TERMIUM Plus^®

Fiche 1,  Justifications,  Français

Fiche 1,  Justifications,  Espagnol

Fiche 2,  Justifications,  Anglais

Record number: 2, Textual support number: 1 CONT

The MLG [main landing gear] retracts inwards into the fuselage wheel well. Each MLG has two doors. The outboard door is rigidly attached at the strut. The inboard door operates by mechanical linkage to the strut and is held in up position by two uplock cylinders. This uplock is released when landing gear lever is placed in down position by hydraulic pressure, or by nitrogen pressure in emergency. The MLG is held, while airborne, in retracted position by hydraulic pressure in the actuator and by the inboard door mechanical uplock, if pressure drops. As the gear is extended, an internal lock in the actuator automatically locks it in fully extended positions.  4, fiche 2, Anglais, - landing%20gear%20control%20lever

Fiche 2,  Justifications,  Français

Record number: 2, Textual support number: 1 CONT

La séquence d'extension/rétraction des trains est conditionnée par la position du levier de commande «rentrée/sortie» des trains et par la réponse des détecteurs de positions du train et des trappes. Elle commande successivement l'ouverture des trappes, le déverrouillage du train, l'extension du train, le verrouillage du train en position basse, puis la fermeture des trappes principales (et inversement lors de la rétraction).  5, fiche 2, Français, - levier%20de%20commande%20train

Record number: 2, Textual support number: 1 OBS

levier de commande train; levier train : termes uniformisés par les Comités d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes et Maintenance.  6, fiche 2, Français, - levier%20de%20commande%20train

Fiche 2,  Justifications,  Espagnol

Fiche 3,  Justifications,  Anglais

Record number: 3, Textual support number: 1 CONT

In the summer of 1994 NASA approved adding an optical-quality nadir-viewing window to the U. S. Laboratory Module of the International Space Station. The window can view 39. 5 degrees forward along the axis of the ISS, 32. 2 degrees aft, and a total of 79. 1 degrees from port to starboard. The window is constructed of three panes of fused silica and a fourth protective kick pane made of glass laminate. From outboard to inboard, the panes are : OUTBOARD-An external debris pane that can be changed by an EVA astronaut if damaged. A redundant pressure pane. A primary pressure pane. A scratch or "kick" pane that protects the primary pressure pane from being damaged if the crew or equipment make contact with the window [and] provides a UV-IR coating to protect the crew members. INBOARD-The kick pane is removed during window research operations to take advantage of the full spectrum of radiation that passes through the fused silica panes. When not in use, the window is protected by the kick pane on the inside, and by an external cover on the outside. The external cover can be rotated in or out of position from within the cabin by an astronaut using a hand crank.  2, fiche 3, Anglais, - external%20debris%20pane

Record number: 3, Textual support number: 1 OBS

external debris pane: term officially approved by the International Space Station official approval Group (ISSOAG).  3, fiche 3, Anglais, - external%20debris%20pane

Fiche 3,  Justifications,  Français

Record number: 3, Textual support number: 1 OBS

vitrage anti-débris : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  1, fiche 3, Français, - vitrage%20anti%2Dd%C3%A9bris

Fiche 3,  Justifications,  Espagnol

Fiche 4,  Justifications,  Anglais

Fiche 4,  Justifications,  Français

Record number: 4, Textual support number: 1 OBS

Les renseignements provenant de la source NUT-3 (Véhicules automobiles, lexique anglais-français) sont reproduits avec l'autorisation de l'Office des Nations-Unies à Genève.  2, fiche 4, Français, - place%20m%C3%A9diane

Fiche 4,  Justifications,  Espagnol