Common use of Second Segment Climb Clause in Contracts

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 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 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. 8B8C-EV LA8B-2/7 LA8C-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 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, run at the altitude and temperature and in the configuration of flap angle and take-off safety speed required to comply with the performance performances 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 Commission2.1.