#1. The total mass of an aircraft is 3700 Kg and its C of G is at 70 inches aft of datum. How much mass must be removed from a cargo hold at 250 inches aft of datum, in order to move the C of G to its forward limit of 40 inches forward of datum?
#2. An aircraft of 12000 Kg mass has its C of G 87 inches aft of datum. What would be the new C of G position after a load of 750 Kg was removed from a hold located at 45 inches aft of datum?
#3. An aircraft loaded to a total mass of 250000 Kg is calculated to have its rear limit. How much mass must be added to a hold at -325 inches, in order to move the C of G to the rear limit at +250 inches?
#4. An aircraft of 25000 Kg mass has its C of G 80 inches aft of datum. What would be the crew C of G position after a load of 5000 Kg was removed from a hold located at 45 inches aft of datum?
#5. How much mass must be added to a hold at -150 inches, in order to move the C of G of a 52900 Kg aircraft 120 inches forward from its initial position of +515 inches.
#6. An aircraft of 125000 Kg mass has its C of G 80 inches aft of datum. What would be the new C of G position after a load of 7500 Kg was removed from a hold located at 45 inches forward of datum?
#7. The total mass of an aircraft is 3700 Kg and its C of G is 70 inches aft of datum. How much mass must be removed from a cargo hold at 250 inches aft of datum, in order to move the C of G to its forward limit of 40 inches aft of datum?
#8. An aircraft of 25000 Kg mass has its C of G 80 inches aft of datum. What would be the new C of G position after a load of 5000 Kg was removed from a hold located at 45 inches forward of datum?
#9. An aircraft loaded to a total mass of 55000 Kg is calculated to have its C of G located 72 inches aft of its rear limit. How much mass must be added to a hold at -300 inches, in order to move the C of G to the rear limit at +200 inches?
#10. An aircraft of 125000 Kg mass has its C of G 80 inches forward of datum. What would be the new C of G position after a load of 7500 Kg was removed from a hold located at 45 inches aft of datum?
#11. The total mass of an aircraft is 35700 Kg and its C of G is at 170 inches aft of datum. How much mass must be removed from a cargo hold at 255 inches aft of datum, in order to move the C of G to its forward limit of 45 inches aft of datum?
#12. An aircraft of 25000 kg mass has its C of 80 inches forward of datum. What would be the new C of G position after a load of 8500 Kg was added to a hold located at 45 inches forward of datum?
#13. How much mass must be added to a hold at +150 inches, in order to move the C of G of a 52900 Kg aircraft 120 inches forward from its initial position of +515 inches.
#14. An aircraft of 155000 Kg mass has its C of G 80 inches forward of datum. What would be the new C of G position after a load of 7000 Kg was added to a hold located at 45 inches forward of datum?
#15. An aircraft loaded to a total mass of 95000 Kg is calculated to have its C of G located 72 inches aft of its rear limit. How much mass must be added to a hold at -300 inches, in order to move the C of G to the rear limit at +200 inches?
#16. An aircraft of 75000 Kg mass has its C of G 80 inches aft of datum. What would be the new C of G position after a load of 3500 Kg was removed from a hold located at 45 inches forward of datum?
#17. How much freight must be removed from a hold 30 inches aft of the datum in order to move the C of G of a 112000 Ib aircraft from 22.62 inches aft of datum to 20 inches aft of datum?
#18. An aircraft of 225000 Kg mass has its C of G 80 inches forward of datum. What would be the new C of G position after a load of 17500 Kg was removed from a hold located at 45 inches aft of datum?
#19. An aircraft loaded to a total mass of 125000 Kg is calculated to have its C of G located 72 inches aft of its rear limit. How much mass must be added to a hold at -300 inches, in order to move the C of G to the rear limit at +200 inches?
#20. An aircraft of 125000 Kg mass has its C of G 98 inches aft of datum. What would be the new C of G position after a load of 7500 Kg was removed from a hold located at 45 inches forward of datum?
#21. An aircraft of total mass 120000 Ib has its C of G 22.75 inches aft of datum. How much freight must be added to a hold 720 inches aft of datum in order to move the C of G to 25 inches aft of datum?
