Publication: Magyar Közlöny
Issue: MK-2007-70 (Year: 2007, Number: 70)
Era: 2004-2010
Section: Melléklet a 2007. évi XLVI. törvényhez
Paragraph Index: 3033

c) a suitably located U F distance measuring e uipment (DME) conforming to the specifications in Chapter and providing continuous distance information during the approach and missed approach phase of flight 2.1.6 Required navigation performance (RNP) for approach, landing and departure operations 2.1.6.1 Where used, RNP for approach, landing and departure operations shall be prescribed by States. 2.1.6.2 Where RNP is prescribed for precision approach and landing operations, the RNP shall only be supported by a standard non-visual aid in accordance with 2.1.1. 2 2 S ort distance aids 2.2.1 In localities and along routes where conditions of traffic density and low visibility necessitate a ground-based short-distance radio aid to navigation for the efficient exercise of air traffic control, or where such short-distance aid is required for the safe and efficient conduct of aircraft operations, the standard aid shall be the VHF omnidirectional radio range (VOR) of the continuous wave phase comparison type conforming to the Standards contained in Chapter 3, 3.3. Note It is not intended that short distance radio aids to navigation provided in accordance with should be re uired primarily to perform the function of a long distance navigation aid Note It is intended that wherever a R conforming to the Standard in has been installed no change in or addition to that Standard will re uire the replacement of such e uipment before anuary 2.2.1.1 Recommendation Means should be provided for the pre flight chec ing of R airborne e uipment at aerodromes regularly used by international air traffic Note uidance material on the pre flight chec ing of R airborne e uipment is contained in Attachment E 2.2.2 At localities where for operational reasons, or because of air traffic control reasons such as air traffic density or proximity of routes, there is a need for a more precise navigation service than that provided by VOR, distance measuring equipment (DME) (conforming to the Standards in Chapter 3, 3.5) shall be installed and maintained in operation as a complement to VOR. 2.2.2.1 DME/N equipment first installed after 1 January 1989 shall also conform to the Standards in Chapter 3, 3.5 denoted by . Note It is intended that wherever a DME conforming to the Standard in has been installed no change in or addition to that Standard will re uire the replacement of such e uipment before anuary 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I 2 3 Radio beacons 2.3.1 Non-directional radio beacons (NDB) 2.3.1.1 An NDB conforming to the Standards in Chapter 3, 3.4 shall be installed and maintained in operation at a locality where an NDB, in conjunction with direction-finding equipment in the aircraft, fulfils the operational requirement for a radio aid to navigation. 2.3.2 En-route VHF marker beacons (75 MHz) 2.3.2.1 Recommendation here a F mar er beacon is re uired to mar a position on any air route a fan mar er beacon conforming to the Standard contained in Chapter should be installed and maintained in operation Note This recommendation does not preclude the use of fan mar er beacons at points other than on an air route as for example an aid to descent under IFR conditions 2.3.2.2 Recommendation here a F mar er beacon is re uired to mar the position of a radio navigation aid giving directional or trac guidance a mar er conforming to the Standard in Chapter should be installed and maintained in operation lobal na igation satellite system SS 2.4.1 A standard aid to navigation shall be the global navigation satellite system (GNSS) conforming to the Standards contained in Chapter 3, 3.7. Note It is intended that any change in or addition to Standards in Chapter that will re uire the replacement of NSS e uipment can become applicable on the basis of a six year advance notice Note NSS is expected to support all phases of flight and aerodrome surface operations however present SARPs provide for en route terminal and approach and landing operations down to Category I precision approach 2.4.2 It shall be permissible to terminate a GNSS satellite service provided by one of its elements (Chapter 3, 3.7.2) on the basis of at least a six-year advance notice by a service provider. 2.4.3 Recording and retention of GNSS data 2.4.3.1 Recommendation A State that approves NSS based operations should ensure that NSS data relevant to those operations are recorded Note These recorded data are primarily intended for use in accident and incident investigations They may also support periodic confirmation that accuracy integrity continuity and availability are maintained within the limits re uired for the operations approved Note uidance material on the recording of NSS parameters is contained in Attachment D 2.4.3.2 Recommendation Recordings should be retained for a period of at least fourteen days hen the recordings are pertinent to accident and incident investigations they should be retained for longer periods until it is evident that they will no longer be re uired 23/11/06 2007/70/II. szám C a ter Annex 10 — Aeronautical Communications Reser ed 2 6 Distance measuring aids 2.6.1 Recommendation If a distance measuring facility is installed and maintained in operation for any radio navigational purpose additional to that specified in it should conform to the specification in Chapter round and flig t testing 2.7.1 Radio navigation aids of the types covered by the specifications in Chapter 3 and available for use by aircraft engaged in international air navigation shall be the subject of periodic ground and flight tests. Note uidance on the ground and flight testing of ICA standard facilities is contained in Attachment C and in the Manual on Testing of Radio Navigation Aids (Doc ) ro ision of information on t e operational status of radio na igation aids 2.8.1 Aerodrome control towers and units providing approach control service shall be provided without delay with information on the operational status of radio navigation aids essential for approach, landing and take-off at the aerodrome(s) with which they are concerned. Secondary po er supply for radio na igation aids and communication systems 2.9.1 Radio