Take-Off definition
Examples of Take-Off in a sentence
The maximum certificated take-off weight, i.e. the maximum permissible total weight with which the aircraft, in accordance with the certificate of air worthiness, may take off under the most favourable circumstances (Maximum Take-Off Weight – MTOW).
The Aircraft shall meet JAR 25 regulations for one engine inoperative climb after take-off, undercarriage retracted, at a weight corresponding to the stated weight at the start of Take-Off Distance Available (TODA), at the altitude and temperature, and in the configuration of flap angle and safety speed required to comply with the performance guaranteed in paragraph 2.1 above.
Off Charges Charges applicable during the WINTER season (January–May / October–December) Charges applicable during the SUMMER season (June–September) General Aviation flights will be charged double the standard Landing and Take-Off Charges.
The Aircraft shall meet JAR 25 regulations for one engine inoperative climb after take- off, undercarriage retracted, at a weight corresponding to the stated weight at the start of Take-Off Distance Available (TODA), at the altitude and temperature, and in the configuration of flap angle and safety speed required to comply with the performance guaranteed in paragraph 2.1 above.
The Aircraft shall meet JAR 25 regulations for one engine inoperative climb after take-off, undercarriage retracted, at a weight corresponding to the stated weight at the start of Take-Off Distance Available (TODA), at the altitude and temperature, and in (the configuration of flap angle and safely speed required to comply with the performance guaranteed in paragraph 2.1 above.
The A319 Aircraft shall meet JAR 25 regulations for one engine inoperative climb after take-off, undercarriage retracted, at a weight corresponding to the stated weight at the start of Take-Off Distance Available (TODA), at the altitude and temperature, and in the configuration of flap angle and safety speed required to comply with the performance guaranteed in paragraph 2.1 above.
The guarantees defined below (the "Guarantees") are applicable to the A340-300 Aircraft as described in the Technical Specification F.000.03000 Issue 6 dated 15th January 1997 ("the Specification") as amended by a Specification Change Notice for the increase in the Design Maximum Take-Off Weight to 606,270 lb (275,000 kg) without taking into account any further changes thereto as provided in the Agreement.
The A321 Aircraft shall meet JAR 25 regulations for one engine inoperative climb after take-off, undercarriage retracted, at a weight corresponding to the stated weight at the start of Take-Off Distance Available (TODA), at the altitude and temperature, and in the configuration of flap angle and safety speed required to comply with the performance guaranteed in paragraph 2.1 above.
By this same deadline, the CONCESSIONAIRE shall also provide the OSINERGMIN and the Ministry of Energy and Mines with source electronic files containing the definitive engineering plans of the Project, which shall include the Work Specifications indicated in Annex 7, and the following sections: Supporting Calculations, Material Take-Off, Supply and Assembly Specifications, and Plans in AutoCAD.
The A320 Aircraft shall meet JAR 25 regulations for one engine inoperative climb after take-off, undercarriage retracted, at a weight corresponding to the stated weight at the start of Take-Off Distance Available (TODA), at the altitude and temperature, and in the configuration of flap angle and safety speed required to comply with the performance guaranteed in paragraph 2.1 above.