#22. An aircraft of 12500 Kg mass has its C of G 50 inches aft of datum. What would be the new C of G position after a load of 750 Kg was removed from a hold located at 45 inches aft of datum?
#23. The total mass of an aircraft is 7000 Kg and its C of G is at 35 inches aft of datum. How much mass must be removed from a cargo hold at 125 inches aft of datum, in order to move the C of G to its forward limit of 33 inches aft of datum?
#24. An aircraft of 95000 Kg mass has its C of G 80 inches aft of datum. What would be the new C of G position after a load of 11500 Kg was removed from a hold located at 45 inches aft of datum?
#25. An aircraft loaded to a total mass of 55000 Kg is calculated to have its C of G located 57 inches aft of its rear limit. How much mass must be added to a hold at -350 inches, in order to move the C of G to the rear limit at +200 inches?
#26. An aircraft of 12000 Kg mass has its C of G 40 inches aft of datum. What would be the new C of G position after a load of 500 Kg was removed from a hold located at 45 inches aft of datum?
#27. The total mass of an aircraft is 17000 Kg and its C of G is at 45 inches aft of datum. How much mass must be removed from a cargo hold at 120 inches aft of datum, in order to move the C of G to its forward limit of 32 inches aft of datum?
#28. An aircraft of 72000 Kg mass has its C of G 50 inches aft of datum. What would be the new C of G position after a load of 500 Kg was removed from a hold located at 45 inches aft of datum?
#29. An aircraft has been loaded to a mass of 75000 Kg and C of G at 6.3 m aft of datum. It is then found that performance limited take-off mass is 73500 kg. The total mass is to be reduced by removing cargo from both the forward and rear holds. Cargo in the forward hold is of lower priority than that in the rear hold. What is the maximum amount of cargo mass that can be removed from the forward hold at 8.4 m forward of datum, without causing the C of G to move beyond the aft limit of 6.5 m aft of datum? Ignore effects of subsequent removal of cargo from the rear hold.
#30. An aircraft of 129000 Kg mass has its C of G 65 inches aft of datum. What would be the new C of G position after a load of 2500 Kg was removed from a hold located at 45 inches aft of datum?
#31. An aircraft loaded to a total mass of 75000 Kg is calculated to have its C of G located 72 inches aft of its rear limit. How much mass must be added to a hold at -350 inches, in order to move the C of G to the rear limit at +200 inches?
#32. An aircraft of 129000 Kg mass has its C of G 65 inches forward of datum. What would be the new C of G position after a load of 3500 Kg was removed from a hold located at 45 inches aft of datum?
#33. The total mass of an aircraft is 75000 Kg and its C of G is at 40 inches aft of datum. How much mass must be removed from a cargo hold at 510 inches aft of datum, in order to move the C of G to its forward limit of 25 inches forward of datum?
#34. An aircraft of 125000 Kg mass has its C of G 75 inches forward of datum. What would be the new C of G position after a load of 5500 Kg was removed from a hold located at 45 inches aft of datum?
#35. The total mass of an aircraft is 73000 Kg and its C of G is at 5 inches aft of datum. How much mass must be removed from a cargo hold at 175 inches aft of datum, in order to move the C of G to its forward limit of 3.5 inches forward of datum?
#36. An aircraft of79000 Kg mass has its C of G 65 inches forward of datum. What would be the new C of G position after a load of 4500 Kg was removed from a hold located at 45 inches aft of datum?
#37. The total mass of an aircraft is 25000 Kg and its C of G is at 15 inches aft of datum. How much mass must be removed from a cargo hold at 100 inches aft of datum, in order to move the C of G to its forward limit of 13 inches forward of datum?
#38. An aircraft of 29000 Kg mass has its C of G 65 inches forward of datum. What would be the new C of G position after a load of 500 Kg was removed from a hold located at 40 inches aft of datum?
#39. How much mass must be added to a hold at +130 inches, in order to move the C of G of a 2900 Kg aircraft 1 inch aft from its initial position of +115 inches.
#40. An aircraft of 59000 Kg mass has its C of G 45 inches forward of datum. What would be the new C of G position after a load of 3500 Kg was removed from a hold located at 45 inches forward of datum?
#41. How much mass must be removed from a hold at +130 inches in order to move the C of G of a 7500 Kg aircraft from +67 inches to +65 inches?
