The Air Navigation (Overseas Territories) (Amendment) Order 1991

Type Statutory-Instrument
Publication 1991-02-05
State In force
Department Queen's Printer of Acts of Parliament
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Made: 5th February 1991

Laid before Parliament: 13th February 1991

Coming into force: 5th March 1991

At the Court at Buckingham Palace, the 5th day of February 1991 Present, The Queen’s Most Excellent Majesty in Council

Her Majesty, in exercise of the powers conferred on Her by sections 8, 41, 57, 58, 59 and 61 of the Civil Aviation Act 1949[^f00001], as extended to certain territories by the Civil Aviation Act 1949 (Overseas Territories) Order 1969[^f00002], as amended by the Civil Aviation Act 1971 (Overseas Territories) Order 1976[^f00003], and all other powers enabling Her in that behalf, is pleased, by and with the advice of Her Privy Council, to order, and it is hereby ordered as follows:

Citation and commencement

1

Amendment of the Air Navigation (Overseas Territories) Order 1989

2

The Air Navigation (Overseas Territories) Order 1989[^f00004] shall be amended as follows:

(b) 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;

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;

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

(v) two or more piston engines, unless it is equipped with an auto-pilot which has been approved by the Governor for the purposes of this Article and which is serviceable on take-off;

(b) the flight is 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.

Subject to paragraph (2) of this Article and to the provisions of Article 62 of this Order, a licence shall remain in force for the period indicated in the licence, not exceeding the period specified in respect of a licence of that class in the said Schedule, and may be renewed by the Governor from time to time upon his being satisfied that the applicant is a fit person and qualified as aforesaid.

(1A) (a) The Governor shall not on or after 5th March 1991 grant a Senior Commercial Pilot’s Licence (Aeroplanes) to any person who was not on 4th March 1991 the holder of such a licence. (b) A Senior Commercial Pilot’s Licence (Aeroplanes) shall remain in force until either: (i) the end of the period indicated in the licence, such period not exceeding 10 years; or (ii) 30th November 1995; whichever is the earlier.

unless carried in accordance with the terms of a written permission granted by the Governor which permission may be granted subject to such conditions as the Governor thinks fit.

of stowing baggage or carried in accordance with the terms of a written permission granted by the Governor which permission may be granted subject to such conditions as the Governor thinks fit.

(4) The operator of the helicopter shall at all times, subject to Article 61 of this Order, preserve:— (a) the last 8 hours of recording made by any flight data recorder specified at sub-paragraph (i) or (ii) of Scale SS of paragraph 5 of Schedule 4 to this Order and required by or under this Order to be carried in the helicopter; (b) in the case of a combined cockpit voice recorder/flight data recorder specified at sub-paragraph (iii) of the said Scale SS and required by or under this Order to be carried in a helicopter either:— (i) the last 8 hours of recording, or (ii) the last 5 hours of recording or the duration of the last flight, whichever is the greater, together with an additional period of recording for either:— (aa) the period immediately preceding the recording required to be retained pursuant to sub-paragraph (b)(ii) above, or (bb) such period or periods as the Governor may permit in any particular case or class of cases or generally. (5) The additional recording retained pursuant to sub-paragraphs (b)(ii)(aa) and (bb) of paragraph (4) above shall, together with the recording required to be retained pursuant to sub-paragraph (b)(ii) thereof, total a period of 8 hours and shall be retained in accordance with arrangements approved by the Governor. (6) An approval granted by the Governor for the purposes of this article shall be in writing and may be subject to such conditions as the Governor thinks fit.

“Passenger” means a person other than a member of the crew;

Provided also that a glider shall not be deemed to fly for the purpose of public transport for the purposes of part 111 of this Order by virtue of sub-paragraph (a)(iii) of this paragraph if the hire or reward given or promised for the primary purpose of conferring on a particular person the right to fly the glider on that flight is given or promised by a member of a flying club and the glider is owned or operated by that flying club.

