AIRCRAFT CONFIGURATION. The guarantees listed below are based on the CRJ-900 Aircraft configuration as defined in Bombardier Aerospace Type Specification RAD-690-100 issue NC, and equipped with GE CF34-8C5 engines as defined in GE Engines Performance Model L0073X. The weight data corresponds to the [***] lb ([***] ) MTOW design weight option. Appropriate adjustments shall be made for any changes in configuration of the Aircraft which have been approved by the Buyer and Bombardier Aerospace, Regional Aircraft ("Bombardier") or otherwise allowed by the Purchase Agreement and which cause changes to the performance of the Aircraft.
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AIRCRAFT CONFIGURATION. The guarantees listed below are for a *** CRJ Aircraft based on the CRJ-900 CRJ700 ER Aircraft configuration as defined in Bombardier Aerospace Type Specification RAD-690-100 issue NC***, with the Buyer Selected Optional Features listed in Schedule 3 or Schedule 3A as applicable, and equipped with GE CF34-8C5 8C1 engines as defined in GE Engines Performance Model L0073X. document CF34-8C1 Installation Manual reference GEK 105093. The weight data corresponds to the [***] lb ([***] ) MTOW * design weight option. Appropriate adjustments shall be made for any changes in configuration of the Aircraft which have been configuration, *** approved by the Buyer and Bombardier Aerospace, Regional Aircraft ("Bombardier") or otherwise allowed by the Purchase Agreement and which cause changes to the performance of the Aircraft.
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AIRCRAFT CONFIGURATION. The guarantees listed below are for a *** CRJ Aircraft based on the CRJ-900 CRJ700 ER Aircraft configuration as defined in Bombardier Aerospace Type Specification RAD-690-100 issue NC***, with the Buyer Selected Optional Features listed in Schedule 3 or Schedule 3A as applicable, and equipped with GE CF34-8C5 8C1 engines as defined in GE Engines Performance Model L0073X. document CF34-8C1 Installation Manual reference GEK 105093. The weight data corresponds to the [***] lb ([***] ) MTOW * design weight option. Appropriate adjustments shall be made for any changes in configuration of the Aircraft which have been *** approved by the Buyer and Bombardier Aerospace, Regional Aircraft ("Bombardier") or otherwise allowed by the Purchase Agreement and which cause changes to the performance of the Aircraft.
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AIRCRAFT CONFIGURATION. The guarantees listed below are based on the CRJ-900 CRJ200 LR Aircraft configuration as defined in Bombardier Aerospace Type Specification RAD-690-100 *** issue NCC, with the Buyer Selected Optional Features listed in Schedule 3 to this Supplement and equipped with GE CF34-8C5 3B1 engines as defined in GE Engines Performance Model L0073X. Specification E1271A. The weight data corresponds to the [***] lb ([***] ) MTOW * design weight optionoption and includes the weight changes associated with the centre-wing fuel tank. Appropriate adjustments shall be made for any changes in configuration of the Aircraft which have been approved by the Buyer and Bombardier Aerospace, Regional Aircraft ("Bombardier") or otherwise allowed by the Purchase Agreement and which cause changes to the performance of the Aircraft.
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AIRCRAFT CONFIGURATION. The guarantees listed below are for a 70 Seat CRJ Aircraft based on the CRJ-900 CRJ700 ER Aircraft configuration as defined in Bombardier Aerospace Type Specification RAD-690RAD-670-100 issue NCE, with the Buyer Selected Optional Features listed in Schedule 3 or Schedule 3A as applicable, and equipped with GE CF34-8C5 8C1 engines as defined in GE Engines Performance Model L0073X. document CF34-8C1 Installation Manual reference GEK 105093. The weight data corresponds to the [***] lb ([***] ) MTOW * design weight option. Appropriate adjustments shall be made for any changes in configuration of the Aircraft which have been ** approved by the Buyer and Bombardier Aerospace, Regional Aircraft ("Bombardier") or otherwise allowed by the Purchase Agreement and which cause changes to the performance of the Aircraft.
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AIRCRAFT CONFIGURATION. The guarantees listed below are based on the CRJ-900 CRJ700 ER Aircraft configuration as defined in Bombardier Aerospace Type Specification RAD-690RAD-670-100 issue NCE, with buyer optional features and equipped with GE CF34-8C5 8C1 engines as defined in GE Engines Performance Model L0073X. document CF34-8C1 Installation Manual reference GEK 105093. The weight data corresponds to the [***] 75000 lb ([***] ) MTOW design weight option. Appropriate adjustments shall be made for any changes in configuration of the Aircraft which have been approved by the Buyer and Bombardier Aerospace, Regional Aircraft ("Bombardier") or otherwise allowed by the Purchase Agreement and which cause changes to the performance of the Aircraft.
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AIRCRAFT CONFIGURATION. The guarantees listed below are based on the CRJ-900 CRJ-700ER Series 701 Aircraft configuration as defined in Bombardier Aerospace Type Specification RAD-690RAD-670-100 issue NCC, and equipped with GE CF34-8C5 8C1 engines as defined in GE Engines Performance Model L0073X. document CF34-8C1 Installation Manual reference GEK 105093. The weight data corresponds to the [***] lb ([***] ) MTOW design weight option. Appropriate adjustments shall be made for any changes in configuration of the Aircraft which have been approved by the Buyer and Bombardier Aerospace, Regional Aircraft ("Bombardier") or otherwise allowed by the Purchase Agreement and which cause changes to the performance of the Aircraft.
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AIRCRAFT CONFIGURATION. The guarantees listed below are based on the CRJ-900 CRJ700 Series 705-ER Aircraft configuration as defined in new Bombardier Aerospace Type Specification RAD-690-100 issue NC***, with buyer the Buyer Selected Optional Features listed in Annex A to this Schedule 13, and equipped with GE CF34-8C5 engines as defined in GE Engines Performance Model L0073X. G0173F/pip82b. The weight data corresponds to the [***] lb ([***] ) MTOW design weight option. Appropriate adjustments shall be made for any changes in configuration of the Aircraft which have been approved by the Buyer and Bombardier Aerospace, Regional Aircraft ("Bombardier") or otherwise allowed by the Purchase Agreement and which cause changes to the performance of the Aircraft.
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