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Record 1,  Textual support,  English

Record number: 1, Textual support number: 1 CONT

The autopilot control panel... provides the pilot with fingertip controls by which he can conveniently engage or disengage the system, adjust the alertness or speed of its responses to flight deviations, or trim the system for varying load and flight conditions.  4, record 1, English, - autopilot%20controller%20panel

Record 1,  Textual support,  French

Record number: 1, Textual support number: 1 DEF

Panneau qui permet de sélecter les modes de pilotage automatiques souhaités.  4, record 1, French, - panneau%20de%20commande%20pilote%20automatique

Record number: 1, Textual support number: 1 OBS

panneau de commande pilote automatique; panneau de commande PA : termes uniformisés par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes.  5, record 1, French, - panneau%20de%20commande%20pilote%20automatique

Record 1,  Textual support,  Spanish

Record 2,  Textual support,  English

Record number: 2, Textual support number: 1 CONT

The digital fly-by-wire control system [on the J8IIM plane] has been successfully developed. It mainly consists of such sub-systems as the flying control computer, the pilot sensor assembly, the accelerometer, the caution panel and trim interface, and the rate gyro, etc.  2, record 2, English, - digital%20fly%2Dby%2Dwire%20control

Record 2,  Textual support,  French

Record number: 2, Textual support number: 1 CONT

Le couple plan de canard et commande de vol numérique très en vogue à l'heure actuelle confère à l'Eurofighter une excellente manœuvrabilité.  2, record 2, French, - commande%20de%20vol%20num%C3%A9rique

Record number: 2, Textual support number: 1 PHR

commande de vol électrique numérique  3, record 2, French, - commande%20de%20vol%20num%C3%A9rique

Record 2,  Textual support,  Spanish

Record 3,  Textual support,  English

Record number: 3, Textual support number: 1 CONT

The elevator trim tab control system incorporates an autopilot servomotor. This system provides automatic trimming of the aircraft in the pitch axis.  3, record 3, English, - autopilot%20servo

Record 3,  Textual support,  French

Record number: 3, Textual support number: 1 OBS

servo pilote automatique : terme uniformisé par le Comité d’uniformisation de la terminologie aéronautique (CUTA) – Opérations aériennes.  5, record 3, French, - servomoteur%20du%20pilote%20automatique

Record 3,  Textual support,  Spanish

Record 4,  Textual support,  English

Record number: 4, Textual support number: 1 DEF

A rudimentary manual control of the aircraft using pitch trim and rudder pedals to facilitate recovery at the aircraft electrical system or land the aircraft as soon as is practicable.  2, record 4, English, - manual%20reversion

Record 4,  Textual support,  French

Record 4,  Textual support,  Spanish

Record 5,  Textual support,  English

Record number: 5, Textual support number: 1 DEF

Act or process of building up a complete unit (as a motor vehicle) using parts already in themselves finished manufactured products.  1, record 5, English, - assembly

Record number: 5, Textual support number: 1 CONT

Starting with a bare chassis, components are attached successively as the growing assemblage moves along the conveyor.... An intricate system of production scheduling and control ensures that the right body type and colour, trim, engine and optional equipment arrive together for assembly, for a number of individual assembly combinations are on the line simultaneously.  2, record 5, English, - assembly

Record 5,  Textual support,  French

Record number: 5, Textual support number: 1 DEF

Opération qui consiste à assembler les éléments mécaniques d'une automobile (moteur et suspension) à la carrosserie.  1, record 5, French, - coiffage

Record number: 5, Textual support number: 1 CONT

L'avantage du convoyeur double rail est de permettre [...] d'utiliser des sections élévatrices (notamment pour le poste de coiffage ou la dépose de voitures finies).  1, record 5, French, - coiffage

Record 5,  Textual support,  Spanish

Record 6,  Textual support,  English

Record number: 6, Textual support number: 1 OBS

Speed-attitude correction is provided by the mach trim compensation system. Mach trim compensation automatically provides forces to the control column(elevator) to compensate for nosedown pitching moments of the airplane at high Mach number.  2, record 6, English, - Mach%20trim%20compensator

Record number: 6, Textual support number: 2 OBS

pitch trim compensator (DC-8); PTC (DC-8).  3, record 6, English, - Mach%20trim%20compensator

