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Record 1,  Textual support,  English

Record number: 1, Textual support number: 1 CONT

In the case of a twin-engine aircraft, a configuration featuring one single propeller driven by two engines mounted side-by-side will eliminate any risk of yaw should one engine fail, and improve the aircraft's handling when reverse pitch is engaged on landing.  2, record 1, English, - reverse%20pitch

Record number: 1, Textual support number: 1 OBS

The pitch with a negative blade angle.  3, record 1, English, - reverse%20pitch

Record number: 1, Textual support number: 2 OBS

reverse pitch: term officially approved by the International Civil Aviation Organization (ICAO).  4, record 1, English, - reverse%20pitch

Record 1,  Textual support,  French

Record number: 1, Textual support number: 1 OBS

Dans le cas d'un modèle bimoteur, la réalisation d'une configuration avec une seule hélice entraînée par deux propulseurs disposés côte à côte éliminera tout risque de lacet incontrôlé lors de panne éventuelle d'un moteur, et améliorera le comportement de l'avion à l'atterrissage au moment de l'inversion de pas.  4, record 1, French, - pas%20inverse

Record number: 1, Textual support number: 2 OBS

pas inverse : terme uniformisé par l'Organisation de l'aviation civile internationale (OACI).  5, record 1, French, - pas%20inverse

Record 1,  Textual support,  Spanish

Record number: 1, Textual support number: 1 OBS

paso inverso: término aceptado oficialmente por la Organización de Aviación Civil Internacional (OACI).  3, record 1, Spanish, - paso%20inverso

Record 2,  Textual support,  English

Record number: 2, Textual support number: 1 CONT

The electrical system has four engine-driven generators, each powerful enough to supply the aircraft with sufficient electricity. Each of the two main landing gear pods carries an auxiliary power unit(APU) and air turbine motor(ATM) to supply electric/pneumatic and hydraulic power, respectively, for engine starts, ground air conditioning and heating, main landing gear kneeling operations, and forward/aft cargo door operations.  3, record 2, English, - air%20turbine%20motor

Record 2,  Textual support,  French

Record number: 2, Textual support number: 1 OBS

moteur à turbine à air; ATM : terme et abréviation uniformisés par les Comités d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes et Maintenance.  3, record 2, French, - moteur%20%C3%A0%20turbine%20%C3%A0%20air

Record 2,  Textual support,  Spanish

Record 3,  Textual support,  English

Record number: 3, Textual support number: 1 DEF

A unit which converts pneumatic energy into mechanical energy.  3, record 3, English, - air%20motor

Record number: 3, Textual support number: 1 CONT

The electrical system has four engine-driven generators, each powerful enough to supply the aircraft with sufficient electricity. Each of the two main landing gear pods carries an auxiliary power unit(APU) and [an] air turbine motor(ATM) to supply electric/pneumatic and hydraulic power, respectively, for engine starts, ground air conditioning and heating, main landing gear kneeling operations, and forward/aft cargo door operations.  2, record 3, English, - air%20motor

Record 3,  Textual support,  French

Record number: 3, Textual support number: 1 DEF

Appareil transformant l'énergie pneumatique en énergie mécanique.  2, record 3, French, - moteur%20pneumatique

Record number: 3, Textual support number: 1 CONT

[Le Concorde] était l'un des rares avions à utiliser les inverseurs en vol. Ces coquilles servaient aussi à moduler le flux du réacteur. Ces inverseurs sont actionnés par un moteur pneumatique commandé par la manette inverseur de poussée situé en avant des manettes de poussée au poste de pilotage.  3, record 3, French, - moteur%20pneumatique

Record 3,  Textual support,  Spanish

Record 4,  Textual support,  English

Record number: 4, Textual support number: 1 CONT

Ex. 18-Autorotations. Aim. To determine that, in the event of an engine failure, the candidate has the ability to make a safe autorotational approach and landing to a suitable landing area.... Landing or Power Recovery to the Hover/Hover-Taxi. Description. The candidate will be required to carry out two types of autorotational approaches, one of which will include a 180 degree turn. The exercise will be initiated above ground that has previously been assessed as suitable for practice autorotation landings. The autorotation will be commenced from cruise at a safe height, but in no instance lower than 500 feet above ground. The approaches will terminate at the discretion of the examiner, in either a landing, or a power recovery to the hover/hover-taxi.  1, record 4, English, - power%20recovery%20to%20the%20hover%2Dtaxi

Record 4,  Textual support,  French

Record number: 4, Textual support number: 1 CONT

Ex. 18 - Autorotations. But. Déterminer si le candidat peut effectuer, en cas de panne de moteur, une approche en autorotation vers une zone d'atterrissage propice, se terminant par un atterrissage en sécurité. [...] Atterrissage ou remise des gaz au cours d'un vol en stationnaire ou en circulation près du sol. Description. Le candidat doit effectuer deux approches en autorotation dont une doit comprendre un virage de 180°. L'exercice sera amorcé au-dessus d'une zone reconnue au préalable comme étant propice pour la pratique de ce genre d'atterrissage. Les autorotations seront amorcées en vol de croisière à une hauteur sécuritaire (500 pieds minimum) au-dessus du sol. L'approche en autorotation se terminera soit par un atterrissage ou un rattrapage avec puissance au vol stationnaire ou une circulation prè du sol, à la discrétion de l'examinateur.  1, record 4, French, - remise%20des%20gaz%20au%20cours%20d%27un%20vol%20en%20circulation%20pr%C3%A8s%20du%20sol

Record 4,  Textual support,  Spanish

Record 5,  Textual support,  English

Record number: 5, Textual support number: 1 CONT

Two single engine second segment climb pressure switches are provided to shut down both air-conditioning systems at any altitude in the event of engine failure, provided the air-conditioning supply switch is in the armed position. Second segment climb/starts at the time the landing gear is fully retracted and continues until the airplane reaches an altitude of at least 400 feet above the runway. The system is normally energized prior to takeoff and deenergized after airplane climb is complete.  2, record 5, English, - second%20stage%20segment%20climb%20switch

Record 5,  Textual support,  French

Record number: 5, Textual support number: 1 OBS

contacteur d'arrêt automatique de conditionnement d'air : terme accepté par le Comité d'étude de la terminologie des cartes de travail du DC-9.  2, record 5, French, - contacteur%20d%27arr%C3%AAt%20automatique%20de%20conditionnement%20d%27air

Record 5,  Textual support,  Spanish

Record 6,  Textual support,  English

Record 6,  Textual support,  French

Record number: 6, Textual support number: 1 OBS

terme d'usage obligatoire au Bureau des Traductions.  2, record 6, French, - atterrissage%20sur%20deux%20r%C3%A9acteurs

Record 6,  Textual support,  Spanish