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Record 1,  Textual support,  English

Record number: 1, Textual support number: 1 DEF

Any stabilizing surface of an aircraft, including the wings, control surfaces, rotors, propellers, horizontal stabilizers, vertical stabilizers and, in the case of an aircraft that has rear-mounted engines, the upper surface of its fuselage.  1, record 1, English, - critical%20surface

Record number: 1, Textual support number: 1 OBS

critical surface: designation and definition standardized by the Glossary for Pilots and Air Traffic Services Personnel Committee.  2, record 1, English, - critical%20surface

Record 1,  Textual support,  French

Record number: 1, Textual support number: 1 DEF

Toute surface stabilisante de l'aéronef, ce qui comprend les ailes, les gouvernes, les rotors, les hélices, les stabilisateurs et les plans fixes verticaux, ainsi que la partie supérieure du fuselage des aéronefs avec moteur monté à l'arrière.  1, record 1, French, - surface%20critique

Record number: 1, Textual support number: 1 OBS

surface critique : désignation et définition normalisées par le Comité sur le Glossaire à l'intention des pilotes et du personnel des services de la circulation aérienne.  2, record 1, French, - surface%20critique

Record 1,  Textual support,  Spanish

Record 2,  Textual support,  English

Record number: 2, Textual support number: 1 OBS

each [transverse] beam has openings for installation of cables and electrical leads, and the openings at FS [fuselage station] 344(...) have pulley bracket assemblies for control cable support.  1, record 2, English, - pulley%20bracket

Record 2,  Textual support,  French

Record number: 2, Textual support number: 1 OBS

voir figure no. 801 dans MECAR. Le code de source complet est MECAR-SE-210F,1972,6,53-47-6,801.  2, record 2, French, - support%20de%20poulie

Record 2,  Textual support,  Spanish

Record 3,  Textual support,  English

Record number: 3, Textual support number: 1 CONT

The fire extinguishing equipment for an airliner such as the Douglas DC-10 incorporates three systems with six pressurized agent containers, two for each engine. The containers for the wing-mounted engines are located in pairs in the leading edge of the wing between the nacelle and the fuselage on each side of the aircraft.... The discharge cartridge is an electrically fired explosive unit that provides force to rupture the disk seal in the outlet port of the container and release the extinguishing agent to the deployment lines. One discharge cartridge is installed on each wing-mounted container and two are installed on the aft-engine container. The discharge cartridge contains two squibs(explosive charges) that are fired by an electric circuit that heats the powder to the ignition point. When the fire extinguisher control handle is pulled down, the electric circuit is closed and the squibs are fired. The force of the explosion ruptures the disk seal, thus releasing the extinguishing agent. A screen in the discharge head prevents particles of the disk from entering the deployment line.  2, record 3, English, - fire%20control%20handle

Record number: 3, Textual support number: 1 OBS

This system is specific to the McDonnell Douglas Corporation aircraft (DC-9, DC-10).  3, record 3, English, - fire%20control%20handle

Record number: 3, Textual support number: 2 OBS

fire control handle : term officially approved by the Aeronautical Terminology Standardization Committee (ATSC) - Helicopters.  4, record 3, English, - fire%20control%20handle

Record 3,  Textual support,  French

Record number: 3, Textual support number: 1 OBS

poignée coupe-feu : terme uniformisé par les Comités d'uniformisation de la terminologie aéronautique (CUTA) - Hélicoptères et Maintenance.  2, record 3, French, - poign%C3%A9e%20coupe%2Dfeu

Record 3,  Textual support,  Spanish

Record 4,  Textual support,  English

Record number: 4, Textual support number: 1 DEF

Normally applied to aeroplanes and gliders only and usually meaning that there is no separate horizontal stabilizing or control surface, though there may be a vertical tail.  4, record 4, English, - tailless%20aeroplane

Record number: 4, Textual support number: 1 OBS

[This type of aircraft consists] of a single wing without conventional fuselage or tail, housing cargo and personnel within the wing structure, and achieving stability and control by means of vertical external surfaces mounted on the wing tips or booms attached to the wing.  5, record 4, English, - tailless%20aeroplane

Record number: 4, Textual support number: 2 OBS

tailless aeroplane: term standardized by ISO.  6, record 4, English, - tailless%20aeroplane

Record 4,  Textual support,  French

Record number: 4, Textual support number: 1 CONT

En fonction de la forme, on distingue, en sus de l'avion classique, l'avion-canard et l'avion sans queue, qui ne comporte aucun empennage horizontal [...]  2, record 4, French, - avion%20sans%20queue

Record number: 4, Textual support number: 1 OBS

Se dit uniquement des avions et des planeurs sans stabilisateur horizontal ni gouverne, mais pouvant comporter un empennage vertical.  2, record 4, French, - avion%20sans%20queue

Record 4,  Textual support,  Spanish

Record 5,  Textual support,  English

Record number: 5, Textual support number: 1 CONT

Using the latest pneumatic technologies, the Centralised Air Control Module is a safer and more efficient way of inflating the Airbags and controlling the lifting operation.... The Centralised Air Control Module is the first Aircraft lifting system to allow a single operator, the ability to control the recovery of an Aircraft. The complications of communicating instructions over large areas, and synchronising the other recovery personnel are eliminated. The operator can view the pressures of all the Airbags, from fuselage to outer wing, using the pressure gauges on the control panel, giving the operator complete confidence and control over the recovery situation.  2, record 5, English, - centralised%20air%20control%20module

