TERMIUM Plus^®

Record 1,  Textual support,  English

Record number: 1, Textual support number: 1 OBS

[A poster from Transport Canada which] depicts a light helicopter on final approach to a landing pad, when a fuel truck suddenly appears to not have seen, heard or known about the approaching aircraft, and creates a risk of collision on the pad.... This poster is primarily targeted to all helicopter pilots and operators, and holders of an airside vehicle operator permit(AVOP).  1, record 1, English, - Final%20Approach%2E%20All%20Clear%3F%20Be%20Sure%21%20Runway%20Incursions%20are%20Real%21

Record number: 1, Textual support number: 2 OBS

TP 14007: publication code used by Transport Canada.  2, record 1, English, - Final%20Approach%2E%20All%20Clear%3F%20Be%20Sure%21%20Runway%20Incursions%20are%20Real%21

Record 1,  Textual support,  French

Record number: 1, Textual support number: 1 CONT

TP 14007 : code de publication en usage à Transports Canada.  2, record 1, French, - L%27approche%20finale%20est%20libre%3F%20Soyez%2Den%20s%C3%BBr%21%20Une%20incursion%20sur%20piste%20est%20si%20vite%20arriv%C3%A9e%21

Record 1,  Textual support,  Spanish

Record 2,  Textual support,  English

Record 2,  Textual support,  French

Record number: 2, Textual support number: 1 OBS

salle de pompage de carburant hélicoptère : désignation uniformisée par le Comité de normalisation de la terminologie navale.  1, record 2, French, - salle%20de%20pompage%20de%20carburant%20pour%20h%C3%A9licopt%C3%A8re

Record 2,  Textual support,  Spanish

Record 3,  Textual support,  French

Record 3,  Textual support,  Spanish

Record 4,  Textual support,  English

Record 4,  Textual support,  French

Record number: 4, Textual support number: 1 OBS

pompe à carburant hélicoptère : désignation uniformisée par le Comité de normalisation de la terminologie navale.  3, record 4, French, - pompe%20%C3%A0%20carburant%20pour%20h%C3%A9licopt%C3%A8re

Record 4,  Textual support,  Spanish

Record 5,  Textual support,  French

Record 5,  Textual support,  Spanish

Record 6,  Textual support,  English

Record number: 6, Textual support number: 1 DEF

A site where fuel drums are stored for use during CCG [Canadian Coast Guard] helicopter operations in remote areas.  1, record 6, English, - refuelling%20site

Record 6,  Textual support,  French

Record 6,  Textual support,  Spanish

Record 7,  Textual support,  English

Record number: 7, Textual support number: 1 CONT

A helicopter refuelling system normally consists of : tank laydown skid, deluge system, storage tank(stationary or transportable), fuel pump(s), filter/water separator(s), filter monitor(s), air eliminators, local control panel, hose reel with filling nozzle, earth prover system and flow meter.  2, record 7, English, - helicopter%20refuelling%20system

Record 7,  Textual support,  French

Record 7,  Textual support,  Spanish

Record 8,  Textual support,  English

Record number: 8, Textual support number: 1 CONT

The helicopter landing platform can be used in support of helicopter assaults and logistic operations. The helicopter deck is removable and has one landing spot. Up to 90 tons JP-5 fuel is carried for helicopters. The ships’ habitability features provide for the berthing, messing and cargo transportation of approximately 300 fully equipped combat troops of the landing force in addition to the 360 crew members assigned.  2, record 8, English, - helicopter%20landing%20platform

Record 8,  Textual support,  French

Record number: 8, Textual support number: 1 OBS

Pluriel : des plateformes, des plates-formes.  2, record 8, French, - plateforme%20d%27appontage%20d%27h%C3%A9licopt%C3%A8re

Record number: 8, Textual support number: 2 OBS

plateforme (sing.); plateformes (pl.) : Ces graphies, puisées des Rectifications de l'orthographe recommandées par le Conseil supérieur de la langue française, sont attestées dans le Petit Robert (2004).  3, record 8, French, - plateforme%20d%27appontage%20d%27h%C3%A9licopt%C3%A8re

