Hammersmith Bridge, (512918N)    (0001351W)  ,
Greenwich Reach, (512906N)    (0000043W)  ,

The Air Navigation ( No. 2) Order 1995,S.I.  1995/1970,
The Air Navigation (Amendment) Order 1996,S.I.  1996/1301,
The Air Navigation (Second Amendment) Order 1997,S.I.  1997/287,
The Air Navigation (Third Amendment) Order 1998,S.I.  1998/753,
The Air Navigation (Fourth Amendment) Order 1999,S.I.  1999/1123,
The Air Navigation (Fifth Amendment) Order 1999,S.I.  1999/2059,
The Air Navigation (Cosmic Radiation) Order 2000,S.I.  2000/1104,

Aircraft,{ Lighter than air aircraft,{ Non-power driven, { Free Balloon    { Captive Balloon  ,,
{ Power driven,{ Airship,,
{ Heavier than air aircraft,{ Non-power driven, { Glider    { Kite  ,,
{ Power driven (flying machines), { Aeroplane (Landplane)    { Aeroplane (Seaplane)    { Aeroplane (Amphibian)    { Aeroplane (Self-launching Motor Glider)  ,,
,{ Rotorcraft, { Helicopter    { Gyroplane  ,

Transport Category (Passenger),Any purpose,
Transport Category (Cargo),Any purpose other than the public transport of passengers,
Aerial Work Category,Any purpose other than public transport,
Private Category,Any purpose other than public transport or aerial work,
Special Category,Any purpose, other than public transport, specified in the certificate of airworthiness but not including the carriage of passengers unless expressly permitted,

 *  For the purpose of this Table, flying time shall be calculated on the assumption that the aircraft is flying in still air at the speed specified in the relevant certificate of airworthiness as the speed for compliance with regulations governing flights over water.   ,
 *  For the purpose of this Table, flying time shall be calculated on the assumption that the helicopter or gyroplane is flying in still air at the speed specified in the relevant certificate of airworthiness as the speed for compliance with regulations governing flights over water.   ,
 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 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 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 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),

Not more than 8 liferafts,2 survival beacon radio apparatus,
For every additional 4 or proportion of 4 liferafts,1 additional survival beacon radio apparatus,


   The whole period during which, after a failure to maintain a pressure greater than 700 hectopascals in the control compartment and in the compartments in which passengers are carried has occurred, the flying machine flies above flight level 100.      The whole period during which, after a failure to maintain such pressure has occurred, the flying machine flies above flight level 150.      The whole period during which, after a failure to maintain such pressure has occurred, the flying machine flies above flight level 100, but not above flight level 150.      The flying machine is capable, at the time when a failure to maintain such pressure occurs, of descending in accordance with the emergency descent procedure specified in the relevant flight manual and without flying below the minimum altitudes for safe flight specified in the operations manual relating to the aircraft, to flight level 150 within 6 minutes, and of continuing at or below that flight level to its place of intended destination or any other place at which a safe landing can be made.      The flying machine is capable, at the time when a failure to maintain such pressure occurs, of descending in accordance with the emergency descent procedure specified in the relevant flight manual and without flying below the minimum altitudes for safe flight specified in the operations manual relating to the aircraft, to flight level 150 within 4 minutes, and of continuing at or below that flight level to its place of intended destination or any other place at which a safe landing can be made.    ,
Above flight level 100,—,30 minutes or the period specified at A hereunder whichever is the greater,In addition to any passengers for whom oxygen is provided as specified below, all the crew,
Above flight level 100 but not above flight level 300,{ Flying machine is either flying at or below flight level 150 or is capable of descending and continuing to destination as specified at X hereunder,30 minutes or the period specified at A hereunder whichever is the greater,10% of number of passengers,
{ Flying machine is flying above flight level 150 and is not so capable,{ 10 minutes or the period specified at B hereunder whichever is greater,All passengers,
and in addition,
{ 30 minutes or the period specified at C hereunder whichever is the greater,10% of number of passengers,
Above flight level 300 but not above flight level 350,{ Flying machine is capable of descending and continuing to destination as specified at Y hereunder,30 minutes or the period specified at A hereunder whichever is the greater,15% of number of passengers,
{ Flying machine is not so capable,10 minutes or the period specified at B hereunder whichever is the greater,All passengers,
and in addition,
{ 30 minutes or the period specified at C hereunder whichever is the greater,15% of number of passengers,
Above flight level 350,—,{ 10 minutes or the period specified at B hereunder whichever is the greater,All pasengers,
and in addition,
{ 30 minutes or the period specified at C hereunder whichever is the greater,15% of number of passengers,

 a   Members of the flight crew   ,Any period during which the aircraft flies above flight level 100,
 b   Cabin attendants and 10% of passengers   ,For any continuous period exceeding 30 minutes during which the aircraft flies above flight level 100 but not exceeding flight level 120, the duration shall be the period by which 30 minutes is exceeded,

