Publication: Magyar Közlöny
Issue: MK-2007-70 (Year: 2007, Number: 70)
Era: 2004-2010
Section: Melléklet a 2007. évi XLVI. törvényhez
Paragraph Index: 2034

g) wheel brakes are not used in a manner such as to produce excessive wear of brakes or tires, and the operating pressures on the braking system are not in excess of those approved. 3.3.2 The gradient of the steady approach and the details of the technique used in determining the landing distance, together with such variations in the technique as are recommended for landing with the critical engine inoperative, and any appreciable variation in landing distance resulting therefrom, are entered in the flight manual. Example 3 Purpose and scope The purpose of the following example is to illustrate the level of performance intended by the provisions of Chapter 5 as applicable to turbine-powered subsonic transport type aeroplanes over 5 700 kg maximum certificated take-off mass having two or more engines. However, where relevant, it can be applied to all turbine-powered or piston-engined subsonic aeroplanes having two, three or four engines. This example is shown to be compatible with principal national airworthiness codes in effect in 1969. No study has been made of the applicability of this material to turbine-powered subsonic aeroplanes having characteristics other than those of the transport aeroplanes introduced into service up to 1969. This example is not intended for application to aeroplanes having short take-off and landing (STOL) or vertical take-off and landing (VTOL) capabilities. No detailed study has been made of the applicability of this example to operations in all-weather conditions. The validity of this example has not therefore been established for operations which may involve low decision heights and be associated with low minima operating techniques and procedures. 1. General 1.1 The provisions of 1 to 5 are to be complied with, unless deviations therefrom are specifically authorized by the State of Registry on the ground that the special circumstances of a particular case make a literal observance of these provisions unnecessary for safety. 1.2 Compliance with 1 to 5 is to be established using performance data in the flight manual and in accordance with other applicable operating requirements. In no case may the limitations in the flight manual be exceeded. However, 2007/70/II. szám Annex 6 — Operation of Aircraft Part I 1/11/01 ATT C-18 additional limitations may be applied when operational conditions not included in the flight manual are encountered. 1.3 The procedures scheduled in the flight manual are to be followed except where operational circumstances require the use of modified procedures in order to maintain the intended level of safety. Note.— See the Airworthiness Manual (Doc 9760) for the related airworthiness performance guidance material. 2. Aeroplane take-off performance limitations 2.1 No aeroplane is taken off at a mass which exceeds the take-off mass specified in the flight manual for the altitude of the aerodrome and for the ambient temperature existing at the time of the take-off. 2.2 No aeroplane is taken off at a mass such that, allowing for normal consumption of fuel and oil in flight to the aerodrome of destination and to the destination alternate aerodromes, the mass on arrival will exceed the landing mass specified in the flight manual for the altitude of each of the aerodromes involved and for the ambient temperatures anticipated at the time of landing. 2.3 No aeroplane is taken off at a mass which exceeds the mass at which, in accordance with the minimum distances for take-off scheduled in the flight manual, compliance with 2.3.1 to 2.3.3 inclusive is shown. These distances correspond with the altitude of the aerodrome, the runway, stopway and clearway to be used, the runway slope, the stopway slope, the clearway plane slope, and the ambient temperature and wind existing at the time of take-off. 2.3.1 The take-off run required does not exceed the length of the runway. 2.3.2 The accelerate-stop distance required does not exceed the length of the runway plus the length of the stopway, where present. 2.3.3 The take-off distance required does not exceed the length of the runway, plus the length of the clearway, where present, except that the sum of the lengths of the runway and the clearway is in no case considered as being greater than 1.5 times the length of the runway. 2.4 Credit is not taken for the length of the stopway or the length of the clearway unless they comply with the relevant specifications in Annex 14, Volume I. Note.— In determining the length of the runway available, account is taken of the loss, if any, of runway length due to alignment of the aeroplane prior to take-off. 3. Take-off obstacle clearance limitations 3.1 No aeroplane is taken off at a mass in excess of that shown in the flight manual to correspond with a net take-off flight path which clears all obstacles either by at least a height of 10.7 m (35 ft) vertically or at least 90 m plus 0.125D laterally, where D is the horizontal distance the aeroplane has travelled from the end of take-off distance available, except as provided in 3.1.1 to 3.1.3 inclusive. In determining the allowable deviation of the net take-off flight path in order to avoid obstacles by at least the distances specified, it is assumed that the aeroplane is not banked before the clearance of the net take-off flight path above obstacles is at least 15.2 m (50 ft) and that the bank thereafter does not exceed 15 degrees. The net take-off flight path considered is for the altitude of the aerodrome and for the ambient temperature and wind component existing at the time of take-off. 3.1.1 Where the intended track does not include any change of heading greater than 15 degrees,

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