時(shí)間：2015-01-22 15:18來(lái)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. 14 CFR: Part 91, Appendix A FAA AC 91-61 7.2.1.8 INSTRUMENTS AND EQUIPMENT FOR CATEGORY III OPERATIONS (a) The instruments and equipment listed in this subsection shall be installed, approved and maintained in accordance with international acceptable criteria and the AFM in each aircraft operated in a Category III operation: Note 1: This subsection does not require duplication of instruments and equipment required by § 7.2.1.2, and § 7. 2.1.7 or any other provisions of Part 7. Note 2: Acceptable international criteria may include: ICAO Doc 9365, Manual on All Weather Operations; the current edition of FAA AC 120-28 or JAR AWO. (b) Airborne systems for CAT IIIA minima not less than RVR 200 m (600 ft). The following equipment in addition to the instrument and navigation equipment required by this Part for IFR flight and CAT II operations is the minimum aircraft equipment required for CAT IIIA: (1) A redundant flight control or guidance system demonstrated in accordance with international acceptable criteria. Acceptable flight guidance or control systems include the following— (i) A Fail Operational or Fail Passive automatic landing system as least to touchdown; (ii) A Fail Operational or Fail Passive manual flight guidance system providing suitable head-up or head-down command guidance, and suitable monitoring capability at least to touchdown; (iii) A hybrid system, using automatic landing capability as the primary means of landing at least to touchdown; or (iv) Other system that can provide an equivalent level of performance and safety. (2) An automatic throttle or automatic thrust control system that meets approved criteria as specified in the AFM. However, for operations with a 15 m (50 ft) DH, or other operations that have been specifically evaluated such as for engine inoperative landing capability, automatic throttles may not be required if it has been demonstrated that operations can be safely conducted, with an acceptable work load, without their use. (3) At least two independent navigation receivers/sensors providing lateral and vertical position or displacement information, typically with the first pilot’s station receiving the information from one and the second pilot’s station receiving the information from the other. The navigation receivers/sensors shall meet the criteria specified for CAT IIIA operations. (4) At least two approved radio altimeter systems that meet the performance requirements criteria as specified in the AFM, typically with the first pilot’s station receiving information from one and the second pilot’s station receiving information from the other. (5) Failure detection, annunciation, and warning capability, as determined acceptable by criteria in the AFM. (6) Missed approach guidance provided by one or more of the following means: (i) Attitude displays that include suitable pitch attitude markings, or a pre-established computed pitch command display. (ii) An approved flight path angle display, or (iii) An automatic or flight guidance go-around capability. (7) Suitable forward and side flight deck visibility for each pilot as specified in the AFM. (8) Suitable windshield rain removal, ice protection, or defog capability as specified in the AFM. (c) Airborne systems for CAT IIIB minima less than RVR 200 m (600 ft) but not less than RVR 125 m (400 ft). The following equipment in addition to the instrument and navigation equipment required by this Part for IFR flight and CAT II and CAT IIIA operations is the minimum aircraft equipment required for CAT IIIB plus the following extra equipment requirements: (1) A redundant flight control or guidance system demonstrated in accordance with international acceptable criteria. Acceptable flight guidance or control systems include the following – (i) A Fail Operational landing system with a Fail Operational or Fail Passive automatic rollout system; or (ii) A Fail Passive landing system, limited to touchdown zone RVR not less than RVR 200 m (600 ft), with Fail Passive rollout provided automatically or by a flight guidance system providing suitable head-up or head-down guidance, and suitable monitoring capability, or (iii) A Fail Operational hybrid automatic landing and rollout system with comparable manual flight guidance system, using automatic landing capability as the primary means of landing; or (iv) Other system that can provide an equivalent level of performance and safety. (2) An automatic throttle or automatic thrust control that meets the appropriate criteria as specified in the AFM. However for operations with a 15 m (50 ft) DH, automatic throttles may not be required if it has been demonstrated that operations can safely be conducted, with an acceptable work load, without their use. (3) At least two independent navigation