Common use of Takeoff Clause in Contracts

Takeoff. 2.1.1 The FAA approved takeoff field length at a gross weight at the start of the ground roll of [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] kilograms, at a temperature of [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT], at a sea level altitude, with an alternate forward center of gravity limit of per cent of the mean aerodynamic chord, and using maximum takeoff thrust, shall not be more than the following guarantee value: GUARANTEE: [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] Meters 2.1.2 The FAA approved takeoff field length at a gross weight at the start of the ground roll of [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] kilograms, at a temperature of [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT], at a sea level altitude, with an alternate forward center of gravity limit of per cent of the mean aerodynamic chord, and using maximum takeoff thrust, shall not be more than the following guarantee value: GUARANTEE: [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] Meters Engine derated to CFM56-7B24 thrust level. Attachment to Letter Agreement No. 6-1162-DME-1153 CFM56-7B27/B1 Engines Page 3 2.1.3 The FAA approved takeoff gross weight at the start of ground roll, at a temperature of [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT], at an altitude of feet and satisfying the conditions defined below, with an alternate forward center of gravity limit of [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] percent of the mean aerodynamic chord, and using maximum takeoff thrust, shall not be less than the following guarantee value: GUARANTEE: [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] Kilograms Conditions: The takeoff runway available (TORA) is [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] meters. The takeoff distance available (TODA) is [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] meters. The accelerate-stop distance available (ASDA) is [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] meters. The lineup allowance adjustment to TORA and TODA is [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] meters. The lineup allowance adjustment to ASDA is [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] meters. The following obstacle definition is based on a straight-out departure where obstacle height and distance are specified with reference to the liftoff end of the runway: 1. [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT]meters [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] 2.2.1 The FAA approved landing gross weight from a [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] meter runway, at a temperature of [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] and at an altitude of [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] feet, shall not be less than the following guarantee value: GUARANTEE: [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] Kilograms 2.2.2 The FAA approved landing field length at a gross weight of [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] kilograms and at a sea level altitude, shall not be more than the following guarantee value: GUARANTEE: [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] Meters Attachment to Letter Agreement No. 6-1162-DME-1153 CFM56-7B27/B1 Engines Page 4

Takeoff. 2.1.1 The FAA approved takeoff field length at a gross weight at the start of ground roll, at a temperature of 86 degrees F,at a sea level altitude, from a 10,500 foot runway and using maximum takeoff thrust, shall not be less than the ground roll of following guarantee value: NOMINAL: [*CONFIDENTIAL PORTION MATERIAL OMITTED TOLERANCE: AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] kilograms, at a temperature of [CONFIDENTIAL PORTION OMITTED GUARANTEE: SECURITIES AND FILED SEPARATELY WITH THE EXCHANGE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] 2.1.2 The FAA approved takeoff climb limited gross weight without using the improved climb performance procedure at a temperature of 86 degrees F, and at a sea level altitude, altitude and with an alternate forward center of gravity limit of per cent of the mean aerodynamic chord, Aircraft configuration used to show compliance with Paragraph 2. 1.1 and using maximum takeoff thrust, shall not be more less than the following guarantee value: GUARANTEEG95-001 Attachment A to Letter Agreement No. 6-1162-RCN-925 PW4090 Engines Page 3 NOMINAL: [*CONFIDENTIAL PORTION MATERIAL OMITTED TOLERANCE: AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] Meters 2.1.2 The FAA approved takeoff field length at a gross weight at the start of the ground roll of [CONFIDENTIAL PORTION OMITTED GUARANTEE: SECURITIES AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] kilograms, at a temperature of [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE EXCHANGE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT], at a sea level altitude, with an alternate forward center of gravity limit of per cent of the mean aerodynamic chord, and using maximum takeoff thrust, shall not be more than the following guarantee value: GUARANTEE: [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] Meters Engine derated to CFM56-7B24 thrust level. Attachment to Letter Agreement No. 6-1162-DME-1153 CFM56-7B27/B1 Engines Page 3 2.1.3 The FAA approved takeoff gross weight at the start of ground roll, at a temperature of [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT]86 degrees F, at an altitude of feet and satisfying the conditions defined below5,431 feet, with an alternate forward center of gravity limit of [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] percent of the mean aerodynamic chord, from a 12,000 foot runway and using maximum takeoff thrust, shall not be less than the following guarantee value: GUARANTEENOMINAL: [*CONFIDENTIAL PORTION MATERIAL OMITTED TOLERANCE: AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] Kilograms ConditionsGUARANTEE: The takeoff runway available (TORA) is [CONFIDENTIAL PORTION OMITTED SECURITIES AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] meters. The takeoff distance available (TODA) is [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] meters. The accelerate-stop distance available (ASDA) is [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] meters. The lineup allowance adjustment to TORA and TODA is [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] meters. The lineup allowance adjustment to ASDA is [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] meters. The following obstacle definition is based on a straight-out departure where obstacle height and distance are specified with reference to the liftoff end of the runway: 1. [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT]meters [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE EXCHANGE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] 2.2.1 2.1.4 The FAA approved landing takeoff climb limited gross weight from a [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] meter runway, without using the improved climb performance procedure at a temperature of [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] 86 degrees F, and at an altitude of [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] feet5,431 feet and with the Aircraft configuration used to show compliance with Paragraph 2.1.3 and using maximum takeoff thrust, shall not be less than the following guarantee value: GUARANTEENOMINAL: [*CONFIDENTIAL PORTION MATERIAL OMITTED TOLERANCE: AND FILED SEPARATELY WITH THE GUARANTEE: SECURITIES AND EXCHANGE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] Kilograms2.2 Landing 2.2.2 2.2.1 The FAA approved landing field length at a gross weight of [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] kilograms 460,000 pounds and at a sea level altitude, shall not be more than the following guarantee value: GUARANTEENOMINAL: [*CONFIDENTIAL PORTION MATERIAL OMITTED TOLERANCE: AND FILED SEPARATELY WITH THE GUARANTEE: SECURITIES AND EXCHANGE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] 2.2.2 The FAA approved landing climb limited gross weight at a temperature of 86 degrees F, and at a sea level altitude, with the Aircraft configuration used to show compliance with Paragraph 2.2.1, and with engine bleed for air conditioning with two packs operating, shall not be less than the following guarantee value: NOMINAL: [*CONFIDENTIAL MATERIAL OMITTED TOLERANCE: AND FILED SEPARATELY WITH THE GUARANTEE: SECURITIES AND EXCHANGE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] 2.2.3 The FAA approved landing field length at a gross weight of 460,000 pounds and at an altitude of 5,431 feet, shall not be more than the following guarantee value: NOMINAL: [*CONFIDENTIAL MATERIAL OMITTED TOLERANCE: AND FILED SEPARATELY WITH THE GUARANTEE: SECURITIES AND EXCHANGE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] Meters Attachment G95-001 2.2.4 The FAA approved landing climb limited gross weight at a temperature of 86 degrees F, and at an altitude of 5,431 feet, with the Aircraft configuration used to Letter Agreement No. 6-1162-DME-1153 CFM56-7B27/B1 Engines Page 4show compliance with Paragraph 2.2.3, and with engine bleed for air conditioning with two packs operating, shall not be less than the following guarantee value: NOMINAL: [*CONFIDENTIAL MATERIAL TOLERANCE: OMITTED AND FILED SEPARATELY GUARANTEE: WITH THE SECURITIES AND EXCHANGE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT]