Common use of Climb Clause in Contracts

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 below may be such as to optimize the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing.

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 6.3 below may be such as to optimize the A321 Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing.

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph paragraph 5.3 below may be such as to optimize the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing. Cruise performance at *** and above is based on a centre of gravity position of ***.

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 below may be such as to optimize the A319 Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing.

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 below may be such as to optimize the A320 Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing.

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 below may be such as to optimize the A321 Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing.

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 below may be such as to optimize the A330-200 Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing.

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-21- 30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 6.3 below may be such as to optimize the A320 Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing.

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 below may be such as to optimize the A340-200 Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing.

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph paragraph 5.3 below may be such as to optimize optimise the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing. Cruise performance at *** and above assumes a centre of gravity position of ***, unless otherwise stated.

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 8.3 below may be such as to optimize the A330-300 Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing.

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 below may be such as to optimize the A340-300 Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing.

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-21- 30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 6.3 below may be such as to optimize the A319 Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing.

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph paragraph 5.3 below may be such as to optimize the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing.. Cruise performance at *** and above is based on a centre of gravity position of ***

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 6.3 below may be such as to optimize the A319 Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing.

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 6.3 below may be such as to optimize the A320 Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing.

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. **Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 paragraph 6.3 below may be such as to optimize the New A320 (IAE Powered) Aircraft performance while meeting the minimum air conditioning requirements defined above. ** Unless otherwise stated no air will be bled from the engines for anti-icing.**

Climb. cruise cruise, descent and descent holding performance associated with elements of the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 paragraph 7.3 below may be such as to optimize the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing.. Cruise performance are based on a center of gravity position of *

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph Clause 5.3 below may be such as to optimize the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing.

Climb. cruise and descent performance associated with the Guarantees will shall include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 below Paragraph 7.3 may be such as to optimize the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will shall be bled from the engines for anti-icing.

Climb. cruise and descent performance associated with the Guarantees will shall include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 below Paragraph 6.3 may be such as to optimize the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will shall be bled from the engines for anti-icing.

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. ** Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 paragraph 6.3 below may be such as to optimize the New A321 (CFM Powered) Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing.**

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph Clause 5.3 below may be such as to optimize the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing. Cruise performance at *** and above is based on a centre of gravity position of ***.

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. ** Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 paragraph 6.3 below may be such as to optimize the New A321 (IAE Powered) Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing.**

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 6.3 below may be such as to optimize optimise the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing. Cruise performance at ** and above is based on a centre of gravity position of **.

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph Clause 5.3 below may be such as to optimize the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing.. Cruise performance at *** and above is based on a centre of gravity position of ***

Climb. cruise and descent performance associated with the Guarantees will shall include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 below Paragraph 8.3 may be such as to optimize the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will shall be bled from the engines for anti-icing.

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification**. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 paragraph 6.3 below may be such as to optimize the Aircraft New A320 (CFM Powered) performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing.**

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 below Paragraph 6.3 may be such as to optimize the A319 Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing.

Climb. cruise and descent performance associated with elements of the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 paragraph 9.3 below may be such as to optimize the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing. Cruise performance at 20,000 ft and above are based on a center of gravity position of 30% MAC.

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 below paragraph 6.3 may be such as to optimize optimise the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing. Cruise performance at *** and above assumes a centre of gravity position (MAC) giving the best results, unless otherwise stated.

Climb. cruise and descent performance associated with elements of the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 paragraph 6.3 below may be such as to optimize the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing. Cruise performance at 20,000 ft and above are based on a center of gravity position of 34% MAC.

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 8.3 below may be such as to optimize optimise the Aircraft performance while meeting the minimum normal air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing. Cruise performance at 20,000 ft and above is based on an optimized centre of gravity position.

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 below Paragraph 6.3 may be such as to optimize the A320 Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing.

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 7.3 below may be such as to optimize optimise the Aircraft performance while meeting the minimum normal air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing. Cruise performance at ** and above is based on an optimized centre of gravity position.

Climb. cruise cruise, descent and descent holding performance associated with elements of the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 paragraph 7.3 below may be such as to optimize the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing. Cruise performance are based on a center of gravity position of * MAC.

Climb. cruise and descent performance associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 8.3 below may be such as to optimize optimise the Aircraft performance while meeting the minimum normal air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing. Cruise performance at ** and above is based on an optimized centre of gravity position.

Climb. cruise and descent performance associated with the Guarantees will shall include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in Subparagraph 5.3 below paragraph 6.3 may be such as to optimize the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will shall be bled from the engines for anti-icing. Cruise performance at *** and above assumes a centre of gravity position of *** MAC.