GroundBound
29th Aug 2005, 13:46
I came across this description of approach speed considerations in documentation intended for budding ATCOs.
The ground speed on final approach will be affected by the following factors:
Aircraft mass -
As aircraft mass increases, more lift is required to balance the weight. The minimum speed at which the required lift can be achieved will be higher when the aircraft has a greater mass (already explained with the flight envelope). Thus the airspeed on final approach depends on aircraft mass, that is, an aircraft is expected to fly with higher airspeed on final approach when its mass is greater (minimum speed increases with aircraft mass).
This could be understood as a heavier B747 will have a higher approach speed than a lighter B747.
Does the approach speed within a given aircraft type differ depending on its weight/mass? I wouldn't have thought so, but then I'm not qulified on such types.
I can understand the stall speed will increase with weight, but I thought the approach speed would have sufficient margin above the stall speed that the weight/mass differences would not have any significant effect.
Any clarifications would be greatly received?
GB
The ground speed on final approach will be affected by the following factors:
Aircraft mass -
As aircraft mass increases, more lift is required to balance the weight. The minimum speed at which the required lift can be achieved will be higher when the aircraft has a greater mass (already explained with the flight envelope). Thus the airspeed on final approach depends on aircraft mass, that is, an aircraft is expected to fly with higher airspeed on final approach when its mass is greater (minimum speed increases with aircraft mass).
This could be understood as a heavier B747 will have a higher approach speed than a lighter B747.
Does the approach speed within a given aircraft type differ depending on its weight/mass? I wouldn't have thought so, but then I'm not qulified on such types.
I can understand the stall speed will increase with weight, but I thought the approach speed would have sufficient margin above the stall speed that the weight/mass differences would not have any significant effect.
Any clarifications would be greatly received?
GB