Position Points Flashcards

1
Q

What is the definition of equitime point (ETP)?

A

POINT where it takes EQUAL TIME to fly to either a PAIR of ALTERNATES UNDER a given set of CONDITIONS;
The pair of ALTERNATES MAY or MAY NOT on TRACK

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2
Q

Why do we calculate ETP?

A

Allows us to QUICKLY DECIDE which of chose ALTERNATE airfields is CLOSEST in TIME if there is any NON-NORMAL CONDITIONS

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3
Q

When may ETPs become essential?

A

ENGINE FAILURE;
DEPRESSURISATION;
MAJOUR SYSTEM FAILURE;
ILLNESS ON BOARD

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4
Q

What does the term ground speed OUT refer to?

A

GROUND SPEED at which the aircraft TRAVELLED TO the POINT at which EVENT TOOK PLACE

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5
Q

What does the term ground speed ON refer to?

A

The GROUND SPEED to PROCEED to the DESTINATION at the TAS and the WINDS at revised altitude (if any) under NON-NORMAL CONDITIONS

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6
Q

What does the term ground speed HOME refer to?

A

The GROUND SPEED to travel BACK to the DEPARTURE aerodrome at the TAS and the WINDS at revised altitude (if any) under NON-NORMAL CONDITIONS

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7
Q

What ground speeds do we use to calculate distance to ETP?

A

Both ground speed ON and HOME;

NON-NORMAL CONDITIONS are used

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8
Q

What ground speeds do we use to calculate time to ETP?

A

Ground speed OUT;

NORMAL CONDITIONS are used

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9
Q

What may ETO also be referred to as?

A

CRITICAL POINT;

POINT OF EQUAL TIME (PET)

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10
Q

What are the points and distances represented in ETP?

What do they mean?

A
D - Total distance;
X - Distance from CP to A;
D-X - Distance from CP to B;
H - Ground speed HOME from CP;
O - Ground speed ON from CP
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11
Q

What is the formula that represents ETP?

A

X = D x H / O + H

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12
Q

What is the formula that represents ETP time?

A

T = X / G/S OUT

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13
Q

What does ETP(N) represent?

A

All engine ETP

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14
Q

What does ETP(1) represent?

A

SINGLE engine FAILURE on a TWIN engine aircraft ETP

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15
Q

What does ETP(3) represent?

A

SINGLE engine FAILURE on a 4 engine aircraft

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16
Q

What does ETP(D) represent?

A

DEPRESSURISATION FAILURE ETP

17
Q

What does ETP(1D) represent?

A

ONE engine DEPRESSURISATION on a TWIN engine aircraft

18
Q

What does ETP(3D) represent

A

ONE engine DEPRESSURISATION on a 4 engine aircraft ETP

19
Q

How much fuel should an aircraft ideally carry?

Is this practical? Why or why not?

A

SUFFICIENT FUEL for a RETURN flight from DESTINATION TO DEPARTURE aerodrome;
NO, in order TO CARRY more fuel, more fuel must be BURNED, it also REDUCES commercially valuable PAYLOAD, CHANCE of DIVERSION is LOW

20
Q

What is the definition of point of no return (PNR)?

A

The MAXIMUM DISTANCE outboard an aircraft can travel EN-ROUTE and RETURN to the DEPARTURE aerodrome, ARRIVING overhead with specified FUEL RESERVES WITHIN the constraints of its SAFE ENDURANCE

21
Q

When must PNR be calculated?

A

When an ISOLATED DESTINATION aerodrome has NO SUITABLE ALTERNATES for the aircraft to DIVERT to in case it is NO LONGER FEASIBLE to land at DESTINATION

22
Q

When are PNRs essential?

A

MARGINAL WEATHER at DESTINATION;
ENGINE FAILURE;
DEPRESSURISATION;
ILLNESS ON BOARD

23
Q

What does it mean if you have crossed your PNR?

A

You are COMMITTED to LANDING at that aerodrome

24
Q

What are the points and distances represented in PNR?

What do they mean?

A
E - (Fuel on board / fuel flow) - (mandatory reserves / fuel flow);
O - Ground speed OUT;
H - Ground speed HOME;
D - Distance to PNR;
T - Time to PNR
25
Q

What is the formula that represents PNR?

A

D = E x O x H / O + H

26
Q

What is the formula that represents PNR time?

A

T = E x H / O + H

27
Q

What effect does wind, fuel and speed have on PNR?

A

NIL WIND: Gives MAXIMUM PNR DP;
ANY WIND: Reduces the PNR DP;
MORE FUEL: INCREASES PNR DP;
GREATER SPEED: INCREASES PNR DP (when all other factors are constant)

28
Q

What is the definition of point of safe return (PSR)?

A

.

29
Q

What is the definition of last point of diversion?

A

A PNR DO calculated to ARRIVE over the LAST EN-ROUTE ALTERNATE available with FUEL EQUAL to the specified RESERVES

30
Q

What is the derived formula for PNR including the wind factor?

A

D = (E x TAS / 2) - (E x W^2 / 2 x TAS)