TERMIUM Plus^®

Fiche 1,  Justifications,  Anglais

Record number: 1, Textual support number: 1 OBS

The somatosensory system consists of numerous pressure receptors contained within the muscles, tendons, joints, and skin. This system reacts to the sensations resulting from pressures or stretch on joints, muscles and skin and also from slight changes in the position of internal organs. These are the forces that act on the seated pilot in flight. It is closely associated with the vestibular system and to a lesser degree, the visual system. They allow the pilot to sense certain complex motions and forces of flight such as aircraft feel(buffet, control forces, rudder, trim force) and "G" forces.  2, fiche 1, Anglais, - seat%2Dof%2Dthe%2Dpants%20flying

Fiche 1,  Justifications,  Français

Fiche 1,  Justifications,  Espagnol

Fiche 2,  Justifications,  Anglais

Record number: 2, Textual support number: 1 CONT

The other component of the turn coordinator is the inclinometer, better known as the rudder ball. This is a black ball in a liquid-filled, curved and sealed tube. The ball is there to help keep your turns coordinated. That is, to prevent the airplane's tail from skidding to the outside of a turn or slipping to the inside. In a skid, the ball will roll opposite to the direction of the turn; In a [slip], the ball moves to the inside of the turn. To prevent slips or skids, pilots are told to "step on the ball, "meaning apply pressure to the rudder corresponding to the ball' s location. Ball left? Step on the left rudder until the ball centers.  2, fiche 2, Anglais, - step%20on%20the%20ball

Fiche 2,  Justifications,  Français

Record number: 2, Textual support number: 1 OBS

Noter la transposition de la locution verbale à la locution nominale; sorte de commandement ou de rappel invitant le pilote à appuyer sur la pédale du palonnier côté bille.  1, fiche 2, Français, - palonnier%20sur%20la%20bille

Fiche 2,  Justifications,  Espagnol

Fiche 3,  Justifications,  Anglais

Record number: 3, Textual support number: 1 CONT

Carry out leak test as follows : with rudder "neutral", very slowly apply pressure to 304 knots & close leak test valve, let stand for 2 minutes. If pressure drops below 295 knots, corrective action must be taken before proceeding. Open leak test valve & slowly reduce pressure to "zero".  2, fiche 3, Anglais, - leak%20test

Fiche 3,  Justifications,  Français

Record number: 3, Textual support number: 1 OBS

essai d'étanchéité : terme accepté par le Comité d'étude de la terminologie des cartes de travail du DC-9.  2, fiche 3, Français, - essai%20d%27%C3%A9tanch%C3%A9it%C3%A9

Fiche 3,  Justifications,  Espagnol

Fiche 4,  Justifications,  Anglais

Record number: 4, Textual support number: 1 CONT

The nose gear uplock release mechanism provides a mechanical means for upsetting the nose gear overcenter linkage and releasing the nose gear from the uplocked position when hydraulic pressure is not available to extend the gear. The uplock release mechanism consists of a cable, cable sector, shaft, return spring, and upset arm.  2, fiche 4, Anglais, - uplock%20release%20mechanism

Record number: 4, Textual support number: 2 CONT

The uplock release mechanism and pressure can are installed on the pressure bulkhead above the nosegear strut. Part of the mechanism is installed inside the pressure can and is accessible through the floor panel under the rudder pedals in the forward part of the flight compartment. The external portion of the mechanism is accessible through the nosegear doors.  3, fiche 4, Anglais, - uplock%20release%20mechanism

Fiche 4,  Justifications,  Français

Record number: 4, Textual support number: 1 OBS

mécanisme de déverrouillage train rentré : terme accepté par le Comité d'étude de la terminologie des cartes de travail du DC-9.  2, fiche 4, Français, - m%C3%A9canisme%20de%20d%C3%A9verrouillage%20train%20rentr%C3%A9

Fiche 4,  Justifications,  Espagnol

Fiche 5,  Justifications,  Anglais

Record number: 5, Textual support number: 1 CONT

The rudder hydraulic power shutoff system controls the supply of hydraulic pressure to the rudder hydraulic power package. The system is mechanically controlled by a lever in the flight compartment. The shutoff system consists of a hydraulic shutoff valve, located in the aft accessory compartment below the right air conditioning unit, connected by a two-way cable system to a control lever on the control pedestal. The shutoff valve is connected, by hydraulic lines, to the right hydraulic power system and the hydraulic power package.  2, fiche 5, Anglais, - rudder%20hydraulic%20power%20shutoff%20system

Fiche 5,  Justifications,  Français

Record number: 5, Textual support number: 1 OBS

circuit d'arrêt hydraulique gouverne de direction : terme accepté par le Comité d'étude de la terminologie des cartes de travail du DC-9.  2, fiche 5, Français, - circuit%20d%27arr%C3%AAt%20hydraulique%20gouverne%20de%20direction

Fiche 5,  Justifications,  Espagnol

Fiche 6,  Justifications,  Anglais

Record number: 6, Textual support number: 1 CONT

The [nosegear] uplock release mechanism and pressure can are installed on the pressure bulkhead above the nosegear strut. Part of the mechanism is installed inside the pressure can and is accessible through the floor panel under the rudder pedals in the forward part of the flight compartment. The external portion of the mechanism is accessible through the nosegear doors.  2, fiche 6, Anglais, - pressure%20can

Fiche 6,  Justifications,  Français

Record number: 6, Textual support number: 1 OBS

logement pressurisé : terme accepté par le Comité d'étude de la terminologie des cartes de travail du DC-9.  2, fiche 6, Français, - logement%20pressuris%C3%A9

Fiche 6,  Justifications,  Espagnol

Fiche 7,  Justifications,  Anglais

Record number: 7, Textual support number: 1 OBS

ICAO C-88-an 74-II, p. 5.  1, fiche 7, Anglais, - rudder%20pressure

Fiche 7,  Justifications,  Français

Fiche 7,  Justifications,  Espagnol