Publication: Magyar Közlöny
Issue: MK-2009-104 (Year: 2009, Number: 104)
Era: 2004-2010
Section: 
Paragraph Index: 1345

c) equipment for making the pyrotechnical distress signals described in Annex 2. Section III, Chapter 4 Annex 6 — Operation of Aircraft III-4-5 22/11/07 4.3.2.2 When taking off or landing at a heliport where, in the opinion of the State of the Operator, the take-off or approach path is so disposed over water that in the event of a mishap there would be likelihood of a ditching, at least the equipment required in 4.3.2.1 a) shall be carried. 4.3.2.3 Each life jacket and equivalent individual flotation device, when carried in accordance with this 4.3, shall be equipped with a means of electric illumination for the purpose of facilitating the location of persons. 4.3.2.4 Recommendation.— On any helicopter for which the individual certificate of airworthiness is first issued on or after 1 January 1991, at least 50 per cent of the life rafts carried in accordance with the provisions of 4.3.2 should be deployable by remote control. 4.3.2.5 Recommendation.— Rafts which are not deployable by remote control and which have a mass of more than 40 kg should be equipped with some means of mechanically assisted deployment. 4.3.2.6 Recommendation.— On any helicopter for which the individual certificate of airworthiness was first issued before 1 January 1991, the provisions of 4.3.2.4 and 4.3.2.5 should be complied with no later than 31 December 1992. 4.4 All helicopters on flights over designated land areas Helicopters, when operated across land areas which have been designated by the State concerned as areas in which search and rescue would be especially difficult, shall be equipped with such signalling devices and life-saving equipment (including means of sustaining life) as may be appropriate to the area overflown. 4.5 All helicopters on high altitude flights 4.5.1 Unpressurized helicopters Unpressurized helicopters intended to be operated at high altitudes shall carry equipment for storing and dispensing the oxygen supplies required in 2.9.1. 4.5.2 Pressurized helicopters Recommendation.— Pressurized helicopters intended to be operated at high altitudes should carry emergency oxygen storage and dispensing equipment capable of storing and dispensing the oxygen supplies required in 2.9.2. 4.6 All helicopters required to comply with the noise certification Standards in Annex 16, Volume I All helicopters required to comply with the noise certification Standards of Annex 16, Volume I, shall carry a document attesting noise certification. When the document, or a suitable statement attesting noise certification as contained in another document approved by the State of Registry, is issued in a language other than English, it shall include an English translation. Note 1.— The attestation may be contained in any document, carried on board, approved by the State of Registry in accordance with the relevant provisions of Annex 16, Volume I. Annex 6 — Operation of Aircraft Part III 22/11/07 III-4-6 Note 2.— The various noise certification Standards of Annex 16, Volume I, which are applicable to helicopters are determined according to the date of application for a type certificate, or the date of acceptance of an application under an equivalent prescribed procedure by the certificating authority. Some helicopters are not required to comply with any noise certification Standard. For details see Annex 16, Volume I, Part II, Chapters 8 and 11. 4.7 Flight recorders Note 1.— Flight recorders comprise two systems — a flight data recorder (FDR) and a cockpit voice recorder (CVR). Note 2.— Combination recorders (FDR/CVR) can only be used to meet the flight recorder equipage requirements as specifically indicated in this Annex. Note 3.— Detailed guidance on flight recorders is contained in Attachment B. 4.7.1 Flight data recorders — types 4.7.1.1 Type IV FDRs 4.7.1.1.1 A Type IV FDR shall record the parameters required to determine accurately the helicopter flight path, speed, attitude, engine power and operation. 4.7.1.1.2 A Type IVA FDR shall record the parameters required to determine accurately the helicopter flight path, speed, attitude, engine power, operation and configuration. 4.7.1.2 A Type V FDR shall record the parameters required to determine accurately the helicopter flight path, speed, attitude and engine power. 4.7.1.3 The use of engraving metal foil FDRs shall be discontinued by 1 January 1995. 4.7.1.4 Recommendation.— The use of analogue FDRs using frequency modulation (FM) should be discontinued by 5 November 1998. 4.7.1.4.1 The use of photographic film FDRs shall be discontinued from 1 January 2003. 4.7.1.5 All helicopters for which the individual certificate of airworthiness is first issued after 1 January 2005, which utilize data link communications and are required to carry a CVR, shall record on a flight recorder all data link communications to and from the helicopter. The minimum recording duration shall be equal to the duration of the CVR and shall be correlated to the recorded cockpit audio. 4.7.1.5.1 From 1 January 2007, all helicopters which utilize data link communications and are required to carry a CVR, shall record on a flight recorder, all data link communications to and from the helicopter. The minimum recording duration shall be equal to the duration of the CVR and shall be correlated to the recorded cockpit audio. 