Second Segment Climb Sample Clauses

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 shall meet JAR 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 2.3.
Second Segment Climb. The A319 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.
Second Segment Climb. The A318 Aircraft will **.
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.
Second Segment Climb. The Aircraft shall **.
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. LA 8-2 - 2 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 A350XWB-800 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 safety speed required to comply with the performances guaranteed in paragraph 2.1. *** Confidential Treatment Requested Hawaiian Airlines, Inc. [...***...] Letter Agreement

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