時(shí)間：2015-01-22 15:21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: 121.599; 121.601(b); 121.603(a) 8.13.1.9 FLIGHT RELEASE — IN ICING CONDITIONS (a) No person may release an aircraft, when in their opinion or that of the PIC, the icing conditions that may be expected or are met exceed that for which the aircraft is certified and has sufficient operational de-icing or anti-icing equipment. (b) No person may release an aircraft any time conditions are such that frost, ice or snow may reasonably be expected to adhere to the aircraft, unless there is available to the PIC at the aerodrome of departure adequate facilities and equipment to accomplish the procedures approved for the AOC holder by the Authority for ground de-icing and anti-icing. (c) No person may issue a flight release for a commercial air transport operation unless the requirements of Subsection 8.13.1.5 for operational flight planning have been complied met. (d) Completed flight preparation forms shall be kept by an operator for a period of 3 months. Note: ICAO Doc 9640, Manual of Aircraft Ground De-Icing/Anti-Icing, provides additional guidance. ICAO Annex 6, Part I: 4.3.2; 4.3.3.1; 4.3.5.5; 4.3.5.6 ICAO Annex 6, Part III, Section II: 2.3.5.3; 2.3.5.4 14 CFR: 121.629; 135.227 8.13.1.10 FLIGHT RELEASE — UNDER VFR OR IFR (a) No person may release a flight under VFR or IFR unless the weather reports and forecasts indicated that the flight can reasonably be expected to be completed as specified in the release. ICAO Annex 6, Part I: 4.3.5.1; 4.3.5.2 ICAO Annex 6, Part III, Section II: 2.3.5.1; 2.3.5.2 14 CFR: 121.611, 121.613 8.13.1.11 FLIGHT RELEASE—MINIMUM FUEL SUPPLY (a) No person may issue a flight release for a commercial air transport operation unless the fuel supply specified in the release is equivalent to or greater than the minimum flight planning requirements of this Part, including anticipated contingencies. (b) No person may issue a flight release for a commercial air transport operation unless the requirements of 8.13.1.5 for operational flight planning have been met. (c) Completed flight preparation forms shall be kept by an operator for a period of 3 months. ICAO Annex 6, Part I: 4.3.2; 4.3.3.1; 4.3.6.1; 4.3.6.2; 4.3.6.3; 4.3.6.4R ICAO Annex 6, Part III, Section II: 2.3.6.1; 2.3.6.2; 2.3.6.3; 2.3.6.3.1; 2.3.6.3.2; 2.3.6.4 14 CFR: 121.639, 121.641; 121.643; 121.654 8.13.1.12 FLIGHT RELEASE—AIRCRAFT LOADING AND PERFORMANCE (a) No person may issue a flight release unless he or she is familiar with the anticipated loading of the aircraft and is reasonably certain that the proposed operation will not exceed the— (1) Centre of gravity limits; (2) Aircraft operating limitations; and (3) Minimum performance requirements. (b) No person may issue a flight release for a commercial air transport operation unless any load carried is properly distributed and safely secured. (c) No person may issue a flight release for a commercial air transport operation unless the requirements of § 8.13.1.5 for operational flight planning have been met. (d) Completed flight preparation forms shall be kept by an operator for a period of 3 months. ICAO Annex 6, Part I: 4.3.1(d)(e)(f); 4.3.2; 4.3.3.1; 5.1.1; 5.2.3 ICAO Annex 6, Part III, Section II: 2.3.1(d)(e); 3.1.1; 3.2.3 14 CFR: 121.663; 121.665; 121.693 FAA AC 120-27E (as amended), Aircraft Weight and Balance Control 8.13.1.13 FLIGHT RELEASE—AMENDMENT OR RE-RELEASE EN ROUTE (a) Each person who amends a flight release while the flight is en route shall record that amendment. (b) No person may amend the original flight release to change the destination or alternate aerodrome while the aircraft is en route unless the flight preparation requirements for routing, aerodrome selection and minimum fuel supply are met at the time of amendment or re-release. (c) No person may allow a flight to continue to an aerodrome to which it has been released if the weather reports and forecasts indicate changes that would render that aerodrome unsuitable for the original flight release. (d) No person may issue a flight release for a commercial air transport operation unless the requirements of Subsection 8.13.1.5 for operational flight planning have been met. (e) Completed flight preparation forms shall be kept by an operator for a period of 3 months. ICAO Annex 6, Part I: 4.3.2; 4.3.3.1; 4.3.6.5, 4.4.1.1 ICAO Annex 6, Part III, Section II: 2.3.6.4 (Note); 2.4.1.1 14 CFR: 121.631 8.13.1.14 FLIGHT RELEASE—WITH AIRBORNE WEATHER RADAR EQUIPMENT (a) No person may release a large aircraft carrying passengers under IFR or night VFR conditions when current weather reports indicate that thunderstorms, or other potentially hazardous weather conditions that can be detected with airborne weather radar, may reasonably be expected along the route to be flown, unless the airborne weather