4.7.1.5.2 Sufficient information to derive the content of the data link communications message and, whenever practical, the time the message was displayed to or generated by the crew shall be recorded. Note.— Data link communications include, but are not limited to, automatic dependent surveillance — contract (ADS-C), controller-pilot data link communications (CPDLC), data link-flight information services (D-FIS) and aeronautical operational control (AOC) messages. Section III, Chapter 4 Annex 6 — Operation of Aircraft III-4-7 22/11/07 4.7.1.6 Recommendation.— All helicopters of a maximum certificated take-off mass over 2 730 kg, required to be equipped with an FDR and/or a CVR, may alternatively be equipped with one combination recorder (FDR/CVR) 4.7.2 Flight data recorders — duration Types IV and V FDRs shall be capable of retaining the information recorded during at least the last ten hours of their operation. 4.7.3 Flight data recorders — helicopters for which the individual certificate of airworthiness is first issued on or after 1 January 1989 4.7.3.1 All helicopters of a maximum certificated take-off mass of over 7 000 kg shall be equipped with a Type IV FDR. 4.7.3.2 Recommendation.— All helicopters of a maximum certificated take-off mass of over 2 730 kg, up to and including 7 000 kg, should be equipped with a Type V FDR. 4.7.4 Flight data recorders — helicopters for which the individual certificate of airworthiness is first issued after 1 January 2005 All helicopters of a maximum certificated take-off mass of over 3 175 kg shall be equipped with a Type IVA FDR with a recording duration of at least 10 hours. Note.— A single, combination CVR/FDR is acceptable. 4.7.5 Cockpit voice recorders — helicopters for which the individual certificate of airworthiness is first issued on or after 1 January 1987 Note.— CVR performance requirements are as contained in the Minimum Operational Performance Specification (MOPS) document for Flight Recorder Systems of the European Organization for Civil Aviation Equipment (EUROCAE) or equivalent documents. 4.7.5.1 All helicopters of a maximum certificated take-off mass of over 7 000 kg shall be equipped with a CVR, the objective of which is the recording of the aural environment on the flight deck during flight time. For helicopters not equipped with an FDR, at least main rotor speed shall be recorded on one track of the CVR. 4.7.5.2 Recommendation.— All helicopters of a maximum certificated take-off mass of over 3 175 kg, up to and including 7 000 kg, should be equipped with a CVR, the objective of which is the recording of the aural environment on the flight deck during flight time. For helicopters not equipped with an FDR, at least main rotor speed should be recorded on one track of the CVR. 4.7.6 Cockpit voice recorders — duration 4.7.6.1 A CVR shall be capable of retaining the information recorded during at least the last 30 minutes of its operation. 4.7.6.2 Recommendation.— A CVR, installed in helicopters for which the individual certificate of airworthiness is first issued on or after 1 January 1990, should be capable of retaining the information recorded during at least the last two hours of its operation. Annex 6 — Operation of Aircraft Part III 22/11/07 III-4-8 4.7.6.3 A CVR, installed in helicopters for which the individual certificate of airworthiness is first issued after 1 January 2003, shall be capable of retaining the information recorded during at least the last two hours of its operation. 4.7.7 Flight recorders — construction and installation Flight recorders shall be constructed, located and installed so as to provide maximum practical protection for the recordings in order that the recorded information may be preserved, recovered and transcribed. 4.7.8 Flight recorders — operation 4.7.8.1 Flight recorders shall not be switched off during flight time. 4.7.8.2 To preserve flight recorder records, flight recorders shall be deactivated upon completion of flight time following an accident or incident. The flight recorders shall not be reactivated before their disposition as determined in accordance with Annex 13. Note 1.— The need for removal of the flight recorder records from the aircraft is to be determined by the investigation authority in the State conducting the investigation with due regard to the seriousness of an occurrence and the circumstances, including the impact on the operation. Note 2.— The operator’s responsibilities regarding the retention of flight recorder records are contained in Section II, 9.6. 4.7.9 Flight recorders — continued serviceability Operational checks and evaluations of recordings from the FDR and CVR systems shall be conducted to ensure the continued serviceability of the recorders. Note.— Procedures for the inspections of the flight data and CVR systems are given in Attachment B. 4.8 Emergency locator transmitter (ELT) Applicable until 30 June 2008 4.8.1 Performance Class 1 and 2 helicopters for which the individual certificate of airworthiness is first issued after 1 January 2002, operating on flights over water as described in 4.3.1 a) and performance Class 3 helicopters for which the individual certificate of airworthiness is first issued after 1 January 2002, operating as described in 4.3.1 b) shall be equipped with at least one automatic ELT and one ELT(S) in a raft. 4.8.2 From 1 January 2005, all performance Class 1 and 2 helicopters operating on flights over water as described in 4.3.1 a) and performance Class 3 helicopters operating as described in 4.3.1 b) shall be equipped with at least one automatic ELT and one ELT(S) in a raft. 4.8.3 Helicopters for which the individual certificate of airworthiness is first issued after 1 January 2002, on flights over designated land areas as described in 4.4 shall be equipped with at least one automatic ELT. 4.8.4 From 1 January 2005, helicopters on flights over designated land areas as described in 4.4 shall be equipped with at least one automatic ELT. Section III, Chapter 4 Annex 6 — Operation of Aircraft III-4-9 22/11/07 4.8.5 Recommendation.