 a   Members of the flight crew   ,Any period during which the aircraft flies above flight level 120,
 b   Cabin attendants and all passengers   ,Any period during which the aircraft flies above flight level 120,

 a   Members of the flight crew   ,30 minutes or whenever the cabin pressure altitude exceeds 10 000 ft, whichever is the greater,
 b   Cabin attendants and 10% of passengers   , aa   When the aircraft is capable of descending and continuing to its destination as specified at A hereunder, 30 minutes or whenever the cabin pressure altitude exceeds 10 000 ft, whichever is the greater     bb   When the aircraft is not so capable, whenever the cabin pressure altitude is greater than 10 000 ft but does not exceed 12 000 ft   ,
 c   Cabin attendants and passengers   , aa   When the aircraft is capable of descending and continuing to its destination as specified at A hereunder, no requirement other than that at (ii)(b)(aa) of this Part of this Scale     bb   When the aircraft is not so capable and the cabin pressure altitude exceeds 12 000 ft, the duration shall be the period when the cabin pressure altitude exceeds 12 000 ft or 10 minutes, whichever is the greater   ,

   The flying machine is capable, at the time when a failure to maintain cabin pressurisation occurs, of descending in accordance with the emergency descent procedure specified in the relevant flight manual and without flying below the minimum altitudes for safe flight specified in the operations manual relating to the aircraft, to flight level 120 within 5 minutes and of continuing at or below that flight level to its place of intended destination or any other place at which a safe landing can be made.    ,
 a   Members of the flight crew   ,2 hours or whenever the cabin pressure altitude exceeds 10 000 ft, whichever is the greater,
 b   Cabin attendants   ,Whenever the cabin pressure altitude exceeds10 000 ft, and a portable supply for 15 minutes,
 c   10% of passengers   ,Whenever the cabin pressure altitude exceeds 10 000 ft but does not exceed 12 000 ft,
 d   30% of passengers   ,Whenever the cabin pressure altitude exceeds 12 000 ft but does not exceed 15 000 ft,
 e   All passengers   ,If the cabin pressure altitude exceeds 15 000 ft, the duration shall be the period when the cabin pressure altitude exceeds 15 000 ft or 10 minutes, whichever is the greater,
 f   2% of passengers or 2 passengers, whichever is the greater, being a supply of first aid oxygen which must be available for simultaneous first aid treatment of 2% or 2 passengers wherever they are seated in the aircraft   ,Whenever, after decompression, the cabin pressure altitude exceeds 8000 ft,


 *  Unless the appropriate air traffic control unit otherwise permits in relation to the particular flight and provided that the aircraft complies with any instructions which the air traffic control unit may give in the particular case.   ,
 #  Provided that non-public transport aircraft flying in Class D and E airspace shall not be required to be provided with distance measuring equipment.   ,
 1   All aircraft (other than gliders) within the United Kingdom:   a   when flying under Instrument Flight Rules within controlled airspace     ,A,,,,E,F,
 b   when flying within controlled airspace   ,A,
 c   when making an approach to landing at an aerodrome notified for the purpose of this sub-paragraph   ,,,,,,,G,
 2   All aircraft within the United Kingdom:   a   when flying at or above flight level 245     ,A,
 b   when flying within airspace notified for the purposes of this sub-paragraph   ,A,
 3   All aircraft (other than gliders) within the United Kingdom:   a   when flying at or above flight level 245     ,,,,,E,F,
 b   when flying within airspace notified for the purpose of this sub-paragraph   ,,,,,E,
 c   when flying at or above flight level 100   ,,,,,E,
 4   All aircraft registered in the United Kingdom, wherever they may be:   a   when flying for the purpose of public transport under Instrument Flight Rules:   i   while making an approach to landing       ,A,,C,D,,,,H,
 ii   on all other occasions   ,A,,C,,,,,H,
 b   subject to sub-paragraph (d), multi-engined aircraft when flying for the purpose of public transport under Visual Flight Rules   ,
 c   subject to sub-paragraph (d), single-engined aircraft when flying for the purpose of public transport under Visual Flight Rules:   i   over a route on which navigation is effected solely by visual reference to landmarks     ,A,
 ii   on all other occasions   ,A,B,
 d   when flying under Instrument Flight Rules within controlled airspace and not required to comply with paragraph (4)(a) above   ,A,
 5   All aeroplanes registered in the United Kingdom, wherever they may be, and all aeroplanes wherever registered when flying in the United Kingdom, powered by one or more turbine jets or turbine propeller engines and either having a maximum take-off weight exceeding 15,000 kg or which in accordance with the certificate of airworthiness in force in respect thereof may carry more than 30 passengers   ,,,,,,,,,J,

