gga - cost index

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  • 7/31/2019 GGA - Cost Index

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    IN-FLIGHT PERFORMANCE

    Cost Index

    Version 1.4

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    Content

    Cost Index2

    Specific Range1

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    Content

    Cost Index2

    Specific Range1

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    1. Specific Range

    SR variations with Mach number

    SR: distance coveredper fuel mass unit burnt

    SR reaches a maximum

    at the MACH of MAXI-RANGE (MMR)

    At the Mach of Maxi-Range, the

    fuel consumption is minimumas regards to the distance crossed

    at the given altitude and weight.

    SR (NM/t)

    40

    50

    60

    70

    Given :- Altitude- Weight

    MMR

    Maxi Range

    Mach.76 .80 .84

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    1. Specific Range

    SR variations with Mach number

    M < MMR SR

    For a given fuel quantity, thecovered distance is lower.

    For a given distance,

    consumption is higher.

    M < MMR time

    MMR = Inferior limit

    SR (NM/t)

    40

    50

    60

    70

    Mach

    Maxi Range

    .76 .80 .84

    Given :- Altitude- Weight

    MMR

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    1. Specific Range

    MMR: advantages and drawbacks

    Very advantageous regarding the trip fuel

    But MMR is too low Trip time is quite long

    Solution

    Increasing cruise speed without increasing too muchthe fuel consumption This is what Long Range Cruise Mach aims at

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    1. Specific Range

    Long Range Cruise Mach

    Definition:

    SR: distance covered

    per fuel mass unit burnt

    Flying at LRC Machenables a low fuelconsumption (but

    NOT minimum), whilethe speed is higherthan MMR

    SRLRC = 99 % SRMAX

    Mach

    SR

    .76 .80 .84

    MMR

    LRCMax SR

    -1%

    Given :- Altitude- Weight

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    SR: distance covered

    per fuel mass unit burnt

    1. Specific Range

    Long Range Cruise Mach

    Advantages of LRC onMMR:

    The 1% fuel consumptionincrement is compensated

    by an important gain onspeed and consequently onflight time.

    Any selected Mach number

    under LRC would result in adecrease in the fuelconsumption.

    Mach

    SR

    .76 .80 .84

    LRC

    MMR

    Given :- Altitude- Weight

    SR: distance covered

    per fuel mass unit burnt

    Givenaltitude

    A330FL 350

    ISA

    Example :

    Max SR = 68.44 NM/tMMR = M 0.796

    99% of Max SR = 67.75 NM/tLRC = M 0.811 + 9 kt TAS

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    Content

    Cost Index2

    Specific Range1

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    2. Cost Index

    Direct Operating Costs: D.O.C.

    Do not take as a reference

    Cyclic

    Maintenance

    7%

    Cockpit crew

    13%

    Hourly

    Maintenance6%

    Insurance

    2%

    Cabin crew13%

    Fuel

    15%

    Depreciation

    27%

    Financial

    charges

    17%

    Example of Direct Operating Costs

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    2. Cost Index

    Direct Operating Costs: D.O.C.

    D.O.C. are made of:

    Fixed costs Flight time related

    costs

    Fuel consumptionrelated costs

    ECONOMY=

    Minimize D.O.C.

    Lower fuelconsumption

    Lowerflight time

    Compromise Time / Fuel ...

    And

    / Or

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    2. Cost Index

    Direct Operating Costs: D.O.C.

    Fixed costs: CC

    Aircraft ownership (depreciation, lease rentals unrelated toflight hours, insurance) ($)

    Cyclic maintenance ($)

    Fixed flight crew ($)

    Fixed cabin crew ($)

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    2. Cost Index

    Direct Operating Costs: D.O.C.

    Time-related costs: CT . T

    CT : Time related costs per flight hour:- Hourly maintenance costs ($/h)

    - Airport charges ($/h)

    - Air Traffic Service charges ($/h)

    - Variable flight crew ($/h)

    - Variable cabin crew ($/h)

    T: Number of flight hours (h)

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    2. Cost Index

    Direct Operating Costs: D.O.C.

