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SUBCHAPTER A—DEFINITIONS AND GENERAL 

REQUIREMENTS 

PART 1—DEFINITIONS AND 

ABBREVIATIONS 

Sec. 
1.1

General definitions. 

1.2

Abbreviations and symbols. 

1.3

Rules of construction. 

A

UTHORITY

: 49 U.S.C. 106(f), 106(g), 40113, 

44701. 

§ 1.1

General definitions. 

As used in Subchapters A through K 

of this chapter, unless the context re-
quires otherwise: 

Administrator 

means the Federal 

Aviation Administrator or any person 
to whom he has delegated his authority 
in the matter concerned. 

Aerodynamic coefficients means non- 

dimensional coefficients for aero-
dynamic forces and moments. 

Air carrier means a person who under-

takes directly by lease, or other ar-
rangement, to engage in air transpor-
tation. 

Air commerce means interstate, over-

seas, or foreign air commerce or the 
transportation of mail by aircraft or 
any operation or navigation of aircraft 
within the limits of any Federal airway 
or any operation or navigation of air-
craft which directly affects, or which 
may endanger safety in, interstate, 
overseas, or foreign air commerce. 

Aircraft  means a device that is used 

or intended to be used for flight in the 
air. 

Aircraft engine means an engine that 

is used or intended to be used for pro-
pelling aircraft. It includes turbo-
superchargers, appurtenances, and ac-
cessories necessary for its functioning, 
but does not include propellers. 

Airframe  means the fuselage, booms, 

nacelles, cowlings, fairings, airfoil sur-
faces (including rotors but excluding 
propellers and rotating airfoils of en-
gines), and landing gear of an aircraft 
and their accessories and controls. 

Airplane 

means an engine-driven 

fixed-wing aircraft heavier than air, 
that is supported in flight by the dy-
namic reaction of the air against its 
wings. 

Airport  means an area of land or 

water that is used or intended to be 
used for the landing and takeoff of air-
craft, and includes its buildings and fa-
cilities, if any. 

Airship means an engine-driven light-

er-than-air aircraft that can be steered. 

Air traffic means aircraft operating in 

the air or on an airport surface, exclu-
sive of loading ramps and parking 
areas. 

Air traffic clearance means an author-

ization by air traffic control, for the 
purpose of preventing collision between 
known aircraft, for an aircraft to pro-
ceed under specified traffic conditions 
within controlled airspace. 

Air traffic control means a service op-

erated by appropriate authority to pro-
mote the safe, orderly, and expeditious 
flow of air traffic. 

Air Traffic Service (ATS) route is a 

specified route designated for chan-
neling the flow of traffic as necessary 
for the provision of air traffic services. 
The term ‘‘ATS route’’ refers to a vari-
ety of airways, including jet routes, 
area navigation (RNAV) routes, and ar-
rival and departure routes. An ATS 
route is defined by route specifications, 
which may include: 

(1) An ATS route designator; 
(2) The path to or from significant 

points; 

(3) Distance between significant 

points; 

(4) Reporting requirements; and 
(5) The lowest safe altitude deter-

mined by the appropriate authority. 

Air transportation means interstate, 

overseas, or foreign air transportation 
or the transportation of mail by air-
craft. 

Alert Area. An alert area is estab-

lished to inform pilots of a specific 
area wherein a high volume of pilot 
training or an unusual type of aero-
nautical activity is conducted. 

Alternate airport means an airport at 

which an aircraft may land if a landing 
at the intended airport becomes inad-
visable. 

Altitude engine means a reciprocating 

aircraft engine having a rated takeoff 

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14 CFR Ch. I (1–1–24 Edition) 

§ 1.1 

power that is producible from sea level 
to an established higher altitude. 

Amateur rocket means an unmanned 

rocket that: 

(1) Is propelled by a motor or motors 

having a combined total impulse of 
889,600 Newton-seconds (200,000 pound- 
seconds) or less; and 

(2) Cannot reach an altitude greater 

than 150 kilometers (93.2 statute miles) 
above the earth’s surface. 

Appliance  means any instrument, 

mechanism, equipment, part, appa-
ratus, appurtenance, or accessory, in-
cluding communications equipment, 
that is used or intended to be used in 
operating or controlling an aircraft in 
flight, is installed in or attached to the 
aircraft, and is not part of an airframe, 
engine, or propeller. 

Approved, unless used with reference 

to another person, means approved by 
the FAA or any person to whom the 
FAA has delegated its authority in the 
matter concerned, or approved under 
the provisions of a bilateral agreement 
between the United States and a for-
eign country or jurisdiction. 

Area navigation (RNAV) is a method 

of navigation that permits aircraft op-
erations on any desired flight path. 

Area navigation (RNAV) route is an 

ATS route based on RNAV that can be 
used by suitably equipped aircraft. 

Armed Forces means the Army, Navy, 

Air Force, Marine Corps, and Coast 
Guard, including their regular and re-
serve components and members serving 
without component status. 

Autorotation means a rotorcraft flight 

condition in which the lifting rotor is 
driven entirely by action of the air 
when the rotorcraft is in motion. 

Auxiliary rotor means a rotor that 

serves either to counteract the effect of 
the main rotor torque on a rotorcraft 
or to maneuver the rotorcraft about 
one or more of its three principal axes. 

Balloon  means a lighter-than-air air-

craft that is not engine driven, and 
that sustains flight through the use of 
either gas buoyancy or an airborne 
heater. 

Brake horsepower means the power de-

livered at the propeller shaft (main 
drive or main output) of an aircraft en-
gine. 

Calibrated airspeed means the indi-

cated airspeed of an aircraft, corrected 

for position and instrument error. Cali-
brated airspeed is equal to true air-
speed in standard atmosphere at sea 
level. 

Canard  means the forward wing of a 

canard configuration and may be a 
fixed, movable, or variable geometry 
surface, with or without control sur-
faces. 

Canard configuration means a configu-

ration in which the span of the forward 
wing is substantially less than that of 
the main wing. 

Category: 
(1) As used with respect to the cer-

tification, ratings, privileges, and limi-
tations of airmen, means a broad clas-
sification of aircraft. Examples in-
clude: airplane; rotorcraft; glider; and 
lighter-than-air; and 

(2) As used with respect to the cer-

tification of aircraft, means a grouping 
of aircraft based upon intended use or 
operating limitations. Examples in-
clude: transport, normal, utility, acro-
batic, limited, restricted, and provi-
sional. 

Category A, with respect to transport 

category rotorcraft, means multien-
gine rotorcraft designed with engine 
and system isolation features specified 
in Part 29 and utilizing scheduled take-
off and landing operations under a crit-
ical engine failure concept which 
assures adequate designated surface 
area and adequate performance capa-
bility for continued safe flight in the 
event of engine failure. 

Category B, with respect to transport 

category rotorcraft, means single-en-
gine or multiengine rotorcraft which 
do not fully meet all Category A stand-
ards. Category B rotorcraft have no 
guaranteed stay-up ability in the event 
of engine failure and unscheduled land-
ing is assumed. 

Category II operations, with respect to 

the operation of aircraft, means a 
straight-in ILS approach to the runway 
of an airport under a Category II ILS 
instrument approach procedure issued 
by the Administrator or other appro-
priate authority. 

Category III operations, with respect 

to the operation of aircraft, means an 
ILS approach to, and landing on, the 
runway of an airport using a Category 
III ILS instrument approach procedure 

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Federal Aviation Administration, DOT 

§ 1.1 

issued by the Administrator or other 
appropriate authority. 

Ceiling  means the height above the 

earth’s surface of the lowest layer of 
clouds or obscuring phenomena that is 
reported as ‘‘broken’’, ‘‘overcast’’, or 
‘‘obscuration’’, and not classified as 
‘‘thin’’ or ‘‘partial’’. 

Civil aircraft means aircraft other 

than public aircraft. 

Class: 
(1) As used with respect to the cer-

tification, ratings, privileges, and limi-
tations of airmen, means a classifica-
tion of aircraft within a category hav-
ing similar operating characteristics. 
Examples include: single engine; multi-
engine; land; water; gyroplane; heli-
copter; airship; and free balloon; and 

(2) As used with respect to the cer-

tification of aircraft, means a broad 
grouping of aircraft having similar 
characteristics of propulsion, flight, or 
landing. Examples include: airplane; 
rotorcraft; glider; balloon; landplane; 
and seaplane. 

Clearway means: 
(1) For turbine engine powered air-

planes certificated after August 29, 
1959, an area beyond the runway, not 
less than 500 feet wide, centrally lo-
cated about the extended centerline of 
the runway, and under the control of 
the airport authorities. The clearway 
is expressed in terms of a clearway 
plane, extending from the end of the 
runway with an upward slope not ex-
ceeding 1.25 percent, above which no 
object nor any terrain protrudes. How-
ever, threshold lights may protrude 
above the plane if their height above 
the end of the runway is 26 inches or 
less and if they are located to each side 
of the runway. 

(2) For turbine engine powered air-

planes certificated after September 30, 
1958, but before August 30, 1959, an area 
beyond the takeoff runway extending 
no less than 300 feet on either side of 
the extended centerline of the runway, 
at an elevation no higher than the ele-
vation of the end of the runway, clear 
of all fixed obstacles, and under the 
control of the airport authorities. 

Climbout speed, with respect to rotor-

craft, means a referenced airspeed 
which results in a flight path clear of 
the height-velocity envelope during 
initial climbout. 

Commercial operator means a person 

who, for compensation or hire, engages 
in the carriage by aircraft in air com-
merce of persons or property, other 
than as an air carrier or foreign air 
carrier or under the authority of Part 
375 of this title. Where it is doubtful 
that an operation is for ‘‘compensation 
or hire’’, the test applied is whether 
the carriage by air is merely incidental 
to the person’s other business or is, in 
itself, a major enterprise for profit. 

Configuration, Maintenance, and Pro-

cedures (CMP) document means a docu-
ment approved by the FAA that con-
tains minimum configuration, oper-
ating, and maintenance requirements, 
hardware life-limits, and Master Min-
imum Equipment List (MMEL) con-
straints necessary for an airplane-en-
gine combination to meet ETOPS type 
design approval requirements. 

Consensus standard means, for the 

purpose of certificating light-sport air-
craft, an industry-developed consensus 
standard that applies to aircraft de-
sign, production, and airworthiness. It 
includes, but is not limited to, stand-
ards for aircraft design and perform-
ance, required equipment, manufac-
turer quality assurance systems, pro-
duction acceptance test procedures, op-
erating instructions, maintenance and 
inspection procedures, identification 
and recording of major repairs and 
major alterations, and continued air-
worthiness. 

Controlled airspace means an airspace 

of defined dimensions within which air 
traffic control service is provided to 
IFR flights and to VFR flights in ac-
cordance with the airspace classifica-
tion. 

N

OTE

: Controlled airspace is a generic term 

that covers Class A, Class B, Class C, Class 
D, and Class E airspace. 

Controlled Firing Area. A controlled 

firing area is established to contain ac-
tivities, which if not conducted in a 
controlled environment, would be haz-
ardous to nonparticipating aircraft. 

Crewmember  means a person assigned 

to perform duty in an aircraft during 
flight time. 

Critical altitude means the maximum 

altitude at which, in standard atmos-
phere, it is possible to maintain, at a 
specified rotational speed, a specified 
power or a specified manifold pressure. 

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14 CFR Ch. I (1–1–24 Edition) 

§ 1.1 

Unless otherwise stated, the critical al-
titude is the maximum altitude at 
which it is possible to maintain, at the 
maximum continuous rotational speed, 
one of the following: 

(1) The maximum continuous power, 

in the case of engines for which this 
power rating is the same at sea level 
and at the rated altitude. 

(2) The maximum continuous rated 

manifold pressure, in the case of en-
gines, the maximum continuous power 
of which is governed by a constant 
manifold pressure. 

Critical engine means the engine 

whose failure would most adversely af-
fect the performance or handling quali-
ties of an aircraft. 

Decision altitude (DA) is a specified al-

titude in an instrument approach pro-
cedure at which the pilot must decide 
whether to initiate an immediate 
missed approach if the pilot does not 
see the required visual reference, or to 
continue the approach. Decision alti-
tude is expressed in feet above mean 
sea level. 

Decision height (DH) is a specified 

height above the ground in an instru-
ment approach procedure at which the 
pilot must decide whether to initiate 
an immediate missed approach if the 
pilot does not see the required visual 
reference, or to continue the approach. 
Decision height is expressed in feet 
above ground level. 

Early ETOPS means ETOPS type de-

sign approval obtained without gaining 
non-ETOPS service experience on the 
candidate airplane-engine combination 
certified for ETOPS. 

EFVS operation means an operation in 

which visibility conditions require an 
EFVS to be used in lieu of natural vi-
sion to perform an approach or landing, 
determine enhanced flight visibility, 
identify required visual references, or 
conduct a rollout. 

Enhanced flight visibility (EFV) means 

the average forward horizontal dis-
tance, from the cockpit of an aircraft 
in flight, at which prominent topo-
graphical objects may be clearly dis-
tinguished and identified by day or 
night by a pilot using an enhanced 
flight vision system. 

Enhanced flight vision system (EFVS) 

means an installed aircraft system 
which uses an electronic means to pro-

vide a display of the forward external 
scene topography (the natural or man-
made features of a place or region espe-
cially in a way to show their relative 
positions and elevation) through the 
use of imaging sensors, including but 
not limited to forward-looking infra-
red, millimeter wave radiometry, milli-
meter wave radar, or low-light level 
image intensification. An EFVS in-
cludes the display element, sensors, 
computers and power supplies, indica-
tions, and controls. 

Equivalent airspeed means the cali-

brated airspeed of an aircraft corrected 
for adiabatic compressible flow for the 
particular altitude. Equivalent air-
speed is equal to calibrated airspeed in 
standard atmosphere at sea level. 

ETOPS Significant System means an 

airplane system, including the propul-
sion system, the failure or malfunc-
tioning of which could adversely affect 
the safety of an ETOPS flight, or the 
continued safe flight and landing of an 
airplane during an ETOPS diversion. 
Each ETOPS significant system is ei-
ther an ETOPS group 1 significant sys-
tem or an ETOPS group 2 significant 
system. 

(1) An ETOPS group 1 Significant 

System— 

(i) Has fail-safe characteristics di-

rectly linked to the degree of redun-
dancy provided by the number of en-
gines on the airplane. 

(ii) Is a system, the failure or mal-

function of which could result in an 
IFSD, loss of thrust control, or other 
power loss. 

(iii) Contributes significantly to the 

safety of an ETOPS diversion by pro-
viding additional redundancy for any 
system power source lost as a result of 
an inoperative engine. 

(iv) Is essential for prolonged oper-

ation of an airplane at engine inoper-
ative altitudes. 

(2) An ETOPS group 2 significant sys-

tem is an ETOPS significant system 
that is not an ETOPS group 1 signifi-
cant system. 

