aircraft loading Flashcards
1
Q
main forces of aircraft
A
thrust, lift, weight, drag, tail load, center of gravity
2
Q
ultimate design load equation
A
UTL = Limit design load * factor of safety (1.5)
3
Q
factor of safety far code
A
FAR 25.303
4
Q
factor of safety constant
A
1.5
5
Q
ultimate factor of safety equation
A
UFS = ultimate load / limit load
6
Q
Limit MOS equation
A
Limit MOS = (tested limit load - limit load) / limit load
7
Q
Ultimate MOS equation
A
ulti MOS = (tested ulti load - ulti load) / ulti load
8
Q
design limit equation
A
design limit = n limit * weight
9
Q
n values for civil transport and fighter jets
A
civil : 3 - 4
fighter: 6.5 - 9
