Fuel Consumption Measurement Sample Clauses

Fuel Consumption Measurement. The inflight data required for administration of this Guarantee will be obtained by New Air during stable cruise conditions using ECM data recordings and the ECM II software available from IAE (requires the ECM sales order option from Airbus). Provided that:
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Fuel Consumption Measurement. The inflight data required for administration of this Guarantee will be obtained by Midway during steady state cruise conditions using methods which will be mutually agreed between Midway and IAE. Steady state cruise conditions are defined as a minimum of five minutes at the same altitude, Mach number and thrust setting Engine Pressure Ratio in clear, smooth air with normal bleed and power extraction and autothrottle disengaged (unless flight evaluation shows this disengagement to be unnecessary). Data points falling within the following envelope of altitude, Mach number and Engine Pressure Ratio: Mach No. -- TBD to TBD, Altitude - TBD to TBD feet, Engine Pressure Ratio - TBD to TBD will be deemed to be Acceptable Data Points, provided that: a) the fuel consumption data for any Eligible Engine on which the engine parameters indicate a possible malfunction (including associated Aircraft systems), other than normal gas path deterioration, that is subsequently confirmed by maintenance action will not be considered acceptable data, and b) data which is obviously inaccurate under normal engine monitoring practices will not be considered acceptable data; this type of data will be rejected unless Midway validity checks have established that Total Air Temperature, Fuel Flow Aircraft and Engine Bleed Systems and other Aircraft parameters are within normal operating ranges. The data to be recorded will be that normally recorded for Engine Condition Monitoring purposes and will include the following: Altitude Mach Number Total Air Temperature (TAT) Indicated Airspeed (IAS) Engine Pressure Ratio (EPR) Fuel Flow Low Compressor Rotor Speed (N(1)) High Compressor Rotor Speed (N(2)) Exhaust Gas Temperature (EGT) Bleed Air Configuration Engine Fuel flow measurements will be referred to in the Standard Engine Fuel Flow-Engine Pressure Ratio Relationship which will be defined for installed Engines by the Aircraft manufacturer during the Aircraft flight test certification program.
Sample 1
Fuel Consumption Measurement. The inflight data required for administration of this Guarantee will be obtained by ACA during steady state cruise conditions using methods which shall be mutually agreed between ACA and IAE prior to entry into service of the first Aircraft and may include, at ACA's option, ECM data recordings and the ECM II software available from IAE (requires the ECM sales order option from Airbus). Provided that: a) the fuel consumption data for any Eligible Engine on which the engine parameters indicate a possible malfunction (including associated Aircraft systems), other than normal gas path deterioration, that is subsequently confirmed by maintenance action will not be considered acceptable data, and b) data which is obviously inaccurate under normal engine monitoring practices will not be considered acceptable data; this type of data will be rejected unless ACA validity checks have established that Total Air Temperature, Fuel Flow Aircraft and Engine Bleed Systems and other Aircraft parameters are within normal operating ranges. The data to be recorded will be that normally recorded for Engine Condition Monitoring purposes and will include the following: Altitude Mach Number Total Air Temperature (TAT) Indicated Airspeed (IAS) Engine Pressure Ratio (EPR) Fuel Flow Low Compressor Rotor Speed (N1) High Compressor Rotor Speed (N2) Exhaust Gas Temperature (EGT) Bleed Air Configuration Engine Fuel Flow measurements will be referred to in the Standard Engine Fuel Flow-Engine Pressure Ratio Relationship which will be defined for installed Engines by the Aircraft manufacturer during the Aircraft flight test certification program.
Sample 1

Related to Fuel Consumption Measurement

  • Mileage Measurement Where required, the mileage measurement for LIS rate elements is determined in the same manner as the mileage measurement for V&H methodology as outlined in NECA Tariff No. 4.

  • Temperature Measurement Temperature will be measured by the nearest automatic Melbourne Bureau of Meteorology Monitoring Station for example (but not limited to): Melbourne, Moorabbin, Dunns Hill, Melbourne Airport, Frankston, and Point Xxxxxx. At the commencement of each project, the onsite management and employee representatives shall agree which is to be the applicable automatic weather monitoring station.

  • Usage Measurement Usage measurement for calls shall begin when answer supervision or equivalent Signaling System 7 (SS7) message is received from the terminating office and shall end at the time of call disconnect by the calling or called subscriber, whichever occurs first.

  • Interim Measures Notwithstanding any requirements for alternative dispute resolution procedures as set forth in Articles 18(B), any party to the Dispute may apply to a court for interim measures (i) prior to the constitution of the arbitral tribunal (and thereafter as necessary to enforce the arbitral tribunal’s rulings); or (ii) in the absence of the jurisdiction of the arbitral tribunal to rule on interim measures in a given jurisdiction. The Parties agree that seeking and obtaining such interim measures shall not waive the right to arbitration. The arbitrators (or in an emergency the presiding arbitrator acting alone in the event one or more of the other arbitrators is unable to be involved in a timely fashion) may grant interim measures including injunctions, attachments and conservation orders in appropriate circumstances, which measures may be immediately enforced by court order. Hearings on requests for interim measures may be held in person, by telephone, by video conference or by other means that permit the parties to the Dispute to present evidence and arguments.

  • Measuring EPP parameters Every 5 minutes, EPP probes will select one “IP address” of the EPP servers of the TLD being monitored and make an “EPP test”; every time they should alternate between the 3 different types of commands and between the commands inside each category. If an “EPP test” result is undefined/unanswered, the EPP service will be considered as unavailable from that probe until it is time to make a new test.

  • Performance Measurement The Uniform Guidance requires completion of OMB-approved standard information collection forms (the PPR). The form focuses on outcomes, as related to the Federal Award Performance Goals that awarding Federal agencies are required to detail in the Awards.

  • Measuring DNS parameters Every minute, every DNS probe will make an UDP or TCP “DNS test” to each of the public-­‐DNS registered “IP addresses” of the name servers of the domain name being monitored. If a “DNS test” result is undefined/unanswered, the tested IP will be considered unavailable from that probe until it is time to make a new test.

  • Non-tariff Measures 1. A Party shall not adopt or maintain any non-tariff measures on the importation of any good of the other Party or on the exportation of any good destined for the territory of the other Party except in accordance with its WTO rights and obligations or in accordance with other provisions of this Agreement. 2. Each Party shall ensure its non-tariff measures permitted in paragraph 1 are not prepared, adopted or applied with a view to, or with the effect of, creating unnecessary obstacles to trade between the Parties.

  • Corrective Measures If the Participating Generator fails to meet or maintain the requirements set forth in this Agreement and/or the CAISO Tariff, the CAISO shall be permitted to take any of the measures, contained or referenced in the CAISO Tariff, which the CAISO deems to be necessary to correct the situation.

  • Measurement Should the State terminate this contract as herein provided, no fees other than fees due and payable at the time of termination shall thereafter be paid to the Engineer. In determining the value of the work performed by the Engineer prior to termination, the State shall be the sole judge. Compensation for work at termination will be based on a percentage of the work completed at that time. Should the State terminate this contract under paragraph (4) or (5) above, the Engineer shall not incur costs during the thirty-day notice period in excess of the amount incurred during the preceding thirty days.

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