In
aviation, V-speeds are standard terms used to define
airspeeds important or useful to the operation of all
aircraft.
These speeds are derived from data obtained by aircraft designers and manufacturers during
flight testing for aircraft
type-certification. Using them is considered a
best practice to maximize
aviation safety, aircraft performance, or both.
The actual speeds represented by these designators are specific to a particular model of aircraft. They are expressed by the aircraft's
indicated airspeed (and not by, for example, the
ground speed), so that pilots may use them directly, without having to apply correction factors, as aircraft instruments also show indicated airspeed.
In
general aviation aircraft
General aviation (GA) is defined by the International Civil Aviation Organization (ICAO) as all civil aviation aircraft operations with the exception of commercial air transport or aerial work, which is defined as specialized aviation services ...
, the most commonly used and most safety-critical airspeeds are displayed as color-coded arcs and lines located on the face of an aircraft's
airspeed indicator. The lower ends of the white arc and the green arc are the
stalling speed
In fluid dynamics, a stall is a reduction in the lift coefficient generated by a foil as angle of attack increases.Crane, Dale: ''Dictionary of Aeronautical Terms, third edition'', p. 486. Aviation Supplies & Academics, 1997. This occurs when t ...
with wing flaps in landing configuration, and stalling speed with wing flaps retracted, respectively. These are the stalling speeds for the aircraft at its maximum weight.
The yellow band is the range in which the aircraft may be operated in smooth air, and then only with caution to avoid abrupt control movement. The red line is the V
NE, the never-exceed speed.
Proper display of V-speeds is an airworthiness requirement for type-certificated aircraft in most countries.
Regulations
The most common V-speeds are often defined by a particular government's
aviation regulations. In the United States, these are defined in title 14 of the United States
Code of Federal Regulations
In the law of the United States, the ''Code of Federal Regulations'' (''CFR'') is the codification of the general and permanent regulations promulgated by the executive departments and agencies of the federal government of the United States. ...
, known as the
Federal Aviation Regulations (FARs).
In
Canada, the regulatory body,
Transport Canada, defines 26 commonly used V-speeds in their Aeronautical Information Manual.
V-speed definitions in FAR 23, 25 and equivalent are for designing and certification of airplanes, not for their operational use. The descriptions below are for use by pilots.
Regulatory V-speeds
These V-speeds are defined by regulations. They are typically defined with constraints such as weight, configuration, or phases of flight. Some of these constraints have been omitted to simplify the description.
Other V-speeds
Some of these V-speeds are specific to particular types of aircraft and are not defined by regulations.
Mach numbers
Whenever a limiting speed is expressed by a
Mach number
Mach number (M or Ma) (; ) is a dimensionless quantity in fluid dynamics representing the ratio of flow velocity past a boundary to the local speed of sound.
It is named after the Moravian physicist and philosopher Ernst Mach.
: \mathrm = \frac ...
, it is expressed relative to the local speed of sound, e.g. V
MO: Maximum operating speed, M
MO: Maximum operating Mach number.
V1 definitions
V
1 is the critical engine failure recognition speed or takeoff decision speed. It is the speed above which the takeoff will continue even if an engine fails or another problem occurs, such as a blown tire.
The speed will vary among aircraft types and varies according to factors such as aircraft weight, runway length,
wing flap setting, engine thrust used and runway surface contamination, thus it must be determined by the pilot before takeoff. Aborting a takeoff after V
1 is strongly discouraged because the aircraft may not be able to stop before the end of the runway, thus suffering a
runway overrun.
V
1 is defined differently in different jurisdictions, and definitions change over time as aircraft regulations are amended.
*The US
Federal Aviation Administration defines it as: "the maximum speed in the takeoff at which the pilot must take the first action (e.g., apply brakes, reduce thrust, deploy speed brakes) to stop the airplane within the accelerate-stop distance. V
1 also means the minimum speed in the takeoff, following a failure of the critical engine at V
EF, at which the pilot can continue the takeoff and achieve the required height above the takeoff surface within the takeoff distance."
V
1 thus includes reaction time.
In addition to this reaction time, a safety margin equivalent to 2 seconds at V
1 is added to the accelerate-stop distance.
*
Transport Canada defines it as: "Critical engine failure recognition speed" and adds: "This definition is not restrictive. An operator may adopt any other definition outlined in the aircraft flight manual (AFM) of TC type-approved aircraft as long as such definition does not compromise operational safety of the aircraft."
See also
*
ICAO recommendations on use of the International System of Units
*
Balanced field takeoff
Notes
References
Further reading
*
{{Flight instruments
Airspeed
Aircraft performance