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16 Cards in this Set

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Gradient formula

Pitch change * 100 or ft/NM

Pitch Change

100's of feet/NM

VVI (fpm)

ft/NM * NM/Min

TAS=

IAS + (2% per 1000') x IAS


or


IAS + FL/2

NM/Min to Mach

NM/MIN = IMN x 10

VVI for 3 deg Glide Slope

GS x 5

Distance to station (DME)

(TAS x MIN) / Radials

Time to station in minutes

sec / radials

VDP (NM)

HAT / 300



Assumes 3 deg glide slope

VDP (Sec)

10% of HAT. Subtract this from timing.



Assumes 120kts

Turn Radius=


(Mach)

IMN x 10 - 2.



Assumes 90 deg turn

Turn Radius=


(NM/MIN)

NM/MIN -2

Distance for turns other than 90 deg.

180 deg = 2 x TR


120 deg=1 1/2 x TR


90 deg = 1 x TR


60 deg = 1/2 x TR

Radar tilt and altitude given. How to determine tops of thunderstorm?

Distance x Tilt x 100 + current altitude = Tops

Speed of sound change per deg C ?

1.2 kts

Holding Speeds for given altitudes ?

MHA - 6,000 : 200kts


6,001 - 14,000 : 230kts


14,001and above : 265kts (IAS and MSL)