CHAPTER 5 AEROPLANE PERFORMANCE OPERATING LIMITATIONS

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1 CHAP 5-1 CHAPTER 5 PERFORMANCE OPERATING LIMITATIONS 5.1 GENERAL Aeroplanes shall be operated in accordance with a comprehensive and detailed code of performance established by the Civil Aviation Authority of Nepal in compliance with the applicable requirements of this chapter Single-engine aeroplanes shall only be operated in conditions of weather and light, and over such routes and diversions therefrom, that permit a safe forced landing to be executed in the event of engine failure RESERVED 5.2 APPLICABLE TO S CERTIFICATED IN ACCORDANCE WITH PARTS IIIA AND IIIB OF ICAO ANNEX The requirements contained in to inclusive are applicable to the large aeroplanes to which Parts IIIA and IIIB of ICAO Annex 8 are applicable The level of performance defined by the appropriate parts of the comprehensive and detailed national code referred to in for the aeroplanes designated in shall be at least substantially equivalent to the overall level embodied in the requirements of this chapter. Note. APPENDIX 13 contains guidance material which indicates the level of performance intended by the requirements of this chapter An aeroplane shall be operated in compliance with the terms of its Certificate of Airworthiness and within the approved operating limitations contained in its flight manual.

2 CHAP The State of Registry shall take such precautions as are reasonably possible to ensure that the general level of safety contemplated by these provisions is maintained under all expected operating conditions, including those not covered specifically by the provisions of this chapter A flight shall not be commenced unless the performance information provided in the flight manual indicates that the requirements of to can be complied with for the flight to be undertaken When applying the requirements of this chapter, account shall be taken of all factors that significantly affect the performance of the aeroplane, including but not limited to: the 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 conditions of the runway, i.e. presence of slush, water and/or ice, for landplanes, water surface condition for seaplanes. Such factors shall be taken into account directly as operational parameters or indirectly by means of allowances or margins, which may be provided in the scheduling of performance data or in the comprehensive and detailed code of performance in accordance with which the aeroplane is being operated Mass limitations a) The mass of the aeroplane at the start of take-off shall not exceed the mass at which is complied with, nor the mass at which 5.2.9, and are complied with, allowing for expected reductions in mass as the flight proceeds, and for such fuel jettisoning as is envisaged in applying and and, in respect of alternate aerodromes, c) and b) In no case shall the mass at the start of take-off exceed the maximum take-off mass specified in the flight manual for the pressure-altitude appropriate to the elevation of the aerodrome, and, if used as a parameter to determine the maximum take-off mass, any other local atmospheric condition. c) In no case shall the estimated mass for the expected time of landing at the aerodrome of intended landing and at any destination alternate aerodrome, exceed the maximum landing mass specified in the flight manual for the pressure-altitude appropriate to the elevation of those aerodromes, and if used as a parameter to determine the maximum landing mass, any other local atmospheric condition. d) In no case shall the mass at the start of take-off, or at the expected time of landing at the aerodrome of intended landing and at any destination alternate aerodrome, exceed the relevant maximum masses at which compliance has been demonstrated with the applicable noise certification mentioned in Annex-16, Vol-1 Aircraft Noise, Part II Aircraft Noise Certification unless otherwise authorized in

