TERMIUM Plus^®

Fiche 1,  Justifications,  Anglais

Record number: 1, Textual support number: 1 CONT

To select reverse thrust after landing, the flight crew lifts the reverse-thrust levers. An electrically operated "balk" blocks each lever at the reverse-idle position until the thrust reversers deploy. Then each balk is removed to allow selection of full-reverse thrust. This electrically operated balk replaces the thrust control cable interlock used on previous 737s.  3, fiche 1, Anglais, - balk

Fiche 1,  Justifications,  Français

Record number: 1, Textual support number: 1 OBS

butée : terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Maintenance.  2, fiche 1, Français, - but%C3%A9e

Fiche 1,  Justifications,  Espagnol

Fiche 2,  Justifications,  Anglais

Record number: 2, Textual support number: 1 OBS

The aileron trim control system controls the movement of the aileron trim tabs to provide lateral trim. The system is controlled mechanically by a control knob on the control pedestal in the flight compartment.... The control knob is mounted on the end of a shaft in the trim control mechanism. A drum on the opposite end of the shaft is connected by a two-way cable system to a drum on a shaft located in the right wheel well. Another drum at the base of the same shaft is connected by a second cable system routed along the rear spar of each wing to the trim tab actuators. The actuators are connected to the trim tabs by a pushrod. A trim position indicator is connected mechanically to the trim control knob.  2, fiche 2, Anglais, - output%20drum

Fiche 2,  Justifications,  Français

Record number: 2, Textual support number: 1 OBS

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

Fiche 2,  Justifications,  Espagnol

Fiche 3,  Justifications,  Anglais

Record number: 3, Textual support number: 1 OBS

The aileron trim control system controls the movement of the aileron trim tabs to provide lateral trim. The system is controlled mechanically by a control knob on the control pedestal in the flight compartment.... The control knob is mounted on the end of a shaft in the trim control mechanism. A drum on the opposite end of the shaft is connected by a two-way cable system to a drum on a shaft located in the right wheel well. Another drum at the base of the same shaft is connected by a second cable system routed along the rear spar of each wing to the trim tab actuators. The actuators are connected to the trim tabs by a pushrod. A trim position indicator is connected mechanically to the trim control knob.  2, fiche 3, Anglais, - input%20drum

Fiche 3,  Justifications,  Français

Record number: 3, Textual support number: 1 OBS

tambour de commande : terme accepté par le Comité d'étude de la terminologie des cartes de travail du DC-9.  2, fiche 3, Français, - tambour%20de%20commande

Fiche 3,  Justifications,  Espagnol

Fiche 4,  Justifications,  Anglais

Record number: 4, Textual support number: 1 OBS

The aileron torque tube and override mechanism is located below the flight compartment floor in the electrical/electronics compartment. The torque tube interconnects the two aileron cable systems so that either control wheel can operate both systems. The override mechanism allows either control wheel to operate one control tab if the other tab becomes inoperative.  2, fiche 4, Anglais, - aileron%20torque%20tube

Fiche 4,  Justifications,  Français

Record number: 4, Textual support number: 1 OBS

tube de torsion de commande d'aileron : terme accepté par le Comité d'étude de la terminologie des cartes de travail du DC-9.  2, fiche 4, Français, - tube%20de%20torsion%20de%20commande%20d%27aileron

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 aileron sectors and load-feel cranks are located on the rear spar of each wing at the inboard end of the aileron. The sectors transmit movement of the cable systems through mechanical linkage to the control tabs and ailerons. The load-feel cranks provide a simulated feel of aileron flight load at the aileron control wheels and also act as a centering device to return the aileron control system to neutral. The two sectors and two load-feel cranks are mounted on a common bolt in the inboard aileron hinge support bracket.... The load-feel cranks are installed between the two sectors and are connected to each other by a spring at one end. Adjustable stopbolts at the other end of each crank are in contact with a stop on the wing structure. Adjustable stopbolts, midway along each crank, are in contact with stopbolts on a boss on the control tab sector.  2, fiche 6, Anglais, - load%2Dfeel%20crank

Fiche 6,  Justifications,  Français

Record number: 6, Textual support number: 1 OBS

biellette de sensation artificielle : terme accepté par le Comité d'étude de la terminologie des cartes de travail du DC-9.  2, fiche 6, Français, - biellette%20de%20sensation%20artificielle

Fiche 6,  Justifications,  Espagnol

Fiche 7,  Justifications,  Français

Fiche 7,  Justifications,  Espagnol

Fiche 8,  Justifications,  Anglais

Record number: 8, Textual support number: 1 CONT

Each elevator is driven in parallel by three individual powered control units and a separate cable run links each elevator to the control column on its side of the flight deck. The control columns are linked by a load-limiting coupling and the elevator actuators themselves by a transverse cable loop.  1, fiche 8, Anglais, - load%2Dlimiting%20coupling

Fiche 8,  Justifications,  Français

Record number: 8, Textual support number: 1 CONT

Chaque gouverne de profondeur est actionnée en parallèle par trois servocommandes distinctes et reliée par un câble à celui des deux manches qui est situé du même côté du poste de pilotage. Les deux manches sont interconnectés par l'intermédiaire d'un coupleur-limiteur de réaction et les actionneurs des gouvernes de profondeur sont reliés par un câble transversal aller-retour.  1, fiche 8, Français, - coupleur%2Dlimiteur%20de%20r%C3%A9action

Fiche 8,  Justifications,  Espagnol

Fiche 9,  Justifications,  Anglais

Record number: 9, Textual support number: 1 CONT

Each elevator is driven in parallel by three individual powered control units and a separate cable run links each elevator to the control column on its side of the flight deck. The control columns are linked by a load-limiting coupling and the elevator actuators themselves by a transverse cable loop.  1, fiche 9, Anglais, - transverse%20cable%20loop

Fiche 9,  Justifications,  Français

Record number: 9, Textual support number: 1 CONT

Chaque gouverne de profondeur est actionnée en parallèle par trois servocommandes distinctes et reliée par un câble à celui des deux manches qui est situé du même côté du poste de pilotage. Les deux manches sont interconnectés par l'intermédiaire d'un coupleur-limiteur de réaction et les actionneurs des gouvernes de profondeur sont reliés par un câble transversal aller-retour.  1, fiche 9, Français, - c%C3%A2ble%20transversal%20aller%2Dretour

Fiche 9,  Justifications,  Espagnol

Fiche 10,  Justifications,  Anglais

Record number: 10, Textual support number: 1 CONT

(The Capstan) consists of a grooved drum, the cable attached to the flight control linkage is wound around this drum.  1, fiche 10, Anglais, - grooved%20drum

Fiche 10,  Justifications,  Français

Record number: 10, Textual support number: 1 CONT

[le cabestan] est composé d'un tambour à gorges sur lequel est enroulé un câble relié à la timonerie de la commande de gouverne.  1, fiche 10, Français, - tambour%20%C3%A0%20gorges

Fiche 10,  Justifications,  Espagnol

Fiche 11,  Justifications,  Français

Fiche 11,  Justifications,  Espagnol