時(shí)間：2015-01-22 15:21來源：藍(lán)天飛行翻譯公司 作者：民航翻譯 點(diǎn)擊：次
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To view this page ensure that Adobe Flash Player version 9.0.124 or greater is installed. (e) Systems and Equipment. Single-engine turbine-powered aeroplanes approved to operate at night and/or in IMC shall be equipped with the following systems and equipment intended to ensure continued safe flight and to assist in achieving a safe forced landing after an engine failure, under all allowable operating conditions: (1) Two separate electrical generating systems, each one capable of supplying all probable combinations of continuous in-flight electrical loads for instruments, equipment and systems required at night and/or in IMC; (2) A radio altimeter; (3) An emergency electrical supply system of sufficient capacity and endurance, following loss of all generated power, to as a minimum: (i) Maintain the operation of all essential flight instruments, communication and (ii) Navigation systems during a descent from the maximum certificated altitude in a glide configuration to the completion of a landing; (iii) Lower the flaps and landing gear, if applicable; (iv) Provide power to one pitot heater, which must serve an air speed indicator clearly visible to the pilot; (v) Provide for operation of the landing light specified in (e)(10) below; (vi) Provide for one engine restart, if applicable; and (vii) Provide for the operation of the radio altimeter; (4) Two attitude indicators, powered from independent sources; (5) A means to provide for at least one attempt at engine re-start; (6) Airborne weather radar; (7) A certified area navigation system capable of being programmed with the positions of aerodromes and safe forced landing areas, and providing instantly available track and distance information to those locations; (8) For passenger operations, passenger seats and mounts which meet dynamically-tested performance standards and which are fitted with a shoulder harness or a safety belt with a diagonal shoulder strap for each passenger seat; (9) In pressurised aeroplanes, sufficient supplemental oxygen for all occupants for descent following engine failure at the maximum glide performance from the maximum certificated altitude to an altitude at which supplemental oxygen is no longer required; (10) A landing light that is independent of the landing gear and is capable of adequately illuminating the touchdown area in a night forced landing; and (11) An engine fire warning system. (f) Minimum Equipment List (MEL). An AOC holder shall develop an MEL approved by the Authority that is appropriate to the type of single-engine turbine-powered aeroplane operated specifying the operating equipment required for night and/or IMC operations, and for day/VMC operations. (g) Aeroplane Flight Manual (AFM) Information. The AFM shall include limitations, procedures, approval status and other information relevant to operations by single-engine turbine-powered aeroplanes at night and/or in IMC. (h) Event Reporting. An AOC holder operating turbine-powered aeroplanes at night and/or in IMC shall report all significant failures, malfunctions or defects to the Authority who in turn will notify the State of Design. (i) Operator Planning. Each AOC holder operating single-engine turbine-powered aeroplanes at night and/or in IMC shall take account of all relevant information in the assessment of intended routes or areas of operations, including the following: (1) The nature of the terrain to be overflown, including the potential for carrying out a safe forced landing in the event of an engine failure or major malfunction; (2) Weather information, including seasonal and other adverse meteorological influences that may affect the flight; and (3) Other criteria and limitations as specified by the Authority. (j) Each AOC holder shall identify aerodromes or safe forced landing areas available for use in the event of engine failure and the position of these shall be programmed into the area navigation system. Note 1: A ‘safe’ forced landing in this context means a landing in an area at which it can reasonably be expected that it will not lead to serious injury or loss of life, even though the aeroplane may incur extensive damage. Note 2: Operation over routes and in weather conditions that permit a safe forced landing in the event of an engine failure, as specified in Subsection 8.8.1.30 (a) is not required for aeroplanes approved in accordance with Subsection 8.8.1.30 (a)(1). The availability of forced landing areas at all points along a route is not specified for these aeroplanes because of the very high engine reliability, additional systems and operational equipment, procedures and training requirements specified in this implementing standard. (k) Flight Crew Experience, Training and Checking (1) No person may serve and no AOC holder shall use a flight crewmember in single-engine turbine-powered aeroplanes