radar equipment is in satisfactory operating condition. (b) No person may issue a flight release for a commercial air transport operation unless the requirements of § 8.13.1.5 for operational flight planning have been met. (c) Completed flight preparation forms shall be kept by an operator for a period of 3 months. ICAO Annex 6, Part I: 4.3.2; 4.3.3.1; 6.11R ICAO Annex 6, Part III, Section II: 4.12 R 14 CFR: 121.357(c)(1) MODEL CIVIL AVIATION REGULATIONS PART 8—IMPLEMENTING STANDARDS [STATE] VERSIONS 2.8 NOVEMBER 2014 For ease of reference, the number assigned to each implementing standard corresponds to its associated regulation. For example, IS: 8.2.1.5 would reflect a standard required in Subsection 8.2.1.5. PART 8—IMPLEMENTING STANDARDS IS: 8.7.2.2(B) GENERAL – ROTORCRAFT CLASS 1, 2, AND 3 CODE OF PERFORMANCE (a) The following guidance material is the basis of the code of helicopter performance referenced in Part 8, Subpart: 8.7.2 - Aircraft Used In Commercial Air Transport. (b) Definitions: (1) Category A. With respect to helicopters, means a multi-engined helicopter designed with engine and system isolation features and capable of operations using take-off and landing data scheduled under a critical engine failure concept which assures adequate designated surface area and adequate performance capability for continued safe flight or safe rejected take-off. (2) Category B. With respect to helicopters, means a single engine or multi-engined helicopter which does not meet Category A standards. Category B helicopters have no guaranteed capability to continue safe flight in the event of an engine failure, and a forced landing is assumed (c) General guidance: (1) Helicopters operating in performance Classes 1 and 2 should be certificated in Category A (2) Helicopters operating in performance Class 3 should be certificated in either Category A or Category B (or equivalent) (3) Except as permitted by the appropriate Authority: (i) Take-off or landing from/to heliports in a congested hostile environment should only be conducted in performance Class 1 (ii) Operations in performance Class 2 should only be conducted with a safe forced landing capability during take-off and landing. (iii) Operations in performance Class 3 should only be conducted in a non-hostile environment (4) The Authority may grant a waiver from the provisions of (3) (i) (ii) & (iii) upon receiving a commercial air transport operator’s application for waiver and undertaking a risk assessment of the operational conditions proposed, including: (i) The type of operation and the circumstances of the flight; (ii) The area/terrain over which the flight is being conducted; (iii) The probability of a critical power-unit failure and the consequence of such an event; (iv) The procedures to maintain the reliability of the power-unit(s); (v) The training and operational procedures to mitigate the consequences of the critical power-unit failure; and (vi) Installation and utilisation of a usage monitoring system. ICAO Annex 6, Part III, Section II: 3.1.1; 3.1.2; 3.1.3, and Attachment A 14 CFR: 135.181 IS: 8.7.2.3 SINGLE AND MULTI-ENGINE AEROPLANE OPERATIONS (a) In addition to the requirements in outlined under Subsection 8.7.2.3, an AOC holder seeking approval from the Authority to operate single-engine turbine-powered aeroplanes at night and/or in IMC shall comply with the additional requirements of this implementing standard. (b) An AOC holder shall not operate single-engine, turbine-powered aeroplanes at night and/or in IMC unless the following airworthiness and operational requirements have been satisfied by the operator and approved by the Authority. (1) Turbine Engine Reliability (2) Turbine engine reliability shall be shown to have a power loss rate of less than 1 per 100000 engine hours Note: Power loss in this context is defined as any loss of power, the cause of which may be traced to faulty engine or engine component design or installation, including design or installation of the fuel ancillary or engine control systems. (c) The operator shall be responsible for engine trend monitoring. (d) To minimize the probability of in-flight engine failure, the engine shall be equipped with: (1) An ignition system that activates automatically, or is capable of being operated manually for take-off and landing, and during flight, in visible moisture (2) A magnetic particle detection or equivalent system that monitors the engine, accessories gearbox, and reduction gearbox, and which includes a flight deck caution indication; and (3) An emergency engine power control device that permits continuing operation of the engine through a sufficient power range to safely complete the flight in the event of any reasonably probable failure of the fuel control unit. |
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