#42. An aircraft of 59000 Kg mass has its C of G 45 inches forward of datum. What would be the new C of G position after a load of 3500 Kg was removed from a hold located at 55 inches forward of datum?
#43. How much mass must be added to a hold at +150 inches, in order to move the C of G of a 52900 Kg aircraft 120 inches forward from its initial position of +515 inches.
#44. An aircraft of 69000 Kg mass has its C of G 65 inches forward of datum. What would be the new C of G position after a load of 3500 Kg was removed from a hold located at 45 inches aft of datum?
#45. An aircraft loaded to a total mass of 65000 Kg is calculated to have its C of G located 75 inches aft of its rear limit. How much mass must be added to a hold at -350 inches, in order to move the C of G to the rear limit at +250 inches?
#46. An aircraft of 259000 Kg mass has its C of G 150 inches forward of datum. What would be the new C of G position after a load of 9500 Kg was removed from a hold located at 45 inches aft of datum?
#47. An aircraft loaded to a total mass of 155000 Kg is calculated to have its C of G located 75 inches aft of its rear limit. How much mass must be added to a hold at -350 inches, in order to move the C of G to the rear limit at +250 inches?
#48. An aircraft loaded to a total mass of 55000 Kg is calculated to have its C of G located 72 inches aft of its rear limit. How much mass must be added to a hold at -370 inches, in order to move the C of G to the rear limit at +250 inches?
#49. An aircraft of 250000 Kg mass has its C of G 165 inches forward of datum. What would be the new C of G position after a load of 13500 Kg was added to a hold located at 145 inches aft of datum?
#50. An aircraft loaded to a total mass of 145000 Kg is calculated to have its C of G located 77 inches aft of its rear limit. How much mass must be added to a hold at -745 inches, in order to move the C of G to the rear limit at +250 inches?
#51. An aircraft of 250000 Kg mass has its C of G 165 inches forward of datum. What would be the new of C of G position after a load of 13500 Kg was added to a hold located at 145 inches forward of datum?
#52. An aircraft loaded to a total mass of 175000 Kg is calculated to have its C of G located 67 inches aft of its rear limit. How much mass must be added to a hold at -370 inches, in order to move the C of G to the rear limit at +250 inches?
#53. An aircraft of 25000 Kg mass has its C of G 160 inches forward of datum. What would be the new C of G position after a load of 1500 Kg was added to a hold located at 140 inches forward of datum?
#54. An aircraft loaded to a total mass of 55000 Kg is calculated to have its C of G located 72 inches forward of its real limit. How much mass must be removed from a hold at -370 inches, in order to move the C of G to the rear limit at +250 inches?
#55. An aircraft of 200000 Kg mass has its C of G 175 inches forward of datum. What would be the new C of G position after a load of 17500 Kg was added to a hold located at 145 inches aft of datum?
#56. An aircraft loaded to a total mass of 155000 Kg is calculated to have its C of G located 72 inches forward of its rear limit. How much mass must be removed from a hold at -370 inches, in order to move the C of G to the rear limit at +250 inches?
#57. An aircraft loaded to a total mass of 155000 Kg is calculated to have its C of G located 72 inches forward of its rear limit. How much mass must be removed from a hold at -370 inches, in order to move the C of G to the rear limit at +250 inches?
#58. An aircraft of 85000 Kg mass as its C of G 165 inches forward of datum. What would be the new C of G position after a load of 1000 Kg was added to a hold located at 145 inches aft of datum?
#59. An aircraft of 7900 Kg mass has its C of G 82 inches aft of datum. What would be the new C of G position after a load of 250 Kg was added 35 inches aft of datum?
#60. An aircraft of 12500 Kg mass has its C of G 16 inches forward of datum. What would be the new C of G position after a load of 500 Kg was added to a hold located at 14 inches aft of datum?
#61. An aircraft loaded to a total mass of 95000 Kg is calculated to have its C of G located 75 inches forward of its rear limit. How much mass must be removed from a hold at -370 inches, in order to move the C of G to the rear limit at +250 inches?
#62. An aircraft of 27000 Kg mass has its C of G 26.5 inches forward of datum. What would be the new C of G position after a load of 1500 Kg was added to a hold located at 14.5 inches aft of datum?
