry more than 30 passengers: (a) except any such aeroplanes as come within sub-paragraph (b)	When flying for the purpose of public transport prior to 1 January 2005	X(i)
(b) for which an individual certificate of airworthiness was first issued (whether in the United Kingdom of elsewhere) on or after 1st January 2001	When flying for the purpose of public transport on or after 1st January 2005	X(ii)
(c) for which an individual certificate of airworthiness was first issued (whether in the United Kingdom or elsewhere) before 1st January 2001	When flying for the purpose of public transport on or after 1 January 2005	X(ii)
(10) Aeroplanes which are powered by one or more turbine jets or one or more turbine propeller engines and which have a maximum total weight authorised exceeding 5 700 kg but not exceeding 15 000 kg or which in accordance with the certificate of airworthiness in force in respect thereof may carry more than 9 passengers but not exceeding 30 passengers: (a) except any such aeroplanes as come within sub-paragraph (b)	When flying for the purpose of public transport on or after 1st October 2001, except when flying under and in accordance with the terms of a police air operator's certificate	X(ii)
(b) which have equipment capable of giving warning to the pilot of the potentially hazardous proximity of ground or water installed before 1st April 2000	When flying for the purpose of public transport on or after 1st January 2005, except when flying under and in accordance with the terms of a police air operator's certificate	X(ii)
(11) Aeroplanes which are powered by one or more turbine jets or one or more turbine propeller engines and which have a maximum total weight authorised exceeding 5 700 kg or which in accordance with the certificate of airworthiness in force in respect thereof may carry more than 9 passengers: (a) in respect of which there is in force a certificate of airworthiness except any such aeroplanes as come within sub-paragraph (b)	When flying for purposes other than public transport on or after 1st October 2001	X(ii)
(b) in respect of which there is in force a certificate of airworthiness and which have equipment capable of giving warning to the pilot of the potentially hazardous proximity of ground or water installed before 1st April 2000	When flying for purposes other than public transport on or after 1st January 2005	X(ii)
(12) Aeroplanes: (a) powered by one or more turbo-jets and which have a maximum total weight authorised exceeding 22 700 kg; or	when flying by night for the purpose of the public transport of passengers	Z (i) and (ii)
(b) having a maximum total weight authorised exceeding 5700 kg and which conform to a type for which a certificate of airworthiness was first applied for (whether in the United Kingdom or elsewhere) after 30th April 1972 but not including any aeroplane which in the opinion of the CAA is identical in all matters affecting the provision of emergency evacuation facilities to an aeroplane for which a certificate of airworthiness was first applied for before that date; or	when flying for the purpose of the public transport of passengers	Z (i) and (ii)
(c) which in accordance with the certificate of airworthiness in force in respect thereof may carry more than 19 passengers; or	when flying by night for the purpose of the public transport of passengers	Z (i)
(d) having a maximum total weight authorised exceeding 5700 kg and which conform to a type for which a certificate of airworthiness was first applied for (whether in the United Kingdom or elsewhere) after 30th April 1972 but not including any aeroplane which in the opinion of the CAA is identical in all matters affecting the provision of emergency evacuation facilities to an aeroplane for which a certificate of airworthiness was first applied for before that date; or	when flying for the purpose of the public transport of passengers	Z (iii)
(e) powered by one or more turbo-jets and which have a maximum total weight authorised exceeding 22 700 kg; or	when flying for the purpose of the public transport of passengers	Z (iii)
(f) first issued with a type certificate (whether in the United Kingdom or elsewhere) on or after 1st January 1958 and which in accordance with the certificate of airworthiness in force in respect thereof may carry more than 19 passengers	when flying for the purpose of the public transport of passengers	Z (iii)
(13) Aeroplanes: (a) powered by one or more turbine jets	when flying on any flight	AA
(b) powered by one or more turbine propeller engines and having a maximum total weight authorised exceeding 5700 kg and first issued with a certificate of airworthiness in the United Kingdom on or after 1st April 1989	when flying on any flight	AA
(14) Aeroplanes in respect of which there is in force a certificate of airworthiness in the Transport Category (Passenger)	when flying for the purpose of public transport of passengers	Y (iv)
(15) Helicopters and Gyroplanes	(a) flying for purposes other than public transport; and	A (i) and (ii) and B (i)
	(i) when flying by day under Visual Flight Rules with visual ground reference	D
	(ii) when flying by day under Instrument Flight Rules or without visual ground reference
	(aa) outside controlled airspace	E with E (ii) duplicated
