Formulas Flashcards

1
Q

Mass and Balance

A
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2
Q

Dry/Empty Operating Mass(D/EOM)

A

BEM + Variable Load = DOM

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3
Q

Operating Mass (OM)

A

DOM + TOF = OM
BEM + VL(variable load) + TOF = OM

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4
Q

Zero Fuel Mass(ZFM)

A

DOM + TL(traffic load) = ZFM
BEM + VL + TL = ZFM

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5
Q

Take-Off Fuel(TOF)

A

Block Fuel - Start Fuel = TOF

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6
Q

Landing Fuel

A

Take Off Fuel - Trip Fuel = Landing Fuel

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7
Q

1-Total Moment About Datum
2-CG Pos Relative To Datum

A

1- M x D = Total Moment
With multiple : (M1 x d1) + (M2 x d2) = Total Moment
2-CG Pos = Total Moment/Total Mass

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8
Q

MAC :
1-What are the A, C and D distances
2-what is the formula for calculating MAC

A

1-A-Distance from Datum to CG
C-Distance from Datum to LeMAC
D-Length of MAC
2-(A-C)/D x 100 = %MAC

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9
Q

Floor Loading

A

FL = Max Weight On Floor/Area On Floor

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10
Q

Load Shifting

A

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

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11
Q

Traffic Load

A

TL = MZFM - DOM
TL = MTOM - (DOM + Fuel at TO)
TL = MLM - (DOM + Fuel at Landing)

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12
Q

Flight Planning

A
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13
Q

Point Of Equal Time

A

PET = GSH / (GSO + GSH) x Total Distance

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14
Q

Steps to solve PET

A

-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

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15
Q

Critical Point

A

CP Dist(nm) = RGSH / (RGSO + RGSH) x Total Distance

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16
Q

Steps to solve CP

A

-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

17
Q

Point Of No (Safe) Return (PNR/PSR)

A

PNR Time = GSR / (GSO+GSH) x Safe endurance

18
Q

Steps to solve PNR/PSR

A

-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

19
Q

Performance Related PNR

A

PNR Dist = Safe endurance in kg / (kg/gnm Out + kg/gnm Return)

Reserve fuel:
(total volume of fuel x 100) / (100 + X%)
X=%endurance

20
Q

Range and Endurance

A

GNM = ANM x (GS/TAS)

21
Q

Basic Performance

A

1- TAS/Fuel Flow = performance(ANM/KG)
2- GS/Fuel Flow = performance(GNM/KG)

22
Q

Rate and Angle of Climb

A

Climb Gradient = Height Gained / Distance Travelled
Climb Angle = RoC(fpm) / Speed(kts)

23
Q

Climb Calculations

A

GNM = ANM + ( (Time x Wind) / 60)

24
Q

Climb and Cruise
Construction of the Drift down Profile

A

Dist(nm) = (Height interval(ft) / %gradient) x 100

25
Q

Performance Related PNR

A

PNR Dist=Safe endurance in kg / (Kg/GNM Out + Kg/GNM Return)

26
Q

Structural Limitations

A

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

27
Q

Operating Mass

A

DOM + TOF = OM
BEM + VL + TOF = OM

28
Q

Zero Fuel Mass

A

DOM + TL = ZFM
BEM + VL + TL = ZFM

29
Q

Climbing
%Gradient
Time
Distance

A

%Gradient = ROC/GS x 100
Time = Height Gain/ROC
Dist = GS x Time

30
Q

Drift Down Profile

A

Dist(nm) = Height Interval(ft) / %Gradient x 100