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Record 1,  Textual support,  English

Record number: 1, Textual support number: 1 CONT

Afterburning gives a significant thrust boost for takeoff particularly from short runways such as those on aircraft carriers, for transonic acceleration and for combat maneuvers, though it is very fuel intensive.  2, record 1, English, - thrust%20boost

Record 1,  Textual support,  French

Record 1,  Textual support,  Spanish

Record 2,  Textual support,  English

Record number: 2, Textual support number: 1 DEF

... a pump, in the aircraft fuel system, meant to prevent vapor locks and cavitation of fuel as well as to maintain a satisfactory supply of low pressure fuel to the engine driven pump.  5, record 2, English, - fuel%20booster%20pump

Record number: 2, Textual support number: 1 OBS

fuel boost pump : designation officially approved by the Aeronautical Terminology Standardization Committee-Helicopters.  6, record 2, English, - fuel%20booster%20pump

Record 2,  Textual support,  French

Record number: 2, Textual support number: 1 OBS

pompe d'appoint; pompe de gavage : désignations uniformisées par le Comité d'uniformisation de la terminologie aéronautique - Opérations aériennes.  5, record 2, French, - pompe%20de%20suralimentation%20en%20carburant

Record number: 2, Textual support number: 2 OBS

pompe de gavage carburant : désignation uniformisée par le Comité d'uniformisation de la terminologie aéronautique - Hélicoptères.  5, record 2, French, - pompe%20de%20suralimentation%20en%20carburant

Record 2,  Textual support,  Spanish

Record 3,  Textual support,  English

Record number: 3, Textual support number: 1 CONT

A less likely reason for the Tank 2 boost pumps to be off would be if the FSC(fuel system control) were attempting to send fuel to Engine 2 from the main manifold because it was unable to use the Tank 2 fill valve.  2, record 3, English, - main%20manifold

Record 3,  Textual support,  French

Record number: 3, Textual support number: 1 CONT

Il est peu probable que les pompes d'appoint du réservoir 2 ne fonctionnaient pas si le contrôleur du circuit carburant (FSC) tentait d'envoyer du carburant au moteur 2 à partir de la rampe d'alimentation principale parce qu'il n'était pas capable d'utiliser le robinet de remplissage du réservoir 2.  2, record 3, French, - rampe%20de%20distribution%20principale

Record number: 3, Textual support number: 1 OBS

rampe de distribution principale : terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes.  3, record 3, French, - rampe%20de%20distribution%20principale

Record 3,  Textual support,  Spanish

Record 4,  Textual support,  English

Record number: 4, Textual support number: 1 CONT

A fuel boost pump bypass valve allows engine driven pumps to draw fuel from the main tanks if all boost pumps in the tank are inoperative.  1, record 4, English, - engine%20driven%20pump

Record 4,  Textual support,  French

Record number: 4, Textual support number: 1 CONT

Le carburant refoulé par les pompes B.P. [...] après avoir été [...] filtré, est pris en charge par une pompe entraînée par le réacteur. Cette pompe augmente la pression du carburant [jusqu'à] 50 à 100 bars.  3, record 4, French, - pompe%20entra%C3%AEn%C3%A9e%20par%20r%C3%A9acteur

Record number: 4, Textual support number: 1 OBS

pompe entraînée par réacteur; pompe réacteur : termes uniformisés par les Comités d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes et Maintenance.  4, record 4, French, - pompe%20entra%C3%AEn%C3%A9e%20par%20r%C3%A9acteur

Record 4,  Textual support,  Spanish

Record 5,  Textual support,  English

Record number: 5, Textual support number: 1 CONT

At 0045 : 37, when the airplane was at an altitude of about 3, 000 feet, the captain started the in-range checklist stating, "bypass is down. hydraulic pressure. quantity checks. AC [alternating current] pump is on. green light. fuel panel. boost pumps on. "  3, record 5, English, - alternating%20current%20pump

Record number: 5, Textual support number: 1 OBS

A.C.: Alternating current.  4, record 5, English, - alternating%20current%20pump

Record number: 5, Textual support number: 2 OBS

alternating current: Electric current that reverses direction periodically, usually many times per second.  5, record 5, English, - alternating%20current%20pump

Record 5,  Textual support,  French

Record number: 5, Textual support number: 1 OBS

électropompe : Ensemble d'une pompe rotative et d'un moteur qui en assure l'entraînement.  2, record 5, French, - %C3%A9lectropompe%20c%2Ea%2E

Record number: 5, Textual support number: 2 OBS

alternatif : [Se dit d'un courant] dont l'intensité varie selon une sinusoïde (opposé à continu).  3, record 5, French, - %C3%A9lectropompe%20c%2Ea%2E

Record number: 5, Textual support number: 3 OBS

c.a. : courant alternatif.  4, record 5, French, - %C3%A9lectropompe%20c%2Ea%2E

Record number: 5, Textual support number: 4 OBS

électropompe c.a. : terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Maintenance.  4, record 5, French, - %C3%A9lectropompe%20c%2Ea%2E

Record 5,  Textual support,  Spanish

Record 6,  Textual support,  English

Record number: 6, Textual support number: 1 DEF

Fuel additive used to boost octane level.  4, record 6, English, - octane%20enhancer

Record number: 6, Textual support number: 1 OBS

Lead has been the main octane booster till recently but now other, more environmentally friendly substances, such as ether, are being used.  4, record 6, English, - octane%20enhancer

Record 6,  Textual support,  French

Record number: 6, Textual support number: 1 CONT

Ces remonteurs d'octane sont tous des composants oxygénés : alcools et éthers.  5, record 6, French, - remonteur%20d%27octane

Record number: 6, Textual support number: 1 OBS

Ne pas confondre avec «antidétonant», «antiknock agent» en anglais.  6, record 6, French, - remonteur%20d%27octane

Record 6,  Textual support,  Spanish

Record 7,  Textual support,  English

Record number: 7, 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 7, English, - fuel%2Doil%20heater

Record number: 7, 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 7, English, - fuel%2Doil%20heater

Record 7,  Textual support,  French

Record 7,  Textual support,  Spanish

Record 8,  Textual support,  English

Record number: 8, Textual support number: 1 DEF

Device which limits the maximum fuel delivery in relation to the engine boost(charge air) pressure.  1, record 8, English, - boost%20pressure%20controlled%20maximum%20fuel%20stop

Record 8,  Textual support,  French

Record number: 8, Textual support number: 1 DEF

Dispositif qui limite le débit de combustible maximal en fonction de la pression de suralimentation d'air à l'admission du moteur.  1, record 8, French, - but%C3%A9e%20de%20d%C3%A9bit%20maximal%20pilot%C3%A9e%20par%20pression%20de%20suralimentation

Record 8,  Textual support,  Spanish

Record 9,  Textual support,  English

Record number: 9, Textual support number: 1 OBS

[The chapter "Fuel"] includes engine driven fuel pumps for reciprocating engines, includes tanks(bladder), valves, boost pumps, etc., and those components which furnish a means of dumping fuel overboard.  1, record 9, English, - reciprocating%20engine

Record 9,  Textual support,  French

Record number: 9, Textual support number: 1 OBS

[Le chapitre «Carburant»] comprend les pompes de carburant entraînées par le moteur pour l'alimentation des moteurs à pistons, réservoirs (réservoirs souples) clapets, pompes auxiliaires, etc. et dispositifs de vide-vite.  3, record 9, French, - moteur%20%C3%A0%20piston

Record 9,  Textual support,  Spanish

Record 10,  Textual support,  English

Record number: 10, Textual support number: 1 OBS

(fuel boost pump).  2, record 10, English, - scroll%20housing

Record 10,  Textual support,  French

Record number: 10, Textual support number: 1 OBS

Terme uniformisé par le CUTA opérations aériennes.  2, record 10, French, - carter%20de%20volute

Record 10,  Textual support,  Spanish

Record 11,  Textual support,  English

Record number: 11, Textual support number: 1 DEF

... [an integral] reservoir [which] is formed by closing the second and sixth inboard bulkheads with flapper valves. These valves permit fuel to flow inboard but prevent fuel from flowing outboard away from the boost pumps in a wing-low attitude or other similar situation. The retained fuel provides a head of fuel to keep the boost pumps submerged at all normal flight altitudes and during all normal manoeuvres.  2, record 11, English, - secondary%20reservoir

