Publication: Magyar Közlöny
Issue: MK-2007-70 (Year: 2007, Number: 70)
Era: 2004-2010
Section: Melléklet a 2007. évi XLVI. törvényhez
Paragraph Index: 6254

2. Take-off thrust representative of the mean characteristics of the production engine. 2007/70/II. szám Part II — Chapter 2 Annex 16 — Environmental Protection II-2-3 24/11/05 2.6.2.3 The configuration of the aeroplane shall be with maximum allowable landing flap setting. Note.— Guidance material on the use of equivalent procedures is provided in the Environmental Technical Manual on the Use of Procedures in the Noise Certification of Aircraft (Doc 9501). 2007/70/II. szám ANNEX 16 — VOLUME I II-3-1 24/11/05 CHAPTER 3. 1.— SUBSONIC JET AEROPLANES — Application for Certificate of Airworthiness for the Prototype accepted on or after 6 October 1977 and before 1 January 2006 2.— PROPELLER-DRIVEN AEROPLANES OVER 5 700 kg — Application for Certificate of Airworthiness for the Prototype accepted on or after 1 January 1985 and before 17 November 1988 3.— PROPELLER-DRIVEN AEROPLANES OVER 8 618 kg — Application for Certificate of Airworthiness for the Prototype accepted on or after 17 November 1988 and before 1 January 2006 3.1 Applicability Note 1.— See also Chapter 1, 1.9. Note 2.— See Attachment E for guidance on interpretation of these applicability provisions. 3.1.1 The Standards of this chapter shall be applicable to:

Source: https://magyarkozlony.hu/hivatalos-lapok/7e70cec03f34e3c2efd8610b865b65591eafd701/dokumentumok/a55dc160549d57fa4db0035e37c6a6a98dd1a0b9/letoltes