Extended Operations (ETOPS) means 

an airplane flight operation, other than 
an all-cargo operation in an airplane 
with more than two engines, during 

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Federal Aviation Administration, DOT 

§ 1.1 

which a portion of the flight is con-
ducted beyond a time threshold identi-
fied in part 121 or part 135 of this chap-
ter that is determined using an ap-
proved one-engine-inoperative cruise 
speed under standard atmospheric con-
ditions in still air. 

Extended over-water operation means— 
(1) With respect to aircraft other 

than helicopters, an operation over 
water at a horizontal distance of more 
than 50 nautical miles from the nearest 
shoreline; and 

(2) With respect to helicopters, an op-

eration over water at a horizontal dis-
tance of more than 50 nautical miles 
from the nearest shoreline and more 
than 50 nautical miles from an off- 
shore heliport structure. 

External load means a load that is 

carried, or extends, outside of the air-
craft fuselage. 

External-load attaching means means 

the structural components used to at-
tach an external load to an aircraft, in-
cluding external-load containers, the 
backup structure at the attachment 
points, and any quick-release device 
used to jettison the external load. 

Final approach fix (FAF) defines the 

beginning of the final approach seg-
ment and the point where final seg-
ment descent may begin. 

Final takeoff speed means the speed of 

the airplane that exists at the end of 
the takeoff path in the en route con-
figuration with one engine inoperative. 

Fireproof— 
(1) With respect to materials and 

parts used to confine fire in a des-
ignated fire zone, means the capacity 
to withstand at least as well as steel in 
dimensions appropriate for the purpose 
for which they are used, the heat pro-
duced when there is a severe fire of ex-
tended duration in that zone; and 

(2) With respect to other materials 

and parts, means the capacity to with-
stand the heat associated with fire at 
least as well as steel in dimensions ap-
propriate for the purpose for which 
they are used. 

Fire resistant— 
(1) With respect to sheet or struc-

tural members means the capacity to 
withstand the heat associated with fire 
at least as well as aluminum alloy in 
dimensions appropriate for the purpose 
for which they are used; and 

(2) With respect to fluid-carrying 

lines, fluid system parts, wiring, air 
ducts, fittings, and powerplant con-
trols, means the capacity to perform 
the intended functions under the heat 
and other conditions likely to occur 
when there is a fire at the place con-
cerned. 

Flame resistant means not susceptible 

to combustion to the point of propa-
gating a flame, beyond safe limits, 
after the ignition source is removed. 

Flammable,  with respect to a fluid or 

gas, means susceptible to igniting read-
ily or to exploding. 

Flap extended speed means the highest 

speed permissible with wing flaps in a 
prescribed extended position. 

Flash resistant means not susceptible 

to burning violently when ignited. 

Flightcrew member means a pilot, 

flight engineer, or flight navigator as-
signed to duty in an aircraft during 
flight time. 

Flight level means a level of constant 

atmospheric pressure related to a ref-
erence datum of 29.92 inches of mer-
cury. Each is stated in three digits 
that represent hundreds of feet. For ex-
ample, flight level 250 represents a bar-
ometric altimeter indication of 25,000 
feet; flight level 255, an indication of 
25,500 feet. 

Flight plan means specified informa-

tion, relating to the intended flight of 
an aircraft, that is filed orally or in 
writing with air traffic control. 

Flight simulation training device 

(FSTD) means a full flight simulator or 
a flight training device. 

Flight time means: 
(1) Pilot time that commences when 

an aircraft moves under its own power 
for the purpose of flight and ends when 
the aircraft comes to rest after land-
ing; or 

(2) For a glider without self-launch 

capability, pilot time that commences 
when the glider is towed for the pur-
pose of flight and ends when the glider 
comes to rest after landing. 

Flight training device (FTD) means a 

replica of aircraft instruments, equip-
ment, panels, and controls in an open 
flight deck area or an enclosed aircraft 
cockpit replica. It includes the equip-
ment and computer programs nec-
essary to represent aircraft (or set of 
aircraft) operations in ground and 

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10 

14 CFR Ch. I (1–1–24 Edition) 

§ 1.1 

flight conditions having the full range 
of capabilities of the systems installed 
in the device as described in part 60 of 
this chapter and the qualification per-
formance standard (QPS) for a specific 
FTD qualification level. 

Flight visibility means the average for-

ward horizontal distance, from the 
cockpit of an aircraft in flight, at 
which prominent unlighted objects 
may be seen and identified by day and 
prominent lighted objects may be seen 
and identified by night. 

Foreign air carrier means any person 

other than a citizen of the United 
States, who undertakes directly, by 
lease or other arrangement, to engage 
in air transportation. 

Foreign air commerce means the car-

riage by aircraft of persons or property 
for compensation or hire, or the car-
riage of mail by aircraft, or the oper-
ation or navigation of aircraft in the 
conduct or furtherance of a business or 
vocation, in commerce between a place 
in the United States and any place out-
side thereof; whether such commerce 
moves wholly by aircraft or partly by 
aircraft and partly by other forms of 
transportation. 

Foreign air transportation means the 

carriage by aircraft of persons or prop-
erty as a common carrier for com-
pensation or hire, or the carriage of 
mail by aircraft, in commerce between 
a place in the United States and any 
place outside of the United States, 
whether that commerce moves wholly 
by aircraft or partly by aircraft and 
partly by other forms of transpor-
tation. 

Forward wing means a forward lifting 

surface of a canard configuration or 
tandem-wing configuration airplane. 
The surface may be a fixed, movable, or 
variable geometry surface, with or 
without control surfaces. 

Full flight simulator (FFS) means a 

replica of a specific type; or make, 
model, and series aircraft cockpit. It 
includes the assemblage of equipment 
and computer programs necessary to 
represent aircraft operations in ground 
and flight conditions, a visual system 
providing an out-of-the-cockpit view, a 
system that provides cues at least 
equivalent to those of a three-degree- 
of-freedom motion system, and has the 
full range of capabilities of the systems 

installed in the device as described in 
part 60 of this chapter and the quali-
fication performance standards (QPS) 
for a specific FFS qualification level. 

Glider  means a heavier-than-air air-

craft, that is supported in flight by the 
dynamic reaction of the air against its 
lifting surfaces and whose free flight 
does not depend principally on an en-
gine. 

Ground visibility means prevailing 

horizontal visibility near the earth’s 
surface as reported by the United 
States National Weather Service or an 
accredited observer. 

Go-around power or thrust setting 

means the maximum allowable in- 
flight power or thrust setting identi-
fied in the performance data. 

Gyrodyne  means a rotorcraft whose 

rotors are normally engine-driven for 
takeoff, hovering, and landing, and for 
forward flight through part of its speed 
range, and whose means of propulsion, 
consisting usually of conventional pro-
pellers, is independent of the rotor sys-
tem. 

Gyroplane  means a rotorcraft whose 

rotors are not engine-driven, except for 
initial starting, but are made to rotate 
by action of the air when the rotorcraft 
is moving; and whose means of propul-
sion, consisting usually of conven-
tional propellers, is independent of the 
rotor system. 

Helicopter  means a rotorcraft that, 

for its horizontal motion, depends prin-
cipally on its engine-driven rotors. 

Heliport means an area of land, water, 

or structure used or intended to be 
used for the landing and takeoff of heli-
copters. 

Idle thrust means the jet thrust ob-

tained with the engine power control 
level set at the stop for the least thrust 
position at which it can be placed. 

IFR conditions means weather condi-

tions below the minimum for flight 
under visual flight rules. 

IFR over-the-top, with respect to the 

operation of aircraft, means the oper-
ation of an aircraft over-the-top on an 
IFR flight plan when cleared by air 
traffic control to maintain ‘‘VFR con-
ditions’’ or ‘‘VFR conditions on top’’. 

