Formulas Flashcards
Mass and Balance
Dry/Empty Operating Mass(D/EOM)
BEM + Variable Load = DOM
Operating Mass (OM)
DOM + TOF = OM
BEM + VL(variable load) + TOF = OM
Zero Fuel Mass(ZFM)
DOM + TL(traffic load) = ZFM
BEM + VL + TL = ZFM
Take-Off Fuel(TOF)
Block Fuel - Start Fuel = TOF
Landing Fuel
Take Off Fuel - Trip Fuel = Landing Fuel
1-Total Moment About Datum
2-CG Pos Relative To Datum
1- M x D = Total Moment
With multiple : (M1 x d1) + (M2 x d2) = Total Moment
2-CG Pos = Total Moment/Total Mass
MAC :
1-What are the A, C and D distances
2-what is the formula for calculating MAC
1-A-Distance from Datum to CG
C-Distance from Datum to LeMAC
D-Length of MAC
2-(A-C)/D x 100 = %MAC
Floor Loading
FL = Max Weight On Floor/Area On Floor
Load Shifting
m d (CIC)
— x ———–
M M (CIA)
Where : m = Mass to be moved
M = Total mass of a/c
d(CIC/change in CG) = distance CG will move from original pos
D(CIA/Change in Arm) = greatest distance the mass m is moved/added/subtracted
Traffic Load
TL = MZFM - DOM
TL = MTOM - (DOM + Fuel at TO)
TL = MLM - (DOM + Fuel at Landing)
Flight Planning
Point Of Equal Time
PET = GSH / (GSO + GSH) x Total Distance
Steps to solve PET
-Draw sketch, taking note of direction of arrows
-Calc GSO and GSH for each leg
-Apply formula to calculate distance to PET
-Apply leg time function on pathfinder to calculate time to PET
Critical Point
CP Dist(nm) = RGSH / (RGSO + RGSH) x Total Distance