#63. An aircraft of 9900 Kg mass has its C of G 85 inches aft of datum. What would be the new C of G position after a load of 250 Kg was added 35 inches aft of datum?
#64. An aircraft of 55000 Kg mass has its C of G 65 inches aft of datum. What would be the new C of G position after a load of 4500 Kg was removed from a hold located at 49 inches aft of datum?
#65. An aircraft loaded to a total mass of 35000 Kg is calculated to have its C of G located 72 inches forward of its rear limit. How much mass must be removed from a hold at -300 inches, in order to move the C of G to the rear limit at +250 inches?
#66. An aircraft of 250000 Kg mass has its C of G 265 inches forward of datum. What would be the new C of G position after a load of 23500 Kg was added to a hold located at 145 inches aft of datum?
#67. An aircraft of 8900 Kg mass has its C of G 80 inches aft of datum. What would be the new C of G position after a load of 250 Kg was added 45 inches aft of datum?
#68. An aircraft of 235000 Kg mass has its C of G 165 inches forward of datum. What would be the new C of G position after a load of 33500 Kg was removed from a hold located at 145 inches aft of datum?
#69. An aircraft loaded to a total mass of 55000 Kg is calculated to have its C of G located 70 inches forward of its rear limit. How much mass must be removed from a hold at -370 inches, in order to move the C of G to the rear limit at +270 inches?
#70. An aircraft of 125000 Kg mass has its C of G 97 inches forward of datum. What would be the new C of G position after a load of 3500 Kg was added to a hold located at 75 inches aft of datum?
#71. An aircraft of 10900 Kg mass has its C of G 80 inches aft of datum. What would be the new C of G position after a load of 250 Kg was added 55 inches aft of datum?
#72. An aircraft of 172000 Kg mass has its C of G 165 inches forward of datum. What would be the new C of G position after a load of 23500 Kg was added to a hold located at 145 inches aft of datum?
#73. An aircraft loaded to a total mass of 155000 Kg is calculated to have its C of G located 97 inches forward of its rear limit. How much mass must be removed from a hold at -370 inches, in order to move the C of G to the rear limit at +250 inches?
#74. An aircraft of 50000 Kg mass has its C of G inches forward of datum. What would be the new C of G position after a load of 1350 Kg was added to a hold located at 45 inches aft of datum?
#75. An aircraft of 25000 Kg mass has its C of G 80 inches aft of datum. What would be the new C of G position after a load of 2500 Kg was added 45 inches aft of datum?
#76. An aircraft of 9500 Kg mass has its C of G 16 inches forward of datum. What would be the new C of G position after a load of 135 Kg was added to a hold located at 14 inches aft of datum?
#77. An aircraft of 125000 Kg mass has its C of G 380 inches aft of datum. What would be the new C of G position after a load of 2500 Kg was added 450 inches aft of datum?
#78. An aircraft of 50000 Kg mass has its C of G 95 inches aft of datum. What would be the new C of G position after a load of 7000 Kg was added to a hold located at 37 inches forward of datum?
#79. An aircraft of 25000 Kg mass has its C of G 80 inches aft of datum. What would be the new C of G position after a load of 2500 Kg was added 45 inches aft of datum?
#80. An aircraft of 25000 Kg mass has its C of G 35 inches forward of datum. What would be the new C of G position after a load of 500 Kg was added to a hold located at 14.5 inches aft of datum?
#81. An aircraft of 25000 Kg mass has its C of G 80 inches aft of datum. What would be the new C of G position after a load of 2500 Kg was removed from a hold located at 45 inches aft of datum?
#82. An aircraft of 125000 Kg mass has its C of G 80 inches aft of datum. What would be the new C of G position after a load of 7500 Kg was removed from a hold located at 45 inches aft of datum?
#83. An aircraft has been loaded to a total mass of 53000 Kg with a C of G 45 inches aft of datum. What is the maximum mass that can be added to a hold 750 inches forward of datum if the C of G limits are +10 inches to +40 inches?
#84. An aircraft has been loaded to a total mass of 150000 Kg with a C of G 100 inches aft of datum. What is the maximum mass that can be added to a hold 750 inches forward of datum if the C of G limits are +10 inches to +75 inches?