	(bb) within controlled airspace	E with both E (ii) and E(iv) duplicated and F with F (iv) for all weights
	(iii) when flying at night (aa) with visual ground reference	C, E, G (iii) and G (v)
	(bb) without visual ground reference (aaa) outside controlled airspace	C, E with E (ii) duplicated G (iii) and G (v)
	(bbb) within controlled airspace	C, E with both E (ii) and E (iv) duplicated, F with F (iv) for all weights, G (iii) and G (v)
	(b) flying for the purpose of public transport; and	A, B (i) and (ii), F (i) and F (iv) for all weights
	(i) when flying by day under Visual Flight Rules with visual ground reference	D
	(ii) when flying by day under Instrument Flight Rules or without visual ground reference	E with both E (ii) and E (iv) duplicated, F (ii), F (iii) and F (v)
	(iii) when flying by night with visual ground reference (aa) when flying with one pilot	C, E with E(ii) duplicted and either E(iv) duplicatede or a radio altimeter, F(ii), F(iii), F(v) and G
	(bb) when flying in circumstances where two pilots are required	C, E, F (ii), F (iii), F (v) and G for each pilot's station
	(iv) when flying by night without visual ground reference	C, E with both E (ii) and E (iv) duplicated, F (ii), F (iii), F (v) and G
	(v) when flying over water (aa) in the case of a helicopter or gyroplane classified in its certificate of airworthiness as being of performance group A2 or B when beyond autorotational gliding distance from land suitable for an emergency landing	E and H
	(bb) on all flights on which in the event of any emergency occurring during the take-off or during the landing at the intended destination or any likely alternate destination it is reasonably possible that the helicopter or gyroplane would be forced to land onto water	H
	(cc) in the case of a helicopter or gyroplane classified in its certificate of airworthiness as being of performance group A2 when beyond 10 minutes flying time*[32] from land	E, H, K and T
	(dd) for more than a total of 3 minutes in any flight	EE
	(ee) in the case of a helicopter or a gyroplane classified in its certificate of airworthiness as being of performance group A2 which is intended to fly beyond 10 minutes flying time from land or which actually flies beyond 10 minutes flying time from land, on a flight which is either in support of or in connection with the offshore exploitation, or exploration of mineral resources (including gas) or is on a flight under and in accordance with the terms of a police air operator's certificate, when in either case the weather reports or forecasts available to the commander of the aircraft indicate that the sea temperature will be less than plus 10°C during the flight or when any part of the flight is at night	I
	(vi) on all flights which involve manoeuvres on water	H, J and K
	(vii) when flying at a height of 10 000 ft or more above mean sea level: (aa) having a certificate of airworthiness first issued (whether in the United Kingdom or elsewhere) before 1st January 1989	L1 or L2
	(bb) having a certificate of airworthiness first issued (whether in the United Kingdom or elsewhere) on or after 1st January 1989	L2
	(viii) on flights when the weather reports or forecasts available at the aerodrome at the time of departure indicate that conditions favouring ice formation are likely to be met	M
	(ix) on all flights on which the aircraft carries a flight crew of more than one person	N
	(x) on all flights for the purpose of the public transport of passengers	Y(i), (ii) and (iii)
	(xi) when flying over substantially uninhabited land areas where, in the event of an emergency landing, tropical conditions are likely to be met	U
	(xii) when flying over substantially uninhabited land or other areas where, in the event of an emergency landing, polar conditions are likely to be met	V
(16) Helicopters and Gyroplanes: (a) having a maximum total weight authorised exceeding 5700 kg and which conform to a type for which a certificate of airworthiness was first applied for (whether in the United Kingdom or elsewhere) after 30th April 1972 but not including any helicopter or gyroplane which in the opinion of the CAA is identical in all matters affecting the provision of emergency evacuation facilities to a helicopter or gyroplane for which a certificate of airworthiness was first applied for before that date; or	when flying by night for the purpose of the public transport of passengers	Z (i) and (ii)
(b) which, in accordance with the certificate of airworthiness in force in respect thereof may carry more than 19 passengers; or	when flying by night for the purpose of the public transport of passengers	Z (i)
(c) which have a certificate of airworthiness issued in the Transport Category (Passenger or Cargo) and helicopters and gyroplanes in respect of which application has been made and not withdrawn or refused for such a certificate of airworthiness and which fly under the 'A Conditions' or which have a certificate of airworthiness in the Special Category and (i) which have a maximum total weight authorised exceeding 2730 kg but not exceeding 7000 kg or which in accordance with the certificate of airworthiness in force in respect thereof may carry more than 9 passengers, or both	when flying on any flight	SS(i) or (iii)
(ii) which have a maximum total weight authorised exceeding 7000 kg	when flying on any flight	SS(ii) or (iii)