Record 6,  Textual support,  French

Record number: 6, Textual support number: 1 OBS

Un «pitch trim actuator» peut parfois être un vérin compensateur de Mach, mais il existe de nombreux avions auxquels la notion de Mach ne s'applique pas, mais qui sont quand même munis d'un «pitch trim actuator». Ce serait le cas, par exemple, du très populaire Dash8. Dans ce cas, on parlerait de «vérin de compensateur de profondeur», par exemple. Sur de nombreux avions, il n'y a pas de vérin distinct pour la compensation de Mach, mais simplement un circuit qui agit sur le compensateur de profondeur quand le centre de poussée recule à mesure que la vitesse de l'écoulement sur l'aile s'approche de la vitesse du son.  4, record 6, French, - compensateur%20de%20Mach

Record number: 6, Textual support number: 2 OBS

compensateur de Mach; MTC; PTC : terme et abréviations uniformisés par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes.  5, record 6, French, - compensateur%20de%20Mach

Record number: 6, Textual support number: 3 OBS

compensateur de Mach; compensateur de tangage : termes acceptés par le Comité d'étude de la terminologie des cartes de travail du DC-9.  5, record 6, French, - compensateur%20de%20Mach

Record 6,  Textual support,  Spanish

Record 7,  Textual support,  English

Record number: 7, Textual support number: 1 PHR

Aileron, brake, control surface, failsafe nozzle, landing gear, leading-edge slat, main landing gear door, slat, trim actuator, wing flap actuating system.  2, record 7, English, - actuating%20system

Record number: 7, Textual support number: 2 PHR

Electrical, hydraulic, pneumatic actuating system.  2, record 7, English, - actuating%20system

Record 7,  Textual support,  French

Record number: 7, Textual support number: 1 OBS

système d'actionnement : terme uniformisé par les Comités d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes et Maintenance.  2, record 7, French, - syst%C3%A8me%20d%27actionnement

Record number: 7, Textual support number: 1 PHR

Système d'actionnement des gouvernes, des volets, d'un inverseur de poussée, d'une surface de commande de vol.  2, record 7, French, - syst%C3%A8me%20d%27actionnement

Record number: 7, Textual support number: 2 PHR

Système d'actionnement électrique, hydraulique.  2, record 7, French, - syst%C3%A8me%20d%27actionnement

Record 7,  Textual support,  Spanish

Record 8,  Textual support,  English

Record number: 8, Textual support number: 1 CONT

The elevator feel system supplies feel forces to the control system. The feel forces developed will vary depending upon airspeed and stabilizer trim. The feel system contains two basic units : the feel and centering mechanism [and] the feel computer. The feel and centering unit consists of a cam, spring-loaded follower, two hydraulic actuators and related linkage.  2, record 8, English, - elevator%20feel%20system

Record number: 8, Textual support number: 1 OBS

The "feel" is what allows the pilot to know how much pressure is needed for system operation.  3, record 8, English, - elevator%20feel%20system

Record 8,  Textual support,  French

Record number: 8, Textual support number: 1 OBS

système de sensation profondeur : terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Maintenance.  2, record 8, French, - syst%C3%A8me%20de%20sensation%20profondeur

Record 8,  Textual support,  Spanish

Record 9,  Textual support,  English

Record number: 9, Textual support number: 1 CONT

An independent manual trim system provides elevator back-up control and works on a simple worm gear mechanism.  3, record 9, English, - worm%20gear%20mechanism

Record 9,  Textual support,  French

Record number: 9, Textual support number: 1 CONT

Le circuit de compensation de la gouverne de profondeur est un mécanisme à vis sans fin actionné par câble.  2, record 9, French, - m%C3%A9canisme%20%C3%A0%20vis%20sans%20fin

Record 9,  Textual support,  Spanish

Record 10,  Textual support,  English

Record number: 10, 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, record 10, English, - seat%2Dof%2Dthe%2Dpants%20flying

Record 10,  Textual support,  French

Record 10,  Textual support,  Spanish

Record 11,  Textual support,  English

Record number: 11, Textual support number: 1 CONT

The POES satellites include an integrated system for guidance and control of orbital injection following separation from the Atlas vehicle. The Reaction Control Equipment(RCE) provides ascent phase, attitude control(3 axis), and orbital velocity trim for final injection. The RCE is operational from Atlas separation to handover to the orbital control system.  2, record 11, English, - reaction%20control%20equipment

Record 11,  Textual support,  French

Record 11,  Textual support,  Spanish

Record 12,  Textual support,  English

Record number: 12, Textual support number: 1 DEF

Generally in an aerodynamic vehicle, a system wherein horizontal surfaces used for trim and control are forward of the main lifting surfaces.  1, record 12, English, - canard%20system

Record 12,  Textual support,  French

Record 12,  Textual support,  Spanish

Record 13,  Textual support,  English

Record number: 13, 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, record 13, English, - input%20drum

Record 13,  Textual support,  French

Record number: 13, 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, record 13, French, - tambour%20de%20commande

