Enroute One-Engine-Inoperative Altitude Sample Clauses

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
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Enroute One-Engine-Inoperative Altitude. The FAA-approved enroute one-engine-inoperative altitude at which the available gross climb gradient equals [**] at a [**] on an [**] day using not more than maximum continuous thrust, will not be less than the following guarantee value: NOMINAL: [**] TOLERANCE: [**] GUARANTEE: [**]

Related to Enroute One-Engine-Inoperative Altitude

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