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  • FLIGHT THEORY

    ATPL(A) ANNEXES 031Rev. W

    www.flight-theory.eu

  • 031-1569 A

    031-1580 A

  • 031-2946 A

  • 031-11069-A, 11070-A, 11071-A, 11072-A, 11205-A, 11222-A,11246-A, 11247-A , 11248-A,11249-A, 11250-A, 11251-A, 11257-A,11258-A, 11273-A, 11275-A

    DATA SHEETLRJT 1

    LOAD AND TRIM SHEETLOADINGWEIGHT and BALANCE

    SEQ B

    This chart allows the determination of the aircraft CG location function of dry operating weightpantry adjustment, cargo loads. passengers and fuel on board. The operational limits shown onthe load and trim sheet are more restrictive than the certified limits because error margins havebeen taken into account. The load and trim sheet needs to be updated when:

    - a modification which changes the aircraft certified limits is included or- a modification (cabin layout, cargo arrangement..) which influences the operational limits

    is made.It is the airline's responsibility to define a load and trim sheet and to keep it up to date. Hereafteris a description of the load and trim sheet utilization in the Standard Airbus Industry format (seeexample p3) and for a typical passenger cabin arrangement. Refer to customized load and trimsheet for preparing a revenue flight.

    DATADry operating weight = 110 000 kg and CG = 31%Deviation or adjustment = + 100 kg in zone FCargo = 11 500 kg as : cargo 1=2 500 kg ; cargo 2 = 3 000 kg ;cargo 3 = 3 000 kg ; cargo 4 = 2 000 kg ; cargo 5 = 1 000 kgPassengers (75 kg/PAX) = 240 PAX with the following distribution:cabin OA - 20; cabin OB = 120 ; cabin OC = 100Fuel = 72 000 kg

    DESCRIPTIONa. Enter master data in (1).b. Compute dry operating weight index using the formula indicated in (2) and report in (3).

    Dry operating index = 119.1.c. Enter weight deviation in (4) and read corresponding index in (5): - 0.51.d. Calculate corrected index and report in (6): CORRECTED INDEX = 118.6e. Enter cargo weight and FAX number in (7).f. Enter index scale (8) with corrected index and proceed through cargo and passengers

    scales as shown in (9). Then, from the final point (cabin OC). draw a vertical line down tothe zero fuel fine (10): 139600 .kg.

    g. Check that the intersection with zero fuel line determined in table (11) is within themaximum zero fuel weight and zero fuel operational limits. If not rearrange cargo loading.

    h. Read in table 2.01.40 p5 fuel index correction.Fuel on Board : 72 000 kg.Fuel density: 0.780. Read in fuel index table FUEL INDEX = + 8.

    i. Carry in scale (12). From this point draw a vertical line down to takeoff weight line (13) at211 600 kg.

    j. Check that intersection with takeoff fine determined in table (11) is within maximumtakeoff weight and takeoff operational limits. ff not rearrange cargo loading.

    k. Read takeoff CG on CG scale (14): CG = 29.8 %.

    CAUTION

    If there is no customized trimsheet for your airline in thissection 2.01.40 do not usethe Information enclosedherein for day to dayOperation as margins andload CG vary with cabin andcargo layout.

  • 031-11069 B, 11070-B, 11071-B, 11072-B, 11205-B, 11222-B, 11246-B, 11247-B,11257-B, 11258-B

  • 031-11219 A, 031-11227 A

  • 031-11248 B, 11249-B, 11250-B, 11251-B

    WEICHT (kg)

    INDEX

    WEICHT(kg)

    DENSITY (kg/L)

    0.760 0.765 0.770 0.775 0.780 0.785 0.790 0.795 0.800 0.805 0.810 0.815 0.820 0.825 0.830

    200040006000800090001000011000120001400016000180002000022000240002600028000900003200034000360003800040000450005000055000600006400064250645006475065000652506550065750660006625066500670006800069000

    - 2- 4- 6- 3- 1

    + 2+ 4+ 6+ 4+ 2

    0- 2- 4- 6- 8- 9- 11- 13- 14- 16- 18- 19- 23- 25- 26- 26- 24- 21- 19- 16- 13- 10- 7- 5-2

    +1+3+3+4+4

    69000700007100072000722507250072750730007325073500737507400074250745007475075000752507550075750760007625076500767507700077250775007775078000782507850078750790007925079500797508000080250805008075081000

    + 7+ 8+ 9+ 10+ 12+ 15+ 18+ 20+ 23+ 26+ 29+ 32+ 35---------------------------

    + 6+ 7+ 9+ 10+ 10+ 10+ 12+ 15+ 18+ 21+ 24+ 27+ 30+ 33+ 36--------------------------