Record 8,  Textual support,  Spanish

Record 9,  Textual support,  English

Record number: 9, Textual support number: 1 CONT

The Rotary Rocket Company is developing the Roton which is a fully reusable, single-stage-to-orbit, commercial launch vehicle. It will be piloted by a crew of two and is being designed to carry 7, 000 lbs to low-earth-orbit. The Roton will takeoff vertically like a conventional rocket powered by a new rotary engine burning liquid oxygen and jet fuel. Once its payload is delivered to orbit, the Roton returns to Earth via a nose-mounted rotor which is deployed in space and used during reentry to help stabilize the craft. Once in the atmosphere, the vehicle will glide like an autorotating helicopter and land vertically, assisted by rotor tip thrusters.  7, record 9, English, - Roton

Record 9,  Textual support,  French

Record number: 9, Textual support number: 1 CONT

Le Roton de la Société Rotary Rocket décolle verticalement, propulsé par un moteur de fusée rotatif. Après la libération de la charge utile, le véhicule retourne sur Terre en dépliant des pales d'hélicoptère. Il rentre dans l'atmosphère par la base. Les pales sont d'abord en rotation passive, puis elles sont entraînées par de petites fusées montées à leurs extrémités lors de l'atterrissage vertical.  1, record 9, French, - Roton

Record 9,  Textual support,  Spanish

Record 10,  Textual support,  English

Record number: 10, Textual support number: 1 CONT

Helicopter Familiarization and Preparation for Flight.... Weight and Balance, Loading.... The candidate will be required, using actual weights where possible, to apply the approved weight and balance data for the helicopter used in the test to make practical computations of the permissible fuel and payload distribution. If a loading graph or computer is available with the helicopter, it may be used. Knowledge of weight and balance graphs, envelopes, and the effect of various centre of gravity locations on the helicopter flight characteristics shall be demonstrated.  1, record 10, English, - loading%20graph

Record 10,  Textual support,  French

Record number: 10, Textual support number: 1 CONT

Connaissance de l'hélicoptère et préparation au vol. [...] Masse, centrage et chargement. [...] Le candidat doit effectuer les calculs pratiques de répartition de la charge et du carburant en se servant du poids réel des passagers, lorsque cela est possible, et des données homologuées de masse et de centrage de l'hélicoptère utilisé pour le test en vol. Il peut utiliser un graphique de chargement ou un calculateur, si ces derniers sont fournis avec l'hélicoptère. Il doit également démontrer qu'il connaît les graphiques de masse et de centrage, ainsi que leurs limites et l'influence du centrage sur les caractéristiques de vol de l'hélicoptère.  1, record 10, French, - graphique%20de%20chargement

Record 10,  Textual support,  Spanish

Record 11,  Textual support,  English

Record number: 11, Textual support number: 1 CONT

Helicopter Familiarization and Preparation for Flight.... Weight and Balance, Loading.... The candidate will be required, using actual weights where possible, to apply the approved weight and balance data for the helicopter used in the test to make practical computations of the permissible fuel and payload distribution. If a loading graph or computer is available with the helicopter, it may be used. Knowledge of weight and balance graphs, envelopes, and the effect of various centre of gravity locations on the helicopter flight characteristics shall be demonstrated.  1, record 11, English, - balance%20graph

Record 11,  Textual support,  French

Record number: 11, Textual support number: 1 CONT

Connaissance de l'hélicoptère et préparation au vol. [...] Masse, centrage et chargement. [...] Le candidat doit effectuer les calculs pratiques de répartition de la charge et du carburant en se servant du poids réel des passagers, lorsque cela est possible, et des données homologuées de masse et de centrage de l'hélicoptère utilisé pour le test en vol. Il peut utiliser un graphique de chargement ou un calculateur, si ces derniers sont fournis avec l'hélicoptère. Il doit également démontrer qu'il connaît les graphiques de masse et de centrage, ainsi que leurs limites et l'influence du centrage sur les caractéristiques de vol de l'hélicoptère.  1, record 11, French, - graphique%20de%20centrage