Indicated airspeed means the speed of 

an aircraft as shown on its pitot static 
airspeed indicator calibrated to reflect 

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11 

Federal Aviation Administration, DOT 

§ 1.1 

standard atmosphere adiabatic com-
pressible flow at sea level uncorrected 
for airspeed system errors. 

In-flight shutdown (IFSD) means, for 

ETOPS only, when an engine ceases to 
function (when the airplane is air-
borne) and is shutdown, whether self 
induced, flightcrew initiated or caused 
by an external influence. The FAA con-
siders IFSD for all causes: for example, 
flameout, internal failure, flightcrew 
initiated shutdown, foreign object in-
gestion, icing, inability to obtain or 
control desired thrust or power, and 
cycling of the start control, however 
briefly, even if the engine operates nor-
mally for the remainder of the flight. 
This definition excludes the airborne 
cessation of the functioning of an en-
gine when immediately followed by an 
automatic engine relight and when an 
engine does not achieve desired thrust 
or power but is not shutdown. 

Instrument  means a device using an 

internal mechanism to show visually 
or aurally the attitude, altitude, or op-
eration of an aircraft or aircraft part. 
It includes electronic devices for auto-
matically controlling an aircraft in 
flight. 

Instrument approach procedure (IAP) is 

a series of predetermined maneuvers by 
reference to flight instruments with 
specified protection from obstacles and 
assurance of navigation signal recep-
tion capability. It begins from the ini-
tial approach fix, or where applicable, 
from the beginning of a defined arrival 
route to a point: 

(1) From which a landing can be com-

pleted; or 

(2) If a landing is not completed, to a 

position at which holding or en route 
obstacle clearance criteria apply. 

Interstate air commerce means the car-

riage by aircraft of persons or property 
for compensation or hire, or the car-
riage of mail by aircraft, or the oper-
ation or navigation of aircraft in the 
conduct or furtherance of a business or 
vocation, in commerce between a place 
in any State of the United States, or 
the District of Columbia, and a place in 
any other State of the United States, 
or the District of Columbia; or between 
places in the same State of the United 
States through the airspace over any 
place outside thereof; or between 
places in the same territory or posses-

sion of the United States, or the Dis-
trict of Columbia. 

Interstate air transportation means the 

carriage by aircraft of persons or prop-
erty as a common carrier for com-
pensation or hire, or the carriage of 
mail by aircraft in commerce: 

(1) Between a place in a State or the 

District of Columbia and another place 
in another State or the District of Co-
lumbia; 

(2) Between places in the same State 

through the airspace over any place 
outside that State; or 

(3) Between places in the same pos-

session of the United States; 

Whether that commerce moves wholly 
by aircraft of partly by aircraft and 
partly by other forms of transpor-
tation. 

Intrastate air transportation means the 

carriage of persons or property as a 
common carrier for compensation or 
hire, by turbojet-powered aircraft capa-
ble of carrying thirty or more persons, 
wholly within the same State of the 
United States. 

Kite  means a framework, covered 

with paper, cloth, metal, or other ma-
terial, intended to be flown at the end 
of a rope or cable, and having as its 
only support the force of the wind mov-
ing past its surfaces. 

Landing gear extended speed means 

the maximum speed at which an air-
craft can be safely flown with the land-
ing gear extended. 

Landing gear operating speed means 

the maximum speed at which the land-
ing gear can be safely extended or re-
tracted. 

Large aircraft means aircraft of more 

than 12,500 pounds, maximum certifi-
cated takeoff weight. 

Light-sport aircraft means an aircraft, 

other than a helicopter or powered-lift 
that, since its original certification, 
has continued to meet the following: 

(1) A maximum takeoff weight of not 

more than— 

(i) 1,320 pounds (600 kilograms) for 

aircraft not intended for operation on 
water; or 

(ii) 1,430 pounds (650 kilograms) for 

an aircraft intended for operation on 
water. 

(2) A maximum airspeed in level 

flight with maximum continuous power 
(V

H

) of not more than 120 knots CAS 

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12 

14 CFR Ch. I (1–1–24 Edition) 

§ 1.1 

under standard atmospheric conditions 
at sea level. 

(3) A maximum never-exceed speed 

(V

NE

) of not more than 120 knots CAS 

for a glider. 

(4) A maximum stalling speed or min-

imum steady flight speed without the 
use of lift-enhancing devices (V

S1

) of 

not more than 45 knots CAS at the air-
craft’s maximum certificated takeoff 
weight and most critical center of 
gravity. 

(5) A maximum seating capacity of 

no more than two persons, including 
the pilot. 

(6) A single, reciprocating engine, if 

powered. 

(7) A fixed or ground-adjustable pro-

peller if a powered aircraft other than 
a powered glider. 

(8) A fixed or feathering propeller 

system if a powered glider. 

(9) A fixed-pitch, semi-rigid, tee-

tering, two-blade rotor system, if a gy-
roplane. 

(10) A nonpressurized cabin, if 

equipped with a cabin. 

(11) Fixed landing gear, except for an 

aircraft intended for operation on 
water or a glider. 

(12) Fixed or retractable landing 

gear, or a hull, for an aircraft intended 
for operation on water. 

(13) Fixed or retractable landing gear 

for a glider. 

Lighter-than-air aircraft means air-

craft that can rise and remain sus-
pended by using contained gas weigh-
ing less than the air that is displaced 
by the gas. 

Load factor means the ratio of a spec-

ified load to the total weight of the air-
craft. The specified load is expressed in 
terms of any of the following: aero-
dynamic forces, inertia forces, or 
ground or water reactions. 

Long-range communication system 

(LRCS).  A system that uses satellite 
relay, data link, high frequency, or an-
other approved communication system 
which extends beyond line of sight. 

Long-range navigation system (LRNS). 

An electronic navigation unit that is 
approved for use under instrument 
flight rules as a primary means of navi-
gation, and has at least one source of 
navigational input, such as inertial 
navigation system or global posi-
tioning system. 

Mach number means the ratio of true 

airspeed to the speed of sound. 

Main rotor means the rotor that sup-

plies the principal lift to a rotorcraft. 

Maintenance  means inspection, over-

haul, repair, preservation, and the re-
placement of parts, but excludes pre-
ventive maintenance. 

Major alteration means an alteration 

not listed in the aircraft, aircraft en-
gine, or propeller specifications— 

(1) That might appreciably affect 

weight, balance, structural strength, 
performance, powerplant operation, 
flight characteristics, or other quali-
ties affecting airworthiness; or 

(2) That is not done according to ac-

cepted practices or cannot be done by 
elementary operations. 

Major repair means a repair: 
(1) That, if improperly done, might 

appreciably affect weight, balance, 
structural strength, performance, pow-
erplant operation, flight characteris-
tics, or other qualities affecting air-
worthiness; or 

(2) That is not done according to ac-

cepted practices or cannot be done by 
elementary operations. 

Manifold pressure means absolute 

pressure as measured at the appro-
priate point in the induction system 
and usually expressed in inches of mer-
cury. 

Maximum engine overtorque, as it ap-

plies to turbopropeller and turboshaft 
engines incorporating free power tur-
bines for all ratings except one engine 
inoperative (OEI) ratings of two min-
utes or less, means the maximum 
torque of the free power turbine rotor 
assembly, the inadvertent occurrence 
of which, for periods of up to 20 sec-
onds, will not require rejection of the 
engine from service, or any mainte-
nance action other than to correct the 
cause. 

Maximum speed for stability character-

istics, V

FC

/M

FC

means a speed that may 

not be less than a speed midway be-
tween maximum operating limit speed 
(V

MO

/M

MO

) and demonstrated flight div-

ing speed (V

DF

/M

DF

), except that, for al-

titudes where the Mach number is the 
limiting factor, M

FC

need not exceed 

the Mach number at which effective 
speed warning occurs. 

