Second Segment Climb Sample Clauses

The Second Segment Climb clause defines the required aircraft performance during the second segment of a takeoff, which is the phase immediately after liftoff when the aircraft must clear obstacles with one engine inoperative. This clause typically specifies the minimum climb gradient or rate that must be achieved, often in compliance with regulatory standards, and may detail the conditions under which these requirements apply, such as aircraft weight, configuration, and environmental factors. Its core practical function is to ensure the safety of flight operations by mandating that the aircraft can safely continue takeoff and clear obstacles even in the event of an engine failure.
Second Segment Climb. 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.
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Second Segment Climb. The Aircraft will meet FAR 25 regulations for one engine inoperative climb after take-off, undercarriage retracted, at a weight corresponding to the stated weight at the start of ground run, 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 and 2.
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Second Segment Climb. The Aircraft shall meet FAR regulations for one engine inoperative climb after take-off, undercarriage retracted, at a weight corresponding to the stated weight at the start of ground run, at the altitude and temperature and in the configuration of flap angle and take-off safety speed required to comply with the performance guaranteed in paragraph 2.1 above. INTREPID – A330-200F – Letter Agreement No. 8B-EV LA8B-2/7 CONFIDENTIAL AND PROPRIETARY INFORMATION ***** Confidential portions of the material have been omitted and filed separately with the Securities and Exchange Commission.
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Second Segment Climb. The A318 Aircraft will **.
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Second Segment Climb. The A320 Aircraft shall meet the FAR requirements for one engine inoperative climb after take-off, undercarriage retracted, at a weight corresponding to the stated weight at the start of ground run 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.
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Second Segment Climb. The Aircraft shall meet **
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Second Segment Climb. The A330-300 Aircraft will meet FAR regulations for one engine inoperative climb after take-off, undercarriage retracted, at a weight corresponding to the stated weight at the start of ground run at the altitude and temperature and in the configuration of flap angle and safety speed required to comply with the performance guaranteed in Subparagraph 2.1. 2.3 En-route One Engine Inoperative The A330-300 Aircraft will meet FAR regulations minimum en-route climb gradient one engine inoperative and the other operating at the maximum continuous thrust with air conditioning on and anti-icing off at an A330-300 Aircraft gross weight of 450,000 lb in the cruise configuration in ISA+10(degree)C conditions at a pressure altitude of not less than the guarantee value.
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Second Segment Climb. The Aircraft shall meet FAR 25 regulations for one engine inoperative climb after take-off, undercarriage retracted, at a weight corresponding to the stated weight at the start of ground run, at the altitude and temperature, and in the configuration of flap angle and safety speed required to comply with the performance guaranteed in Paragraphs 2.1 and 2.3. ***** CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT. USA – Amended and Restated Letter Agreement No. 8-2 to Amended and Restated Airbus A350 XWB Purchase Agreement EXECUTION PRIVILEGED AND CONFIDENTIAL
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Second Segment Climb. The Original A320 Aircraft will **
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