時間：2015-01-22 15:21來源：藍(lán)天飛行翻譯公司 作者：民航翻譯 點擊：次
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To view this page ensure that Adobe Flash Player version 9.0.124 or greater is installed. (d) The PIC signing the operational flight plan shall have access to the applicable flight planning information for fuel supply, alternate aerodromes, weather reports and forecasts and NOTAMs for the routing and aerodrome. (e) No person may continue a flight from an intermediate aerodrome without a new operational flight plan if the aircraft has been on the ground more than 6 hours. ICAO Annex 6, Part I: 4.3.1(g); 4.6.1 ICAO Annex 6, Part III, Section II: 2.3.1(g); 2.6.1 14 CFR: 121.595(a), 121.595(b), 121.597 8.7 AIRCRAFT OPERATING AND PERFORMANCE LIMITATIONS 8.7.1 ALL AIRCRAFT 8.7.1.1 APPLICABILITY (a) This Section prescribes the operating and performance limitations for all civil aircraft. ICAO Annex 6, Part I: 5.1.1 ICAO Annex 6, Part II: 5.1 ICAO Annex 6, Part III, Section II: 3.1.1; Annex 6, Part III, Section III: 3.1 8.7.1.2 GENERAL (a) No person may operate an aircraft that— (1) Exceeds its designed performance limitations for any operation, as established by the State of Registry; (2) Exceeds the operating limitations contained in the aircraft flight manual, or its equivalent; (3) Exceeds the terms of its certificate of airworthiness; or (4) Exceeds the mass limitations, if applicable, imposed by the terms of its noise certification standards, as contained in the applicable part of ICAO Annex 16, Volume I, unless otherwise approved by the Authority. ICAO Annex 6, Part I, 5.1.1, 5.2.3; 5.2.7(d) Annex 6, Part II: 5.1 ICAO Annex 6, Part III, Section II: 3.1.1; 3.2.3; 3.2.7(d); Annex 6, Part III, Section III: 3.1 14 CFR: 121.173(d) 8.7.1.3 AIRCRAFT PERFORMANCE CALCULATIONS (a) Each operator shall ensure that the performance data contained in the AFM, RFM, or other authorised source is used to determine compliance with the appropriate requirements of Subpart 8.7. (b) When applying performance data, each person performing calculations shall account for all factors that significantly affect the performance of the aircraft configuration, including, but not limited to: mass of the aeroplane, the operating procedures, the pressure-altitude appropriate to the elevation of the aerodrome, the ambient temperature, the wind, the runway slope, and surface conditions of the runway i.e., environmental conditions, snow, slush, water, ice, for landplanes, water surface condition for seaplanes, and the operation of any system or systems that may have an adverse effect on performance. (c) The factors described in subpart (b) of the aircraft performance calculations shall be taken into account directly as operations parameters or indirectly by means of allowances or margins, which may be provided in the design performance limits or in the terms of the AOC in accordance with which the aeroplane is being operated. ICAO Annex 6, Part I, 5.2.5, 5.2.6 ICAO Annex 6, Part II: 5.1 ICAO Annex 6, Part III, Section II:3.2.5; 3.2.6; Annex 6, Part III, Section III: 3.1; 3.3; 3.4R JAR-OPS: 1.485 8.7.1.4 GENERAL MASS AND OBSTRUCTION CLEARANCE LIMITATIONS (a) No person may takeoff an aircraft without ensuring that the maximum allowable mass for a flight does not exceed the maximum allowable takeoff or landing mass, or any applicable en route performance or landing distance limitations considering the— (1) Condition of the takeoff and landing areas to be used; (2) Gradient of runway to be used (landplanes only); (3) Pressure altitude; (4) Ambient temperature; (5) Current and forecast winds; and (6) Any known conditions (e.g., atmospheric and aircraft configuration) which may adversely affect aircraft performance, or compliance with noise certification standards if required. (b) No person may takeoff an aircraft at a mass that, assuming normal engine operation, cannot safely clear all obstacles during all phases of flight, including all points along the intended en route path or any planned diversions. ICAO Annex 6, Part I: 4.3.1(d)(e)(f); 5.2.7 ICAO Annex 6, Part II: 4.4.1(d)(e)(f); 4.4.2R ICAO Annex 6, Part III, Section II: 2.3.1(f); 2.7; Annex 6, Part III, Section III: 2.4(d)(e)(f) 14 CFR: 121.693(b)(1-4)) JAR-OPS: 1.475 (b), 1.480. 8.7.2 AIRCRAFT USED IN COMMERCIAL AIR TRANSPORT 8.7.2.1 APPLICABILITY (a) This Section prescribes aircraft performance and operating limitations for aircraft used in commercial air transport operations, except for those used by air transport operators holding a special authorization or waiver granted by the Authority, that exempts the aircraft from specific operating and performance limitations. ICAO Annex 6: Part I: 5.1.1 ICAO Annex 6, Part III, Section II: 3.1.1 8.7.2.2 GENERAL (a) Each person operating an aircraft engaged in commercial air transport shall comply with the provisions of Section 8.7.2. (b) Each person operating a rotorcraft identified as Class 1, 2, or 3 in international commercial air transport shall comply with the code of performance