Common use of Basic Mode Clause in Contracts

Basic Mode. 4.1.1 The Aircraft shall be capable of carrying a guaranteed payload of ***** over a still air stage distance of ***** nautical miles when operated under the conditions defined below. 4.1.2 The departure and the destination airport conditions are such as to allow the required take-of weight and landing weight to be used without restriction. Pressure altitude at departure and destination is sea level. 4.1.3 An allowance of 1,600 lb of fuel is included for take-off and initial climb to 1,500 ft above the departure airport. 4.1.4 Climb from 1,500 ft above the departure airport up to cruise altitude using maximum climb thrust and cruise at Long Range Cruise Mach number at pressure altitudes between 33,000 ft and 37,000 ft with steps of 4,000 ft and descent to 1,500 ft above the destination airport is conducted in ISA conditions. Climb and descent speeds below 10,000 ft shall be 250 knots CAS. 4.1.5 An allowance of 400 lb of fuel is included for approach and landing at the destination airport. 4.1.6 Still air stage distance is defined as the distance covered during climb, cruise and descent as defined in Paragraph 4.1.4 above. INTREPID – A330-200F – Letter Agreement No. 8A LA8B - 3/13 CONFIDENTIAL AND PROPRIETARY INFORMATION ***** Confidential portions of the material have been omitted and filed separately with the Securities and Exchange Commission. Trip fuel is defined as the fuel burnt during take-off and initial climb, climb, cruise, descent, approach and landing as defined in Paragraphs 4.1.3, 4.1.4 and 4.1.5 above. 4.1.7 At the end of approach and landing 17,600 lb of usable fuel shall remain in the tanks. This represents the estimated fuel required for: 1) En-route contingency: 5% of trip fuel 2) Missed approach 3) Diversion in ISA conditions over a still air stage distance of 150 nautical miles starting and ending at 1,500 ft pressure altitude 4) Holding for 30 minutes at 1,500 ft pressure altitude in ISA conditions 5) Approach and landing at the alternate.

Basic Mode. 4.1.1 The Aircraft shall be capable of carrying a guaranteed payload of ***** over a still air stage distance of ***** nautical miles when operated under the conditions defined below. 4.1.2 The departure and the destination airport conditions are such as to allow the required take-of weight and landing weight to be used without restriction. Pressure altitude at departure and destination is sea level. 4.1.3 An allowance of 1,600 lb of fuel is included for take-off and initial climb to 1,500 ft above the departure airport. 4.1.4 Climb limb from 1,500 ft above the departure airport up to cruise altitude using maximum climb thrust and cruise at Long Range Cruise Mach number at pressure altitudes between 33,000 ft and 37,000 ft with steps of 4,000 ft and descent to 1,500 ft above the destination airport is conducted in ISA conditions. Climb and descent speeds below 10,000 ft shall be 250 knots CAS. 4.1.5 An allowance of 400 lb of fuel is included for approach and landing at the destination airport. 4.1.6 Still air stage distance is defined as the distance covered during climb, cruise and descent as defined in Paragraph 4.1.4 above. INTREPID – A330-200F – Letter Agreement No. 8A LA8B - 3/13 8-EV LA8-3/11 CONFIDENTIAL AND PROPRIETARY INFORMATION ***** Confidential portions of the material have been omitted and filed separately with the Securities and Exchange Commission. 4.1.6 Still air stage distance is defined as the distance covered during climb, cruise and descent as defined in Paragraph 4.1.4 above. Trip fuel is defined as the fuel burnt during take-off and initial climb, climb, cruise, descent, approach and landing as defined in Paragraphs 4.1.3, 4.1.4 and 4.1.5 above. 4.1.7 At the end of approach and landing 17,600 lb ***** of usable fuel shall remain in the tanks. This represents the estimated fuel required for: 1) En-route contingency: 5% of trip fuel 2) Missed approach 3) Diversion in ISA conditions over a still air stage distance of 150 nautical miles starting and ending at 1,500 ft pressure altitude 4) Holding for 30 minutes at 1,500 ft pressure altitude in ISA conditions 5) Approach and landing at the alternate.

Basic Mode. 4.1.1 4.2.1 The Aircraft shall be capable of carrying a guaranteed payload of ***** over a still air stage distance of ***** nautical miles when operated under the conditions defined below. 4.1.2 4.2.2 The departure and the destination airport conditions are such as to allow the required take-of weight and landing weight to be used without restriction. Pressure altitude at departure and destination is sea level. 4.1.3 4.2.3 An allowance of 1,600 lb of fuel is included for take-off and initial climb to 1,500 ft above the departure airport. 4.1.4 4.2.4 Climb from 1,500 ft above the departure airport up to cruise altitude using maximum climb thrust and cruise at Long Range Cruise Mach number at pressure altitudes between 33,000 ft and 37,000 41,000 ft with steps of 4,000 ft and descent to 1,500 ft above the destination airport is conducted in ISA conditions. Climb and descent speeds below 10,000 ft shall be 250 knots CAS. 4.1.5 4.2.5 An allowance of 400 lb of fuel is included for approach and landing at the destination airport. 4.1.6 4.2.6 Still air stage distance is defined as the distance covered during climb, cruise and descent as defined in Paragraph 4.1.4 4.2.4 above. INTREPID – A330-200F – Letter Agreement No. 8A LA8B - 3/13 CONFIDENTIAL AND PROPRIETARY INFORMATION ***** Confidential portions of the material have been omitted and filed separately with the Securities and Exchange Commission. Trip fuel is defined as the fuel burnt during take-off and initial climb, climb, cruise, descent, approach and landing as defined in Paragraphs 4.1.34.2.3, 4.1.4 4.2.4 and 4.1.5 4.2.5 above. 4.1.7 4.2.7 At the end of approach and landing 17,600 19,800 lb of usable fuel shall remain in the tanks. This represents the estimated fuel required for: 1) En-route contingency: 5% of trip fuel 2) Missed approach 3) Diversion in ISA conditions over a still air stage distance of 150 nautical miles starting and ending at 1,500 ft pressure altitude 4) Holding for 30 minutes at 1,500 ft pressure altitude in ISA conditions 5) Approach and landing at the alternate. INTREPID – A330-200F – Letter Agreement No. 8A LA8B - 4/13 CONFIDENTIAL AND PROPRIETARY INFORMATION ***** Confidential portions of the material have been omitted and filed separately with the Securities and Exchange Commission.