(102) In relation to any of his functions pursuant to any of the provisions of this Order the Governor may, either absolutely or subject to such conditions as he thinks fit, approve a person as qualified to furnish reports to him and may accept such reports.

(d) having a maximum total weight authorised exceeding 5,700 kg. and which conform to a type for which a certificate of airworthiness was first applied for (whether in the Territory or elsewhere) after 30th April 1972 but not including an aeroplane which in the opinion of the Governor 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 (e) which are a turbo-jet and which have a maximum total weight authorised exceeding 22,700 kg; or (f) first issued with a type certificate (whether in the Territory 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.

(d) in respect of which there is in force 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 weight authorised exceeding 2,730 kg. but not exceeding 7,000 kg. or which in accordance with the certificate of airworthiness in force in respect thereof may carry more than 9 passengers or both (ii) which have a maximum total weight authorised exceeding 7,000 kg.

SCALE SS (i) A 4 channel cockpit voice recorder capable of recording and retaining the data recorded during at least the last 30 minutes of its operation and a flight data recorder capable of recording and retaining the data recorded during at least the last 8 hours of its operation being the data required to determine by reference to a time scale the following matters accurately in respect of the helicopter or gyroplane: (a) flight path; (b) speed; (c) attitude; (d) engine power; (e) main rotor speed; (f) outside air temperature; (g) position of pilot’s primary flight controls; (h) use of VHF transmitters; (j) use of automatic flight controls (if any); (k) use of stability augmentation system (if any); (l) cockpit warnings relating to the master warning system; and (m) selection of hydraulic system and cockpit warnings of failure of essential hydraulic systems. (ii) A 4 channel cockpit voice recorder capable of recording and retaining the data recorded during at least the last 30 minutes of its operation and a flight data recorder capable of recording and retaining the data recorded during at least the last 8 hours of its operation being the data required to determine by reference to a time scale the information specfied in paragraph (i) of this Scale together with the following matters accurately in respect of the helicopter or gyroplane: (n) landing gear configuration; (p) indicated sling load force if an indicator is provided in the helicopter or gyroplane of such a nature as to enable this information to be recorded with reasonable practicability; (q) radio altitude; (r) instrument landing system deviations; (s) marker beacon passage; (t) ground speed/drift angle or latitude/longitude if the navigational equipment provided in the helicopter or gyroplane is of such a nature as to enable this information to be recorded with reasonable practicability; and (u) main gear box oil temperature and pressure. (iii) (a) A combined cockpit voice recorder/flight data recorder which meets the following requirements— (aa) in respect of a helicopter or gyroplane which is otherwise required to carry a flight data recorder specified at paragraph (i) of this Scale the flight data recorder shall be capable of recording the data specified therein and retaining it for the duration therein specified; (bb) in the case of a helicopter or gyroplane which is otherwise required to carry a flight data recorder specified at paragraph (ii) of this Scale, the flight data recorder shall be capable of recording the data specified therein and retaining it for the duration therein specified; (cc) the cockpit voice recorder shall be capable of recording and retaining at least the last hour of cockpit voice recording information on not less that three separate channels. (b) In any case when a combined cockpit voice recorder/flight data recorder specified at paragraph (iii)(a) of this Scale is required to be carried by or under this Order, the flight data recorder shall be capable of retaining as protected data the data recorded during at least the last 5 hours of its operation or the maximum duration of the flight, whichever is the greater. lt shall also be capable of retaining additional data as unprotected data for a period which together with the period for which protected data is required to be retained amounts to a total of 8 hours: Provided that the flight data recorder need not be capable of retaining the said additional data if additional data is retained which relates to the period immediately preceding the period to which the required protected data relates or for such other period or periods as the Governor may permit pursuant to Article 37 of this Order and the additional data is retained in accordance with arrangements approved by the Governor. With the exception of flight data which it is expressly stated above may be unprotected, the cockpit voice recorder, flight data recorder or combined cockpit voice recorder and flight data recorder, as the case may be, shall be so constructed and installed that the record (herein referred to as “protected data”) would be likely to be preserved in the event of an accident and each cockpit voice recorder, flight data recorder or combined cockpit voice recorder/ flight data recorder required to be carried on the helicopter or gyroplane shall have attached an automatically activated underwater sonar location device or an emergency locator radio transmitter as appropriate: - Provided that a helicopter or gyroplane shall not be required to carry the said equipment if, before take-off, the equipment is found to be unserviceable and the aircraft flies in accordance with arrangements approved by the Governor.

(iii) An emergency floor path lighting system in the passenger compartments sufficient to facilitate the evacuation of the aircraft notwithstanding the failure of the lighting systems specified in paragraph (ii) of Scale G. Provided that if the equipment becomes unserviceable the aircraft may fly or continue to fly in accordance with arrangements approved by the Governor.

(4) (a) In the case of a person who is the holder of such a licence on 4th March 1991 then for so long as that licence or a renewal thereof is valid but not after 30th November 1995 he shall be entitled to fly as co-pilot of any aeroplane of a type specified in the aircraft rating included in the licence when the aeroplane is engaged on a flight for any purpose whatsoever, provided that he shall not be entitled to fly as co-pilot of an aeroplane which is engaged on a flight for the purpose of public transport unless he has more than 400 hours of flying experience as pilot in command of aeroplanes other than self-launching motor gliders and microlight aircraft and the maximum total weight authorised of the aeroplane does not exceed 5,700 kg. (b) On and after 1st December 1995 and in the case of a person who is the holder of such a licence granted on or after 5th March 1991 (not being a renewal of such a licence held on 4th March 1991) forthwith upon the grant of the licence, he shall be entitled to fly as co-pilot of any aeroplane of a type specified in the aircraft rating included in the licence when the aeroplane is engaged on a flight for any purpose whatsoever, provided that he shall not be entitled to fly as co-pilot of an aeroplane which is engaged on a flight for the purpose of public transport unless he has more that 400 hours of flying experience as pilot in command of aeroplanes other than self-launching motor gliders and microlight aircraft and the aeroplane is certificated for single pilot operation.

(d) (i) in the case of a person who is the holder of such a licence on 4th March 1991 then for so long as that licence or a renewal thereof is valid but not after 30th November 1995 he shall not fly such an aeroplane on a flight for the purpose of public transport if its maximum total weight authorised exceeds 5,700 kg; (ii) on and after 1st December 1995, and in the case of a person who is the holder of such a licence granted on or after 5th March 1991 (not being a renewal of such a licence held on 4th March 1991) forthwith upon the grant of the licence, he shall not fly such an aeroplane on a flight for the purpose of public transport unless it is certified for single pilot operation;

(b) (i) in the case of a person who is the holder of such a licence on 4th March 1991, then for so long as that licence or a renewal thereof is valid but not after 30th November 1995, he shall not fly such a helicopter or gyroplane on a flight for the purpose of public transport if its maximum total weight authorised exceeds 5,700 kg.; (ii) on and after 1st December 1995, and in the case of a person who is the holder of such a licence granted on or after 5th March 1991 (not being a renewal of such a licence held on 4th March 1991) forthwith upon the grant of the licence, he shall not fly such a helicopter or gyroplane on a flight for the purpose of public transport unless it is certificated for single pilot operation;

(7) Area Radar Control (Aerodrome) Rating shall entitle the holder of the licence, at any aerodrome for which the rating is valid, to provide air traffic control service with the aid of any type of surveillance radar equipment for which the rating is valid.

Signed

G. I. de Deney — Clerk of the Privy Council

Explanatory note

(This note is not part of the Order)

This Order amends the Air Navigation (Overseas Territories) Order 1989. In addition to minor and drafting amendments the following changes are made—

Footnotes

[^f00001]: 1949 c. 67.

[^f00002]: S.I. 1969/592.

[^f00003]: S.I. 1976/1912.

[^f00004]: S.I. 1989/2395.

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