INTRODUCTION
MODEL 560
Residual Ice: That ice which is not completely removed from the leading edge of
the wing and horizontal stabilizer by the surface anti-ice/deice
system during operation in icing conditions. Refer to Sections II
and IV of the airplane flight manual for applicable procedures.
Reverse Thrust: The thrust produced when the thrust reverser deflectors are
deployed into the engine exhaust stream.
RH: Right Hand
RMI: Radio Magnetic Indicator
RNAV: Area Navigation
RPM: Revolutions-per-Minute.
R/T: Receiver Transmitter
SAT: Static Air Temperature. The temperature of the air undisturbed by
the presence or motion of the airplane. SAT and OAT are similar
terms.
SSB: Single Side Band
Standard Empty Weight: Weight of a standard airplane including unusable fuel, full oil and full
operating fluids.
Station: A location along the airplane fuselage given in terms of distance
from the reference datum plane.
Takeoff Field Length: The Takeoff Field Length given for each combination of gross
weight, ambient temperature, altitude, wind and runway gradients is
the greatest of the following:
a. 115 percent of the two-engine horizontal takeoff distance from
start to a height of 35 feet above runway surface.
b. Accelerate-stop distance.
c. The engine-out accelerate-go distance.
No specific identification is made on the charts as to which of these
distances governs a specific case. In all cases considered by the
charts, the field length is governed by either b. or c., as the
factored two-engine takeoff distance is always shorter.
Takeoff Power: Power setting used for takeoff, limited to 5 minutes duration, not to
exceed 720°C ITT or 100.0 percent N
1
RPM.
TAS: True Airspeed. The airspeed relative to undisturbed air which is the
CAS corrected for altitude, temperature and compressibility factor.
TAT: Total Air Temperature. Air which has had its temperature increased
due to adiabatic compression caused by the speed of the airplane.
TAT and RAT are similar terms.
Temperature Compressibility Effects: An error in the indication of temperature caused by airflow over the
temperature probe. The error varies depending on altitude and
airspeed.
Tower Wind: Wind
reported
by the tower or from an FAA source, usually
measured at a height of 30 feet above the runway, used for
computation of takeoff and landing data.
I
Introduction-10 Configuration AA 56OMB-01
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