CP/PNR Flashcards

1
Q

What is the formula for CP?

A

Distance to CP (from HOME) =

Total Distance (between aerodrome) x Ground Speed HM
—————————————————————
Ground Speed HM+ Ground Speed ON

CP=
DIST x GSH
—————
GSH + GSO

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2
Q

What is the EPNR formula?

A

EPNR =

FFA (-1600 if BRW)
———————-
ESGR OUT + ESGR HOME

To estimate PNR don’t forget to revise FFA if fix is not overhead HOME. Use standard SGRs with allowances for EPNR.

Flight plan to EPNR

Adjust PNR accordingly.

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3
Q

What RSWT and Mach is used for 1 Engine INOP?

A

Need to find altitude capability

FL235 RSWT and LRC Mach for EMZW (approx TAS 420)

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4
Q

What RSWT and Mach is used for DEPRESSURISED?

A

FL185 RSWT and M.59

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5
Q

What effect does wind have on CP?

A

CP mostly always into wind

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6
Q

Where does the estimated CP lie?

A

Estimate CP as half way or close waypoint/subdivision into wind

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7
Q

What effect does wind have on PNR?

A

PNR farthest from departure in NIL WIND

PNR closer to departure in ANY WIND

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8
Q

What is the PNR dependant on?

A

Flight Fuel Available

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9
Q

How do you calculate Flight Fuel Available for the calculation of a PNR?

A

FFA =
FOB-taxi/shutdown (unless in flight calc), holding, fixed reserve, variable reserve (not for DP).

Revise FFA if in flight calc being made and fix not over HOME.

RFFA =
FFA - (appropriate SGR x distance from fix to HOME)

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10
Q

What would you estimate a PNR Minimum Landing Weight?

A

ELW = BRW or GW at fix - FFA

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11
Q

What information is required to calculate Depressurised Critical Point?

A
  • Total distance
  • Ground speeds ON and HOME @FL130
  • Average tracks, winds and temperatures from roughly half way ON and a HOME
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12
Q

What information is required to calculate OEI Critical Point?

A
  • Total distance
  • Ground speeds ON and HOME at hemispherical level according to GW altitude capability
  • Average track, wind and temps
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