Common use of Climb Clause in Contracts

Climb. cruise and descent performance associated with the Guarantees 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 Paragraph 10.3 may be such as to optimize the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air shall be bled from the engines for anti-icing. Cruise performance at [DELETED] ft and above is based on a center of gravity position of TBD % MAC, unless otherwise stated.

Climb. cruise and descent performance associated with the Guarantees 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 Paragraph 10.3 9.3 may be such as to optimize the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air shall be bled from the engines for anti-icing. Cruise performance at [DELETED] ft and above is based on a center of gravity position of TBD [DELETED] % MAC, unless otherwise stated.

Climb. cruise and descent performance associated with the Guarantees 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 Paragraph 10.3 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 shall be bled from the engines for anti-icing. Cruise performance at [DELETED] ft DELETED]ft and above is based on a center of gravity position of TBD [DELETED] % MAC, unless otherwise stated.

Climb. cruise and descent performance associated with elements of the Guarantees shall 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 Paragraph 10.3 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 shall will be bled from the engines for anti-icing. Cruise performance at [DELETED] 20,000 ft and above is are based on a center of gravity position of TBD 30% MAC, unless otherwise stated.

Climb. cruise and descent performance associated with the Guarantees 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 Paragraph 10.3 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 shall be bled from the engines for anti-icing. Cruise performance at [DELETED] ft and above is based on a center of gravity position of TBD [DELETED] % MAC, unless otherwise stated.

Climb. cruise and descent performance associated with the Guarantees shall 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 Paragraph 10.3 Subparagraph 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 shall will be bled from the engines for anti-icing. Cruise performance at [DELETED] 20,000 ft and above is based on a center centre of gravity position of TBD 34% MAC, unless otherwise stated.