engaged in commercial air transport unless he or she has completed the appropriate flight crewmember training as specified in this Part and approved by the Authority. (2) The AOC holder’s approved flight crew training and checking shall be appropriate to night and/or IMC operations by single engine turbine-powered aeroplanes, covering normal, abnormal and emergency procedures and, in particular, engine failure, including descent to a forced landing in night and/or in IMC conditions. (l) Route Limitations Over Water (1) An AOC holder shall not conduct over water operations using single-engine turbine-powered aeroplanes operating at night and/or in IMC except in areas of operation or over specific routes identified in the AOC holder’s operation specifications. (2) No AOC holder may conduct over water operations using single-engine turbine-powered aeroplanes operating at night and/or in IMC except in accordance with procedures approved by the Authority in the AOC holder’s operations manual for over water operations covering flight beyond gliding distance from an area suitable for a safe forced landing/ditching having regard to the characteristics of the aeroplane, seasonal weather influences, including likely sea state and temperature, and the availability of search and rescue services. (m) Operator Certification or Validation. (1) An AOC holder applying for operations specifications granting authorisation to conduct single-engine turbine-powered aeroplane operations at night and/or in IMC shall demonstrate to the Authority consistent with Part 9 Air Operator Certification & Administration, the ability to conduct operations by single-engine turbine-powered aeroplanes at night and/or in IMC through a certification and approval process specified by the Authority. ICAO Annex 6: Part I: 5.1.1; 5.1.2; 5.2.2; 5.4.1; 5.4.2 & Appendix 3 ICAO Annex 6, Part III, Section II: 3.1.1; 3.1.2; 3.1.3 14 CFR: 135.181 IS: 8.8.1.7 INSTRUMENT APPROACH OPERATING MINIMA (a) Each operator establishing aerodrome-operating minima shall have its method for determining such minima approved by the Authority. (b) Each operator’s method for determining aerodrome-operating minima shall accurately account for— (1) The type, performance and handling characteristics of the aircraft; (2) The composition and experience of the flight crew; (3) The dimensions and characteristics of the runways selected for use; (4) Aircraft equipment used for navigation and aircraft control during the approach to landing and the missed approach; (5) Obstacles in the approach and missed approach areas and the obstacle clearance altitude/height for the intended instrument approach procedures; (6) The means used to determine and report meteorological conditions; and (7) The obstacles in the climb out areas and the necessary clearance margins. (8) The adequacy and performance of the available visual and non-visual ground aids. (9) The declared distances, for helicopters. ICAO Annex 6, Part 1: 4.2.8.1; 4.2.8.2; 4.2.8.3; 4.2.8.4R ICAO Annex 6, Part II: 4.2 ICAO Annex 6, Part III, Section II: 2.2.7.1; 2.2.7.2; 2.2.7.4R; Annex 6, Part III, Section III: 2.6.3 IS: 8.8.1.9 CATEGORY II AND III MANUAL (a) Application for approval. An applicant for approval of a Category II or III manual or an amendment to an approved Category II or III manual shall submit the proposed manual or amendment to the Authority. If the application requests an evaluation programme, it shall include the following: (1) The location of the aircraft and the place where the demonstrations are to be conducted. (2) The date the demonstrations are to commence (at least 10 days after filing the application). (b) Contents. Each Category II or III manual must contain: (1) The registration mark, make, and model of the aircraft to which it applies. (2) A maintenance programme. (3) The procedures and instructions related to recognition of DH, use of runway visual range (RVR) information, approach monitoring, the decision region (the region between the middle marker and the decision height), the maximum permissible deviations of the basic ILS indicator within the decision region, a missed approach, use of airborne low approach equipment, minimum altitude for the use of the autopilot, instrument and equipment failure warning systems, instrument failure, and other procedures, instructions, and limitations that may be found necessary by the Authority. Note 1: Category II approval is required to prior to obtaining Category III approval. Note 2: ICAO Doc 9365, Manual on All Weather Operations, provides additional guidance. ICAO Annex 6, Part 1: 4.2.8.2; 4.2.8.3 ICAO Annex 6, Part III, Section II: 2.2.7.3 14 CFR: 91.191 IS: 8.8.1.28 INTERCEPTION OF CIVIL AIRCRAFT (a) [STATE] shall observe the following principles regarding the interception of civil aircraft. (1) Interception of civil aircraft will be undertaken only as a last resort. |
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