TERMIUM Plus^®

Record 1,  Textual support,  English

Record number: 1, Textual support number: 1 CONT

The command bars move up for a climb or down for descent, and roll left or right to provide lateral guidance. They display the computed angle of bank for standard-rate turns to enable the pilot to reach and fly a selected heading or track. The bars also show pitch commands that allow the pilot to capture and fly an ILS [instrument landing system] glide slope, a preselected pitch attitude, or maintain a selected barometric altitude.  2, record 1, English, - pitch%20command

Record 1,  Textual support,  French

Record number: 1, Textual support number: 1 OBS

directive en tangage : terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA)- Opérations aériennes.  2, record 1, French, - directive%20en%20tangage

Record 1,  Textual support,  Spanish

Record 2,  Textual support,  English

Record number: 2, Textual support number: 1 DEF

A rotor system in which each of the blades is connected to the rotor hub in such a way that it is free to change its pitch angle, and move up and down and fore and aft in its plane of rotation.  2, record 2, English, - articulated%20rotor

Record number: 2, Textual support number: 1 OBS

articulated rotor: term officially approved by the Aeronautical Terminology Standardization Committee (ATSC) - Helicopters.  3, record 2, English, - articulated%20rotor

Record 2,  Textual support,  French

Record number: 2, Textual support number: 1 OBS

rotor articulé : terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA) – Hélicoptères.  2, record 2, French, - rotor%20articul%C3%A9

Record 2,  Textual support,  Spanish

Record 3,  Textual support,  French

Record 3,  Textual support,  Spanish

Record 4,  Textual support,  English

Record number: 4, Textual support number: 1 CONT

To recover from the microburst, the crew apply maximum power and pitch up toward an angle that can attain 15 degrees. The inertial acceleration(acceleration in reference to the ground, as opposed to acceleration within the airmass) experienced by the pilots, combined with the unstable attitude of the aircraft may cause a dangerous illusion. The pilots may believe that the aircraft has reached a very high excess energy and thus, try to pitch down or reduce the engine power. In reality, the aircraft performance is still low as it penetrates the energy-reducing downdraft and tailwind components of the microburst.  2, record 4, English, - inertial%20acceleration

Record 4,  Textual support,  French

Record number: 4, Textual support number: 1 CONT

Rossby (nombre de) : Quantité sans dimension, utile dans l'étude du mouvement des atmosphères planétaires et égale au rapport de l'accélération inertielle (force d'inertie) à l'accélération de Coriolis due à la rotation de la planète.  2, record 4, French, - acc%C3%A9l%C3%A9ration%20inertielle

Record 4,  Textual support,  Spanish

Record 5,  Textual support,  English

Record number: 5, Textual support number: 1 CONT

V-bar : Flight Director Indicator... The V-bar command indicator is a pair of yellow, wedge-shaped V-bars that move up or down to command a climb or descent, and roll left or right to command a bank. The flight director system commands the V-bars to capture and track the selected heading or radio signals; or to maintain a desired pitch angle, glidepath, or an optimum speed during SC(speed command) operation. To satisfy the commands, the aircraft is maneuvered so that the airplane symbol is flown into the V-bars until the two are aligned. Input signals to the V-bars depend upon the mode of operation. The V-bars are biased from view by the instrument failure warning system; when loss of signal occurs, or sensing circuits fail that are associated with the selected mode of operation. They are also out of view when the mode selector control is in the OFF position.  3, record 5, English, - tendency%20bar

Record 5,  Textual support,  French

Record number: 5, Textual support number: 1 CONT

L'indicateur HZ-4 [horizon directeur de vol] assume deux fonctions. Il réalise la combinaison d'un horizon artificiel et d'un indicateur de tendances du type "zero reader". [...] Les deux barres, verticales et horizontale, sont les barres de tendance liées au calculateur de vol. La barre verticale reçoit les informations du canal de direction, la barre horizontale celles fournies par le canal de profondeur.  3, record 5, French, - barre%20de%20tendance

Record number: 5, Textual support number: 2 CONT

[...], dès que l'avion ne sera plus dans la situation requise, les 2 barres ou repères, appelés BARRES ou REPÈRES DE TENDANCES ne seront plus dans une position médiane vis à vis du cadran de l'indicateur.  2, record 5, French, - barre%20de%20tendance

Record number: 5, Textual support number: 1 OBS

barre de tendance : terme accepté par le Comité d'étude de la terminologie des cartes de travail du DC-9.  4, record 5, French, - barre%20de%20tendance

Record 5,  Textual support,  Spanish

Record 6,  Textual support,  English

Record number: 6, Textual support number: 1 CONT

ACMRI has four basic sub-systems. First is a sidewinder-shaped external pod which attaches to the aircraft's missile mounting rack and contains instrumentation independent of the aircraft's own systems to measure altitude, airspeed, Mach number, angle of attack and sideslip, plus a compact inertial sensor which measures pitch, roll, heading and acceleration/deceleration. The instrumentation package... also contains a transponder-like radio link which transmits all this information down on command from the second sub-system, the ground tracking station network... the third sub-system-the Control and Computation facility... precise aircraft position determination, and data formatting prior to reaching the fourth... sub-system... the Display and Debriefing Sub-system.  3, record 6, English, - air%20combat%20manoeuvering%20range%20instrumentation

Record 6,  Textual support,  French

Record 6,  Textual support,  Spanish

Record 7,  Textual support,  English

Record number: 7, Textual support number: 1 CONT

With the German government research establishment DFVLR, Dornier is developing an Open-Loop Gust Alleviation(OLGA) system. Gusts are sensed by an angle of attack vane at the nose, pitch rate gyro and vertical accelerometer : gust responses are dampened by moving both ailerons up or down simultaneously in association with the elevator.  1, record 7, English, - Open%2DLoop%20Gust%20Alleviation%20system

Record 7,  Textual support,  French

Record number: 7, Textual support number: 1 CONT

A noter par ailleurs qu'il met au point, en collaboration avec l'institut de recherches DFVLR, un système amortisseur de turbulences à boucle ouverte (...)  1, record 7, French, - syst%C3%A8me%20amortisseur%20de%20turbulences%20%C3%A0%20boucle%20ouverte

Record 7,  Textual support,  Spanish