Record 11,  Textual support,  Spanish

Record 12,  Textual support,  English

Record number: 12, Textual support number: 1 CONT

Helicopter Familiarization and Preparation for Flight.... Weight and Balance, Loading.... The candidate will be required, using actual weights where possible, to apply the approved weight and balance data for the helicopter used in the test to make practical computations of the permissible fuel and payload distribution. If a loading graph or computer is available with the helicopter, it may be used. Knowledge of weight and balance graphs, envelopes, and the effect of various centre of gravity locations on the helicopter flight characteristics shall be demonstrated.  1, record 12, English, - weight%20graph

Record 12,  Textual support,  French

Record number: 12, Textual support number: 1 CONT

Connaissance de l'hélicoptère et préparation au vol. [...] Masse, centrage et chargement. [...] Le candidat doit effectuer les calculs pratiques de répartition de la charge et du carburant en se servant du poids réel des passagers, lorsque cela est possible, et des données homologuées de masse et de centrage de l'hélicoptère utilisé pour le test en vol. Il peut utiliser un graphique de chargement ou un calculateur, si ces derniers sont fournis avec l'hélicoptère. Il doit également démontrer qu'il connaît les graphiques de masse et de centrage, ainsi que leurs limites et l'influence du centrage sur les caractéristiques de vol de l'hélicoptère.  1, record 12, French, - graphique%20de%20masse

Record 12,  Textual support,  Spanish

Record 13,  Textual support,  English

Record number: 13, Textual support number: 1 CONT

The fuel-oil heater serves a twofold purpose, it is designed to cool the oil and preheat the fuel for combustion.  2, record 13, English, - fuel%2Doil%20heater

Record number: 13, Textual support number: 2 CONT

Bell 212 helicopter... Engine power loss. Engine tear-down inspections revealed that the number two engine was not operating on impact and the fuel oil heater had malfunctioned, however this malfunction alone would not cause the engine to stop operating. If fuel pressure upstream from the engine driven boost pump is lost when the fuel oil heater has malfunctioned(allowing the fuel to be heated), the engine will stop operating. Since the investigation revealed no other reason for the engine to stop operating, it is likely that the number two engine shut down due to a loss of line fuel pressure provided by the electrical boost pumps, coincident with the malfunctioning fuel oil heater.  3, record 13, English, - fuel%2Doil%20heater

Record 13,  Textual support,  French

Record 13,  Textual support,  Spanish

Record 14,  Textual support,  English

Record 14,  Textual support,  French

Record number: 14, Textual support number: 1 OBS

Source(s) : Pêches - avril 1995.  1, record 14, French, - syst%C3%A8me%20d%27approvisionnement%20en%20carburant%20pour%20un%20h%C3%A9licopt%C3%A8re

Record 14,  Textual support,  Spanish

Record 15,  Textual support,  English

Record number: 15, Textual support number: 1 CONT

From an energetic standpoint, however, the helicopter remains poorly efficient : where a light five-seater helicopter requires virtually its empty weight(approximately 750 kg) in fuel and 450 horsepower to carry five persons over a distance of 650 kilometres, a light aeroplane requires only 280 horsepower and a fraction of the fuel to carry its five occupants over twice the distance.  1, record 15, English, - light%20five%2Dseater%20helicopter

Record 15,  Textual support,  French

Record number: 15, Textual support number: 1 CONT

Sur un hélicoptère léger à cinq places par exemple, il faut en gros un poids de carburant égal à la masse à vide (environ 750 kg) et un moteur de 450 cv pour transporter cinq personnes sur 650 km alors qu'un avion léger transportera ces mêmes personnes deux fois plus loin avec une fraction de ce carburant et un moteur de 280 cv seulement.  1, record 15, French, - h%C3%A9licopt%C3%A8re%20l%C3%A9ger%20%C3%A0%20cinq%20places

