Hallo leute!
Hab eine Frage gefunden aus der JAA ATPL Question Bank.
Wer kann mir helfen, wie man auf das ergebnis kommt.
The loaded mass of the aircraft is found to be 1850 lb and the CG moment 154 000 lb in. How much mass must be moved from the forward hold 40 inches aft of the datum, to the rear hold, 158 inches aft of the datum, to bring the CG on to the forward limit? CG limits are 86 inches fwd and 90 inches aft.
A) 23.1 lb
B) 50.9 lb
C) 43.2 lb
D) 66.0 lb
Hab eine Frage gefunden aus der JAA ATPL Question Bank.
Wer kann mir helfen, wie man auf das ergebnis kommt.
The loaded mass of the aircraft is found to be 1850 lb and the CG moment 154 000 lb in. How much mass must be moved from the forward hold 40 inches aft of the datum, to the rear hold, 158 inches aft of the datum, to bring the CG on to the forward limit? CG limits are 86 inches fwd and 90 inches aft.
A) 23.1 lb
B) 50.9 lb
C) 43.2 lb
D) 66.0 lb
