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TEST BORRADO, QUIZÁS LE INTERESECapitulo 7

COMENTARIOS ESTADÍSTICAS RÉCORDS
REALIZAR TEST
Título del test:
Capitulo 7

Descripción:
Pulentation

Autor:
javierefix
(Otros tests del mismo autor)

Fecha de Creación:
30/11/2023

Categoría:
Ocio

Número preguntas: 20
Comparte el test:
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Últimos Comentarios
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Temario:
The primary thrust indicator for the PW 530 A is: a) Fuel Flow. b) N1. c) ITT. d) N2.
If one ignitor plug has failed, the result will be: a) A normal engine start. b) A hot start. c) No combustion. d) No start button light.
In a normal engine start, ignition activates by: a) Turning the ignition switches to ON at 8 to 10% N2. b) Moving the power lever to idle at 8 to 10% N2. c) Depressing the start button. d) Motive flow fuel pressure.
Ignition during engine start is normally terminated by: a) Turning the ignition switches to OFF. b) The speed sensing switch on the starter/generator. c) Turning the boost pump off. d) Opening the IGN circuit breakers on the circuit breaker panel.
With the ignition switch in NORM, power will automatically be applied to the ignitors: a) When the start button is pressed and the power lever is out of cutoff. b) When an emergency descent is initiated. c) When ENG ANTI-ICE is on. d) a and c.
Which statement is correct? a) Fuel is used to cool the engine oil via a fuel oil heat exchanger. b) The accessory gearbox has its own lubricating system. c) The only indication of alow oil pressure condition is the red OIL PRESS WARN light on the annunciator panel. d) The ITT gauge provides it is own electrical power for activation.
The maximum allowable oil consumption for the PW530A is approximately: a) One quart every 10 hours b) One quart every 4 hours measured over a 10–hour period c) 1/2 gallon every 40 hours d) Oil consumption should be zero.
If the N1 shaft shifts to the rear beyond a predetermined distance: a) The engine automatically shutsdown. b) The vibration detector causes illumination of the master warning lights. c) The synchronizer shuts the engine down. d) All of the above.
The following engine instruments are available in the event of a loss of normal DC electrical power: a) N1 and ITT. b) N1, N2, and ITT. c) N1 tapes and digits. d) N1 tapes only.
The ground idle system: a) Reduces N1 rpm to 49.5%. b) Increases N2 rpm to 45.5%. c) Can be pneumatically operated. d) Is deactivated at liftoff.
The GROUND IDLE light: a) Is on when the switch is in HIGH. b) Is on with system failure. c) Requires emergency bus power to illuminate. d) Is on when the switch is in NORM, aircraft on the ground and normal DC power is available.
The ground idle system: a) Should be in NORM for cross generator starts. b) Requires main DC power for operation. c) Should be in NORM with anti-ice system on while taxiing. d) Reduces takeoff field length requirements.
The ground idle system: a) Requires electrical power to reduce N2 rpm. b) Requires electrical power to increase N2 rpm. c) Fails to 45.5% N2. d) Reduces N2 rpm to 49.5% on touchdown with the switch in NORM.
An increase of ITT should take place: a) 15 seconds after pressing the start button. b) 10 seconds after pressing the start button. c) 10 seconds or less after coming out of idle cutoff. d) Within 38-42% N1 rpm.
Start sequence termination is indicated by: a) Boost pump activation. b) Ignition lights on. c) Start button light comes on. d) Engine instrument flood light goes out.
The start sequence is terminated by: a) The starter disengage button. b) The speed sensing switch in the starter/generator. c) The GCU sensing an overvoltage condition. d) a or b.
If one channel of the ignition exciter box fails: a) There will be no green ignition light. b) There will be a green ignition light. c) Both ignition lights will come on for that engine start. d) There will be no ignition.
When the start button is pressed, the: a) FUEL BOOST ON light goes out, the instrument floodlight comes on, and the FUEL LOW PRESS light comes on. b) Ignition light comes on immediately. c) Instrument floodlight comes on, the FUEL BOOST ON light comes on, and the FUEL LOW PRESS light goes out. d) Ignition light comes on, the HYD FLOW LOW light comes on, and the N1 tape indicates an immediate but gradual rpm increase.
The cockpit indications that a generator assisted start is in process is: a) Both ignition lights are on. b) Both boost pump lights are on. c) Both start button lights are on. d) Both generator lights are on.
A generator assisted start: a) Can be done on the ground only. b) Needs the ground idle switch in HIGH. c) Counts as 1/3 of a battery start. d) Any or all of the above.
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