Common use of Enroute One-Engine-Inoperative Altitude Clause in Contracts

Enroute One-Engine-Inoperative Altitude. The FAA approved gross weight at an enroute one-engine-inoperative altitude of *** feet at which the available gross climb gradient equals *** percent on an ISA+10°C day using not more than maximum continuous thrust with engine and wing anti-ice bleed on, shall not be less than the following guarantee value: NOMINAL: *** Pounds TOLERANCE: *** Pounds GUARANTEE: *** Pounds

Appears in 2 contracts

Samples: Purchase Agreement (Continental Airlines, Inc.), Purchase Agreement (United Air Lines Inc)

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Enroute One-Engine-Inoperative Altitude. The FAA approved gross weight at an enroute one-engine-inoperative altitude of *** feet at which the available gross climb gradient equals *** percent on an ISA+10°C day using not more than maximum continuous thrust with engine and wing anti-ice bleed onthrust, shall not be less than the following guarantee value: NOMINAL: *** Pounds TOLERANCE: *** Pounds GUARANTEE: *** Pounds

Appears in 2 contracts

Samples: Purchase Agreement (Continental Airlines, Inc.), Purchase Agreement (United Air Lines Inc)

Enroute One-Engine-Inoperative Altitude. The FAA approved gross weight at an enroute one-engine-inoperative altitude of *** feet at which the available gross climb gradient equals *** percent at a gross weight of *** pounds on an ISA+10°C day using not more than maximum continuous thrust with engine and wing anti-ice bleed onthrust, shall not be less than the following guarantee value: NOMINAL: *** Pounds TOLERANCE: *** Pounds GUARANTEE: *** PoundsFeet

Appears in 2 contracts

Samples: Letter Agreement (United Air Lines Inc), Purchase Agreement (United Air Lines Inc)

Enroute One-Engine-Inoperative Altitude. The FAA approved gross weight at an enroute one-engine-inoperative altitude of *** feet at which the available gross climb gradient equals *** percent at a gross weight of *** on an ISA+10°C a standard day using not more than maximum continuous thrust with engine and wing anti-ice bleed onthrust, shall not be less than the following guarantee value: NOMINAL: *** Pounds TOLERANCE: *** Pounds GUARANTEE: *** Pounds

Appears in 1 contract

Samples: Letter Agreement (Northwest Airlines Corp)

Enroute One-Engine-Inoperative Altitude. The FAA approved gross weight at an enroute one-engine-inoperative altitude of *** feet at which the available gross climb gradient equals *** 1.1 percent at a gross weight of 195,500 kilograms on an ISA+10°C day using not more than maximum continuous thrust with engine and wing anti-ice bleed onthrust, shall not be less than the following guarantee value: NOMINAL: *** Pounds TOLERANCE: *** Pounds GUARANTEE: *** Pounds:

Appears in 1 contract

Samples: Letter Agreement (Lan Airlines SA)

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Enroute One-Engine-Inoperative Altitude. The FAA approved gross weight at an enroute one-engine-inoperative altitude of *** feet at which the available gross climb gradient equals *** percent at a gross weight of *** pounds on an ISA+10°C *** day using not more than maximum continuous thrust with engine and wing anti-ice bleed onthrust, shall not be less than the following guarantee value: NOMINAL: ** ** Pounds Feet TOLERANCE: ** ** Pounds Feet GUARANTEE: ** ** PoundsFeet

Appears in 1 contract

Samples: Supplemental Agreement (United Airlines, Inc.)

Enroute One-Engine-Inoperative Altitude. 2.3.1 The FAA FAA-approved gross weight at an enroute one-engine-inoperative altitude of *** feet at which the available gross climb gradient equals *** percent at a gross weight of *** pounds on an ISA+10***°C day using not more than maximum continuous thrust with engine and wing anti-ice bleed onthrust, shall will not be less than the following guarantee *** value: NOMINAL: *** Pounds TOLERANCE: *** Pounds GUARANTEE: *** Poundsfeet

Appears in 1 contract

Samples: Letter Agreement (United Airlines, Inc.)

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