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13 

Federal Aviation Administration, DOT 

§ 1.1 

Medical certificate means acceptable 

evidence of physical fitness on a form 
prescribed by the Administrator. 

Military operations area. A military 

operations area (MOA) is airspace es-
tablished outside Class A airspace to 
separate or segregate certain nonhaz-
ardous military activities from IFR 
Traffic and to identify for VFR traffic 
where theses activities are conducted. 

Minimum descent altitude (MDA) is the 

lowest altitude specified in an instru-
ment approach procedure, expressed in 
feet above mean sea level, to which de-
scent is authorized on final approach or 
during circle-to-land maneuvering 
until the pilot sees the required visual 
references for the heliport or runway of 
intended landing. 

Minor alteration means an alteration 

other than a major alteration. 

Minor repair means a repair other 

than a major repair. 

National defense airspace means air-

space established by a regulation pre-
scribed, or an order issued under, 49 
U.S.C. 40103(b)(3). 

Navigable airspace means airspace at 

and above the minimum flight alti-
tudes prescribed by or under this chap-
ter, including airspace needed for safe 
takeoff and landing. 

Night  means the time between the 

end of evening civil twilight and the 
beginning of morning civil twilight, as 
published in the Air Almanac, con-
verted to local time. 

Nonprecision approach procedure 

means a standard instrument approach 
procedure in which no electronic glide 
slope is provided. 

Operate,  with respect to aircraft, 

means use, cause to use or authorize to 
use aircraft, for the purpose (except as 
provided in § 91.13 of this chapter) of air 
navigation including the piloting of 
aircraft, with or without the right of 
legal control (as owner, lessee, or oth-
erwise). 

Operational control, with respect to a 

flight, means the exercise of authority 
over initiating, conducting or termi-
nating a flight. 

Overseas air commerce means the car-

riage by aircraft of persons or property 
for compensation or hire, or the car-
riage of mail by aircraft, or the oper-
ation or navigation of aircraft in the 
conduct or furtherance of a business or 

vocation, in commerce between a place 
in any State of the United States, or 
the District of Columbia, and any place 
in a territory or possession of the 
United States; or between a place in a 
territory or possession of the United 
States, and a place in any other terri-
tory or possession of the United States. 

Overseas air transportation means the 

carriage by aircraft of persons or prop-
erty as a common carrier for com-
pensation or hire, or the carriage of 
mail by aircraft, in commerce: 

(1) Between a place in a State or the 

District of Columbia and a place in a 
possession of the United States; or 

(2) Between a place in a possession of 

the United States and a place in an-
other possession of the United States; 
whether that commerce moves wholly 
by aircraft or partly by aircraft and 
partly by other forms of transpor-
tation. 

Over-the-top means above the layer of 

clouds or other obscuring phenomena 
forming the ceiling. 

Parachute  means a device used or in-

tended to be used to retard the fall of 
a body or object through the air. 

Person  means an individual, firm, 

partnership, corporation, company, as-
sociation, joint-stock association, or 
governmental entity. It includes a 
trustee, receiver, assignee, or similar 
representative of any of them. 

Pilotage  means navigation by visual 

reference to landmarks. 

Pilot in command means the person 

who: 

(1) Has final authority and responsi-

bility for the operation and safety of 
the flight; 

(2) Has been designated as pilot in 

command before or during the flight; 
and 

(3) Holds the appropriate category, 

class, and type rating, if appropriate, 
for the conduct of the flight. 

Pitch setting means the propeller 

blade setting as determined by the 
blade angle measured in a manner, and 
at a radius, specified by the instruction 
manual for the propeller. 

Portable oxygen concentrator means a 

medical device that separates oxygen 
from other gasses in ambient air and 
dispenses this concentrated oxygen to 
the user. 

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14 

14 CFR Ch. I (1–1–24 Edition) 

§ 1.1 

Positive control means control of all 

air traffic, within designated airspace, 
by air traffic control. 

Powered parachute means a powered 

aircraft comprised of a flexible or semi- 
rigid wing connected to a fuselage so 
that the wing is not in position for 
flight until the aircraft is in motion. 
The fuselage of a powered parachute 
contains the aircraft engine, a seat for 
each occupant and is attached to the 
aircraft’s landing gear. 

Powered-lift  means a heavier-than-air 

aircraft capable of vertical takeoff, 
vertical landing, and low speed flight 
that depends principally on engine- 
driven lift devices or engine thrust for 
lift during these flight regimes and on 
nonrotating airfoil(s) for lift during 
horizontal flight. 

Precision approach procedure means a 

standard instrument approach proce-
dure in which an electronic glide slope 
is provided, such as ILS and PAR. 

Preventive maintenance means simple 

or minor preservation operations and 
the replacement of small standard 
parts not involving complex assembly 
operations. 

Prohibited area. A prohibited area is 

airspace designated under part 73 with-
in which no person may operate an air-
craft without the permission of the 
using agency. 

Propeller  means a device for propel-

ling an aircraft that has blades on an 
engine-driven shaft and that, when ro-
tated, produces by its action on the air, 
a thrust approximately perpendicular 
to its plane of rotation. It includes con-
trol components normally supplied by 
its manufacturer, but does not include 
main and auxiliary rotors or rotating 
airfoils of engines. 

Public aircraft means any of the fol-

lowing aircraft when not being used for 
a commercial purpose or to carry an 
individual other than a crewmember or 
qualified non-crewmenber: 

(1) An aircraft used only for the 

United States Government; an aircraft 
owned by the Government and operated 
by any person for purposes related to 
crew training, equipment development, 
or demonstration; an aircraft owned 
and operated by the government of a 
State, the District of Columbia, or a 
territory or possession of the United 
States or a political subdivision of one 

of these governments; or an aircraft ex-
clusively leased for at least 90 contin-
uous days by the government of a 
State, the District of Columbia, or a 
territory or possession of the United 
States or a political subdivision of one 
of these governments. 

(i) For the sole purpose of deter-

mining public aircraft status, 

commer-

cial purposes means the transportation 
of persons or property for compensa-
tion or hire, but does not include the 
operation of an aircraft by the armed 
forces for reimbursement when that re-
imbursement is required by any Fed-
eral statute, regulation, or directive, in 
effect on November 1, 1999, or by one 
government on behalf of another gov-
ernment under a cost reimbursement 
agreement if the government on whose 
behalf the operation is conducted cer-
tifies to the Administrator of the Fed-
eral Aviation Administration that the 
operation is necessary to respond to a 
significant and imminent threat to life 
or property (including natural re-
sources) and that no service by a pri-
vate operator is reasonably available 
to meet the threat. 

(ii) For the sole purpose of deter-

mining public aircraft status, 

govern-

mental function means an activity un-
dertaken by a government, such as na-
tional defense, intelligence missions, 
firefighting, search and rescue, law en-
forcement (including transport of pris-
oners, detainees, and illegal aliens), 
aeronautical research, or biological or 
geological resource management. 

(iii) For the sole purpose of deter-

mining public aircraft status, 

qualified 

non-crewmember  means an individual, 
other than a member of the crew, 
aboard an aircraft operated by the 
armed forces or an intelligence agency 
of the United States Government, or 
whose presence is required to perform, 
or is associated with the performance 
of, a governmental function. 

(2) An aircraft owned or operated by 

the armed forces or chartered to pro-
vide transportation to the armed forces 
if— 

(i) The aircraft is operated in accord-

ance with title 10 of the United States 
Code; 

(ii) The aircraft is operated in the 

performance of a governmental func-
tion under title 14, 31, 32, or 50 of the 

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15 

Federal Aviation Administration, DOT 

§ 1.1 

United States Code and the aircraft is 
not used for commercial purposes; or 

(iii) The aircraft is chartered to pro-

vide transportation to the armed forces 
and the Secretary of Defense (or the 
Secretary of the department in which 
the Coast Guard is operating) des-
ignates the operation of the aircraft as 
being required in the national interest. 

(3) An aircraft owned or operated by 

the National Guard of a State, the Dis-
trict of Columbia, or any territory or 
possession of the United States, and 
that meets the criteria of paragraph (2) 
of this definition, qualifies as a public 
aircraft only to the extent that it is 
operated under the direct control of 
the Department of Defense. 

Rated 30-second OEI Power, with re-

spect to rotorcraft turbine engines, 
means the approved brake horsepower 
developed under static conditions at 
specified altitudes and temperatures 
within the operating limitations estab-
lished for the engine under part 33 of 
this chapter, for continuation of one 
flight operation after the failure or 
shutdown of one engine in multiengine 
rotorcraft, for up to three periods of 
use no longer than 30 seconds each in 
any one flight, and followed by manda-
tory inspection and prescribed mainte-
nance action. 

Rated 2-minute OEI Power, with re-

spect to rotorcraft turbine engines, 
means the approved brake horsepower 
developed under static conditions at 
specified altitudes and temperatures 
within the operating limitations estab-
lished for the engine under part 33 of 
this chapter, for continuation of one 
flight operation after the failure or 
shutdown of one engine in multiengine 
rotorcraft, for up to three periods of 
use no longer than 2 minutes each in 
any one flight, and followed by manda-
tory inspection and prescribed mainte-
nance action. 

Rated continuous OEI power, with re-

spect to rotorcraft turbine engines, 
means the approved brake horsepower 
developed under static conditions at 
specified altitudes and temperatures 
within the operating limitations estab-
lished for the engine under part 33 of 
this chapter, and limited in use to the 
time required to complete the flight 
after the failure or shutdown of one en-
gine of a multiengine rotorcraft. 

Rated maximum continuous augmented 

thrust,  with respect to turbojet engine 
type certification, means the approved 
jet thrust that is developed statically 
or in flight, in standard atmosphere at 
a specified altitude, with fluid injec-
tion or with the burning of fuel in a 
separate combustion chamber, within 
the engine operating limitations estab-
lished under Part 33 of this chapter, 
and approved for unrestricted periods 
of use. 

Rated maximum continuous power, 

with respect to reciprocating, turbo-
propeller, and turboshaft engines, 
means the approved brake horsepower 
that is developed statically or in flight, 
in standard atmosphere at a specified 
altitude, within the engine operating 
limitations established under part 33, 
and approved for unrestricted periods 
of use. 

Rated maximum continuous thrust, 

with respect to turbojet engine type 
certification, means the approved jet 
thrust that is developed statically or in 
flight, in standard atmosphere at a 
specified altitude, without fluid injec-
tion and without the burning of fuel in 
a separate combustion chamber, within 
the engine operating limitations estab-
lished under part 33 of this chapter, 
and approved for unrestricted periods 
of use. 

Rated takeoff augmented thrust, with 

respect to turbojet engine type certifi-
cation, means the approved jet thrust 
that is developed statically under 
standard sea level conditions, with 
fluid injection or with the burning of 
fuel in a separate combustion chamber, 
within the engine operating limita-
tions established under part 33 of this 
chapter, and limited in use to periods 
of not over 5 minutes for takeoff oper-
ation. 

Rated takeoff power, with respect to 

reciprocating, turbopropeller, and tur-
boshaft engine type certification, 
means the approved brake horsepower 
that is developed statically under 
standard sea level conditions, within 
the engine operating limitations estab-
lished under part 33, and limited in use 
to periods of not over 5 minutes for 
takeoff operation. 

Rated takeoff thrust, with respect to 

turbojet engine type certification, 
means the approved jet thrust that is 

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14 CFR Ch. I (1–1–24 Edition) 

§ 1.1 

developed statically under standard sea 
level conditions, without fluid injec-
tion and without the burning of fuel in 
a separate combustion chamber, within 
the engine operating limitations estab-
lished under part 33 of this chapter, 
and limited in use to periods of not 
over 5 minutes for takeoff operation. 

Rated 30-minute OEI power, with re-

spect to rotorcraft turbine engines, 
means the approved brake horsepower 
developed under static conditions at 
specified altitudes and temperatures 
within the operating limitations estab-
lished for the engine under part 33 of 
this chapter, and limited in use to one 
period of use no longer than 30 minutes 
after the failure or shutdown of one en-
gine of a multiengine rotorcraft. 

Rated 2

1

2

-minute OEI power, with re-

spect to rotorcraft turbine engines, 
means the approved brake horsepower 
developed under static conditions at 
specified altitudes and temperatures 
within the operating limitations estab-
lished for the engine under part 33 of 
this chapter for periods of use no 
longer than 2

1

2

minutes each after the 

failure or shutdown of one engine of a 
multiengine rotorcraft. 

Rating  means a statement that, as a 

part of a certificate, sets forth special 
conditions, privileges, or limitations. 

Reference landing speed means the 

speed of the airplane, in a specified 
landing configuration, at the point 
where it descends through the 50 foot 
height in the determination of the 
landing distance. 

Reporting point means a geographical 

location in relation to which the posi-
tion of an aircraft is reported. 

Restricted area. A restricted area is 

airspace designated under Part 73 with-
in which the flight of aircraft, while 
not wholly prohibited, is subject to re-
striction. 

Rocket means an aircraft propelled by 

ejected expanding gases generated in 
the engine from self-contained propel-
lants and not dependent on the intake 
of outside substances. It includes any 
part which becomes separated during 
the operation. 

Rotorcraft  means a heavier-than-air 

aircraft that depends principally for its 
support in flight on the lift generated 
by one or more rotors. 

Rotorcraft-load combination means the 

combination of a rotorcraft and an ex-
ternal-load, including the external-load 
attaching means. Rotorcraft-load com-
binations are designated as Class A, 
Class B, Class C, and Class D, as fol-
lows: 

(1) 

Class A rotorcraft-load combination 

means one in which the external load 
cannot move freely, cannot be jetti-
soned, and does not extend below the 
landing gear. 

(2) 

Class B rotorcraft-load combination 

means one in which the external load is 
jettisonable and is lifted free of land or 
water during the rotorcraft operation. 

(3) 

Class C rotorcraft-load combination 

means one in which the external load is 
jettisonable and remains in contact 
with land or water during the rotor-
craft operation. 

(4) 

Class D rotorcraft-load combination 

means one in which the external-load 
is other than a Class A, B, or C and has 
been specifically approved by the Ad-
ministrator for that operation. 

Route segment is a portion of a route 

bounded on each end by a fix or naviga-
tion aid (NAVAID). 

Sea level engine means a reciprocating 

aircraft engine having a rated takeoff 
power that is producible only at sea 
level. 

Second in command means a pilot who 

is designated to be second in command 
of an aircraft during flight time. 

Show,  unless the context otherwise 

requires, means to show to the satis-
faction of the Administrator. 

Small aircraft means aircraft of 12,500 

pounds or less, maximum certificated 
takeoff weight. 

Small unmanned aircraft means an un-

manned aircraft weighing less than 55 
pounds on takeoff, including every-
thing that is on board or otherwise at-
tached to the aircraft. 

Small unmanned aircraft system (small 

UAS) means a small unmanned aircraft 
and its associated elements (including 
communication links and the compo-
nents that control the small unmanned 
aircraft) that are required for the safe 
and efficient operation of the small un-
manned aircraft in the national air-
space system. 

Special VFR conditions mean meteoro-

logical conditions that are less than 
those required for basic VFR flight in 

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Federal Aviation Administration, DOT 

§ 1.1 

controlled airspace and in which some 
aircraft are permitted flight under vis-
ual flight rules. 

Special VFR operations means aircraft 

operating in accordance with clear-
ances within controlled airspace in me-
teorological conditions less than the 
basic VFR weather minima. Such oper-
ations must be requested by the pilot 
and approved by ATC. 

Standard atmosphere means the at-

mosphere defined in U.S. Standard At-
mosphere, 1962 (Geopotential altitude 
tables). 

Stopway  means an area beyond the 

takeoff runway, no less wide than the 
runway and centered upon the ex-
tended centerline of the runway, able 
to support the airplane during an 
aborted takeoff, without causing struc-
tural damage to the airplane, and des-
ignated by the airport authorities for 
use in decelerating the airplane during 
an aborted takeoff. 

Suitable RNAV system is an RNAV sys-

tem that meets the required perform-
ance established for a type of oper-
ation, e.g. IFR; and is suitable for oper-
ation over the route to be flown in 
terms of any performance criteria (in-
cluding accuracy) established by the 
air navigation service provider for cer-
tain routes (e.g. oceanic, ATS routes, 
and IAPs). An RNAV system’s suit-
ability is dependent upon the avail-
ability of ground and/or satellite navi-
gation aids that are needed to meet 
any route performance criteria that 
may be prescribed in route specifica-
tions to navigate the aircraft along the 
route to be flown. Information on suit-
able RNAV systems is published in 
FAA guidance material. 

Synthetic vision means a computer- 

generated image of the external scene 
topography from the perspective of the 
flight deck that is derived from air-
craft attitude, high-precision naviga-
tion solution, and database of terrain, 
obstacles and relevant cultural fea-
tures. 

Synthetic vision system means an 

electronic means to display a synthetic 
vision image of the external scene to-
pography to the flight crew. 

Takeoff power: 
(1) With respect to reciprocating en-

gines, means the brake horsepower 
that is developed under standard sea 

level conditions, and under the max-
imum conditions of crankshaft rota-
tional speed and engine manifold pres-
sure approved for the normal takeoff, 
and limited in continuous use to the 
period of time shown in the approved 
engine specification; and 

(2) With respect to turbine engines, 

means the brake horsepower that is de-
veloped under static conditions at a 
specified altitude and atmospheric 
temperature, and under the maximum 
conditions of rotor shaft rotational 
speed and gas temperature approved for 
the normal takeoff, and limited in con-
tinuous use to the period of time shown 
in the approved engine specification. 

Takeoff safety speed means a ref-

erenced airspeed obtained after lift-off 
at which the required one-engine-inop-
erative climb performance can be 
achieved. 

Takeoff thrust, with respect to tur-

bine engines, means the jet thrust that 
is developed under static conditions at 
a specific altitude and atmospheric 
temperature under the maximum con-
ditions of rotorshaft rotational speed 
and gas temperature approved for the 
normal takeoff, and limited in contin-
uous use to the period of time shown in 
the approved engine specification. 

Tandem wing configuration means a 

configuration having two wings of 
similar span, mounted in tandem. 

TCAS I means a TCAS that utilizes 

interrogations of, and replies from, air-
borne radar beacon transponders and 
provides traffic advisories to the pilot. 

TCAS II means a TCAS that utilizes 

interrogations of, and replies from air-
borne radar beacon transponders and 
provides traffic advisories and resolu-
tion advisories in the vertical plane. 

TCAS III means a TCAS that utilizes 

interrogation of, and replies from, air-
borne radar beacon transponders and 
provides traffic advisories and resolu-
tion advisories in the vertical and hori-
zontal planes to the pilot. 

Time in service, with respect to main-

tenance time records, means the time 
from the moment an aircraft leaves the 
surface of the earth until it touches it 
at the next point of landing. 

Traffic pattern means the traffic flow 

that is prescribed for aircraft landing 
at, taxiing on, or taking off from, an 
airport. 

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18 

14 CFR Ch. I (1–1–24 Edition) 

§ 1.2 

True airspeed means the airspeed of 

an aircraft relative to undisturbed air. 
True airspeed is equal to equivalent 
airspeed multiplied by (

r

0/

r

)

1

2

Type: 
(1) As used with respect to the cer-

tification, ratings, privileges, and limi-
tations of airmen, means a specific 
make and basic model of aircraft, in-
cluding modifications thereto that do 
not change its handling or flight char-
acteristics. Examples include: DC–7, 
1049, and F–27; and 

(2) As used with respect to the cer-

tification of aircraft, means those air-
craft which are similar in design. Ex-
amples include: DC–7 and DC–7C; 1049G 
and 1049H; and F–27 and F–27F. 

(3) As used with respect to the cer-

tification of aircraft engines means 
those engines which are similar in de-
sign. For example, JT8D and JT8D–7 
are engines of the same type, and 
JT9D–3A and JT9D–7 are engines of the 
same type. 

United States, in a geographical sense, 

means (1) the States, the District of 
Columbia, Puerto Rico, and the posses-
sions, including the territorial waters, 
and (2) the airspace of those areas. 

United States air carrier means a cit-

izen of the United States who under-
takes directly by lease, or other ar-
rangement, to engage in air transpor-
tation. 

Unmanned aircraft means an aircraft 

operated without the possibility of di-
rect human intervention from within 
or on the aircraft. 

Unmanned aircraft system means an 

unmanned aircraft and its associated 
elements (including communication 
links and the components that control 
the unmanned aircraft) that are re-
quired for the safe and efficient oper-
ation of the unmanned aircraft in the 
airspace of the United States. 

VFR over-the-top, with respect to the 

operation of aircraft, means the oper-
ation of an aircraft over-the-top under 
VFR when it is not being operated on 
an IFR flight plan. 

Warning area. A warning area is air-

space of defined dimensions, extending 
from 3 nautical miles outward from the 
coast of the United States, that con-
tains activity that may be hazardous 
to nonparticipating aircraft. The pur-
pose of such warning areas is to warn 

nonparticipating pilots of the potential 
danger. A warning area may be located 
over domestic or international waters 
or both. 

Weight-shift-control aircraft means a 

powered aircraft with a framed piv-
oting wing and a fuselage controllable 
only in pitch and roll by the pilot’s 
ability to change the aircraft’s center 
of gravity with respect to the wing. 
Flight control of the aircraft depends 
on the wing’s ability to flexibly deform 
rather than the use of control surfaces. 

Winglet or tip fin means an out-of- 

plane surface extending from a lifting 
surface. The surface may or may not 
have control surfaces. 

[Doc. No. 1150, 27 FR 4588, May 15, 1962] 

E

DITORIAL

N

OTE

: For F

EDERAL

R

EGISTER

ci-

tations affecting § 1.1, see the List of CFR 
Sections Affected, which appears in the 
Finding Aids section of the printed volume 
and at 

www.govinfo.gov. 

§ 1.2

Abbreviations and symbols. 

In Subchapters A through K of this 

chapter: 

AFM means airplane flight manual. 
AGL means above ground level. 
ALS means approach light system. 
APU means auxiliary power unit. 
ASR 

means airport surveillance 

radar. 

ATC means air traffic control. 
ATS means Air Traffic Service. 
CAMP  means continuous airworthi-

ness maintenance program. 

CAS means calibrated airspeed. 
CAT II means Category II. 
CMP  means configuration, mainte-

nance, and procedures. 

DH means decision height. 
DME 

means distance measuring 

equipment compatible with TACAN. 

EAS means equivalent airspeed. 
EFVS  means enhanced flight vision 

system. 

Equi-Time Point means a point on the 

route of flight where the flight time, 
considering wind, to each of two se-
lected airports is equal. 

ETOPS means extended operations. 
EWIS, as defined by § 25.1701 of this 

chapter, means electrical wiring inter-
connection system. 

FAA  means Federal Aviation Admin-

istration. 

FFS means full flight simulator. 
FM means fan marker. 

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19 

Federal Aviation Administration, DOT 

§ 1.2 

FSTD  means flight simulation train-

ing device. 

FTD means flight training device. 
GS means glide slope. 
HIRL  means high-intensity runway 

light system. 

IAS means indicated airspeed. 
ICAO means International Civil Avia-

tion Organization. 

IFR means instrument flight rules. 
IFSD means in-flight shutdown. 
ILS  means instrument landing sys-

tem. 

IM means ILS inner marker. 
INT means intersection. 
LDA means localizer-type directional 

aid. 

LFR 

means low-frequency radio 

range. 

LMM  means compass locator at mid-

dle marker. 

LOC means ILS localizer. 
LOM means compass locator at outer 

marker. 

means mach number. 
MAA  means maximum authorized 

IFR altitude. 

MALS  means medium intensity ap-

proach light system. 

MALSR  means medium intensity ap-

proach light system with runway align-
ment indicator lights. 

MCA  means minimum crossing alti-

tude. 

MDA  means minimum descent alti-

tude. 

MEA  means minimum en route IFR 

altitude. 

MEL  means minimum equipment 

list. 

MM means ILS middle marker. 
MOCA  means minimum obstruction 

clearance altitude. 

MRA means minimum reception alti-

tude. 

MSL means mean sea level. 
NDB (ADF) means nondirectional 

beacon (automatic direction finder). 

NM means nautical mile. 
NOPAC  means North Pacific area of 

operation. 

NOPT  means no procedure turn re-

quired. 

OEI means one engine inoperative. 
OM means ILS outer marker. 
OPSPECS means operations specifica-

tions. 

PACOTS  means Pacific Organized 

Track System. 

PAR means precision approach radar. 
PMA  means parts manufacturer ap-

proval. 

POC  means portable oxygen concen-

trator. 

PTRS  means Performance Tracking 

and Reporting System. 

RAIL  means runway alignment indi-

cator light system. 

RBN means radio beacon. 
RCLM 

means runway centerline 

marking. 

RCLS  means runway centerline light 

system. 

REIL  means runway end identifica-

tion lights. 

RFFS  means rescue and firefighting 

services. 

RNAV means area navigation. 
RR  means low or medium frequency 

radio range station. 

RVR  means runway visual range as 

measured in the touchdown zone area. 

SALS means short approach light sys-

tem. 

SATCOM means satellite communica-

tions. 

SSALS  means simplified short ap-

proach light system. 

SSALSR  means simplified short ap-

proach light system with runway align-
ment indicator lights. 

TACAN  means ultra-high frequency 

tactical air navigational aid. 

TAS means true airspeed. 
TCAS  means a traffic alert and colli-

sion avoidance system. 

TDZL means touchdown zone lights. 
TSO  means technical standard order. 
TVOR means very high frequency ter-

minal omnirange station. 

V

A

means design maneuvering 

speed. 

V

B

means design speed for maximum 

gust intensity. 

V

C

means design cruising speed. 

V

D

means design diving speed. 

V

DF

/

M

DF

means demonstrated flight 

diving speed. 

V

EF

means the speed at which the 

critical engine is assumed to fail dur-
ing takeoff. 

V

F

means design flap speed. 

V

FC

/

M

FC

means maximum speed for 

stability characteristics. 

V

FE

means maximum flap extended 

speed. 

V

FTO

means final takeoff speed. 

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20 

14 CFR Ch. I (1–1–24 Edition) 

§ 1.3 

V

H

means maximum speed in level 

flight with maximum continuous 
power. 

V

LE

means maximum landing gear 

extended speed. 

V

LO

means maximum landing gear 

operating speed. 

V

LOF

means lift-off speed. 

V

MC

means minimum control speed 

with the critical engine inoperative. 

V

MO

/

M

MO

means maximum operating 

limit speed. 

V

MU

means minimum unstick speed. 

V

NE

means never-exceed speed. 

V

NO

means maximum structural 

cruising speed. 

V

R

means rotation speed. 

V

REF

means reference landing speed. 

V

S

means the stalling speed or the 

minimum steady flight speed at which 
the airplane is controllable. 

V

S0

means the stalling speed or the 

minimum steady flight speed in the 
landing configuration. 

V

S1

means the stalling speed or the 

minimum steady flight speed obtained 
in a specific configuration. 

V

SR

means reference stall speed. 

V

SRO

means reference stall speed in 

the landing configuration. 

V

SR1

means reference stall speed in a 

specific configuration. 

V

SW

means speed at which onset of 

natural or artificial stall warning oc-
curs. 

V

TOSS

means takeoff safety speed for 

Category A rotorcraft. 

V

X

means speed for best angle of 

climb. 

V

Y

means speed for best rate of 

climb. 

V

1

means the maximum speed in the 

takeoff at which the pilot must take 
the first action (e.g., apply brakes, re-
duce thrust, deploy speed brakes) to 
stop the airplane within the accelerate- 
stop distance. V

1

also means the min-

imum speed in the takeoff, following a 
failure of the critical engine at V

EF

, at 

which the pilot can continue the take-
off and achieve the required height 
above the takeoff surface within the 
takeoff distance. 

V

2

means takeoff safety speed. 

V

2min

means minimum takeoff safety 

speed. 

VFR

means visual flight rules. 

VGSI  means visual glide slope indi-

cator. 

VHF

means very high frequency. 

VOR

means very high frequency om-

nirange station. 

VORTAC

means collocated VOR and 

TACAN. 

[Doc. No. 1150, 27 FR 4590, May 15, 1962] 

E

DITORIAL

N

OTE

: For F

EDERAL

R

EGISTER

ci-

tations affecting § 1.2, see the List of CFR 
Sections Affected, which appears in the 
Finding Aids section of the printed volume 
and at 

www.govinfo.gov. 

§ 1.3

Rules of construction. 

(a) In Subchapters A through K of 

this chapter, unless the context re-
quires otherwise: 

(1) Words importing the singular in-

clude the plural; 

(2) Words importing the plural in-

clude the singular; and 

(3) Words importing the masculine 

gender include the feminine. 

(b) In Subchapters A through K of 

this chapter, the word: 

(1) 

Shall  is used in an imperative 

sense; 

(2) 

May  is used in a permissive sense 

to state authority or permission to do 
the act prescribed, and the words ‘‘no 
person may * * *’’ or ‘‘a person may 
not * * *’’ mean that no person is re-
quired, authorized, or permitted to do 
the act prescribed; and 

(3) 

Includes  means ‘‘includes but is 

not limited to’’. 

[Doc. No. 1150, 27 FR 4590, May 15, 1962, as 
amended by Amdt. 1–10, 31 FR 5055, Mar. 29, 
1966] 

PART 3—GENERAL REQUIREMENTS 

Subpart A—General Requirements Con-

cerning Type Certificated Products or 
Products, Parts, Appliances, or Mate-
rials That May Be Used on Type-Certifi-
cated Products 

Sec. 
3.1

Applicability. 

3.5

Statements about products, parts, appli-

ances and materials. 

Subpart B—Security Threat Disqualification 

3.200

Effect of Transportation Security Ad-

ministration notification on a certificate 
or any part of a certificate held by an in-
dividual. 

3.205

Effect of Transportation Security Ad-

ministration notification on applications 

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