TERMIUM Plus^®

Record 1,  Textual support,  English

Record number: 1, Textual support number: 1 CONT

Suction defuelling can be accomplished with a fuel truck defuelling pump through the pressure fuelling receptacle. Suction defuelling can also be accomplished by inserting a suction hose through the overwing fill ports, but this method is only recommended as a last resort. Aircraft system pumps and suction defuelling performed simultaneously through the pressure fuelling receptacle will provide the highest flow rates possible and should be used when time is critical.  1, record 1, English, - suction%20defuelling

Record 1,  Textual support,  French

Record 1,  Textual support,  Spanish

Record 2,  Textual support,  English

Record number: 2, Textual support number: 1 CONT

Pressure fueling is used on many late model aircraft. This fueling process ... greatly reduces the time required to service large aircraft. There are also other advantages in the pressure fueling process. It eliminates aircraft skin damage and hazards to personnel and reduces the chances for fuel contamination. Pressure fueling also reduces the chance of static electricity igniting fuel vapors.  3, record 2, English, - pressure%20fuelling

Record number: 2, Textual support number: 2 CONT

Pressure refuelling is much quicker than gravity fuelling. The fuel tanks are filled to the desired level according to the sequence selected by the fuelling personnel.  7, record 2, English, - pressure%20fuelling

Record number: 2, Textual support number: 1 OBS

single point refuelling: term officially approved by the Aeronautical Terminology Standardization Committee (ATSC) - Helicopters.  8, record 2, English, - pressure%20fuelling

Record 2,  Textual support,  French

Record number: 2, Textual support number: 1 OBS

avitaillement à point unique : terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Hélicoptères.  3, record 2, French, - avitaillement%20sous%20pression

Record number: 2, Textual support number: 2 OBS

avitaillement à point unique : terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes.  3, record 2, French, - avitaillement%20sous%20pression

Record 2,  Textual support,  Spanish

Record 4,  Textual support,  English

Record number: 4, Textual support number: 1 OBS

The cylindrical tank containing the pressure tubes and moderator, called the "calandria", sits on its side. Thus, the CANDU core is horizontal. A fuelling machine visits each end of the core, one fuelling and the other de-fuelling, allowing operators to insert fresh fuel at alternate ends for neighbouring fuel channels.  1, record 4, English, - heavy%2Dwater%20moderator

Record 4,  Textual support,  French

Record 4,  Textual support,  Spanish

Record 5,  Textual support,  English

Record number: 5, Textual support number: 1 CONT

Normal fuelling is accomplished through dual fuel nozzle adapters located on the right wing leading edge spar at the fuelling stations. All fuelling operations, except fuel pump control, are accomplished at the fuelling station. Opening the station access door applies DC power to the fuelling system and removes the N3 inhibit to the centre tank fuel pumps. Fuel flows through the dual nozzles to pressurise a fuelling manifold. Fuelling valves control the flow of fuel from the fuelling manifold into each of the three switches on the fuelling panel. A fuel quantity may be preselected for each tank. The fuelling valves close automatically when the preselected quantity is reached or when the tank is full, whichever occurs first. A tank overfill system is provided to prevent fuel spillage. If any fuel is sensed in the surge tanks during fuelling, a signal is sent to close all fuelling valves. The aircraft is filled automatically by hydrant or tank truck pressure. All tanks may be fuelled at the same time. The main tanks may also be fuelled manually through over wing fill ports. There are no over wing fill ports for the centre tank.  4, record 5, English, - fuelling%20station

Record 5,  Textual support,  French

Record number: 5, Textual support number: 1 CONT

Chaque raccord de remplissage de réservoir de carburant doit empêcher la pénétration de carburant dans toute partie de l'avion autre que le réservoir lui-même. De plus, [chaque] raccord de remplissage encastré qui peut recueillir une quantité appréciable de carburant doit avoir un drain qui assure un écoulement sans mouiller l'avion, [chaque] bouchon de prise de remplissage doit comporter un joint étanche au carburant, et [chaque] point de remplissage carburant, à l'exception des points de raccord de remplissage de carburant sous pression, doit être aménagé pour relier électriquement l'avion à l'équipement de remplissage de carburant au sol.  2, record 5, French, - point%20de%20remplissage

Record number: 5, Textual support number: 1 OBS

point de remplissage : terme uniformisé par les Comités d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes et Maintenance.  3, record 5, French, - point%20de%20remplissage

Record 5,  Textual support,  Spanish

Record 7,  Textual support,  English

Record number: 7, Textual support number: 1 DEF

That part of the fuelling machine head located behind the snout and separators. It comprises a rotor and drive shaft and is housed in a cylindrical pressure vessel. The rotor has chambers for new or spent fuel bundles(...)  1, record 7, English, - magazine

Record number: 7, Textual support number: 1 OBS

Applies to the fuelling machine of CANDU nuclear reactors.  2, record 7, English, - magazine

Record 7,  Textual support,  French

Record number: 7, Textual support number: 1 DEF

Partie de la tête de la machine à combustible située derrière le bec de raccordement et les séparateurs et comprenant le barillet rotatif et un arbre de commande, le tout contenu dans un récipient cylindrique sous pression. [Il] comprend des chambres pouvant recevoir les grappes de combustible neuf ou épuisé.  1, record 7, French, - barillet

Record 7,  Textual support,  Spanish