#85. An aircraft has been loaded to a total mass of 53000 Kg with a C of G 45 inches forward of datum. What is the minimum load change that must be made to a hold 750 inches forward of datum if the C of G limits are +10 inches to +40 inches?
#86. An aircraft has been loaded to a total mass of 93000 Kg with a C of G 95 inches forward of datum. How much freight must be removed from a hold 375 inches forward of datum if the C of G limits are +10 inches to +60 inches?
#87. An aircraft has been loaded to a total mass of 73000 Kg with a C of G inches aft of datum. What is the maximum load that can be removed from a hold 750 inches forward of datum if the C of G limits are +10 inches to +40 inches?
#88. An aircraft has been loaded to a total mass of 45000 Kg with a C of G 25 inches aft of datum. What is the maximum load that can be added to a hold 750 inches forward of datum if the C of G limits are +10 inches to +40 inches?
#89. The total mass of an aircraft is 13700 Kg and its C of G is at 70 inches aft of datum. How much mass must be removed from a cargo hold at 250 inches aft of datum, in order to move the C of G to its forward limit of 40 inches forward of datum?
#90. An aircraft of 82000 Kg mass has its C of G 80 inches aft of datum. What would be the new C of G position after a load of 750 Kg was removed from a hold located at 45 inches aft of datum?
#91. An aircraft loaded to a total mass of 175000 Kg is calculated to have its C of G located 70 inches aft of its rear limit. How much mass must be added to a hold at -325 inches, in order to move the C of G to the rear limit at +250 inches?
#92. An aircraft of 312000 Kg mass has its C of G 85 inches aft of datum. What would be the new C of G position after a load of 2750 Kg was removed from a hold located at 45 inches aft of datum?
#93. An aircraft loaded to a total mass of 50000 Kg is calculated to have its C of G located 75 inches aft of its rear limit. How much mass must be added to a hold at -325 inches, in order to move the C of G to the rear limit at +250 inches?
#94. An aircraft of 19200 Kg mass has its C of G 87 inches aft of datum. What would be the new C of G position after a load of 3700 Kg was removed from a hold located at 45 inches aft of datum?
#95. An aircraft loaded to a total mass of 43000 Kg is calculated to have its C of G located 70 inches aft of its rear limit. How much mass must be added to a hold at -325 inches, in order to move the C of G to the rear limit at +250 inches?
#96. An aircraft of 178000 Kg mass has its C of G 75 inches aft of datum. What would be the new C of G position after a load of 3700 Kg was removed from a hold located at 45 inches aft of datum?
#97. An aircraft of 92500 Kg mass has its C of G 83 inches forward of datum. What would be the new C of G position after a load of 3900 Kg was removed from a hold located at 49 inches forward of datum?
#98. An aircraft of 92500 Kg mass has its C of G 83 inches forward of datum. What would be the new C of G position after a load of 3900 Kg was added to a hold located at 49 inches forward of datum?
#99. An aircraft of 67000 Kg mass has its C of G 58 inches forward of datum. What would be the new C of G position after a load of 5390 Kg was removed from a hold located at 49 inches forward of datum?
#100. An aircraft of 392500 Kg mass has its C of G 183 inches forward of datum. What would be the new C of G position after a load of 19500 Kg was removed from a hold located at 149 inches forward of datum?
#101. The total mass of an aircraft is 3700 Kg and its C of G is at 70 inches aft of datum. How much mass must be removed from a cargo hold at 250 inches aft of datum, in order to move the C of G to its forward limit of 40 inches forward of datum?
#102. An aircraft of 69000 Kg mass has its C of G 65 inches forward of datum. What would be the new C of G position after a load of 3500 Kg was removed from a hold located at 45 inches aft of datum?
#103. An aircraft loaded to a total mass of 65000 Kg is calculated to have its C of G located 75 inches aft of its rear limit. How much mass must be added to a hold at -350 inches, in order to move the C of G to the rear limit at +250 inches?
#104. An aircraft of total mass 120000 Ib has its C of G 22.75 inches aft of datum. How much freight must be added to a hold 720 inches aft of datum in order to move the C of G to 25 inches aft of datum?
