ED Decision 2003/18/RM
|
n1 |
= |
Aeroplane Positive Manoeuvring Limit Load Factor |
|
n2 |
= |
Aeroplane Negative Manoeuvring Limit Load Factor |
|
n3 |
= |
Aeroplane Positive Gust Limit Load Factor at VC |
|
n4 |
= |
Aeroplane Negative Gust Limit Load Factor at VC |
|
nflap |
= |
Aeroplane Positive Limit Load Factor With Flaps Fully Extended at VF |
|
*VFmin |
= |
Minimum Design Flap Speed = 4.98 |
|
*VAmin |
= |
Minimum Design Manoeuvring Speed = 6.79 |
|
*VCmin |
= |
Minimum Design Cruising Speed = 7.69 |
|
*VDmin |
= |
Minimum Design Dive Speed = 10.86 |
*Also see sub-paragraph A7(e)(2) of this Appendix.
(Speeds in knots, W in kg, S in m2.)