AMC1 CAT.POL.MAB.100(b) Mass and balance, loading

• ED Decision 2014/015/R found in: Air Operations (965/2012) Part-ARO Part-ORO Part-CAT Part-SPA Part-NCC Part-NCO Part-SPO (Feb 2025)

AMC1 CAT.POL.MAB.100(b) Mass and balance, loading ED Decision 2014/015/R WEIGHING OF AN AIRCRAFT (a) New aircraft that have been weighed at the factory may be placed into operation without reweighing if the mass and balance records have been adjusted for alterations or modifications to the aircraft. Aircraft transferred from one EU operator to another EU operator do not have to be weighed prior to use by the receiving operator unless more than 4 years have elapsed since the last weighing. (b) The mass and centre of gravity (CG) position of an aircraft should be revised whenever the cumulative changes to the dry operating mass exceed ±0.5 % of the maximum landing mass or, for aeroplanes, the cumulative change in CG position exceeds 0.5 % of the mean aerodynamic chord. This may be done by weighing the aircraft or by calculation. If the AFM requires to record changes to mass and CG position below these thresholds, or to record changes in any case, and make them known to the commander, mass and CG position should be revised accordingly and made known to the commander. (c) When weighing an aircraft, normal precautions should be taken consistent with good practices such as: (1) checking for completeness of the aircraft and equipment; (2) determining that fluids are properly accounted for; (3) ensuring that the aircraft is clean; and (4) ensuring that weighing is accomplished in an enclosed building. (d) Any equipment used for weighing should be properly calibrated, zeroed, and used in accordance with the manufacturer's instructions. Each scale should be calibrated either by the manufacturer, by a civil department of weights and measures or by an appropriately authorised organisation within two years or within a time period defined by the manufacturer of the weighing equipment, whichever is less. The equipment should enable the mass of the aircraft to be established accurately. One single accuracy criterion for weighing equipment cannot be given. However, the weighing accuracy is considered satisfactory if the accuracy criteria in Table1 are met by the individual scales/cells of the weighing equipment used: Table 1 Accuracy criteria for weighing equipment <table border="1" cellpadding="0" cellspacing="0" width="568"><tr><td valign="top" width="284"><p><b>For a scale/cell load</b></p></td><td valign="top" width="284"><p><b>An accuracy of</b></p></td></tr><tr><td valign="top" width="284"><p>below 2 000 kg</p></td><td valign="top" width="284"><p>±1 %</p></td></tr><tr><td valign="top" width="284"><p>from 2 000 kg to 20 000 kg</p></td><td valign="top" width="284"><p>±20 kg</p></td></tr><tr><td valign="top" width="284"><p>above 20 000 kg</p></td><td valign="top" width="284"><p>±0.1 %</p></td></tr></table> AMC1 CAT.POL.MAB.100(b) Mass and balance, loading ED Decision 2014/015/R WEIGHING OF AN AIRCRAFT (a) New aircraft that have been weighed at the factory may be placed into operation without reweighing if the mass and balance records have been adjusted for alterations or modifications to the aircraft. Aircraft transferred from one EU operator to another EU operator do not have to be weighed prior to use by the receiving operator unless more than 4 years have elapsed since the last weighing. (b) The mass and centre of gravity (CG) position of an aircraft should be revised whenever the cumulative changes to the dry operating mass exceed ±0.5 % of the maximum landing mass or, for aeroplanes, the cumulative change in CG position exceeds 0.5 % of the mean aerodynamic chord. This may be done by weighing the aircraft or by calculation. If the AFM requires to record changes to mass and CG position below these thresholds, or to record changes in any case, and make them known to the commander, mass and CG position should be revised accordingly and made known to the commander. (c) When weighing an aircraft, normal precautions should be taken consistent with good practices such as: (1) checking for completeness of the aircraft and equipment; (2) determining that fluids are properly accounted for; (3) ensuring that the aircraft