— All helicopters should carry an automatic ELT. 4.8.6 ELT equipment carried to satisfy the requirements of 4.8.1, 4.8.2, 4.8.3, 4.8.4 and 4.8.5 shall operate in accordance with the relevant provisions of Annex 10, Volume III. Applicable from 1 July 2008 4.8.7 From 1 July 2008, all helicopters operating in performance Class 1 and 2 shall be equipped with at least one automatic ELT and, when operating on flights over water as described in 4.3.1 a), with at least one automatic ELT and one ELT(S) in a raft or life jacket. 4.8.8 From 1 July 2008, all helicopters operating in performance Class 3 shall be equipped with at least one automatic ELT and, when operating on flights over water as described in 4.3.1 b), with at least one automatic ELT and one ELT(S) in a raft or life jacket. 4.8.9 ELT equipment carried to satisfy the requirements of 4.8.7 and 4.8.8 shall operate in accordance with the relevant provisions of Annex 10, Volume III. Note.— The judicious choice of numbers of ELTs, their type and placement on aircraft and associated floatable life support systems will ensure the greatest chance of ELT activation in the event of an accident for aircraft operating over water or land, including areas especially difficult for search and rescue. Placement of transmitter units is a vital factor in ensuring optimal crash and fire protection. The placement of the control and switching devices (activation monitors) of automatic fixed ELTs and their associated operational procedures will also take into consideration the need for rapid detection of inadvertent activation and convenient manual switching by crew members. 4.9 Helicopters required to be equipped with a pressure-altitude reporting transponder 4.9.1 From 1 January 2003, unless exempted by the appropriate authorities, all helicopters shall be equipped with a pressure-altitude reporting transponder which operates in accordance with the relevant provisions of Annex 10, Volume IV. 4.9.2 Recommendation.— All helicopters should be equipped with a pressure-altitude reporting transponder which operates in accordance with the relevant provisions of Annex 10, Volume IV. Note.— The provisions in 4.9.1 and 4.9.2 are intended to support the effectiveness of ACAS as well as to improve the effectiveness of air traffic services. Effective dates for carriage requirements of ACAS are contained in Annex 6, Part I, 6.18.1 and 6.18.2. The intent is also for aircraft not equipped with pressure-altitude reporting transponders to be operated so as not to share airspace used by aircraft equipped with airborne collision avoidance systems. To this end, exemptions from the carriage requirement for pressure-altitude reporting transponders could be given by designating airspace where such carriage is not required. 4.10 Microphones Recommendation.— All flight crew members required to be on flight deck duty should communicate through boom or throat microphones ___________________ ANNEX 6 — PART III III-5-1 22/11/07 CHAPTER 5. HELICOPTER COMMUNICATION AND NAVIGATION EQUIPMENT 5.1 Communication equipment 5.1.1 A helicopter to be operated in accordance with IFR or at night shall be provided with radio communication equipment. Such equipment shall be capable of conducting two-way communication with those aeronautical stations and on those frequencies prescribed by the appropriate authority. Note.— The requirements of 5.1.1 are considered fulfilled if the ability to conduct the communications specified therein is established during radio propagation conditions which are normal for the route. 5.1.2 When compliance with 5.1.1 requires that more than one communication equipment unit be provided, each shall be independent of the other or others to the extent that a failure in any one will not result in failure of any other. 5.1.3 A helicopter to be operated in accordance with VFR, but as a controlled flight, shall, unless exempted by the appropriate authority, be provided with radio communication equipment capable of conducting two-way communication at any time during flight with such aeronautical stations and on such frequencies as may be prescribed by the appropriate authority. 5.1.4 A helicopter to be operated on a flight to which the provisions of 4.3 or 4.4 apply shall, unless exempted by the appropriate authority, be provided with radio communication equipment capable of conducting two-way communication at any time during flight with such aeronautical stations and on such frequencies as may be prescribed by the appropriate authority. 5.1.5 Recommendation.— The radio communication equipment required in accordance with 5.1.1 to 5.1.4 should provide for communication on the aeronautical emergency frequency. 5.1.6 For flights in defined portions of airspace or on routes where an RCP type has been prescribed, a helicopter shall, in addition to the requirements specified in 5.1.1 to 5.1.5:

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