A, Microlight Licence    SLMG Licence    Private Pilot’s Licence (Gyroplanes)  ,Any flight within the privileges of the licence,Certificate of test or certificate of experience,
B, Commercial Pilot’s Licence (Helicopters and Gyroplanes)    Commercial Pilot’s Licence (Balloons)    Commercial Pilot’s Licence (Gliders)    Commercial Pilot’s Licence (Airships)    Airline Transport Pilot’s Licence (Helicopters and Gyroplanes)  ,Carriage of passengers on a flight in respect of which the holder of the licence receives remuneration,Certificate of test,
C, Commercial Pilot’s Licence (Helicopters and Gyroplanes)    Commercial Pilot’s Licence (Balloons)    Commercial Pilot’s Licence (Gliders)    Commercial Pilot’s Licence (Airships)    Airline Transport Pilot’s Licence (Helicopters and Gyroplanes)  ,For public transport,Certificate of test,
D, Commercial Pilot’s Licence (Helicopters and Gyroplanes)    Commercial Pilot’s Licence (Balloons)    Commercial Pilot’s Licence (Gliders)    Commercial Pilot’s Licence (Airships)    Airline Transport Pilot’s Licence (Helicopters and Gyroplanes)  ,For aerial work,Certificate of test or certificate of experience,
E, Commercial Pilot’s Licence (Helicopters and Gyroplanes)    Commercial Pilot’s Licence (Balloons)    Commercial Pilot’s Licence (Gliders)    Commercial Pilot’s Licence (Airships)    Airline Transport Pilot’s Licence (Helicopters and Gyroplanes)  ,Any flight within the privileges of a Private Pilot’s Licence,Certificate of test or certificate of experience,
F,Flight Navigator’s Licence,Flights to which article 20(4) of this Order applies.,Certificate of experience,

Instrument rating (aeroplane),1.185,
Instrument rating (helicopter),2.185,
Flight instructor (aeroplane),1.355,
 Flying instructor’s rating (aeroplanes)    Assistant flying instructor’s rating (aeroplanes)    Flight instructor (helicopter)  ,2.355,
 Flying instructor’s rating (helicopters)    Assistant flying instructor’s rating (helicopters)    Type rating instructor rating (multi-pilot aeroplane)  ,1.370,
Type rating instructor rating (helicopter),2.370,
Class rating instructor rating (single pilot aeroplane),1.385,
Instrument rating instructor rating (aeroplane),1.400,
Instrument rating instructor rating (helicopter),2.400,

3,Aircraft flying unregistered,
5,Aircraft flying with false or incorrect markings,
10(1)(a),Flight without appropriate maintenance,
10(1)(b),Flight without a certificate of maintenance review,
11,Failure to keep a technical log,
12,Flight without a certificate of release to service issued under the Order,
13(7) and (8),Exercise of privileges of aircraft maintenance engineer’s licence whilst unfit,
14,Flight without required equipment,
15,Flight without required radio equipment,
16,Minimum equipment requirements,
17,Failure to keep log books,
18,Requirement to weigh aircraft and keep weight schedule,
20,Crew requirement,
21,Requirement for appropriate licence,
23(2),Requirement for appropriate certificate of test or experience,
24(2) and (3),Requirement for appropriate certificate of revalidation,
25(1) and (2),Requirement for appropriate certificate of test or revalidation,
26(1),Prohibition of flight after failure of test,
26(2)(a),Flight without valid medical certificate,
26(3),Flight in unfit condition,
29,Instruction in flying without appropriate licence and rating,
31,Operations manual requirement,
32,Police operations manual requirement,
33,Training manual requirement,
34,Operator’s responsibilities in connection with crew,
35,Requirements for loading aircraft,
36,Operational restrictions on aircraft,
37,Prohibition on public transport flights at night or in Instrument Meteorological Conditions by non-UK registered single engined aeroplanes,
38,Aerodrome operating minima— UK registered public transport aircraft,
39,Aerodrome operating minima—foreign registered public transport aircraft,
40,Aerodrome operating minima—non-public transport aircraft,
41,Requirement for pilot to remain at controls,
43,Pre-flight action by commander of aircraft,
44,Requirement for passenger briefing,
45,Additional duties of commander on flight for public transport of passengers,
46,Requirements for radio station in aircraft to be licensed and for operation of same,
47,Requirement for minimum navigation performance equipment,
48,Requirement for height keeping performance equipment-aircraft registered in the United Kingdom,
49,Requirement for height keeping performance equipment-aircraft registered elsewhere than in the United Kingdom,
50,Requirement for area navigation equipment-aircraft registered in the United Kingdom,
51,Requirement for area navigation equipment-aircraft registered elsewhere than in the United Kingdom,
52,Requirement for an airborne collision avoidance system,
53,Use of flight recording systems and preservation of records,
54,Towing of gliders,
55,Towing, picking up and raising of persons and articles by aircraft,
56,Dropping of articles and animals from aircraft,
57,Dropping of persons,
58,Requirement for aerial application certificate,
61,Carriage of persons in or on any part of an aircraft not designed for that purpose,
62,Requirement for exits and break-in markings,
66,Prohibition of smoking in aircraft,
67,Requirement to obey lawful commands of aircraft commander,
68 (a) and (b),Acting in a disruptive manner,
69,Prohibition of stowaways,
70,Flying displays,
72(3),Operator’s obligation to obtain flight time records of flight crew,
73(2),Flight crew member’s obligation to inform operator of flight times,
74,Flight time limitations,
84,Breach of the Rules of the Air,
85,Flight in contravention of restriction of flying regulations,
86,Flight by balloons, kites, airships, gliders and parascending parachutes,
87,Flight by small aircraft,
90,Provision of air traffic services,
91,Use of radio call signs at aerodromes,
94,Requirement for licensing of air traffic controllers,
99,Requirement for licensing of flight information service officers,
100,Requirement for aerodrome information service manual,
101,Requirement for licensed aerodrome,
103(5),Contravention of conditions of aerodrome licence,
104,Use of aeronautical radio stations,
105,Requirement to keep aeronautical radio station records,
109,Use of aeronautical lights,
110(1),Prohibition of dangerous lights,
110(2),Failure to extinguish or screen dangerous lights,
112(1) and (3),Management of aviation fuel at aerodromes,
117 (except (4)),Requirement to report occurrences,
120,Obstruction of persons performing duties under the Order,
JAR–145,
JAR—145.1(a),Flight without a certificate of release to service issued under JAR—145,