Record 11,  Textual support,  French

Record number: 11, Textual support number: 1 OBS

compartiment nourrice secondaire : terme accepté par le Comité d'étude de la terminologie des cartes de travail du DC-9.  2, record 11, French, - compartiment%20nourrice%20secondaire

Record 11,  Textual support,  Spanish

Record 12,  Textual support,  English

Record number: 12, Textual support number: 1 CONT

Additional loads are automatically shed if an engine is shut down. This additional shedding partially offsets the hydraulic system requirement for additional electrical power to operate the electric demand pump. All cabin indirect ceiling lights, the forward direct ceiling lights and the respective fuel override boost pump are shed.  2, record 12, English, - fuel%20override%20boost%20pump

Record number: 12, Textual support number: 1 OBS

(central tank, B-767).  2, record 12, English, - fuel%20override%20boost%20pump

Record 12,  Textual support,  French

Record number: 12, Textual support number: 1 OBS

Terme uniformisé par le CUTA opérations aériennes.  2, record 12, French, - pompe%20d%27appoint%20carburant%20du%20r%C3%A9servoir%20central

Record 12,  Textual support,  Spanish

Record 13,  Textual support,  English

Record number: 13, Textual support number: 1 CONT

A cockpit "clean-up" is due after the landing roll is complete and the aircraft off the runway. If taxi distance to the parking area is short, the check might be delayed until then. The essential of the "after-landing check" usually are : 1. Cowl flaps-open(if adjustable). 2. Wing flaps-up. 3. Propeller and fuel-mixture controls-full advanced and rich. 4. Trim tabs-reset. 5. Fuel boost pump switch-off(if used for landing).  2, record 13, English, - after%20landing%20check

Record 13,  Textual support,  French

Record number: 13, Textual support number: 1 OBS

Le terme "vérification après atterrissage" a été proposé et uniformisé par le CUTA opérations aériennes.  2, record 13, French, - v%C3%A9rification%20apr%C3%A8s%20atterrissage

Record 13,  Textual support,  Spanish

Record 14,  Textual support,  English

Record number: 14, Textual support number: 1 OBS

the fuel heater and strainer assembly(...) is installed below the engine near the oil cooler and receives the incoming fuel under pressure from the boost pump.  1, record 14, English, - fuel%20strainer

Record 14,  Textual support,  French

Record 14,  Textual support,  Spanish

Record 15,  Textual support,  English

Record number: 15, Textual support number: 1 OBS

six double-element fuel boost pump assemblies are used in the fuel system(...)  1, record 15, English, - double%2Delement%20pump

Record 15,  Textual support,  French

Record 15,  Textual support,  Spanish

Record 16,  Textual support,  English

Record number: 16, Textual support number: 1 OBS

a fuel manifold dual check valve(...) is located at the junction of each boost pump discharge port and pump bypass.  1, record 16, English, - dual%20check%20valve

Record 16,  Textual support,  French

Record 16,  Textual support,  Spanish

Record 17,  Textual support,  English

Record number: 17, Textual support number: 1 OBS

a boost pump bypass check valve(...) is installed in a line at the outlet of each fuel boost pump.  1, record 17, English, - bypass%20check%20valve

Record 17,  Textual support,  French

Record 17,  Textual support,  Spanish

Record 18,  Textual support,  English

Record number: 18, Textual support number: 1 CONT

P. C. B. [Plenum Chamber Burning] consists of burning fuel in the front(cold) jet streams to give thrust boost for take-off in supersonic flight and, in consequence, a better thrust/S. F. C. matching in throttle-back subsonic cruise at low altitude.  1, record 18, English, - Plenum%20Chamber%20Burning

Record 18,  Textual support,  French

Record number: 18, Textual support number: 1 DEF

Dans un réacteur double-flux, une partie de l'air, après passage dans le compresseur est utilisé pour refroidir les parties extérieures de la zone de combustion et participer à la poussée: pour augmenter celle-ci on peut injecter ou enflammer du carburant dans le canal d'éjection propre à ce flux.  2, record 18, French, - r%C3%A9chauffe%20du%20flux%20secondaire

Record 18,  Textual support,  Spanish