時間：2011-08-31 13:49來源：藍天飛行翻譯 作者：航空 點擊：次
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a ‘Maximum Contingency Power and/or Thrust’ means the power and/or thrust identified in the performance data for use when a power-unit has failed or been shut down during take-off, baulked landing or prior to a discontinued approach and limited in use for a continuous period of not more than 21.2 minutes. NOTE: The 21.2 minute period for use of maximum contingency power and/or thrust is additional to the 5 minute or 10 minute period at take-off power and/or thrust (see c.) and may be added to the take-off limitation at any point in time. b. ‘Maximum Contingency Power and/or Thrust Rating’ means the minimum test bed acceptance power and/or thrust, as stated in the engine type certificate data sheet, of series and newly overhauled engines when running at the specified conditions and within the appropriate acceptance limitations. c. ‘Take-off Power and/or Thrust’ means the power and/or thrust identified in the performance data for use during take-off, discontinued approach and baulked landing; and i. for aeroplanes and helicopters, limited in use to a continuous period of not more than 5 minutes; and ii. for aeroplanes only (when specifically requested), limited in use to a continuous period of not more than 10 minutes in the event of a power-unit having failed or been shut down. d. ‘Take-off Power and/or Thrust Rating’ means the minimum test bed acceptance power and/or thrust as stated in the engine type certificate data sheet, of series and newly overhauled engines when running at the specified conditions and within the appropriate acceptance limitations. e. ‘Intermediate Contingency Power and/or Thrust’ means the power and/or thrust identified in the performance data for use after take-off when a power-unit has failed or been shut down, during periods of unrestricted duration. f. ‘Intermediate Contingency Power and/or Thrust Rating’ means the minimum test bed acceptance power and/or thrust, as stated in the engine type certificate data sheet, of series and newly overhauled engines when running at the specified conditions and within the appropriate acceptance limitations. |