receivers/sensors providing lateral and vertical position or displacement information, typically with the first pilot’s station receiving information from one and the second pilot’s station receiving information from the other. The navigation receivers/sensors shall meet the criteria specified in the AFM. (4) At least two approved radio altimeter systems that need the performance criteria outlined in the AFM, typically with the first pilot’s station receiving information from one and the second pilot’s station receiving information from the other. (5) Failure detection, annunciation and warning capability as specified in the AFM. (6) Missed approach guidance provided by one or more of the following means: (i) Attitude displays that include calibrated pitch attitude markings, or a pre-established computed pitch command display; or (ii) An approved flight path angle display, or (iii) An automatic or flight guidance go-around capability. (7) Suitable forward and side flight deck visibility for each pilot, as specified in the AFM. (8) Suitable windshield rain removal, ice protection, or defog capability as specified in the AFM. (d) Airborne systems for CAT IIIC minima less than RVR 75 m (300 ft). The following equipment in addition to the instrument and navigation equipment required by this Part for IFR flight and CAT II, CAT IIIA and CAT IIIB operations is the minimum aircraft equipment required for CAT IIIC: (1) A Fail Operational Automatic Flight Control System, or manual flight guidance system designed to meet fail operational system criteria, or a hybrid system in which both the fail-passive automatic system and the monitored manual flight guidance components provide approach and flare guidance to touchdown, and in combination provide full fail operational capability, and (2) A fail operational automatic, manual, or hybrid rollout control system. Note: See also: ICAO PANS-OPS Doc. 8168-OPS/611, Vol. 11; ICAO Doc 9365; and JAR AWO. FAA AC 120-28D 7.2.1.9 AEROPLANES EQUIPPED WITH HEAD-UP DISPLAYS (HUD) AND/OR ENHANCED VISION SYSTEMS (EVS) (a) Where aircraft are equipped with HUD and/or EVS, the use of such systems to gain operational benefit shall be approved by the State of the Operator. Note - Guidance on HUD and EVS is contained in ICAO Annex 6, Part I, Attachment J. ICAO Annex 6, Part I: 6.2.3 ICAO Annex 6, Part II, Section II: 2.4.15 ICAO Annex 6, Part III, Section II: 4.16 ICAO Annex 6, Part III, Section III: 4.11 7.3 COMMUNICATIONS EQUIPMENT 7.3.1.1 RADIO EQUIPMENT (a) [AAC] No person may operate an aircraft unless it is equipped with radio communication equipment required for the kind of operation being conducted. (b) [AAC] All aircraft operated in VFR as a controlled flight, in IFR, at night, extended flight over water, or over land designated by the Authority as especially difficult for search and rescue, shall be equipped with radio communication equipment— (1) Capable of conducting two-way communication at any time with air traffic services or aeronautical stations; (2) Capable of conducting communications on those frequencies prescribed by the Authority, (3) Capable of receiving meteorological information at any time during the flight; (4) Capable of conducting communications on the aeronautical emergency frequency 121.5 MHz; (5) Approved and installed in accordance with the requirements applicable to them, including the minimum performance requirements; (6) Installed such that the failure of any single unit required for communication equipment, will not result in the failure of another unit required for communications purposes; and (7) Meeting any other requirements as prescribed by the Authority. Note: The requirements in (b)(1)-(3) are considered fulfilled if the ability to conduct the communications specified therein is established during radio propagation conditions which are normal for the route. (c) [AAC] For flights in defined portions of airspace or on routes where a Required Communications Performance (RCP) type has been prescribed, the aeroplane shall, in addition to the requirements in (a) and (b) above: (1) Be provided with communication equipment which will enable it to operate in accordance with the prescribe RCP type(s); and (2) Be authorised by [STATE] for operations in such airspace. Note: Information on RCP and associated procedures, and guidance concerning the approval process, are contained in ICAO Doc 9869, Manual on Required Communications Performance (RCP). This document also contains references to other documents produced by States and international bodies concerning communication systems and RCP. (d) [AOC] No person may operate an aircraft in commercial air transport operations, or as otherwise specified by the Authority, unless it is equipped with two independent radio communications systems, appropriate to the route and airspace used. |