3 CHAP 5-3 exceptional circumstances for a certain aerodrome or a runway where there is no noise disturbance problem, in which the aerodrome is situated. e) Before the commencement of a public transport flight, the operator, or the person in charge of the loading of the aircraft or the pilot-in-command, shall prepare load and trim sheets that shall contain: i) the registration mark of the aircraft to which the load and trim sheets relate; ii) particulars of the intended flight; iii) the total mass of the aircraft as loaded for that flight; iv) the mass of several items from which the total mass of the aircraft has been calculated including, in particular, the mass of the aircraft prepared for service and the respective total mass of the crew (unless included in the mass of the aircraft prepared for service), passengers, baggage, and cargo intended to be carried on the flight; v) the manner in which the load is distributed and the resulting position of the centre of gravity of the aircraft; f) Load and trim sheets shall be signed by the Operator, or the person(s) identified by the Operator as responsible for despatching the aircraft who is duly trained and certified, as certifying that it has been loaded in accordance with the instructions issued by the operator and approved by the Director General. g) For the purpose of calculating the total mass of the aircraft, the respective total mass of the passengers and crew entered in the load and trim sheets shall be computed from the actual mass of each person, and for that purpose, each person shall be separately weighed except that in cases of an aircraft which has a seating capacity of 19 or more passengers, the total mass of the passengers and the crew shall be calculated by using the values in the following tabulation; Nepalese and Asian passengers All other foreign passengers Males over 12 years of age 75 kgs. 90 kgs. Females over 12 years of age 65kgs. 75 kgs. Children over 2 years, but not over 12 years of age. 35 kgs. 40 kgs. Infants 2 years old or less.. 10 kgs. 10 kgs. Note: An average of 5 kgs hand baggage per person shall be added to the adult passenger weights.

4 CHAP Take-off. The aeroplane shall be able, in the event of a critical engine failing, or for other reasons, at any point in the take-off, either to discontinue the take-off and stop within the accelerate-stop distance available, or to continue the take-off and clear all obstacles along the flight path by an adequate margin until the aeroplane is in a position to comply with When determining the resulting take-off obstacle accountability area, the operating conditions, such as the crosswind component and navigation accuracy, must be taken into account In determining the length of the runway available, account shall be taken of the loss, if any, of runway length due to alignment of the aeroplane prior to take-off En route one power-unit inoperative. The aeroplane shall be able, in the event of the critical power-unit becoming inoperative at any point along the route or planned diversions therefrom, to continue the flight to an aerodrome at which the requirement of can be met, without flying below the minimum flight altitude at any point En route two power-units inoperative. In the case of aeroplanes having three or more power-units, on any part of a route where the location of en-route alternate aerodromes and the total duration of the flight are such that the probability of a second power-unit becoming inoperative must be allowed for if the general level of safety implied by the requirements of this chapter is to be maintained, the aeroplane shall be able, in the event of any two power-units becoming inoperative, to continue the flight to an en-route alternate aerodrome and land Landing. The aeroplane shall, at the aerodrome of intended landing and at any alternate aerodrome, after clearing all obstacles in the approach path by a safe margin, be able to land, with assurance that it can come to a stop or, for a seaplane, to a satisfactorily low speed, within the landing distance available. Allowance shall be made for expected variations in the approach and landing techniques, if such allowance has not been made in the scheduling of performance data. 5.3 OBSTACLE DATA Obstacle data from the AIP-Nepal shall be used by the operator when developing procedures to comply with when taking off from aerodromes located within Nepal. When using aerodromes located abroad, the operator shall use the obstacle data provided by the local civil aviation authority of the States in which the aerodromes are located The operator shall take account of charting accuracy when assessing compliance with

5 CHAP ADDITIONAL REQUIREMENTS FOR OPERATIONS OF SINGLE- ENGINE TURBINE-POWERED S AT NIGHT AND/OR IN INSTRUMENT METEOROLOGICAL CONDITIONS (IMC) (i) A single-engine aeroplane is not permitted to be operated at night within the territory of Nepal for commercial purposes. (ii) When approving operations by single-engine turbine-powered aeroplanes in day IMC, CAAN shall ensure that the airworthiness certification of the aeroplane is appropriate; that the manufacturer and the State of manufacture have certified the aeroplane for IFR operations and that the overall level of safety intended by the DG, CAAN is provided by: a) the reliability of the turbine engine b) the operator s maintenance procedures, operating practices, flight dispatch procedures and crew training programmes; c) equipment and other requirements provided in accordance with Chapter 6.9. d) the utilization of at least two pilots for the conduction of such operations All single-engine turbine-powered aeroplanes engaged in commercial operations shall have an engine trend monitoring system, and those aeroplanes for which the individual Certificate of Airworthiness is first issued on or after 01 January 2005 shall have an automatic trend monitoring system.

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