时间：2015-01-22 15:18来源：蓝天飞行翻译公司 作者：民航翻译 点击：次
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To view this page ensure that Adobe Flash Player version 9.0.124 or greater is installed. (2) Has been authorised by the [STATE] for MNPS operations concerned through either operations specifications for AOC holders or letter of authorisation for general aviation. Note: Equipment shall comply with minimum navigation performance specifications prescribed in ICAO Doc 7030 in the form of Regional Supplementary Procedures. (h) [AAC] The navigation equipment required for operations in MNPS airspace shall be visible and usable by either pilot seated at his duty station. (i) [AAC] For unrestricted operation in MNPS airspace, an aeroplane shall be equipped with two independent Long-Range Navigation Systems (LRNS). (j) [AAC] For operation in MNPS airspace along notified special routes, an aeroplane shall be equipped with one LRNS, unless otherwise specified. ICAO Annex, Part I: 7.2.3 ICAO Annex 6, Part II: Section II: 2.5.2.3 14 CFR: 91.705 and Appendix C JAR-OPS 1: 1.870 7.4.1.3 REDUCED VERTICAL SEPARATION MINIMUM (a) [AAC] For flights in defined portions of airspace where, based on Regional Air Navigation Agreement, a reduced vertical separation minimum (RVSM) of 300 m (1,000 ft) is applied between FL 290 and FL 410 inclusive, an aeroplane: (1) Shall be provided with equipment that is capable of: (i) Indicating to the flightcrew the flight level being flown; (ii) Automatically maintaining a selected flight level; (iii) Providing an alert to the flightcrew when a deviation occurs from the selected flight level. The threshold for the alert shall not exceed + or – 90 m (300 ft); and (iv) Automatically reporting pressure-altitude and (2) Shall be authorised for operations in the airspace concerned by – (i) The State of Operator for AOC holders through operations specifications, or (ii) The State of Registry for non-AOC holders through letter of authorisation. (3) Shall satisfy the demonstration requirements specified in IS 7.4.1.3 as to the altimetry system performance requirements for vertical navigation performance capability. (b) Prior to granting an RVSM approval required by paragraph (a)(2), the [STATE] shall be satisfied that: (1) The vertical navigation performance capability of the aeroplane satisfies the requirements specified in IS 7.4.1.3 (2) The operator has instituted appropriate procedures in respect of continued airworthiness (maintenance and repair) practices and programmes; and (3) The operator has instituted appropriate flightcrew procedures for operations in RVSM airspace. Note: An RVSM approval is valid globally on the understanding that any operating procedures specific to a given region will be stated in the operations manual or appropriate crew guidance. (c) RVSM. The [STATE] in consultation with the State of Registry, if appropriate, shall ensure that, in respect of those aeroplanes mentioned in item (a)(2) above, adequate provisions exist for: (1) Receiving the reports of height-keeping performance issued by the monitoring agencies established in accordance with ICAO Annex 11, 3.3.4.1; and (2) Taking immediate corrective action for individual aircraft, or aircraft type groups, identified in such reports as not complying with the height-keeping requirements for operations in airspace where RVSM is applied. (d) An operator with RVSM approval shall ensure that a minimum of two aeroplanes of each aircraft type grouping of the operator have their height-keeping performance monitored, at least once every two years or within intervals of 1 000 flight hours per aeroplane, whichever period is longer. If an operator aircraft type grouping consists of a single aeroplane, monitoring of that aeroplane shall be accomplished within the specified period. (e) An operator shall ensure that each aeroplane shall be sufficiently provided with navigation equipment to ensure that, in the event of the failure of one item of equipment at any stage of the flight, the remaining equipment will enable the aeroplane to navigate in accordance with paragraphs (a), (b) and (c) of 7.4.1.3. (f) RVSM. The Authority will take appropriate action in respect of aircraft and operators found to be operating in RVSM airspace in [STATE] without a valid RVSM approval. Note 1: These provisions and procedures need to address both the situation where the aircraft in question is operating without approval in the airspace of the State, and the situation where an operator for which the State has regulatory oversight responsibility is found to be operating without the required approval in the airspace of another State. Note 2: See ICAO Doc 9574, Manual on Implementation of a 300 m (1,000 ft) Vertical Separation Minimum Between FL 290 and FL 410 Inclusive, for guidance relating to the approval for operations in RVSM airspace. ICAO Annex 