AIRLINE TRANSPORT PILOTS LICENCE (A) (FLIGHT PERFORMANCE AND PLANNING)

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Transcription:

031 MASS & BALANCE

AIRLINE TRANSPORT PILOTS LICENCE (A) JAR-FCL 030 00 00 00 FLIGHT PERFORMANCE AND PLANNING 031 00 00 00 MASS AND BALANCE 031 01 00 00 INTRODUCTION TO MASS AND BALANCE 031 01 01 00 Centre of Gravity 031 01 01 01 Definition Define the centre of gravity related to an aeroplane 031 01 01 02 Importance for aircraft stability Explain why the C.G. must be within the certified limits with regard to aeroplane operations 031 01 02 00 Mass and Balance limits 031 01 02 01 Consult aeroplane flight manual: 031 01 02 02 Maximum floor load Describe the effects of operating an aeroplane at its mass and centre of gravity limits Find the certified centre of gravity limits for takeoff, landing and cruise configuration from the aeroplane operating manual AOM State that maximum floor/running loads have to be considered when loading small heavy items. Calculate examples and extract the necessary data from an aeroplane operating manual. 031 01 02 03 Maximum ramp and taxi mass Explain maximum ramp and taxi mass 031 01 02 04 Factors determining maximum permissible mass Describe the limitations for the maximum permissible Takeoff and Landing mass. Issue 1: October 1999 031-MB-2 CJAA Licensing Division

JAR-FCL AIRLINE TRANSPORT PILOTS LICENCE (A) Describe the limitations for the maximum traffic load. Calculate examples for these masses 031 01 02 05 Factors determining centre of gravity limits 031 02 00 00 LOADING 031 02 01 00 Terminology 031 02 01 01 Empty mass State that centre of gravity limits are determined by aircraft stability and manoeuvrability and describe the influence on aeroplane operation Summarise all factors that affect the location of the centre of gravity during aeroplane operation. Describe the effect of extending/retracting flaps on the pitching moment Define take-off mass, landing mass and max. inflight mass Define empty mass, basic mass and basic empty mass. State where these masses can be found. Calculate an example for the basic empty mass 031 02 01 02 Dry operating mass (empty mass + crew + operating items + unusable fuel) 031 02 01 03 Zero fuel mass Define dry operating mass and operating mass and calculate examples Define zero fuel and maximum zero fuel mass. Describe the reason for limiting the zero fuel mass. Calculate examples 031 02 01 04 Standard mass Issue 1: October 1999 031-MB-3 CJAA Licensing Division

AIRLINE TRANSPORT PILOTS LICENCE (A) JAR-FCL State when to apply actual or standard masses for crew, passengers, baggage and cargo according to JAR-OPS1. Find the standard masses for different types of flights with reference to JAR-OPS1. Calculate total traffic loads and total mass of crew Describe the relation between volume, density and mass for fuel, oil and water and calculate examples 031 02 01 05 Useful load (Traffic load + Usable fuel) 031 02 02 00 Aircraft Mass Check 031 02 02 01 Procedure Define traffic load and useful load. Calculate examples for traffic and useful load JAR-OPS1 given State where the results of an aircraft mass check are found. State who is responsible for re-weighing and the issuing the correct dry operating mass. List the practices, according to JAR-OPS1, to be used at re-weighing 031 02 02 02 Requirements for re-weighing of aircraft 031 02 02 03 Equipment lists List the time intervals for the re-weighing of aeroplanes according to JAR-OPS1 State that the equipment list is used to name which items are included in the re-weighing process 031 02 03 00 Procedures for determining aeroplanes mass and balance documentation 031 02 03 01 Determining dry operating mass Aircraft mass and balance data. Extract the dry operating mass DOM, dry operating index DOI for specified crew, trip and service conditions from the aeroplane operating manual AOM Issue 1: October 1999 031-MB-4 CJAA Licensing Division

AIRLINE TRANSPORT PILOTS LICENCE (A) JAR-FCL 031 02 03 02 Intentionally left blank 031 02 03 03 Add mass of passengers and cargo 031 02 03 04 Add mass of fuel Calculate the maximum allowable traffic load, the zero fuel mass and maximum cargo loads for different conditions Calculate the maximum allowable fuel load, the maximum extra fuel and the useful load 031 02 03 05 Check that applicable maximum gross mass limits are not exceeded Calculate takeoff mass, maximum takeoff mass, landing mass and maximum landing mass 031 02 04 00 Effects of Overloading 031 02 04 01 Higher take-off and safety speeds Explain the influence of the aeroplane mass on takeoff and safety speeds 031 02 04 02 Longer take-off and landing distances 031 02 04 03 Lower rate of climb Explain the influence of the aeroplane mass on takeoff and landing distances Explain the influence of the aeroplane mass on the rate of climb. 031 02 04 04 Influence on range and endurance Explain the influence of the aeroplane mass on the range and endurance 031 02 04 05 Decreased engine-out performance Explain the influence of the aeroplane mass on the one-engine out performance 031 02 04 06 Possible structural damage in extreme cases Explain the potential risks during a landing when the aeroplane mass limits are greatly exceeded Issue 1: October 1999 031-MB-5 CJAA Licensing Division

JAR-FCL 031 03 00 00 CENTRE OF GRAVITY (C.G) 031 03 01 00 Basis of C.G. Calculations 031 03 01 01 Datum AIRLINE TRANSPORT PILOTS LICENCE (A) Explain the term datum. Find the datum position from an aeroplane operating manual for calculation purposes. 031 03 01 02 Moment arm Explain the moment arm and its algebraic sign. Extract moment arms for different loading positions from aeroplane operating manual 031 03 01 03 Moment Explain the term moment and calculate examples. Explain the term index and interpret an example of an index formula. Calculate the index with given weight, centre of gravity and index formula and vice versa 031 03 01 04 Expression in percentage of mean aerodynamic chord (% MAC) Explain the general equation for the centre of gravity. Illustrate the advantage of using % MAC as an expression for the centre of gravity location. Calculate centre of gravity positions and express them in % MAC 031 03 02 00 Calculation of C.G. 031 03 02 01 Centre of gravity at empty mass Calculate the aeroplane centre of gravity from scale readings at weighing. Find the centre of gravity at the dry operating mass from the aeroplane manual. 031 03 02 02 Movement of C.G with addition of fuel, load and ballast Issue 1: October 1999 031-MB-6 CJAA Licensing Division

JAR-FCL AIRLINE TRANSPORT PILOTS LICENCE (A) Calculate the effect of shifting loads or additional loads on the centre of gravity. Describe the influence of fuel loading or usage on the centre of gravity. Extract the data for the influence of fuel on the centre of gravity from an aeroplane operating manual. 031 03 02 03 Practical methods of calculation 031 03 03 00 Securing of Load Calculate zero fuel, takeoff and landing masses, the respective moments and centre of gravity positions with the aid of various types of mass and balance documentations Explain the differences between operational and certified limits for the centre of gravity. State where the certified and where the operational limits can be found and extract them 031 03 03 01 Importance of adequate tie-down Mass and balance documents of various Aircraft types. Describe the reasons why loads in cabin and cargo rooms have to be secured or tied down. State that cargo aeroplanes use pallets or containers to secure the load 031 03 03 02 Effect of loadshift Effect of Loadshift See 031 03 02 02 031 03 04 00 Area Load, Running Load, Supporting See 031 01 02 02 Issue 1: October 1999 031-MB-7 CJAA Licensing Division