is clean; and (4) ensuring that weighing is accomplished in an enclosed building. (d) Any equipment used for weighing should be properly calibrated, zeroed, and used in accordance with the manufacturer's instructions. Each scale should be calibrated either by the manufacturer, by a civil department of weights and measures or by an appropriately authorised organisation within two years or within a time period defined by the manufacturer of the weighing equipment, whichever is less. The equipment should enable the mass of the aircraft to be established accurately. One single accuracy criterion for weighing equipment cannot be given. However, the weighing accuracy is considered satisfactory if the accuracy criteria in Table1 are met by the individual scales/cells of the weighing equipment used: Table 1 Accuracy criteria for weighing equipment <table border="1" cellpadding="0" cellspacing="0" width="568"><tr><td valign="top" width="284"><p><b>For a scale/cell load</b></p></td><td valign="top" width="284"><p><b>An accuracy of</b></p></td></tr><tr><td valign="top" width="284"><p>below 2 000 kg</p></td><td valign="top" width="284"><p>±1 %</p></td></tr><tr><td valign="top" width="284"><p>from 2 000 kg to 20 000 kg</p></td><td valign="top" width="284"><p>±20 kg</p></td></tr><tr><td valign="top" width="284"><p>above 20 000 kg</p></td><td valign="top" width="284"><p>±0.1 %</p></td></tr></table> ##### AMC1 CAT.POL.MAB.100(b) Mass and balance, loading *ED Decision 2014/015/R* **WEIGHING OF AN AIRCRAFT** (a) New aircraft that have been weighed at the factory may be placed into operation without reweighing if the mass and balance records have been adjusted for alterations or modifications to the aircraft. Aircraft transferred from one EU operator to another EU operator do not have to be weighed prior to use by the receiving operator unless more than 4 years have elapsed since the last weighing. (b) The mass and centre of gravity (CG) position of an aircraft should be revised whenever the cumulative changes to the dry operating mass exceed ±0.5 % of the maximum landing mass or, for aeroplanes, the cumulative change in CG position exceeds 0.5 % of the mean aerodynamic chord. This may be done by weighing the aircraft or by calculation. If the AFM requires to record changes to mass and CG position below these thresholds, or to record changes in any case, and make them known to the commander, mass and CG position should be revised accordingly and made known to the commander. (c) When weighing an aircraft, normal precautions should be taken consistent with good practices such as: (1) checking for completeness of the aircraft and equipment; (2) determining that fluids are properly accounted for; (3) ensuring that the aircraft is clean; and (4) ensuring that weighing is accomplished in an enclosed building. (d) Any equipment used for weighing should be properly calibrated, zeroed, and used in accordance with the manufacturer's instructions. Each scale should be calibrated either by the manufacturer, by a civil department of weights and measures or by an appropriately authorised organisation within two years or within a time period defined by the manufacturer of the weighing equipment, whichever is less. The equipment should enable the mass of the aircraft to be established accurately. One single accuracy criterion for weighing equipment cannot be given. However, the weighing accuracy is considered satisfactory if the accuracy criteria in Table1 are met by the individual scales/cells of the weighing equipment used: ***Table 1*** Accuracy criteria for weighing equipment <table bgcolor="#d9d9d9" cellpadding="7" cellspacing="0"> <col/> <col/> <tr valign="top"> <td bgcolor="#808080"><p align="center"> <b>For a scale/cell load</b></p> </td> <td bgcolor="#808080"><p align="center"> <b>An accuracy of</b></p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> below 2 000 kg</p> </td> <td bgcolor="#d9d9d9"><p align="left"> ±1 %</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> from 2 000 kg to 20 000 kg</p> </td> <td bgcolor="#d9d9d9"><p align="left"> ±20 kg</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> above 20 000 kg</p> </td> <td bgcolor="#d9d9d9"><p align="left"> ±0.1 %</p> </td> </tr> </table>