FlyBy E6B
SkyWriter Software
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Distance + Time

iOS Simulator Screen shot 2012-08-11 2.30.35 PM
Calculates the distance and time for an altitude change. Inputs are Altitude Change, Groundspeed, and Vertical Speed in Feet per minute.

Rate of Descent
iOS Simulator Screen shot 2012-08-11 2.30.52 PM
Calculates the Rate of Descent and Time required for an altitude change. Inputs are Altitude Change, Groundspeed, and Distance.

Descent Angle
iOS Simulator Screen shot 2012-08-11 2.31.21 PM
Calculates the Rate of Descent, Time, and Distance covered in a descent. Inputs are Altitude Change, Groundspeed, and Descent angle.

Feet per Nm
iOS Simulator Screen shot 2012-08-11 2.31.44 PM
Calculates the climb gradient in feet per nautical mile (Ft/Nm) given Vertical Speed in feet per minute and Groundspeed.

Feet per Nm (%)
iOS Simulator Screen shot 2012-08-11 2.32.02 PM
Calculates the climb gradient in feet per nautical mile (Ft/Nm) given Gradient in percent and Groundspeed.

Rate of Climb
iOS Simulator Screen shot 2012-08-11 2.32.47 PM
Calculates the Rate of Climb (Feet per Minute) and Gradient in percent, given a required climb gradient in Feet per Nautical Mile (Req. Grad) and Groundspeed.

SCDA (Stabilized Constant Descent Angle)
iOS Simulator Screen shot 2012-08-11 2.33.13 PM
Used to calculate a constant descent angle FAF crossing altitude if not included on an instrument approach chart.
Note: Predicated on an assumed Threshold Crossing Height of 50 feet.
Information from this calculation is for reference use only.
Any use of a higher than published FAF crossing altitude is contingent upon prior approval by ATC.

VDP (Visual Descent Point)
iOS Simulator Screen shot 2012-08-11 2.33.33 PM
Used to calculate a visual descent point when not included on an instrument approach chart. Two descent rate values are calculated. The first one (Min. RoD Fix->VDP) is the minimum rate of descent required to descend from the Fix to the MDA/VDP. The second one (RoD VDP->Rnw) is the rate of descent required from the VDP to the Runway based on the flight path angle input in line 5 (VDP->Rnw Angle) and the groundspeed. Note: Information from this calculation is for reference use only.