need help
simple problems but need an explanation for the following how to solve it..
1) aircraft requires headwind comp of at least 10knts and crosswind limit of 35knts. the angle between the wind direction is 60 deg. calculate maximum and min allowable wind speeds?
2) after take off you can accept upto 10knts of tail wind. the runway QDM is 047, the var is 17deg E and the atis gives wind direction 210 what is the max wind strength you can accept?
3) magnetic hdg 311 deg ,
drift 10deg left
relative bearing of NDB270
what is the magnetic bearing of NDB measured from the aircraft?