in IS: 8.7.2.2(b). (c) The Authority may grant exemptions in accordance with Part 1 of these regulations, from the requirements of Section 8.7.2 if special circumstances make a literal observance of a requirement unnecessary for safety. (d) Where full compliance with the requirements of Section 8.7.2 cannot be shown due to specific design characteristics (e.g., seaplanes, airships, or supersonic aircraft), the operator shall apply approved performance standards that ensure a level of safety not less restrictive than those of relevant requirements of this Section. (e) No person may operate a single-engine aircraft or an aircraft type certificated for operation by a single-pilot used for revenue passenger carrying operations unless that aircraft is continually operated in daylight, VFR, excluding over the top, and over routes and diversions there that do not permit a safe forced landing to be executed in the event of an engine failure. (1) Notwithstanding Subsection 8.7.2.2(e), the Authority may approve single-pilot operations in propeller driven, turbine powered aircraft under IFR, at night, or under IMC for aircraft certificated for a maximum take-off weight of 5,700 kg (12566 lb) or less and a maximum approved passenger seating configuration of 9 or less, provided it meets the equipment requirements of Part 7. (2) Notwithstanding Subsection 8.7.2.2(e)(1), the Authority may approve single-pilot operations in propeller driven, turbine powered aircraft under IFR at night, or under IMC for aircraft certificated maximum take-off weight of 5,700 kg (12566 lb) or less with a passenger seating configuration of more than 9 passengers if the aircraft is type certificated for operations by a single pilot, provided it meets the equipment requirements of Part 7 and the Authority has authorised an exemption from Subsection 8.7.2.2(e)(1) in the operators operations specifications. If such operations are to be conducted outside [STATE], the [STATE] shall have an arrangement with the States where operations will be conducted. Note: Subsection 8.7.2.2(e)(2) is not currently in compliance with ICAO Annex 6, Part I, 4.9.1 but is included here at the request of States that operate aircraft with a passenger seating configuration of 14. ICAO is giving consideration to change the passenger seating configuration requirements of 9 or less in propeller-driven aircraft. (f) No person may operate a multiengine aircraft used for revenue passengers carrying operations that is unable to comply with any of the performance limitations of Subsections 8.7.2.5 through 8.7.2.9 unless that aircraft is continually operated— (1) In daylight; (2) In VFR, excluding over the top operations; and (3) At a mass that will allow it to climb, with the critical engine inoperative, at least 15 m (50 ft) a minute when operating at the MEAs of the intended route or any planned diversion, or at 1500 m (5,000 ft) MSL, whichever is higher. (g) Multiengine aircraft that are unable to comply with paragraph (e)(3) are, for the purpose of this Section, considered to be a single engine aircraft and shall comply with the requirements of paragraph (d). Note: ICAO Doc 9388, Manual of Model Regulation for National Control of Flight Operations and Continuing Airworthiness of Aircraft Ed 2, para. 3.2.1.1, 3.2.2.1, provides additional guidance. ICAO Annex 6: Part I: 4.9.1; 4.9.2; 5.1.1; 5.1.2; 5.4.1 ICAO Annex 6, Part III, Section II: 3.1.1; 3.1.2; 3.1.3, and Attachment A 14 CFR: 135.181 JAR-OPS: 1.470, 1.490, 1.495, 1.565, 1.570, 1.575 8.7.2.3 SINGLE AND MULTI-ENGINE AEROPLANE OPERATIONS (a) No person may operate a single-engine aircraft in revenue passenger carrying operations unless that aircraft is continually operated in daylight, VFR over such routes and diversions there from that permit a safe forced landing to be executed in the event of an engine failure. (1) Notwithstanding Subsection 8.7.2.3 (a), the Authority may approve single-engine operations in propeller driven, turbine powered aircraft under IFR, at night, or under IMC for aircraft certificated for a maximum take-off weight of 5,700 kg (12566 lb) or less and a maximum approved passenger seating configuration of 9 or less, provided it meets the equipment requirements of Part 7. (2) Notwithstanding Subsection 8.7.2.3 (a)(1), the Authority may approve single-engine operations in propeller driven, turbine powered aircraft under IFR at night, or under IMC for aircraft certificated maximum take-off weight of 5,700 kg (12566 lb) or less with a passenger seating configuration of more than 9 passengers if the aircraft is type certificated for operations by a single pilot, provided it meets the equipment requirements of Part 7 and the Authority has authorised an exemption from Subsection 8.7.2.3 (a)(1), in the operators operations specifications. If such operations are to be conducted outside [STATE], the [STATE] shall have an arrangement with the States where operations will be conducted |
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