AIRCRAFT CONFIGURATION The guarantees defined below ("the Guarantees") are applicable to the A330-200 Aircraft as described in the Technical Specification ***, as amended by the Specification Change Notices ("SCN's") for:
BOEING PROPRIETARY Attachment C to Letter Agreement No. 6-1162-SKC-977-1 Page 1
Aircraft This peril includes self-propelled missiles and spacecraft.
Engine A. Any internal repairs or replacement of internal components, or replacement of engine assembly.
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.