    Fuel consumption related costs: CF . F

    CF : Cost of fuel unit ($/ton)

    F : Fuel consumed (tons)

    Do not take as a reference

    CyclicMaintenance

    7%

    Cockpit crew13%

    HourlyMaintenance

    6%

    Insurance2%

    Cabin crew13%

    Fuel15%

    Depreciation27%

    Financialcharges

    17%

    Example of Direct Operating Costs

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    ECON Mach

    2. Cost Index

    Costs

    Mach

    Fixed costs

    Cost of Time

    Cost of Fuel

    MMO

    MMR

    LRC

    D.O.C.

    ECON

    Economic Cruise Mach Number(ECON Mach):the Mach number which minimizes the D.O.C.

    Given:- Altitude- Weight

    - Wind

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    2. Cost Index

    ECON Mach

    The ECON Mach is a function of the A/C weight,A/C Altitude and wind conditions.

    Costs

    Mach

    Fixed costs

    Cost of Time

    Cost of Fuel

    MMO

    MMR

    LRC

    D.O.C.

    ECON

    Given:- Altitude- Weight

    - Wind

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    2. Cost Index

    Definition: Cost Index

    Ratio

    Possible Range:

    From 0 to 999

    In operations: from 0 to 300

    The ECON Mach depends on Cost Index

    C.I. =Cost of Time

    Cost of Fuel

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    2. Cost Index

    Speed control and Cost Index

    Increasein Mach

    Increasein C.I.

    C. I. = 0

    C. I. = 999

    ECON Mach =MMR

    ECON Mach =MMO - 0.02

    Fuel strategy

    Time strategy

    C.I. =Cost of Time

    Cost of Fuel

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    Speed control and Cost Index

    2. Cost Index

    Costs

    MachECON

    LRCFixed costs

    Given:- altitude- weight- wind

    LRC

    D.O.C.Cost of Fuel

    Cost of Time

    MMRMMO-0.02 MMO

    Whatever the Cost Index, ECON is always includedbetween MMR (variable) and MMO - 0.02 (fixed).

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    2. Cost Index

    Speed control and Cost Index

    CI depends on each airline, and enables the speed oneach route to be optimized to minimize the DirectOperating Costs.

    It is inserted in the MFD (Multi Function Display) beforedeparture, to enable AFS (Auto Flight System)calculation of ECON Mach according to externalparameters.

    C.I. =Cost of Time

    Cost of Fuel

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    2. Cost Index

    Speed control and Cost Index

    Some flight planning systems allow to calculate the fuelat a fixed cost index, so that the speed is optimized allalong the route as a function of the weight, altitude and

    wind conditions.

    C.I. =Cost of Time

    Cost of Fuel

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    2. Cost Index

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    2. Cost Index

    This table enables

    you to find themost cost effectiveMach number vs.cost index, altitudeand wind as

    calculated by theFMGC.

    CI = 100 kg / min

    FL 350Weight = 200 tWind = 50 kt

    M 0.822

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    AIRBUS S.A.S. All rights reserved. Confidential and

    proprietary document.This document and all information contained herein is the soleproperty of AIRBUS S.A.S.. No intellectual property rights aregranted by the delivery of this document or the disclosure ofits content. This document shall not be reproduced ordisclosed to a third party without the express written consentof AIRBUS S.A.S. This document and its content shall not beused for any purpose other than that for which it is supplied.

    The statements made herein do not constitute an offer. Theyare based on the mentioned assumptions and are expressedin good faith. Where the supporting grounds for these

    statements are not shown, AIRBUS S.A.S. will be pleased toexplain the basis thereof.

    AIRBUS, its logo, A300, A310, A318, A319, A320, A321,A330, A340, A350, A380, A400M are registered trademarks.