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
Steps to solve CP
-Draw sketch noting direction of arrows
-Calculate Reduced GSO and RGSH for each leg
-Apply formula to calculate distance to CP
-Apply leg time function on pathfinder to FULL TAS to calculate the FULL GS and then calculate time to CP
Point Of No (Safe) Return (PNR/PSR)
PNR Time = GSR / (GSO+GSH) x Safe endurance
Steps to solve PNR/PSR
-Draw sketch noting direction of arrows
-Calculate GSO and GSH for each leg
-Apply formula to calculate the time to PNR
-Apply distance function on pathfinder to calculate distance to PNR
Performance Related PNR
PNR Dist = Safe endurance in kg / (kg/gnm Out + kg/gnm Return)
Reserve fuel:
(total volume of fuel x 100) / (100 + X%)
X=%endurance
Range and Endurance
GNM = ANM x (GS/TAS)
Basic Performance
1- TAS/Fuel Flow = performance(ANM/KG)
2- GS/Fuel Flow = performance(GNM/KG)
Rate and Angle of Climb
Climb Gradient = Height Gained / Distance Travelled
Climb Angle = RoC(fpm) / Speed(kts)
Climb Calculations
GNM = ANM + ( (Time x Wind) / 60)
Climb and Cruise
Construction of the Drift down Profile
Dist(nm) = (Height interval(ft) / %gradient) x 100
Performance Related PNR
PNR Dist=Safe endurance in kg / (Kg/GNM Out + Kg/GNM Return)
Structural Limitations
1-BEM
2-BEM + Crew and Special Equipment
=DOM
3-BEM + CSE + TL
=Zero Fuel Mass
4-BEM + CSE + TL + Fuel, start and taxi
=Ramp Mass
5-BEM + CSE + TL + Fuel
=Take Off Mass
Operating Mass
DOM + TOF = OM
BEM + VL + TOF = OM
Zero Fuel Mass
DOM + TL = ZFM
BEM + VL + TL = ZFM
Climbing
%Gradient
Time
Distance
%Gradient = ROC/GS x 100
Time = Height Gain/ROC
Dist = GS x Time
Drift Down Profile
Dist(nm) = Height Interval(ft) / %Gradient x 100