navigation aids and ground elements of communication systems of the types specified in Annex 10 shall be provided with suitable power supplies and means to ensure continuity of service appropriate to the needs of the service provided. Note uidance material on this subject is contained in Section of Attachment C 2 10 Human Factors considerations 2.10.1 Recommendation uman Factors principles should be observed in the design and certification of radio navigation aids Note uidance material on uman Factors principles can be found in the Human Factors Training Manual (Doc ) and Circular (Human Factors Digest No. 11 — Human Factors in CNS/ATM Systems). ___________________ 23/11/06 2007/70/II. szám ANNEX 10 — VOLUME I 3 1 23/11/06 CHA ER 3 S EC F CA O S FOR RAD O A A O A DS Note Specifications concerning the siting and construction of e uipment and installations on operational areas aimed at reducing the ha ard to aircraft to a minimum are contained in Annex Chapter 3 1 Specification for S 3.1.1 Definitions An ular dis lacement sensitivit The ratio of measured DDM to the corresponding angular displacement from the appropriate reference line. ac course sector The course sector which is situated on the opposite side of the localizer from the runway. Course line The locus of points nearest to the runway centre line in any horizontal plane at which the DDM is zero. Course sector A sector in a horizontal plane containing the course line and limited by the loci of points nearest to the course line at which the DDM is 0.155. — i erence in de t o modulation The percentage modulation depth of the larger signal minus the percentage modulation depth of the smaller signal, divided by 100. is lacement sensitivit (locali er) The ratio of measured DDM to the corresponding lateral displacement from the appropriate reference line. Facilit er ormance Cate or I — I An ILS which provides guidance information from the coverage limit of the ILS to the point at which the localizer course line intersects the ILS glide path at a height of 60 m (200 ft) or less above the horizontal plane containing the threshold. Note This definition is not intended to preclude the use of Facility Performance Category I I S below the height of m ( ft) with visual reference where the uality of the guidance provided permits and where satisfactory operational procedures have been established Facilit er ormance Cate or II — I An ILS which provides guidance information from the coverage limit of the ILS to the point at which the localizer course line intersects the ILS glide path at a height of 15 m (50 ft) or less above the horizontal plane containing the threshold. Facilit er ormance Cate or III — I An ILS which, with the aid of ancillary equipment where necessary, provides guidance information from the coverage limit of the facility to, and along, the surface of the runway. Front course sector The course sector which is situated on the same side of the localizer as the runway. al course sector The sector, in a horizontal plane containing the course line and limited by the loci of points nearest to the course line at which the DDM is 0.0775. 2007/70/II. szám Annex 10 — Aeronautical Communications Volume I 23/11/06 3 2 al I lide at sector The sector in the vertical plane containing the ILS glide path and limited by the loci of points nearest to the glide path at which the DDM is 0.0875. I continuit o service That quality which relates to the rarity of radiated signal interruptions. The level of continuity of service of the localizer or the glide path is expressed in terms of the probability of not losing the radiated guidance signals. I lide at That locus of points in the vertical plane containing the runway centre line at which the DDM is zero, which, of all such loci, is the closest to the horizontal plane. I lide at an le The angle between a straight line which represents the mean of the ILS glide path and the horizontal. I lide at sector The sector in the vertical plane containing the ILS glide path and limited by the loci of points nearest to the glide path at which the DDM is 0.175. Note The I S glide path sector is located in the vertical plane containing the runway centre line and is divided by the radiated glide path in two parts called upper sector and lower sector referring respectively to the sectors above and below the glide path I inte rit That quality which relates to the trust which can be placed in the correctness of the information supplied by the facility. The level of integrity of the localizer or the glide path is expressed in terms of the probability of not radiating false guidance signals. I oint A A point on the ILS glide path measured along the extended runway centre line in the approach direction a distance of 7.5 km (4 NM) from the threshold. I oint A point on the ILS glide path measured along the extended runway centre line in the approach direction a distance of 1 050 m (3 500 ft) from the threshold. I oint C A point through which the downward extended straight portion of the nominal ILS glide path passes at a height of 30 m (100 ft) above the horizontal plane containing the threshold. I oint A point 4 m (12 ft) above the runway centre line and 900 m (3 000 ft) from the threshold in the direction of the localizer. I oint A point 4 m (12 ft) above the runway centre line and 600 m (2 000 ft) from the stop end of the runway in the direction of the threshold. Note See Attachment C Figure C I re erence datum ( oint ) A point at a specified height located above the intersection of the runway centre line and the threshold and through which the downward extended straight portion of the ILS glide path passes. wo re uenc lide at s stem An ILS glide path in which coverage is achieved by the use of two independent radiation field patterns spaced on separate carrier frequencies within the particular glide path channel. wo re uenc locali er s stem A localizer system in which coverage is achieved by the use of two independent radiation field patterns spaced on separate carrier frequencies within the particular localizer VHF channel. 2007/70/II. szám C a ter Annex 10 — Aeronautical Communications 3 3 23/11/06 3.1.2 Basic requirements 3.1.2.1 The ILS shall comprise the following basic components:

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