6,Flight for the purpose of public transport without an air operator’s certificate,
7,Flight in the service of a chief officer of police without a police air operator’s certificate,
8,Flight without a certificate of airworthiness,
59,Prohibition of carriage of weapons and munitions of war,
60,Prohibition of carriage of dangerous goods,
63,Endangering safety of aircraft,
64,Endangering safety of persons or property,
65,Prohibition of drunkenness in aircraft,
68(c),Intentional interference,
72(1),Operator’s obligation to regulate flight times of flight crew,
72(2),Operator’s obligation not to allow flight by crew in dangerous state of fatigue,
73(1),Crew’s obligation not to fly in dangerous state of fatigue,
75,Protection of air crew from cosmic radiation,
77,Keeping and production of records of exposure to cosmic radiation,
83 (except (3)),Use of false or unauthorised documents and records,
88,Provision of an air traffic control service without an approval,
96,Prohibition of drunkenness etc of controllers,
97,Controller’s obligation not to act in a dangerous state of fatigue,
112(4),Use of aviation fuel which is unfit for use in aircraft,
113,Restriction of flights for valuable consideration by non-UK registered aircraft,
115,Restriction of flights for aerial photography, aerial survey and aerial work by non-UK registered aircraft,
116,Operators' or commanders' obligations in respect of flights over any foreign country,
117(4),Making false reports,
118,Flight in contravention of direction not to fly,

1,1,
2,2,
3,3,
4,4,
5,5,
6,6,
7,7,
8,8,
9,9,
10,10,
11,11,
12,12,
13,13,
14,14,
15,15,
16,16,
17,17,
18,18,
19,19,
20,20,
21,21,
22,22 23 24 25 26,
23,27,
24,28,
25,29,
26,30,
27,31,
28,32,
29,33,
30,34,
31,35,
32,36,
32A,37,
33,38,
34,39,
35,40,
36,41,
37,42,
38,43,
39,44,
40,45,
41,46,
42,47 48 49,
44,50,
44,51,
—,52,
45,53,
46,54,
47,55,
48,56,
49,57,
50,58,
51,59,
52,60,
53,61,
54,62,
55,63,
56,64,
57,65,
58,66,
59,67,
—,68,
60,69,
61,70,
62,71,
63,72,
64,73,
65,74,
—,75,
66,76,
67,77,
68,78,
69,79,
70,80,
71,81,
72,82,
73,83,
74,84,
75,85,
76,86,
76A,87,
77,88,
78,89,
79,90,
80,91,
81,92,
82,93,
83,94,
84,95,
85,96,
86,97,
87,98,
88,99,
89,100,
90,101,
91,102,
92,103,
93,104,
94,105,
95,106,
96,107,
97,108,
98,109,
99,110,
100,111,
101,112,
102,113,
103,114,
104,115,
105,116,
106,117,
107,118,
108,119,
109,120,
110,121,
111,122,
112,123,
113,124,
114,125,
115,126,
116,127,
117,128,
118,129,
119,130,
120,131,
121,132,
122,133,
123,134,