     5 The scales of equipment indicated in the foregoing Table shall be as follows:

Scale A

(i) Spare fuses for all electrical circuits the fuses of which can be replaced in flight, consisting of 10 per cent of the number of each rating or three of each rating, whichever is the greater.

(ii) Maps, charts, codes and other documents and navigational equipment necessary, in addition to any other equipment required under this Order, for the intended flight of the aircraft including any diversion which may reasonably be expected.

(iii) First aid equipment of good quality, sufficient in quantity, having regard to the number of persons on board the aircraft, and including the following:

     Roller bandages, triangular bandages, adhesive plaster, absorbent gauze, cotton wool (or wound dressings in place of the absorbent gauze and cotton wool), burn dressings, safety pins;

     Haemostatic bandages or tourniquets, scissors;

     Antiseptic, analgesic and stimulant drugs;

     Splints, in the case of aeroplanes the maximum total weight authorised of which exceeds 5700 kg;

     A handbook on first aid.

(iv) In the case of a flying machine used for the public transport of passengers in which, while the flying machine is at rest on the ground, the sill of any external door intended for the disembarkation of passengers, whether normally or in an emergency:


(a) is more than 1.82 metres from the ground when the undercarriage of the machine is in the normal position for taxiing; or

(b) would be more than 1.82 metres from the ground if the undercarriage or any part thereof should collapse, break or fail to function;



apparatus readily available for use at each such door consisting of a device or devices which will enable passengers to reach the ground safely in an emergency while the flying machine is on the ground, and can be readily fixed in position for use.

Scale AA

(i) Subject to sub-paragraph (ii), an altitude alerting system capable of alerting the pilot upon approaching a preselected altitude in either ascent or descent, by a sequence of visual and aural signals in sufficient time to establish level flight at that preselected altitude and when deviating above or below that preselected altitude, by a visual and an aural signal.

(ii) If the system becomes unserviceable, the aircraft may fly or continue to fly, until it first lands at a place at which it is reasonably practicable for the system to be repaired or replaced.

Scale B

(i)


(a) If the maximum total weight authorised of the aircraft is 2730 kg or less, for every pilot's seat and for any seat situated alongside a pilot's seat, either a safety belt with one diagonal shoulder strap or a safety harness, or with the permission of the CAA, a safety belt without a diagonal shoulder strap which permission may be granted if the CAA is satisfied that it is not reasonably practicable to fit a safety belt with one diagonal shoulder strap or a safety harness.

(b) If the maximum total weight authorised of the aircraft exceeds 2730 kg, either a safety harness for every pilot's seat and for any seat situated alongside a pilot's seat, or with the permission of the CAA, a safety belt with one diagonal shoulder strap which permission may be granted if the CAA is satisfied that it is not reasonably practicable to fit a safety harness.

(c) For every seat in use (not being a seat referred to in sub-paragraphs (a), (b), (e) and (f)) a safety belt with or without one diagonal shoulder strap or a safety harness.

(d) In addition and to be attached to or secured by the equipment required in sub-paragraph (c) above, a child restraint device for every child under the age of two years on board.

(e) On all flights for the public transport of passengers by aircraft, for each seat for use by cabin attendants who are required to be carried under this Order, a safety harness.

(f) On all flights in aeroplanes in respect of which a certificate of airworthiness was first issued (whether in the United Kingdom or elsewhere) on or after 1st February 1989 the maximum total weight authorised of which does not exceed 5700 kg which in accordance with the certificate of airworthiness in force thereof is not capable of seating more than 9 passengers (otherwise than in seats referred to under sub-paragraphs (a) and (b)), a safety belt with one diagonal shoulder strap or a safety harness for each seat intended for use by a passenger.



(ii) If the commander cannot, from his own seat, see all the passengers' seats in the aircraft, a means of indicating to the passengers that seat belts should be fastened.

(iii)



(a) Subject to sub-paragraph (b), a safety harness for every seat in use.

(b) In the case of an aircraft carrying out aerobatic manoeuvres consisting only of erect spinning, the CAA may permit a safety belt with one diagonal shoulder strap to be fitted if it is satisfied that such restraint is sufficient for the carrying out of erect spinning in that aircraft and that it is not reasonably practicable to fit a safety harness in that aircraft.

Scale C

(i) Equipment for displaying the lights required by the Rules of the Air.

(ii) Electrical equipment, supplied from the main source of supply in the aircraft, to provide sufficient illumination to enable the flight crew properly to carry out their duties during flight.

(iii) Unless the aircraft is equipped with radio, devices for making the visual signal specified in the Rules of the Air as indicating a request for permission to land.

Scale D

(i)


(a) In the case of a helicopter or gyroplane, a slip indicator.

(b) In the case of any other flying machine either:

(aa) a turn indicator and a slip indicator; or

(bb) a gyroscopic bank and pitch indicator and a gyroscopic direction indicator.



(ii) A sensitive pressure altimeter adjustable for any sea level barometric pressure which the weather report or forecasts available to the commander of the aircraft indicate is likely to be encountered during the intended flight.

Scale E

(i)


(a) In the case of a helicopter or gyroplane, a slip indicator.

(b) In the case of any other flying machine, a slip indicator and either a turn indicator or, at the option of the operator, an additional gyroscopic bank and pitch indicator.



(ii) A gyroscopic bank and pitch indicator.

(iii) A gyroscopic direction indicator.

(iv) A sensitive pressure altimeter adjustable for any sea level barometric pressure which the weather report or forecasts available to the commander of the aircraft indicate is likely to be encountered during the intended flight.

Scale EE

(i) Subject to sub-paragraph (ii), a radio altimeter with an audio voice warning operating below a preset height and a visual warning capable of operating at a height selectable by the pilot.

(ii) A helicopter flying under and in accordance with the terms of a police air operator's certificate may instead be equipped with a radio altimeter with an audio warning and a visual warning each capable of operating at a height selectable by the pilot.

Scale F

(i) A timepiece indicating the time in hours, minutes and seconds.

(ii) A means of indicating whether the power supply to the gyroscopic instrument is adequate.

(iii) A rate of climb and descent indicator.

(iv) If the maximum total weight authorised of the aircraft exceeds 5700 kg a means of indicating outside air temperature.

(v) If the maximum total weight authorised of the aircraft exceeds 5700 kg two air speed indicators.

Scale G

(i) In the case of an aircraft other than a helicopter or gyroplane landing lights consisting of 2 single filament lamps, or one dual filament lamp with separately energised filaments.

(ii) An electrical lighting system to provide illumination in every passenger compartment.

(iii)


(a) One electric torch for each member of the crew of the aircraft; or

(b)

(aa) one electric torch for each member of the flight crew of the aircraft; and

(bb) at least one electric torch affixed adjacent to each floor level exit intended for the disembarkation of passengers whether normally or in an emergency, provided that such torches shall:

(aaa) be readily accessible for use by the crew of the aircraft at all times; and

(bbb) number in total not less than the minimum number of cabin attendants required to be carried with a full passenger complement.



(iv) In the case of an aircraft other than a helicopter or gyroplane of which the maximum total weight authorised exceeds 5700 kg, means of observing the existence and build up of ice on the aircraft.

(v)



(a) In the case of a helicopter or gyroplane in respect of which there is in force a certificate of airworthiness designating the helicopter or gyroplane as being of performance group A, either:

(aa) 2 landing lights both of which are adjustable so as to illuminate the ground in front of and below the helicopter or gyroplane and one of which is adjustable so as to illuminate the ground on either side of the helicopter or gyroplane; or

(bb) one landing light or, if the maximum total weight authorised of the helicopter or gyroplane exceeds 5700 kg, one dual filament landing light with separately energised filaments, or 2 single filament lights, each of which is adjustable so as to illuminate the ground in front of and below the helicopter or gyroplane, and 2 parachute flares.

(b) In the case of a helicopter or gyroplane in respect of which there is in force a certificate of airworthiness designating the helicopter or gyroplane as being of performance group B, either:

(aa) one landing light and 2 parachute flares; or

(bb) if the maximum total weight authorised of the helicopter or gyroplane exceeds 5700 kg, either one dual filament landing light with separately energised filaments or 2 single filament landing lights, and 2 parachute flares.