Record 13,  Textual support,  Spanish

Record 14,  Textual support,  English

Record number: 14, Textual support number: 1 CONT

Speed-attitude correction is provided by the Mach trim compensation system. Mach trim compensation automatically provides forces to the control column(elevator) to compensate for nosedown pitching moments of the airplane at high Mach number. Control column position is effected by the Mach trim actuator installed at the lower part of the first officer's control column control mechanism. The actuator receives command signals from the stability augmentation computer. Mach number is computed from pitot and static air pressure input changes to the air data computer(ADC-1). The air data computer shapes the information and transmits it to the stability augmentation computer where it is further shaped and then transmitted to the actuator to command control column and elevator movement.  1, record 14, English, - Mach%20trim%20servo%20actuator

Record 14,  Textual support,  French

Record number: 14, Textual support number: 1 OBS

servocommande du compensateur de Mach : terme accepté par le Comité d'étude de la terminologie des cartes de travail du DC-9.  2, record 14, French, - servocommande%20du%20compensateur%20de%20Mach

Record 14,  Textual support,  Spanish

Record 15,  Textual support,  English

Record number: 15, 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, record 15, English, - output%20drum

Record 15,  Textual support,  French

Record number: 15, 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, record 15, French, - tambour%20command%C3%A9

Record 15,  Textual support,  Spanish

Record 16,  Textual support,  English

Record number: 16, Textual support number: 1 CONT

The electrical flying control system is based on two independent systems, the Elevator Aileron Computers(ELAC) and the Spoiler Elevator Computers(SEC). The Spoiler Elevator Computer System... consists of a trio of computers, which will produce commands in the roll axis by operating the two outer spoiler panels on each wing; speed-braking in flight by operating the three inner spoiler panels; lift-dumping after landing by raising all ten spoiler panels; stand-by pitch axis control in support of the ELAC by operating the elevators and automatic trim, also as a stand-by to the ELAC, by adjusting tailplane incidence.  1, record 16, English, - spoiler%20elevator%20computer

Record 16,  Textual support,  French

Record number: 16, Textual support number: 1 CONT

L'architecture des CDVE [commandes de vol électriques] comporte deux systèmes indépendants : l'ELAC (Elevator Aileron Computers = calculateurs de profondeur et d'ailerons) et le SEC (Spoiler and Elevator Computers = calculateurs de profondeur et des spoilers). Le système SEC [...] comporte trois calculateurs qui contrôlent la fonction roulis des quatre spoilers extérieurs, la fonction aérofrein au sol par le déploiement des dix spoilers, la fonction tangage en secours de l'ELAC par action sur la gouverne de profondeur, et enfin la fonction auto-trim, également en secours de l'ELAC, par action sur le stabilisateur horizontal.  1, record 16, French, - calculateur%20de%20profondeur%20et%20des%20spoilers

Record 16,  Textual support,  Spanish

Record 17,  Textual support,  English

Record number: 17, Textual support number: 1 CONT

The primary longitudinal trim control system consists of two control wheel switches in the outboard horn of each aileron control wheel; dual control handles located on the left side of the control pedestal....  2, record 17, English, - control%20handle

Record 17,  Textual support,  French

Record number: 17, Textual support number: 1 OBS

poignée de commande : terme accepté par le Comité d'étude de la terminologie des cartes de travail du DC-9.  2, record 17, French, - poign%C3%A9e%20de%20commande

Record 17,  Textual support,  Spanish

Record 18,  Textual support,  English

Record number: 18, Textual support number: 1 CONT

Re-engining with the CFM56 [engine] introduces an advanced concept called power management control(PMC) to DC-8 operation. This is an electrical fuel control trim system designed to improve thrust setting accuracy and compensate for changing flight conditions.  3, record 18, English, - power%20management%20control

Record 18,  Textual support,  French

Record number: 18, Textual support number: 1 OBS

Terme et abréviation uniformisés par le CUTA Opérations aériennes.  2, record 18, French, - syst%C3%A8me%20de%20gestion%20de%20r%C3%A9gime

Record 18,  Textual support,  Spanish

Record 19,  Textual support,  English

Record number: 19, Textual support number: 1 CONT

The Mach trim system smoothly applied a progressive nose-up control force, which gave the impression of natural static stability.  1, record 19, English, - nose%2Dup%20control%20force

Record 19,  Textual support,  French

Record number: 19, Textual support number: 1 CONT

Le système de compensation automatique a progressivement appliqué au manche une force à cabrer que le pilote ressent comme une manifestation de stabilité naturelle.  1, record 19, French, - force%20%C3%A0%20cabrer

Record 19,  Textual support,  Spanish