Common use of Cruise Specific Air Range Clause in Contracts

Cruise Specific Air Range. The average nautical miles per kilogram of fuel (average SAR) at a true Mach number of *** in ISA conditions under the Weight and Altitude conditions given below: shall be not less than a guaranteed value of: a) for CFM: ***

Cruise Specific Air Range. The average nautical miles per kilogram of fuel (average SAR) at a true Mach number of *** 0.78 in ISA ISA+15 conditions under the Weight and Altitude conditions given below: Gross Weight (kg) Pressure Altitude (ft) *** shall be not less than a guaranteed value of: a) for CFM: ***CT1002329 – Issue 2010-10-28 LA No4A Page 2/7

Cruise Specific Air Range. The average nautical miles per kilogram of fuel (average SAR) at a true Mach number of *** 0.78 in ISA ISA+15 conditions under the Weight and Altitude conditions given below: shall be not less than a guaranteed value of: : a) for CFMCFM *** b) for IAE: **** CES – A321 – 2010 Private & Confidential

Cruise Specific Air Range. The average nautical miles per kilogram of fuel (average SAR) at a true Mach number of *** in ISA conditions under the Weight and Altitude conditions given below: shall be not less than a guaranteed value of: : a) for CFM: *** b) for IAE: ***

Cruise Specific Air Range. The average nautical miles per kilogram of fuel (average SAR) at a true Mach number of *** 0.82 in ISA conditions under the Weight and Altitude conditions given below: shall be not less than a guaranteed value of: a) for CFM: ***0.0805 nm/kg

Cruise Specific Air Range. The average nautical miles per kilogram of fuel (average SAR) at a true Mach number of *** 0.78 in ISA ISA+15 conditions under the Weight and Altitude conditions given below: Gross Weight (kg) Pressure Altitude (ft) *** *** shall be not less than a guaranteed value of: : a) for CFM: *** b) for IAE: *** CES - A320 – AM2 to 2010 A320 PA CT10002329 August 2012 LA No.3-D A319 64t Sharklet perfo Private & Confidential Page 2/7

Cruise Specific Air Range. The average nautical miles per kilogram of fuel (average SAR) at a true Mach number of *** 0.78 in ISA ISA+15 conditions under the Weight and Altitude conditions given below: Gross Weight (kg) Pressure Altitude (ft) *** *** shall be not less than a guaranteed value of: : a) for CFM: *** b) for IAE: *** CES - A320 – AM2 to 2010 A320 PA LA No.3-C A321 perfo Private & Confidential

Cruise Specific Air Range. The average nautical miles per kilogram of fuel (average SAR) at a true Mach number of *** 0.78 in ISA ISA+15 conditions under the Weight and Altitude conditions given below: Gross Weight (kg) Pressure Altitude (ft) 60,000 37,000 55,000 39,000 shall be not less than a guaranteed value of: a) for CFM: ***:

Cruise Specific Air Range. The average nautical miles per kilogram of fuel (average SAR) at a true Mach number of *** in ISA conditions under the Weight and Altitude conditions given below: Gross Weight (kg) Pressure Altitude (ft) *** shall be not less than a guaranteed value of: : a) for CFMAircraft equipped with CFM Engines : *** b) for Aircraft equipped with IAE Engines : *** CT1001939 Private & Confidential

Cruise Specific Air Range. The average nautical miles per kilogram of fuel (average SAR) at a true Mach number of *** 0.78 in ISA ISA+15 conditions under the Weight and Altitude conditions given below: shall be not less than a guaranteed value of: : a) for CFM: *** b) for IAE: *** CES - A320 – AM2 to 2010 A320 PA LA No.3-A A319 perfo Private & Confidential

Cruise Specific Air Range. The average nautical miles per kilogram of fuel (average SAR) at a true Mach number of *** in ISA conditions under the Weight and Altitude conditions given below: Gross Weight (kg) Pressure Altitude (ft) *** shall be not less than a guaranteed value of: : a) for CFM: *** b) for IAE: *** *** This information is subject to confidential treatment and has been omitted and filed separately with the Commission. CT0803292 Private & Confidential

Cruise Specific Air Range. The average nautical miles per kilogram of fuel (average SAR) at a true Mach number of *** 0.78 in ISA ISA+15 conditions under the Weight and Altitude conditions given below: Gross Weight (kg) Pressure Altitude (ft) *** *** shall be not less than a guaranteed value of: : a) for CFM: *** b) for IAE: ***