Record 5,  Textual support,  French

Record number: 5, Textual support number: 1 CONT

Les préoccupations croissantes qui entourent la sécurité du personnel et la rapidité de relevage d'aéronefs sont devenues d'importants sujets d'actualité qui ont conduit AMS Systems Engineering à concevoir et à mettre au point un module de commande pneumatique centralisé. Grâce aux dernières technologies de la pneumatique, ce module offre un moyen plus sûr et plus efficace de gonflement des [coussins gonflables] et de maîtrise du levage.  1, record 5, French, - module%20de%20commande%20pneumatique%20centralis%C3%A9

Record 5,  Textual support,  Spanish

Record 6,  Textual support,  English

Record number: 6, Textual support number: 1 CONT

The system is based on a special landing gear called a jump strut, which works by giving the aircraft the proper attitude for take-off,.... First, the system extends the nose gear, raising the nose. A few milliseconds later, the main gear is activated(’jumps’) in its turn, increasing the distance between wheels and fuselage, while rotation continues. After a vertical leap of some 6ft, the aircraft slows and descends slightly because of the increased drag at the higher angle of attack. Finally, and virtually without a pause, the aircraft resumes its climb.... The jump strut is extended under pilot control by a nitrogen-charged actuator. Once fired, it is immediately vented to atmosphere to enable the gear to resume its normal shock-attenuating function should the take-off run have to be aborted.  1, record 6, English, - jump%20strut

Record 6,  Textual support,  French

Record 6,  Textual support,  Spanish

Record 7,  Textual support,  English

Record number: 7, Textual support number: 1 CONT

The [stall warning] system consists of a stall warning tone generator, two angle-of-attack transducers, two flap position transmitters, two stall warning computers, and dual control column shakers, audio recognition, and signal annunciators.... The angle-of-attack transducers are installed on the left and right sides of the fuselage at station 285. The transducers provide an electric signal proportional to the angle-of-attack of the airplane. Upward motion of the trailing edge of the vane produces an increasing angle.  2, record 7, English, - angle%20of%20attack%20transducer

Record 7,  Textual support,  French

Record number: 7, Textual support number: 1 OBS

transducteur d'angle d'attaque : terme accepté par le Comité d'étude de la terminologie des cartes de travail du DC-9.  2, record 7, French, - transducteur%20d%27angle%20d%27attaque

Record 7,  Textual support,  Spanish

Record 8,  Textual support,  English

Record number: 8, Textual support number: 1 CONT

The YF-16 prototype fitted with two canards under the intake duct proved the basic ability to shift the aircraft sideways or up and down in flight without changing its fuselage attitude(direct force control) and pointing the fuselage up, down or sideways without altering its flight path(fuselage aiming or pointing).  1, record 8, English, - direct%20force%20control

Record 8,  Textual support,  French

Record number: 8, Textual support number: 1 CONT

Le prototype YF-16 à commandes automatiques généralisées et avec empennage canard monté au-dessous de l'entrée d'air, a démontré qu'il était possible de modifier la trajectoire d'un avion (vers le haut, vers le bas, vers la droite ou vers la gauche) sans modifier son attitude (c'est le "contrôle direct des forces"), et de changer le cap ou l'assiette en conservant la même trajectoire (c'est le "dépointage" de la ligne de foi du fuselage par rapport à la trajectoire de vol.  1, record 8, French, - contr%C3%B4le%20direct%20des%20forces

Record 8,  Textual support,  Spanish

Record 9,  Textual support,  English

Record number: 9, Textual support number: 1 CONT

The YF-16 prototype fitted with two canards under the intake duct proved the basic ability to shift the aircraft sideways or up and down in flight without changing its fuselage attitude(direct force control) and pointing the fuselage up, down or sideways without altering its flight path(fuselage aiming or pointing).  1, record 9, English, - fuselage%20aiming

Record 9,  Textual support,  French

Record number: 9, Textual support number: 1 OBS

Le prototype YF-16 à commandes automatiques généralisées et avec empennage canard monté au-dessous de l'entrée d'air, a démontré qu'il était possible de modifier la trajectoire d'un avion (vers le haut, vers le bas, vers la droite ou vers la gauche) sans modifier son attitude (c'est le "contrôle direct des forces"), et de changer le cap ou l'assiette en conservant la même trajectoire (c'est le "dépointage" de la ligne de foi du fuselage par rapport à la trajectoire de vol.  2, record 9, French, - d%C3%A9pointage%20de%20fuselage

Record 9,  Textual support,  Spanish

Record 10,  Textual support,  English

Record 10,  Textual support,  French

Record number: 10, Textual support number: 1 OBS

commande dans fuselage  1, record 10, French, - commande%20dans%20fuselage

Record 10,  Textual support,  Spanish

Record 11,  Textual support,  English

Record 11,  Textual support,  French

Record number: 11, Textual support number: 1 OBS

hypersustentateurs  1, record 11, French, - timonerie%20de%20commande%20dans%20fuselage

Record 11,  Textual support,  Spanish