Flight planning · Section IV

Starship Cruise Calculator

Beechcraft Starship Model 2000 · POH cruise tables · 1600 RPM

Flight conditions

ISA temperature−4.8 °C
ISA deviation−5.2 °C

Adjust the inputs, then calculate to display performance.

ISA temperature is derived from pressure altitude; ISA deviation = OAT − ISA temperature. Both are displayed for reference—the calculator uses OAT-derived ISA deviation for the POH table interpolation.

Calculated performance

Not calculated
Indicated airspeed
—
KIAS · knots indicated airspeed
Torque setting
—
percent
Fuel flow per engine
—
lb/hr per engine
Total fuel flow
—
lb/hr · both engines
POH engine speed
1600
RPM · published tables
Enter flight conditions and calculate. Results will appear here.
Interpolation: altitude first, then weight, then ISA deviation, matching the workbook's interpolation order. Values are linearly interpolated between bracketing published POH points. The calculator does not extrapolate beyond the available data.
In sim fuel indications MAY underread from calculated by around 10% due to a limitation in the current version of the Starship. As I have reported previously, you'll find that actual fuel burn over time matches book values very, very closely.
Source: Beechcraft Starship Model 2000 Pilot’s Operating Handbook, Section IV — Flight Planning Data. Data is embedded locally in this page; no network connection is required.
Operational note: This is a flight-planning aid based on published cruise-table data, not a replacement for the current approved POH or operating procedures. Engine anti-ice corrections are not automatically applied; the workbook's POH note states that with engine anti-ice ON, torque decreases, fuel flow increases by 10 lb/hr per engine, and TAS decreases approximately 10 kt.