    + 6+ 7+ 8+ 9+ 9+ 10+ 10+ 10+ 13+ 15+ 18+ 21+ 24+ 27+ 30+ 33+ 36-----------------------

    + 5+ 6+ 7+ 8+ 9+ 9+ 9+ 10+ 10+ 10+ 13+ 16+ 19+ 22+ 25+ 28+ 31+ 34+ 37---------------------

    +5+ 6+ 7+ 8+ 8+ 8+ 9+ 9+.9+ 10+ 10+ 1O+ 13+ 16+ 19+ 22+ 25+28+ 31+ 34+ 37-------------------

    + 4+ 5+ 6+ 7+ 7+ 8+ 8+ 8+ 9+ 9+ 9+ 9+ 10+ 11+ 14+ 16+ 19+ 22+ 25+ 28+ 31+ 34+ 37-----------------

    + 4+ 5+ 6+ 7+ 7+ 7+ 7+ 8+ 8+ 8+ 9+ 9+ 9+ 9+ 10+ 11+ 14+ 17+ 20+ 23+ 26+ 29+ 32+ 35+ 38---------------

    + 4+ 4+ 5+ 6+ 6+ 7+7+ 7+ 7+ 8+ 8+ 8+ 8+ 9+ 9+ 9+ 10+ 11+ 14+ 17+ 20+ 23+ 26+ 29+ 32+ 35+ 38-------------

    + 3+ 4+ 5+ 5+ 6+ 6+ 6+ 6+ 7+ 7+ 7+ 8+ 8+ 8+ 8+ 9+ 9+ 9+ 10+ 12+ 15+ 18+ 20+ 23+ 26+ 29+ 32+ 35+ 38-----------

    + 3+ 3+ 4+ 5+ 5+ 5+ 6+ 6+ 6+ 6+ 7+ 7+ 7+ 7+ 8+ 8+ 8+ 9+.9+ 9+ 10+ 12+ 15+ 18+ 21+ 24+ 27+ 30+ 33+ 36+ 39---------

    + 2+ 3+ 4+ 4+ 5+ 5+ 5+ 5+ 6+ 6+ 6+ 6+ 7+ 7+ 7+ 7+ 8+ 8+ 8+ 9+ 9+ 9+ 10+ 13+ 15+ 18+ 21+ 24+ 27+ 30+ 33+ 36+ 39-------

    + 2+ 2+ 3+ 4+ 4+ 4+ 5+ 5+ 5+ 5+ 6+ 6+ 6+ 6+ 7+ 7+ 7+ 7+ 8+ 8+ 8+ 8+ 9+ 9+ 10+ 13+ 16+ 19+ 22+ 25+ 27+ 30+ 33+ 37+ 40-----

    + 1+ 2+ 3+ 3+ 4+ 4+ 4+ 4+ 4+ 5+ 5+ 5+ 5+ 6+ 6+ 6+ 6+ 7+ 7+ 7+ 8+ 8+ 8+ 8+ 9+ 9+ 10+ 13+ 16+ 19+ 22+ 25+ 28+ 31+ 34+ 37+ 40---

    + 1+

    2+ 2+ 3+ 3+ 3+ 4+ 4+ 4+ 4+ 4+ 5+ 5+ 5+ 5+ 6+ 6+ 6+ 6+ 7+ 7+ 7+ 7+ 8+ 8+ 8+ 9+ 9+ 11+ 14+ 16+ 19+ 22+ 25+ 28+ 31+ 34+ 37+ 40-

    + 1+ 1+ 2+ 3+ 3+ 3+ 3+ 3+ 3+ 4+ 4+ 4+ 4+ 5+ 5+ 5+ 5+ 6+ 6+ 6+ 6+ 7+ 7+ 7+ 7+ 8+ 8+ 8+ 9+ 9+ 11+ 14+ 17+ 20+ 23+ 26+ 29+ 32+ 35+ 38

  • 031-11248 C , 11249-C, 11250-C, 11251-C

  • 031-11273 B, 031-11275 B

  • 031-11590 A, 11605 A

    031-11634 A

    Passengers seats: 20 and moreMaleFemale

    30 and moreAll adult

    All flights exceptholiday charts

    88 kg 70 kg 84 kg

    Holiday charters 83 kg 69 kg 76 kg

    Children 35 kg 35 kg 35 kg

  • 031-12267 A, 031-12268 A

  • 031-12269 A

  • 031-12270 A, 031-12271 A

  • 031-12272 A

  • 031-12273 A, 12274 A