TM 1-1510-223-10
APPENDIX B
ABBREVIATIONS AND TERMS
For the purpose of this manual, the following abbreviations and terms apply. See appropriate technical manuals for
additional terms and abbreviations.
B-1. AIRSPEED TERMINOLOGY.
Vfe
Maximum flap extended
CAS
Calibrated airspeed is indi-
speed is the highest speed
cated airspeed corrected for
permissible with wing flaps
position and instrument error.
a prescribed extended posi-
tion.
GS
Ground speed is the speed of Vle
Maximum landing gear
the aircraft relative to the
extended speed is the maxi-
ground.
mum speed at which an air-
craft can be safely flown with
lAS
Indicated airspeed is the
the landing gear extended.
speed as shown on the air-
.
no instrument error.
Vlo
Maximum landing gear oper-
ating speed is the maximum
KT
Knots.
speed at which the landing
gear can be safely extended or
M
Mach number. The ratio of
retracted.
true airspeed to the speed of
sound.
Vmca
The minimum flight speed at
which the aircraft is direction-
Mmo
Maximum operating Mach
ally controllable as deter-
number.
mined in accordance with
TAS
True airspeed is calibrated
Federal Aviation Regulations.
airspeed corrected for alti-
Aircraft Certification condi-
tude, temperature, pressure,
tions include one engine
and compressibility effects.
becoming inoperative and
propeller feathered; up to a 5°
V1
Takeoff decision speed
bank toward the operative
engine; takeoff power on
V50
Takeoff safety speed is the
operative engine; landing gear
speed at 50 feet AGL (35 feet
up; flaps up, and most rear-
AGL with one engine inoper-
ward CG. This speed has
ative).
been demonstrated to provide
Va
Maneuvering speed is the
satisfactory control above
maximum speed at which
power off stall speed (which
application of full available
varies with weight, configura-
aerodynamic control will not
tion, and flight attitude).
overstress the aircraft.
Vmo
Maximum operating limit
Venr
One engine inoperative
speed.
enroute climb speed.
Vr
Rotation speed.
Vf
Design flap speed is the high- Vref
The indicated airspeed that
est speed permissible at
the aircraft should be at when
which wing flaps may be
50 feet above the runway in
actuated.
the landing configuration.
B-1