6, Part I: 7.2.4; 7.2.5; 7.2.6; 7.2.7; 7.2.8; 7.2.9; 7.2.10 and note, and Appendix 4. ICAO Annex 6, Part II: Section II: 2.5.2.4; 2.5.4.3; 2.5.4.4; 2.5.4.6; 2.5.4.7; 2.5.4.8; 2.5.4.9; 2.5.2.10 and notes 14 CFR: 91.180; 91.706 and Appendix G JAR OPS 1: 1.872 7.4.1.4 ELECTRONIC NAVIGATION DATA MANAGEMENT (a) Electronic navigation data management. [AAC] No person shall employ electronic navigation data products that have been processed for application in the air and on the ground unless the Authority has approved: (1) The operator’s procedures for ensuring that the process applied and the products delivered have acceptable standards of integrity and that the products are compatible with the intended function of the equipment that will use them; (2) The operator’s programme for continual monitoring of both process and products; and (3) The operator’s procedures to ensure the timely distribution and insertion of current and unaltered electronic navigation data to all aircraft that require it. Note: Guidance relating to the processes that data suppliers may follow is contained in RTCA DO -200A/EUROCAE ED-76 and RTCA DO – 201A/EUROCAE ED- 77. ICAO Annex 6, Part I: 7.4.1; 7.4.2 ICAO Annex 6, Part II, Section III: 3.7.3 7.4.1.5 ALTITUDE REPORTING TRANSPONDER (a) [AAC] No person may operate an aeroplane or helicopter unless it is equipped with an operative pressure-altitude reporting transponder that operates in accordance with the requirements of [STATE] air traffic services and the relevant provisions of ICAO Annex 10, Volume 4. (b) [AAC] No person may operate an aircraft in airspace that requires a pressure reporting transponder unless that equipment is operative. (c) [AOC] No person may operate an aeroplane unless it is equipped with a data source that provides pressure-altitude information with a resolution of 7.62 m (25 ft) or better. (d) [AOC] No person may operate an aeroplane that is equipped with an automatic means of detecting airborne/on-the-ground status unless it is equipped with a Mode S transponder. Note 1: These provisions will improve the effectiveness of airborne collision avoidance systems as well as air traffic services that employ Mode S radar. In particular, tracking processes are significantly enhanced with a resolution of 7.62 m (25 ft), or better. Note 2: Mode C replies of transponders always report pressure altitude in 30.50 m (100 ft) increments irrespective of the resolution of the data service. ICAO Annex 6. Part I: 6.19; 6.19.1; 6.19.2; 6.19.3; 6.19.4R ICAO Annex 6, Part II: Section II: 2.4.13; 2.4.13.1; 2.4.13.2 ICAO Annex 6, Part III, Section II: 4.13 ICAO Annex 6, Part III, Section III: 4.9.1 ; 4.9.2 14 CFR: 91.215 7.5 AIRCRAFT LIGHTS AND INSTRUMENT ILLUMINATION 7.5.1.1 REQUIRED AIRCRAFT LIGHTS AND INSTRUMENT ILLUMINATION (a) [AAC] All aircraft operated at night by, shall be equipped with: (1) A landing light; (2) Navigation/position lights; (3) Illumination for all flight instruments and equipment that are essential for the safe operation of the aircraft; (4) Lights in all passenger compartments; and (5) A flashlight for each crewmember station (approval not required). (b) All aircraft type certificated with aviation red or aviation white anti-collision system shall have the anti-collision system operative in both day and night. In the event of the failure of any light of the anti-collision light system, operation of the aircraft may continue to a location where repairs or replacement can be made. 7.5.1.2 REQUIRED AIRCRAFT LIGHTS AND INSTRUMENT ILLUMINATION FOR COMMERCIAL AIR TRANSPORT OPERATIONS (a) [AOC] No person may operate an aircraft in commercial air transport operations unless it is equipped with: (b) Two landing lights or a single light having two separately energised filaments; (c) An anti-collision light system; (d) Illumination for all flight instruments and equipment that are essential for the safe operation of the aircraft; (e) Lights in all passenger compartments; (f) A flashlight for each crew member station; (g) Navigation/position lights; and (h) Lights to conform to the International regulations for preventing collisions at sea if the aircraft is a seaplane or an amphibian aircraft. (i) For helicopters — a landing light that is trainable, at least in the vertical plane. ICAO Annex 2: 3.2.3.1 ICAO Annex 6, Part I: 6.10 ICAO Annex 6, Part II, Section II: 2.4.8 ICAO Annex 6, Part III, Section II: 4.4.2; 4.4.2.R ICAO Annex 6, Part III, Section III: 4.2.2 ICAO Doc. 9388: 2.4.1.6(l); 2.4.2.6(n) 14 CFR: 91.205(b)(11), (c(1))(3); 91.209, 91.507; 121.323, 121.549 JAR-OPS 1: 1.640 7.6 ENGINE INSTRUMENTS 7.6.1.1 ENGINE INSTRUMENTS (a) [AAC] Unless the Authority allows or requires different instrumentation for turbine engine powered aeroplanes to provide equivalent safety, no person may operate any powered aircraft without the following engine instruments: |