Record 15,  Textual support,  Spanish

Record 16,  Textual support,  English

Record number: 16, Textual support number: 1 OBS

helicopter fuel tank cofferdam : Terminology officially approved by the Naval Terminology Standardization Committee.  2, record 16, English, - helicopter%20fuel%20tank%20cofferdam

Record 16,  Textual support,  French

Record number: 16, Textual support number: 1 OBS

cofferdam du réservoir de carburant hélicoptère : Terminologie officialisée par le Comité de normalisation de la terminologie navale.  2, record 16, French, - cofferdam%20du%20r%C3%A9servoir%20de%20carburant%20h%C3%A9licopt%C3%A8re

Record 16,  Textual support,  Spanish

Record 17,  Textual support,  English

Record number: 17, Textual support number: 1 CONT

A third mission [of the XV-15 prototype tilt rotor aircraft] is as helicopter chaser with narrow fuselage, a pilot's night vision system, a mast-mounted sight which can be retracted into the fuselage, a 25 mm gun and defence suppression missiles. In this case, fuel load would be 2, 318 lb(1, 051 kg) and armament load 1, 428 lb(647 kg).  1, record 17, English, - armament%20load

Record 17,  Textual support,  French

Record number: 17, Textual support number: 1 CONT

Une autre application éventuelle serait celle d'un chasseur d'hélicoptères à fuselage effilé, doté d'un système de vision nocturne, d'un viseur télescopique rétractable, d'un canon de 25 mm et de missiles de neutralisation des défenses adverses. Dans ce cas, la charge de carburant serait de 1050 kg et la masse de l'armement de 645 kg.  1, record 17, French, - masse%20de%20l%27armement

Record 17,  Textual support,  Spanish

Record 18,  Textual support,  English

Record number: 18, Textual support number: 1 CONT

A third mission [of the XV-15 prototype tilt rotor aircraft] is as helicopter chaser with narrow fuselage, a pilot's night vision system, a mast mounted sight which can be retracted into the fuselage, a 25 mm gun and defence suppression missiles. In this case, fuel load would be 2, 318 lb(1, 051 kg) and armament load 1, 428 lb(647 kg).  1, record 18, English, - helicopter%20chaser

Record 18,  Textual support,  French

Record number: 18, Textual support number: 1 CONT

Une autre application éventuelle serait celle d'un chasseur d'hélicoptères à fuselage effilé, doté d'un système de vision nocturne, d'un viseur télescopique rétractable, d'un canon de 25 mm et de missiles de neutralisation des défenses adverses. Dans ce cas, la charge de carburant serait de 1050 kg et la masse de l'armement de 645 kg [sic].  1, record 18, French, - chasseur%20d%27h%C3%A9licopt%C3%A8res

Record 18,  Textual support,  Spanish

Record 19,  Textual support,  English

Record number: 19, Textual support number: 1 CONT

A third mission [of the XV-15 prototype tilt rotor aircraft] is as helicopter chaser with narrow fuselage, a pilot's night vision system, a mast-mounted sight which can be retracted into the fuselage, a 25 mm gun and defence suppression missiles. In this case, fuel load would be 2, 318 lb(1, 051 kg) and armament load 1, 428 lb(647 kg).  1, record 19, English, - defence%20suppression%20missile

Record 19,  Textual support,  French

Record number: 19, Textual support number: 1 CONT

Une autre application éventuelle serait celle d'un chasseur d'hélicoptères à fuselage effilé, doté d'un système de vision nocturne, d'un viseur télescopique rétractable, d'un canon de 25 mm et de missiles de neutralisation des défenses adverses. Dans ce cas, la charge de carburant serait de 1 050 kg et la masse de l'armement de 645 kg.  1, record 19, French, - missile%20de%20neutralisation%20des%20d%C3%A9fenses%20adverses

Record 19,  Textual support,  Spanish