Common use of Second Segment Climb Clause in Contracts

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.

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 2.2.3. LA 8A-2 ***Confidential Treatment Requested AWE/USA - A350 PRIVILEGED AND CONFIDENTIAL

Second Segment Climb. The Aircraft will 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 paragraph 2.1 and 22.3.

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 2Subparagraph 1.3 above.

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 22.3.

Second Segment Climb. The Aircraft will shall meet FAR 25 regulations for one engine inoperative climb after take-offtakeoff, undercarriage retracted, at a weight corresponding to the stated weight at the start of ground run, at the altitude and temperature, temperature and in the configuration of flap angle and take-off safety speed required to comply with the performance guaranteed in paragraph 2.1 and 2above.