Cruise Specific Air Range. The average nautical miles per kilogram of fuel (average SAR) at a true Mach number of *** 0.78 in ISA ISA+15 conditions under the Weight and Altitude conditions given below: Gross Weight (kg) Pressure Altitude (ft) *** *** CES - A320 – AM2 to 2010 A320 PA LA No.3-E A319 70t Sharklet perfo Private & Confidential shall be not less than a guaranteed value of: : a) for CFM: *** b) for IAE: ***

Cruise Specific Air Range. The average nautical miles per kilogram of fuel (average SAR) at a true Mach number of *** 0.78 in ISA ISA+15 conditions under the Weight and Altitude conditions given below: Gross Weight (kg) Pressure Altitude (ft) *** *** CES - A320 – AM2 to 2010 A320 PA LA No.3-G A321 Sharklet perfo Private & Confidential shall be not less than a guaranteed value of: : a) for CFM: *** b) for IAE: ***

Cruise Specific Air Range. The average nautical miles per kilogram of fuel (average SAR) at a true Mach number of *** in ISA conditions under the Weight and Altitude conditions given below: Gross Weight (kg) Pressure Altitude (ft) *** shall be not less than a guaranteed value of: : a) for CFM: *** b) for IAE: *** *** This information is subject to confidential treatment and has been omitted and filed separately with the Commission. CT0803292 Private & Confidential

Cruise Specific Air Range. The average nautical miles per kilogram of fuel (average SAR) at a true Mach number of *** in ISA conditions under the Weight and Altitude conditions given below: Gross Weight (kg) Pressure Altitude (ft) *** *** shall be not less than a guaranteed value of: : a) for CFMAircraft equipped with CFM Engines : *** b) for Aircraft equipped with IAE Engines : *** CT1001939 Private & Confidential

Cruise Specific Air Range. The average nautical miles per kilogram of fuel (average SAR) at a true Mach number of *** 0.78 in ISA ISA+15 conditions under the Weight and Altitude conditions given below: Gross Weight (kg) Pressure Altitude (ft) 80,000 33,000 75,000 35,000 70,000 37,000 shall be not less than a guaranteed value of: : a) for CFM: ***0.1603 nm/kg b) for IAE: 0.1637 nm/kg

Cruise Specific Air Range. The average nautical miles per kilogram of fuel (average SAR) at a true Mach number of *** 0.78 in ISA ISA+15 conditions under the Weight and Altitude conditions given below: Gross Weight (kg) Pressure Altitude (ft) * * * * * * shall be not less than a guaranteed value of: : a) for CFM: * * *** b) for IAE: * * * The Seller guarantees a Manufacturer's Weights Empty as below:

Cruise Specific Air Range. The average nautical miles per kilogram of fuel (average SAR) at a true Mach number of *** 0.82 in ISA conditions under the Weight and Altitude conditions given below: shall be not less than a guaranteed value of: a) for CFM: ***:

Cruise Specific Air Range. The average nautical miles per kilogram of fuel (average SAR) at a true Mach number of *** 0.78 in ISA ISA+15 conditions under the Weight and Altitude conditions given below: shall be not less than a guaranteed value of: : a) for CFM: *** b) for IAE: *** CES - A320 – AM2 to 2010 A320 PA LA No.3-B A320 perfo Private & Confidential

Cruise Specific Air Range. The average nautical miles per kilogram of fuel (average SAR) at a true Mach number of *** 0.78 in ISA ISA+15 conditions under the Weight and Altitude conditions given below: Gross Weight (kg) Pressure Altitude (ft) *** *** shall be not less than a guaranteed value of: : a) for CFM: *** b) for IAE: *** CES - A320 – AM2 to 2010 A320 PA LA No.3-F A320 Sharklet perfo Private & Confidential

Cruise Specific Air Range. The average nautical miles per kilogram of fuel (average SAR) at a true Mach number of *** 0.78 in ISA ISA+15 conditions under the Weight and Altitude conditions given below: Gross Weight (kg) Pressure Altitude (ft) 70,000 35,000 65,000 37,000 60,000 39,000 shall be not less than a guaranteed value of: a) for CFM: ***: