TERMIUM Plus^®

Fiche 1,  Justifications,  Anglais

Record number: 1, Textual support number: 1 CONT

When you use an ejector seat, the seat, complete with pilot and parachute and survival pack is ejected from the aircraft by an ejection gun. This gun is fixed to the back of the seat vertically pointing downwards and is powerful enough to throw the seat well clear of the aircraft even if it is travelling at high speeds.  2, fiche 1, Anglais, - ejection%20gun

Fiche 1,  Justifications,  Français

Fiche 1,  Justifications,  Espagnol

Fiche 2,  Justifications,  Anglais

Record number: 2, Textual support number: 1 DEF

A seat that can be propelled out of an aircraft to allow evacuation in case of an emergency.  3, fiche 2, Anglais, - ejection%20seat

Fiche 2,  Justifications,  Français

Record number: 2, Textual support number: 1 DEF

Siège qui peut être propulsé à l'extérieur de l'aéronef pour permettre l'évacuation en cas d'urgence.  3, fiche 2, Français, - si%C3%A8ge%20%C3%A9jectable

Record number: 2, Textual support number: 1 CONT

Le siège éjectable est un système de sécurité visant à permettre au pilote et à l'équipage d'un avion de s'échapper de celui-ci lorsqu'il devient incontrôlable ou sur le point de s'écraser.  4, fiche 2, Français, - si%C3%A8ge%20%C3%A9jectable

Fiche 2,  Justifications,  Espagnol

Fiche 3,  Justifications,  Anglais

Record number: 3, Textual support number: 1 CONT

As in the case of ground test installations, the flight tests are initially carried out with dummies and then with human beings. Only after having passed all the tests and after a determination has been made of the factors which might produce high or low temperatures and vibration regimes in the aircraft can the seat be considered operational.  2, fiche 3, Anglais, - ground%20test%20installation

Record number: 3, Textual support number: 1 OBS

ground test installation: designation usually used in the plural.  3, fiche 3, Anglais, - ground%20test%20installation

Fiche 3,  Justifications,  Français

Record number: 3, Textual support number: 1 OBS

installation d'essais au sol : désignation habituellement utilisée au pluriel.  2, fiche 3, Français, - installation%20d%27essais%20au%20sol

Fiche 3,  Justifications,  Espagnol

Fiche 4,  Justifications,  Anglais

Record number: 4, Textual support number: 1 DEF

A pilot who acts as a lookout for another pilot operating an aircraft in simulated instrument flight.  2, fiche 4, Anglais, - safety%20pilot

Record number: 4, Textual support number: 1 OBS

An aircraft shall not be flown under simulated instrument flight conditions unless :[...] a qualified pilot occupies a control seat to act as safety pilot for the person who is flying under simulated instrument conditions.  3, fiche 4, Anglais, - safety%20pilot

Record number: 4, Textual support number: 2 OBS

safety pilot: term officially approved by the International Civil Aviation Organization (ICAO).  4, fiche 4, Anglais, - safety%20pilot

Record number: 4, Textual support number: 3 OBS

safety pilot: term and definition standardized by the Glossary for Pilots and Air Traffic Services Personnel Committee.  5, fiche 4, Anglais, - safety%20pilot

Fiche 4,  Justifications,  Français

Record number: 4, Textual support number: 1 DEF

Pilote qui agit comme vigie pour un autre pilote qui utilise un aéronef en vol aux instruments simulé.  2, fiche 4, Français, - pilote%20de%20s%C3%A9curit%C3%A9

Record number: 4, Textual support number: 1 OBS

Un aéronef ne volera pas dans des conditions fictives de vol aux instruments à moins : [...] qu'un pilote qualifié n'occupe un siège aux commandes lui permettant d'intervenir comme pilote de sécurité suppléant la personne qui pilote dans les conditions fictives de vol aux instruments.  3, fiche 4, Français, - pilote%20de%20s%C3%A9curit%C3%A9

Record number: 4, Textual support number: 2 OBS

pilote de sécurité : désignation uniformisée par l'Organisation de l'aviation civile internationale (OACI).  4, fiche 4, Français, - pilote%20de%20s%C3%A9curit%C3%A9

Record number: 4, Textual support number: 3 OBS

pilote de sécurité : désignation et définition normalisées par le Comité sur le Glossaire à l'intention des pilotes et du personnel des services de la circulation aérienne.  4, fiche 4, Français, - pilote%20de%20s%C3%A9curit%C3%A9

Fiche 4,  Justifications,  Espagnol

Fiche 6,  Justifications,  Anglais

Record number: 6, Textual support number: 1 CONT

On multi-crew aircraft where space permits and a jump seat has not been provided, a third pilot and/or a second flight engineer(FE) may stand on the flight deck for landing or take-off only in the following circumstances...  2, fiche 6, Anglais, - multi%2Dcrew%20aircraft

Fiche 6,  Justifications,  Français

Record number: 6, Textual support number: 1 CONT

Pour un aéronef à équipage multiple, les deux pilotes doivent : (1) être qualifiés sur type; (2) avoir réussi le plan de cours [...] approuvé; (3) être titulaires d'une qualification aux instruments valide.  2, fiche 6, Français, - a%C3%A9ronef%20%C3%A0%20%C3%A9quipage%20multiple

Fiche 6,  Justifications,  Espagnol

Fiche 7,  Justifications,  Anglais

Record number: 7, Textual support number: 1 DEF

A folding extra seat in a motor vehicle, aircraft, etc.  2, fiche 7, Anglais, - jump%20seat

Record number: 7, Textual support number: 1 CONT

On multi-crew aircraft where space permits and a jump seat has not been provided, a third pilot and/or a second flight engineer(FE) may stand on the flight deck for landing or take-off only in the following circumstances...  3, fiche 7, Anglais, - jump%20seat

Fiche 7,  Justifications,  Français

Record number: 7, Textual support number: 1 CONT

Sur les aéronefs à plusieurs membres d'équipage où l'espace le permet et où aucun strapontin n'est disponible, un troisième pilote ou un second mécanicien de bord (Méc B), ou les deux, peut se tenir debout dans le poste de pilotage durant l'atterrissage et le décollage, mais seulement s'il s'agit ...  2, fiche 7, Français, - strapontin

Record number: 7, Textual support number: 1 OBS

strapontin : terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Hélicoptères.  3, fiche 7, Français, - strapontin

Fiche 7,  Justifications,  Espagnol

Fiche 8,  Justifications,  Anglais

Record number: 8, Textual support number: 1 OBS

Wings will limit cadet flights aboard ejection seat aircraft to a maximum of three flights annually.  2, fiche 8, Anglais, - ejection%20seat%20aircraft

Fiche 8,  Justifications,  Français

Record number: 8, Textual support number: 1 OBS

Les escadres doivent limiter les vols des cadets à bord d’un aéronef à sièges éjectables à un maximum de trois vols par année.  2, fiche 8, Français, - a%C3%A9ronef%20%C3%A0%20si%C3%A8ge%20%C3%A9jectable

Fiche 8,  Justifications,  Espagnol

Fiche 9,  Justifications,  Anglais

Record number: 9, Textual support number: 1 CONT

The Dynamic Flight Simulator, or the DFS, is a manned full system simulation facility which reproduces the total G-force environment common to modern high performance aircraft.  1, fiche 9, Anglais, - dynamic%20flight%20simulator

Record number: 9, Textual support number: 2 CONT

This combination of High-Tech, Low-Tech and Old-Tech is the heart of the Dynamic Flight Simulator at the Naval Warfare Center in Warminster, PA, where the Navy simulates and tests, people and equipment, both of which must function under(often) extreme conditions.... travelling at supersonic speed, or engaging hostile enemy fire, or having to eject from a stricken aircraft and endure the 15 plus G thrust of an ejection seat. When the Navy puts that word "Dynamic" in front of the flight simulator, they really mean it. At the speed levels modern jet fighters attain there aren’t many second chances.  2, fiche 9, Anglais, - dynamic%20flight%20simulator

Fiche 9,  Justifications,  Français

Record number: 9, Textual support number: 1 CONT

Aucun simulateur de vol dynamique actuel n'est en mesure de réaliser des figures liées au combat tournoyant ou à l'évasion de missiles. Ils sont de plus incapables de restituer les effets des manœuvres des chasseurs à poussée vectorielle de nouvelle et future génération. Certaines figures conventionnelles ne peuvent être réalisées en totalité et sont compensées par des effets sonores et visuels de plus en plus réalistes, qui augmentent les déséquilibres sensoriels.  1, fiche 9, Français, - simulateur%20de%20vol%20dynamique

Fiche 9,  Justifications,  Espagnol

Fiche 10,  Justifications,  Anglais

Record number: 10, Textual support number: 1 OBS

The pocket on the back of aircraft passenger seats where safety information documents and other material is stored. It serves the passenger sitting in the seat immediately to the rear of the seat on which it is located.  1, fiche 10, Anglais, - seat%20pocket

Fiche 10,  Justifications,  Français

Fiche 10,  Justifications,  Espagnol

Fiche 11,  Justifications,  Anglais

Record number: 11, Textual support number: 1 CONT

Some aircraft manufacturers provide reference points which the pilot uses while making the seat adjustments.... The intent, of course, is to have the pilot adjust the seat in order for the eyes of the pilot to be at the optimum location for visibility, inside and outside the cockpit, as well as the correct position for access to the cockpit switches and knobs... This optimum position for the pilot's eyes is referred to as the design eye reference point.  2, fiche 11, Anglais, - design%20eye%20reference%20point

Fiche 11,  Justifications,  Français

Record number: 11, Textual support number: 1 CONT

Certains constructeurs d'avions ajoutent des repères dans le poste de pilotage que le pilote peut utiliser comme point de référence visuelle pour pouvoir placer son siège dans la meilleure position possible. [...] Le pilote peut ainsi placer son siège de façon à pouvoir jouir de la meilleure visibilité à l'intérieur et à l'extérieur du poste de pilotage et pour avoir facilement accès aux interrupteurs et aux commandes. Cette position optimale, appelée point de référence visuelle calculé (DERP), est une position statique basée sur la conception du poste de pilotage.  1, fiche 11, Français, - point%20de%20r%C3%A9f%C3%A9rence%20visuelle%20calcul%C3%A9

Fiche 11,  Justifications,  Espagnol

Fiche 12,  Justifications,  Anglais

Record number: 12, Textual support number: 1 OBS

Transportation textiles include :seat, curtain and carpet for automobiles and trains, automotive seat fabrics, interior furnishings that are decorative as well as functional for luxury passenger boats, airplanes, liner motor cars and so on... Transportation Textiles : tires, airbags, seat belts, automotive interior, trim automotive exterior, trim truck and car covers belts, covers for trailers and boats, loose seat covers for cars, cellular foam and aircraft seat cushioning, hoses and filters in cars, textiles for aircraft, textiles as structural elements in transport vehicles, inflatable products used in transportation.  2, fiche 12, Anglais, - transportation%20textiles

Fiche 12,  Justifications,  Français

Fiche 12,  Justifications,  Espagnol

Fiche 13,  Justifications,  Anglais

Record number: 13, Textual support number: 1 CONT

Carry On Wheelchair. Passenger requires assistance to the top of the aircraft steps but is unable to walk to his own seat.  1, fiche 13, Anglais, - carry%20on%20wheelchair

Fiche 13,  Justifications,  Français

Record number: 13, Textual support number: 1 OBS

Le passager a besoin d'aide jusqu'au haut de l'escalier mais peut marcher jusqu'à sa place dans l'avion.  1, fiche 13, Français, - passager%20d%C3%A9ficient

Fiche 13,  Justifications,  Espagnol

Fiche 14,  Justifications,  Anglais

Record number: 14, Textual support number: 1 DEF

A large, flat, usually delta-shaped motorless aircraft with an attached harness or seat, designed to carry a person or two people through the air for a short while.  2, fiche 14, Anglais, - hang%20glider

Record number: 14, Textual support number: 1 CONT

Hang gliders can be rigid or semi-rigid. Semi-rigid, which is the most common type, have aluminium spars and battens in their wings, but are covered in a tight sheath of Dacron cloth. Rigid hang gliders are made of hard, composite materials such as glass fibre and are becoming increasingly popular. In both cases, the pilot is suspended in a harness beneath the glider in a face down position and controls the direction and speed by moving a triangular control frame to shift his or her weight beneath the wing.  3, fiche 14, Anglais, - hang%20glider

Fiche 14,  Justifications,  Français

Record number: 14, Textual support number: 1 CONT

Un deltaplane est un aéronef non motorisé qui ressemble à un cerf-volant de forme triangulaire. Son vol est stable et sécuritaire et il se déplace à des vitesses se situant entre 30 km/h et 120 km/h. La pratique du deltaplane s'adresse surtout aux personnes persévérantes et en bonne condition physique, car la formation est relativement technique et le pilotage de l'aile demande un minimum de force.  4, fiche 14, Français, - deltaplane

Fiche 14,  Justifications,  Espagnol

Fiche 15,  Justifications,  Anglais

Record number: 15, Textual support number: 1 DEF

Part of aircraft ejection seat assembly, a fastener which locks the motor and launcher tubes in telescoped position.  1, fiche 15, Anglais, - prong%20lock

Fiche 15,  Justifications,  Français

Record number: 15, Textual support number: 1 OBS

Verrou à barre. Verrou à tige.  3, fiche 15, Français, - verrou%20%C3%A0%20pince

Record number: 15, Textual support number: 2 OBS

Verrou: dispositif assujettissant des éléments mobiles.  3, fiche 15, Français, - verrou%20%C3%A0%20pince

Fiche 15,  Justifications,  Espagnol

Fiche 16,  Justifications,  Anglais

Record number: 16, Textual support number: 1 CONT

On the A330-200 "Sleeper" aircraft, there are only eight seats in a 1-2-1 configuration(A-E, F-K). They have an 80-inch pitch, a 180-degree recline and are 25-inches wide. Known as the Class 180 seat(because it reclines fully flat, or 180 degrees), the seat transforms into a full-size bed covered with fitted cotton sheets, over-size pillows and duvets. Passengers are also offered pyjamas and there are changing room facilities and a suit pack to store your day clothes.  1, fiche 16, Anglais, - sleeper%20aircraft

Fiche 16,  Justifications,  Français

Record number: 16, Textual support number: 1 CONT

L’avion-couchettes arrive à La Réunion. À compter de la mi-décembre sur la ligne Paris-Réunion-Paris, Air France proposera à bord du B 747-400 en espace affaires un fauteuil au confort inégalé puisqu’il se transforme en lit. Le fauteuil glisse à l’intérieur d’une coque rigide, garantissant à chacun un espace constant et permettant de dormir en position allongée sans gêner ses voisins.  1, fiche 16, Français, - avion%2Dcouchettes

Fiche 16,  Justifications,  Espagnol

Fiche 17,  Justifications,  Anglais

Record number: 17, Textual support number: 1 CONT

... the TSB [Transportation Safety Board of Canada] analyzed specifically the aircraft steering system, while not ignoring the other factors mentioned above, although no indication was found that they could have contributed to the occurrence. To steer the aircraft on the ground, the pilot in the left seat uses the nose-gear steering wheel on the console to the pilot's left. During take-off and landing, directional control of the aircraft is maintained solely by the rudder. The aircraft's ground steering system comprises several components, including the nose-gear steering wheel, a system of cables and pulleys, and a steering control valve fitted to a nose-wheel steering cylinder, which is attached to the nose-wheel strut. The cable and pulley system links the steering wheel to the control valve. When the pilot turns the steering wheel to the left or right, tension is applied to the cables connected to the pulley on the steering control valve. This action determines the direction and the deflection rate of the nose wheel by allowing hydraulic fluid to enter one side or the other side of the nose-wheel steering cylinder; the steering cylinder then deflects the nose wheel through a system of gears.  3, fiche 17, Anglais, - aircraft%20steering%20system

Record number: 17, Textual support number: 1 PHR

Nose landing gear, nosewheel steering system.  4, fiche 17, Anglais, - aircraft%20steering%20system

Fiche 17,  Justifications,  Français

Record number: 17, Textual support number: 1 OBS

[...] le BST [Bureau de la sécurité des transports du Canada] a analysé plus spécifiquement le système de direction de l'appareil sans toutefois négliger les autres facteurs mentionnés précédemment, ceux-ci n'ayant d'ailleurs révélé aucun indice permettant de croire qu'ils auraient pu jouer un rôle dans cet accident. Pour diriger l'appareil au sol, le pilote assis à gauche utilise le volant d'orientation de la roue de nez localisé sur la console à sa gauche. Lors du décollage et de l'atterrissage, le contrôle directionnel de l'appareil est maintenu uniquement par le gouvernail de direction. Le système de contrôle de la direction de l'appareil au sol est constitué de différentes composantes, dont le volant d'orientation de la roue de nez, un système de câbles et poulies, et un robinet de commande d'orientation monté sur un vérin hydraulique de direction du train avant, relié à la jambe de la roue avant. Le système de câbles et poulies relie le volant au robinet de commande. Lorsque le pilote tourne le volant vers la gauche ou la droite, une tension est appliquée sur les câbles reliés à la poulie du robinet de commande d'orientation. Cette action contrôle le taux de braquage et la direction de la roue de nez en permettant au fluide hydraulique de circuler d'un côté ou de l'autre du vérin hydraulique de direction du train avant; ce dernier fait tourner la roue de nez par le biais d'un système d'engrenage.  4, fiche 17, Français, - syst%C3%A8me%20d%27orientation

Record number: 17, Textual support number: 2 OBS

système d'orientation : terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Maintenance.  3, fiche 17, Français, - syst%C3%A8me%20d%27orientation

Record number: 17, Textual support number: 1 PHR

Système d'orientation des roues, du train avant.  3, fiche 17, Français, - syst%C3%A8me%20d%27orientation

Record number: 17, Textual support number: 2 PHR

Système de direction au sol.  3, fiche 17, Français, - syst%C3%A8me%20d%27orientation

Record number: 17, Textual support number: 3 PHR

Pose du système de direction.  3, fiche 17, Français, - syst%C3%A8me%20d%27orientation

Fiche 17,  Justifications,  Espagnol

Fiche 18,  Justifications,  Anglais

Record number: 18, Textual support number: 1 CONT

No aircraft shall be flown under simulated instrument flight conditions unless,(a) the aircraft is equipped with fully functioning dual controls;(b) a competent pilot is occupying a control seat to act as safety pilot;...  1, fiche 18, Anglais, - control%20seat

Fiche 18,  Justifications,  Français

Record number: 18, Textual support number: 1 CONT

Aucun aéronef ne sera piloté dans des conditions fictives de vol aux instruments, sauf a) si l'aéronef est équipé de doubles commandes en parfait état de fonctionnement; b) si un pilote compétent occupe un siège aux commandes et servira de pilote de sécurité; [...]  1, fiche 18, Français, - si%C3%A8ge%20aux%20commandes

Fiche 18,  Justifications,  Espagnol

Fiche 19,  Justifications,  Anglais

Record number: 19, Textual support number: 1 CONT

The local orbital reference system is defined at each point of the orbit by three unit vectors. These vectors are derived from the satellite position and velocity vectors: Vector L is colinear with position vector P (on the axis between the Earth’s centre and the satellite). It defines the yaw axis. Vector T is perpendicular to the orbital plane (vector L, vector V). It defines the pitch axis. Vector R completes the set of orthogonal axes. It lies in the plane defined by Vectors L and V and defines the roll axis. It does not coincide exactly with the velocity vector due to the eccentricity of the orbit.  3, fiche 19, Anglais, - roll%20axis

Record number: 19, Textual support number: 2 CONT

Spacecraft axes. The three orthogonal axes of rotation : roll, pitch and yaw. If the spacecraft has a recognisable longitudinal axis or a specified forward direction of flight, the axes are analogous to those of an aircraft, where the roll axis is the longitudinal axis; the pitch axis is in the plane of the wings; and the yaw axis is the "vertical" axis, orthogonal to both the roll and pitch axes. The axes are mutually perpendicular, with an "origin" at the vehicle's centre of mass. For a winged spacecraft such as a Space Shuttle, the similarity with an aircraft is obvious. For expendable launch vehicles the roll axis is the axis which is vertical at launch and the other axes are more-or-less arbitrarily assigned since the vehicle rotates about the roll axis in flight.... The axes of a cylindrical spacecraft(e. g. Apollo, Suyuz, etc.) are similar to those of an ELV [Expendable Launch Vehicle] at launch, but one orbit assume the axis-definition of an aircraft(i. e. defined relative to the pilot's seat). The axes of a satellite mirror those of an aircraft "flying along the orbital arc" : the roll axis is aligned with the direction of travel; the yaw axis passes through the sub-satellite point; and the pitch axis is orthogonal to the other two. For a satellite in an equatorial orbit, the pitch axis is aligned approximately with the Earth's spin axis. The pitch axis is also the spin axis for the spin-stabilised satellite.  4, fiche 19, Anglais, - roll%20axis

Record number: 19, Textual support number: 1 OBS

In the compilation of engineering drawings the three orthogonal axes are often labelled in Cartesian fashion: x=roll, y=pitch, z=yaw. For the three-axis stabilised spacecraft, the x-axis and y-axis are otherwise known as the east-west and north-south axes, respectively; the z-axis passes through the sub-satellite point. This leads to the definition of the box-shaped satellite’s faces as follows: the "plus-x face" faces east; the "minus-x face" faces west; +y faces south; -y faces north; +z is the Earth-pointing face; and -z is the "anti-Earth face."  4, fiche 19, Anglais, - roll%20axis

Record number: 19, Textual support number: 2 OBS

roll axis; axis of roll: terms officially approved by the International Space Station official approval Group (ISSOAG) and by the RADARSAT-2 Terminology Approval Group (RTAG).  5, fiche 19, Anglais, - roll%20axis

Fiche 19,  Justifications,  Français

Record number: 19, Textual support number: 1 CONT

Le repère orbital local est défini en chaque point de l'orbite par les trois vecteurs unitaires. Ces vecteurs sont construits à partir du vecteur position et du vecteur vitesse du satellite : le vecteur L est colinéaire au vecteur position P (sur l'axe centre Terre, satellite). Il définit l'axe de lacet. Le vecteur T est perpendiculaire au plan de l'orbite (vecteur L, vecteur V). Il définit l'axe de tangage. Le vecteur R complète le trièdre. Il appartient au plan (vecteur L, vecteur V) et définit l'axe de roulis. Il ne coïncide pas exactement avec le vecteur vitesse à cause de l'excentricité de l'orbite.  1, fiche 19, Français, - axe%20de%20roulis

Record number: 19, Textual support number: 1 OBS

axe de roulis : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI) et par le Groupe de travail de la terminologie de RADARSAT-2 (GTTR).  2, fiche 19, Français, - axe%20de%20roulis

Fiche 19,  Justifications,  Espagnol

Fiche 20,  Justifications,  Anglais

Record number: 20, Textual support number: 1 CONT

The local orbital reference system is defined at each point of the orbit by three unit vectors. These vectors are derived from the satellite position and velocity vectors: Vector L is colinear with position vector P (on the axis between the Earth’s centre and the satellite). It defines the yaw axis. Vector T is perpendicular to the orbital plane (vector L, vector V). It defines the pitch axis. Vector R completes the set of orthogonal axes. It lies in the plane defined by Vectors L and V and defines the roll axis. It does not coincide exactly with the velocity vector due to the eccentricity of the orbit.  2, fiche 20, Anglais, - pitch%20axis

Record number: 20, Textual support number: 2 CONT

Spacecraft axes. The three orthogonal axes of rotation : roll, pitch and yaw. If the spacecraft has a recognisable longitudinal axis or a specified forward direction of flight, the axes are analogous to those of an aircraft, where the roll axis is the longitudinal axis; the pitch axis is in the plane of the wings; and the yaw axis is the "vertical" axis, orthogonal to both the roll and pitch axes. The axes are mutually perpendicular, with an "origin" at the vehicle's centre of mass. For a winged spacecraft such as a Space Shuttle, the similarity with an aircraft is obvious. For expendable launch vehicles the roll axis is the axis which is vertical at launch and the other axes are more-or-less arbitrarily assigned since the vehicle rotates about the roll axis in flight.... The axes of a cylindrical spacecraft(e. g. Apollo, Suyuz, etc.) are similar to those of an ELV [Expendable Launch Vehicle] at launch, but one orbit assume the axis-definition of an aircraft(i. e. defined relative to the pilot's seat). The axes of a satellite mirror those of an aircraft "flying along the orbital arc" : the roll axis is aligned with the direction of travel; the yaw axis passes through the sub-satellite point; and the pitch axis is orthogonal to the other two. For a satellite in an equatorial orbit, the pitch axis is aligned approximately with the Earth's spin axis. The pitch axis is also the spin axis for the spin-stabilised satellite.  3, fiche 20, Anglais, - pitch%20axis

Record number: 20, Textual support number: 1 OBS

In the compilation of engineering drawings the three orthogonal axes are often labelled in Cartesian fashion: x=roll, y=pitch, z=yaw. For the three-axis stabilised spacecraft, the x-axis and y-axis are otherwise known as the east-west and north-south axes, respectively; the z-axis passes through the sub-satellite point. This leads to the definition of the box-shaped satellite’s faces as follows: the "plus-x face" faces east; the "minus-x face" faces west; +y faces south; -y faces north; +z is the Earth-pointing face; and -z is the "anti-Earth face."  3, fiche 20, Anglais, - pitch%20axis

Record number: 20, Textual support number: 2 OBS

pitch axis: term officially approved by the International Space Station official approval Group (ISSOAG) and by the RADARSAT-2 Terminology Approval Group (RTAG).  4, fiche 20, Anglais, - pitch%20axis

Fiche 20,  Justifications,  Français

Record number: 20, Textual support number: 1 CONT

Le repère orbital local est défini en chaque point de l'orbite par les trois vecteurs unitaires. Ces vecteurs sont construits à partir du vecteur position et du vecteur vitesse du satellite : Le vecteur L est colinéaire au vecteur position P (sur l'axe centre Terre, satellite). Il définit l'axe de lacet. Le vecteur T est perpendiculaire au plan de l'orbite (vecteur L, vecteur V). Il définit l'axe de tangage. Le vecteur R complète le trièdre. Il appartient au plan (vecteur L, vecteur V) et définit l'axe de roulis. Il ne coïncide pas exactement avec le vecteur vitesse à cause de l'excentricité de l'orbite.  2, fiche 20, Français, - axe%20de%20tangage

Record number: 20, Textual support number: 1 OBS

axe de tangage : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI) et par le Groupe de travail de la terminologie de RADARSAT-2.  3, fiche 20, Français, - axe%20de%20tangage

Fiche 20,  Justifications,  Espagnol

Fiche 21,  Justifications,  Anglais

Record number: 21, Textual support number: 1 DEF

Escape from an aircraft by means of an independently propelled seat or capsule.  3, fiche 21, Anglais, - ejection

Record number: 21, Textual support number: 1 OBS

ejection: term and definition standardized by NATO.  4, fiche 21, Anglais, - ejection

Record number: 21, Textual support number: 2 OBS

ejection; ejec: term and abbreviation officially approved by the Department of National Defence and the Canadian Forces.  4, fiche 21, Anglais, - ejection

Fiche 21,  Justifications,  Français

Record number: 21, Textual support number: 1 DEF

Action d'évacuer un aéronef au moyen de sièges ou de capsules munis d'un système de propulsion autonome.  3, fiche 21, Français, - %C3%A9jection

Record number: 21, Textual support number: 1 OBS

éjection : terme et définition normalisés par l'OTAN.  4, fiche 21, Français, - %C3%A9jection

Record number: 21, Textual support number: 2 OBS

éjection; éjec : terme et abréviation uniformisés par le ministère de la Défense nationale et les Forces canadiennes.  4, fiche 21, Français, - %C3%A9jection

Fiche 21,  Justifications,  Espagnol

Record number: 21, Textual support number: 1 DEF

Acción de salir de una aeronave mediante un asiento o cápsula autopropulsada.  1, fiche 21, Espagnol, - expulsi%C3%B3n

Fiche 22,  Justifications,  Anglais

Record number: 22, Textual support number: 1 DEF

[Compartment used] for the stowing of heavy baggage and freight; usually located in the lower part of the fuselage, under the cabin.  3, fiche 22, Anglais, - baggage%20hold

Record number: 22, Textual support number: 1 OBS

baggage : Personal possessions accompanying a passenger on a flight. Usually luggage which will fit below a seat on the aircraft and several larger pieces which are stowed in the baggage compartment of the aircraft. It includes both checked and unchecked baggage, accompanied and unaccompanied baggage of the passenger.  5, fiche 22, Anglais, - baggage%20hold

Record number: 22, Textual support number: 2 OBS

baggage hold: term standardized by ISO.  6, fiche 22, Anglais, - baggage%20hold

Record number: 22, Textual support number: 1 PHR

Door on baggage compartment floor.  7, fiche 22, Anglais, - baggage%20hold

Fiche 22,  Justifications,  Français

Record number: 22, Textual support number: 1 DEF

Compartiment à bagages aménagé dans le fuselage d'un avion.  3, fiche 22, Français, - soute%20%C3%A0%20bagages

Record number: 22, Textual support number: 1 OBS

soute à bagages : terme normalisé par l'ISO.  4, fiche 22, Français, - soute%20%C3%A0%20bagages

Record number: 22, Textual support number: 2 OBS

soute; soute à bagages : termes uniformisés par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes.  4, fiche 22, Français, - soute%20%C3%A0%20bagages

Record number: 22, Textual support number: 1 PHR

Porte sur plancher soute à bagages.  4, fiche 22, Français, - soute%20%C3%A0%20bagages

Fiche 22,  Justifications,  Espagnol

Fiche 23,  Justifications,  Anglais

Record number: 23, Textual support number: 1 OBS

Several different terminologies have been used to describe physiological acceleration. Since the terminology may be based either on the action of the accelerating vehicle or the reaction of the passenger, the terms used are often confusing to a reader without prior knowledge of the system of terminology used. Probably the most easily understood system is the eyeballs in, eyeballs out, eyeballs down, eyeballs up, etc., terminology used by test pilots, which refers to the sensations experienced by the person being accelerated. Thus, the acceleration experienced in an aircraft pullout or inside loop is eyeballs down. Note that, in the NASA vehicle(center of gravity displacement) terminology, this is-az acceleration. Some physiological-acceleration terminologies designate accelerations in terms of the equivalent displacement acceleration of the subject as if he were starting from rest. In such terminologies a man standing up or sitting down on the surface of the earth is experiencing 1 g of headward acceleration because of gravity. Other descriptive terms used in this way are footward, forward(the acceleration experienced by a man pressed into the seat back by an accelerating vehicle), rearward, leftward, rightward, spineward, sternumward, and tailward. One terminology based on reaction uses the terms head-to-foot(the acceleration generated by a pullout in an aircraft), chest-to-back, foot-to-head, and back-to-chest.  2, fiche 23, Anglais, - chest%2Dto%2Dback%20acceleration

Fiche 23,  Justifications,  Français

Fiche 23,  Justifications,  Espagnol

Fiche 24,  Justifications,  Anglais

Record number: 24, Textual support number: 1 DEF

Acceleration of the body in the direction from back to the chest.  2, fiche 24, Anglais, - back%2Dto%2Dchest%20acceleration

Record number: 24, Textual support number: 1 OBS

Several different terminologies have been used to describe physiological acceleration. Since the terminology may be based either on the action of the accelerating vehicle or the reaction of the passenger, the terms used are often confusing to a reader without prior knowledge of the system of terminology used. Probably the most easily understood system is the eyeballs in, eyeballs out, eyeballs down, eyeballs up, etc., terminology used by test pilots, which refers to the sensations experienced by the person being accelerated. Thus, the acceleration experienced in an aircraft pullout or inside loop is eyeballs down. Note that, in the NASA vehicle(center of gravity displacement) terminology, this is-az acceleration. Some physiological-acceleration terminologies designate accelerations in terms of the equivalent displacement acceleration of the subject as if he were starting from rest. In such terminologies a man standing up or sitting down on the surface of the earth is experiencing 1 g of headward acceleration because of gravity. Other descriptive terms used in this way are footward, forward(the acceleration experienced by a man pressed into the seat back by an accelerating vehicle), rearward, leftward, rightward, spineward, sternumward, and tailward. One terminology based on reaction uses the terms head-to-foot(the acceleration generated by a pullout in an aircraft), chest-to-back, foot-to-head, and back-to-chest.  3, fiche 24, Anglais, - back%2Dto%2Dchest%20acceleration

Fiche 24,  Justifications,  Français

Fiche 24,  Justifications,  Espagnol

Fiche 25,  Justifications,  Anglais

Record number: 25, Textual support number: 1 CONT

The Proteus piloted aircraft was designed and built by Scaled Composites, Inc., and is currently also operated by them. It is a twin turbofan high altitude platform with a crew of two and a seat for one additional person. It has a wingspan of 78 ft, gross weight of 12, 500 lb, fuel capacity of 5500 lb, can carry a 6900 lb podded payload, and supply 20 kW payload power.  2, fiche 25, Anglais, - piloted%20aircraft

Record number: 25, Textual support number: 1 OBS

piloted aircraft: term standardized by ISO.  3, fiche 25, Anglais, - piloted%20aircraft

Fiche 25,  Justifications,  Français

Record number: 25, Textual support number: 1 CONT

Sondage atmosphérique. [...] Ces mesures [pression, température, humidité, vent, etc.] sont effectuées soit par capteurs aérotransportés (ballons libres, ou captifs, aéronefs pilotés ou téléguidés) ou largués par avion ou par fusées [...]  2, fiche 25, Français, - a%C3%A9ronef%20pilot%C3%A9

Record number: 25, Textual support number: 1 OBS

aéronef piloté : terme normalisé par l'ISO.  3, fiche 25, Français, - a%C3%A9ronef%20pilot%C3%A9

Fiche 25,  Justifications,  Espagnol

Fiche 26,  Justifications,  Anglais

Record number: 26, Textual support number: 1 CONT

Heading Rapid Alignment... Placing the MAN/STORE/MAG switch in STORE at the end of a flight stores the A/C’s [aircraft] heading. This heading can be used as a reference for azimuth alignment only if the A/C is not moved from the parked position.  3, fiche 26, Anglais, - azimuth%20alignment

Record number: 26, Textual support number: 2 CONT

The aircraft was initially aligned to the right of the lead-in line as it taxied onto the stand and hence the commander's attention was occupied primarily with the aircraft's correct azimuth alignment. The first officer's duty during this manoeuvre was to monitor the alignment and advise the commander of the aircraft's ground speed displayed on the EFIS(Electronic Flight Instrument System). He could not comment on the aircraft's progress in relation to the PAPA as his view of it was obstructed by a windscreen pillar and its alignment was set up for use only by the aircraft's left seat occupant.  4, fiche 26, Anglais, - azimuth%20alignment

Fiche 26,  Justifications,  Français

Record number: 26, Textual support number: 1 CONT

Alignement rapide de cap [...] En plaçant le sélecteur MAN/STORE/MAG à la position STORE à la fin d'un vol, le cap de l'aéronef est mis en mémoire. Ce cap peut être utilisé comme référence pour l'alignement azimutal, seulement si l'avion n'a pas été déplacé de sa position de stationnement.  1, fiche 26, Français, - alignement%20azimutal

Fiche 26,  Justifications,  Espagnol

Fiche 27,  Justifications,  Anglais

Record number: 27, Textual support number: 1 OBS

Airworthiness Notice (AN) published by Transport Canada.  1, fiche 27, Anglais, - Aircraft%20Seat%20Cushions%2DFlammability%20Requirements%2DPetition%20For%20Exemption

Fiche 27,  Justifications,  Français

Record number: 27, Textual support number: 1 OBS

Avis de navigabilité (AN) publié par Transports Canada.  1, fiche 27, Français, - Coussins%20de%20si%C3%A8ge%20d%27a%C3%A9ronef%20%2D%20exigences%20en%20mati%C3%A8re%20d%27inflammabilit%C3%A9%20%2D%20demande%20d%27exemption

Fiche 27,  Justifications,  Espagnol

Fiche 28,  Justifications,  Anglais

Record number: 28, Textual support number: 1 CONT

Civil aircraft passenger seat.  2, fiche 28, Anglais, - passenger%20seat

Fiche 28,  Justifications,  Français

Record number: 28, Textual support number: 1 CONT

Airline Interiors est spécialisée dans l'aménagement intérieur des cabines d'avions et complète ainsi l'offre de Weber dans les sièges passagers, le mobilier (galleys), les blocs toilettes et les escaliers intégrés.  1, fiche 28, Français, - si%C3%A8ge%20passager

Fiche 28,  Justifications,  Espagnol

Fiche 29,  Justifications,  Anglais

Fiche 29,  Justifications,  Français

Record number: 29, Textual support number: 1 OBS

Terme et équivalent extraits du Lexique du CF-18 de Canadair.  2, fiche 29, Français, - raccord%20d%27oxyg%C3%A8ne%20si%C3%A8ge%2Favion

Fiche 29,  Justifications,  Espagnol

Fiche 30,  Justifications,  Anglais

Record number: 30, Textual support number: 1 OBS

The type 9 seat(...) combines many of the features and some of the components of the traditional seat but it has a revised structure to facilitate aircraft maintenance.  2, fiche 30, Anglais, - aircraft%20maintenance

Fiche 30,  Justifications,  Français

Record number: 30, Textual support number: 1 OBS

l'--. (...) Habituellement, on distingue différents degrés d'entretien: (...) le petit entretien (...) le grand entretien [ ainsi que les révisions générales ]  1, fiche 30, Français, - entretien%20des%20avions

Fiche 30,  Justifications,  Espagnol

Fiche 31,  Justifications,  Anglais

Record number: 31, Textual support number: 1 DEF

part of aircraft ejection seat assembly, consists of a case, primer and propellant charge and is positioned in the breech assembly by a retainer.  1, fiche 31, Anglais, - impulse%20cartridge

Fiche 31,  Justifications,  Français

Fiche 31,  Justifications,  Espagnol

Fiche 32,  Justifications,  Anglais

Record number: 32, Textual support number: 1 DEF

The distance between the front edge of one seat in an aircraft and the front edge of the seat immediately in front when both are in an upright position.  2, fiche 32, Anglais, - seat%20pitch

Record number: 32, Textual support number: 1 CONT

Seat pitch on the 50-seater Dash-7 [aircraft] is 31 inches-about the same as Economy class within Europe./  3, fiche 32, Anglais, - seat%20pitch

Fiche 32,  Justifications,  Français

Record number: 32, Textual support number: 1 CONT

En classe économique, le pas actuel est en moyenne de 32 pouces (81,2) seulement, et la largeur allouée par passager (à hauteur des épaules) n'atteint parfois que 17 à 18 pouces (43,2 à 45,7 cm).  1, fiche 32, Français, - pas

Fiche 32,  Justifications,  Espagnol

Fiche 33,  Justifications,  Anglais

Record number: 33, Textual support number: 1 CONT

The F-7M [Airguard] improvements include a HUD and weapon aiming computer,... Cheng Aircraft Corp. Zero-zero ejection seat and additional outboard pylons.  1, fiche 33, Anglais, - zero%2Dzero%20ejection%20seat

Fiche 33,  Justifications,  Français

Record number: 33, Textual support number: 1 CONT

Parmi les nouveautés que comporte le F-7M figurent notamment un collimateur avec calculateur de tir, (...) un siège éjectable zéro-zéro Cheng Aircraft Corp et des mâts supplémentaires pour charges extérieures.  1, fiche 33, Français, - si%C3%A8ge%20%C3%A9jectable%20z%C3%A9ro%2Dz%C3%A9ro

Fiche 33,  Justifications,  Espagnol

Fiche 34,  Justifications,  Anglais

Record number: 34, Textual support number: 1 CONT

PAPA-Parallax Aircraft Parking Aid. 1. This system is designed for use by the pilot occupying the LEFT seat. 2. The equipment consists of a reference board with either one or two horizontal slots running across its centre. A white fluorescent tube is positioned vertically behind the board. 3. As the aircraft approaches the stand, the fluorescent tube will appear to move along the slot towards the reference marks. 4. When the tubular light registers in line with the appropriate reference mark, the aircraft has reached the correct stopping position.  3, fiche 34, Anglais, - parallax%20aircraft%20parking%20aid

Fiche 34,  Justifications,  Français

Record number: 34, Textual support number: 1 OBS

Terme et abréviation uniformisés par le CUTA Opérations aériennes.  2, fiche 34, Français, - syst%C3%A8me%20parallaxe%20de%20stationnement

Fiche 34,  Justifications,  Espagnol

Fiche 35,  Justifications,  Anglais

Record number: 35, Textual support number: 1 CONT

Other new features [International Passenger Reservation System] include the release of unsold space to unmechanized offices along the route, after the departure of the aircraft. A Preliminary Load Summary will be provided, giving the authorization, by class, out of each boarding-point, together with true seat availability(not adjusted by the over-booking profile).  1, fiche 35, Anglais, - Preliminary%20Load%20Summary

Fiche 35,  Justifications,  Français

Record number: 35, Textual support number: 1 CONT

Des résumés de chargement préliminaire et définitif (Preliminary Load Summary et Final Load Summary) seront également fournis, comportant par classe le nombre de passagers autorisés à embarquer à chaque escale, ainsi que le nombre exact de sièges disponibles, et indiquant l'existence éventuelle de listes d'attente.  1, fiche 35, Français, - r%C3%A9sum%C3%A9%20de%20chargement%20pr%C3%A9liminaire

Fiche 35,  Justifications,  Espagnol

Fiche 36,  Justifications,  Anglais

Record number: 36, Textual support number: 1 DEF

The process of abandonment of an aircraft in flight by use of a parachute. Generally used more specifically for such action unassisted by an ejection seat, escape capsule or similar device.  1, fiche 36, Anglais, - bail%20out

Fiche 36,  Justifications,  Français

Record number: 36, Textual support number: 1 DEF

Action d'abandonner le bord d'un aéronef en vol en utilisant un parachute. généralement ce terme est utilisé d'une manière plus spécifique pour signifier une telle action sans l'assistance d'un siège éjectable, ni d'une capsule éjectable, ni d'un dispositif similaire.  1, fiche 36, Français, - bail%2Dout

Fiche 36,  Justifications,  Espagnol

Fiche 37,  Justifications,  Anglais

Record number: 37, Textual support number: 1 DEF

a system of straps encircling the torso and upper thighs, which may be donned in the crew room and subsequently mated by quick-release fastenings to the seat and/or parachute in the aircraft. This type of harness can thus be readily adjusted to the individual' s bodily configuration and also incorporated in a garment.  1, fiche 37, Anglais, - torso%20harness

Fiche 37,  Justifications,  Français

Record number: 37, Textual support number: 1 DEF

un système de lanières entourant le torse et la partie supérieure des cuisses, qui peuvent être ajustées avant le vol dans la salle du personnel navigant et ensuite être reliées au siège et/ou au parachute dans l'avion par des attaches pouvant être libérées par un dispositif «quick-release». Ce type de harnais peut donc être facilement ajusté à la configuration corporelle de l'individu et aussi être incorporé dans un vêtement.  1, fiche 37, Français, - harnais%20de%20torse

Fiche 37,  Justifications,  Espagnol

Fiche 38,  Justifications,  Français

Fiche 38,  Justifications,  Espagnol