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Mi Daypo

BOEING ACT. 1

COMENTARIOS ESTADÍSTICAS RÉCORDS
REALIZAR TEST
Título del test:
BOEING ACT. 1

Descripción:
ACTUALIZADO

Autor:
NAY
(Otros tests del mismo autor)

Fecha de Creación:
11/01/2022

Categoría:
Personal

Número preguntas: 20
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Temario:
What are the major zones in the aircraft? 100 Lower Half of Fuselage. 200 Upper Half of Fuselage. 300 Empennage. 400 Powerplant and Nacelle Struts. 500 Left Wing. 600 Right Wing. 700 Landing Gear and Landing Gear Doors. 800 Doors. 100 Lower Half of Fuselage. 200 Upper Half of Fuselage. 300 Empennage. 400 Powerplant and Nacelle Struts. 600 Right Wing. 700 Landing Gear and Landing Gear Doors. 800 Doors. 100 Lower Half of Fuselage. 200 Upper Half of Fuselage. 300 Empennage. 400 Powerplant and Nacelle Struts. 500 Left Wing. 600 Right Wing. 700 Landing Gear and Landing Gear Doors. .
What are the models of B737 NG? B737−600. B737−700. B737−800. B737−900. B737−400. B737−500. B737−600. B737−700 B737−100. B737−200. B737−300. .
What is the body Fuselage station? A plane that is perpendicular to the fuselage diagonalline A plane that is perpendicular to the fuselage centerline. A plane that is circul to the fuselage centerline.
Which are the principal and auxiliary points of jacking? The main points are wing jacking points A and B and aft body Jacking point C. The four auxiliary points are forward body jacking Point D and three landing gear points E (Main Landing Gear) and F (Noser) The main points are wing jacking points A and B and aft body Jacking point C. The four auxiliary points are forward body jacking Point D and three landing gear points E (Nose) and F (Main Landing Gear). The main points are wing jacking points C and B and aft body Jacking point C. The four auxiliary points are forward body jacking Point D and three landing gear points E (Nose) and F (Main Landing Gear) .
Where is located p6 and p18 panels? P18 is located behind the first officer’s seat P6 is located behind the captain’s seat P6 is located behind the first officer’s seat. P18 is located behind the captain’s seat. P6 is located behind the the captain’s seat P18 is located behind the first officer’s seat .
. maximum angle of the nose steering is? 78 Degrees 78 Degre 79 Degrees.
How many times the standby electrical power system supplies AC and DC power to the electrical network of the aircraft? A minimum of 30 minutes of AC and DC power to systems Necessary to maintain safe flight. A minimum of 30 minutes of DC and AC power to systems Necessary to maintain safe flight A minimum of 25 minutes of AC and DC power to systems Necessary to maintain safe flight.
What is the function of TRU? Change 115v ac to 28v dc. Change 115v ac to 30v dc Change 28v ac to 115v dc.
Where is located the extenal power connection? Is located on the right side of the fuselage, near the nose. Is located on the left side of the fuselage, near the nose Is located off the right side of the fuselage, near the nose.
.What is the function of the Static Inverter? Supplies a two phase, converter 115 vdc to 28 Vac output to the AC standby bus Supplies a one phase, converter 28 vdc to 115 Vac output to the AC standby bus. Supply a one phase, converter 28 vdc to 115 Vac output to the AC standby bus 1.
What type of alert does the Fire and overheat detection system provide to alert the flight crew? Visual and aural indications. Visual Visual and aural indications.
Where are located the APU remote control panel? Is in the right main wheel well, on the aft Bulkhead. Is in the right main well, on the aft Bulkhead Is in the left main wheel well, on the aft Bulkhead.
What is the function of Nitrogen Generator system? Removes oxygen in the side left tank air to a level which does not support combustion Removes oxygen in the center tank air to a level which does not support combustion. Is in the right main wheel well, on the aft Bulkhead.
.How many fuel tanks are installed in the aircraft? There are 3 fuel tank: • Main tank 1 • Main tank 2 • Center tank. 3 There are 3 fuel tank: • Main tank 1 • Main tank 2 • Center tank. Two are 2 fuel tank: • Main tank 1 • Main tank 2 .
.What is the function of the Fuel Spar valve battery? Makes sure that the engine fuel feed system Makes sure that the engine fuel feed system always has power to close the engine fuel spar valve. Makes sure that the engine fuel feed system never she power to close the engine fuel spar valve.
What is the function of the water scavenge ejector pumps? Remove water from the low points of each tank to prevent corrosion. Remove popo from the low points of each tank to prevent corrosion Remove water from the low points on each tank to prevent detecion.
.During refueling procedures of the main tanks center tanks, the BLUE valve position lights come on? When the refueling shutoff valve have power When the refueling shutoff valve solenoids have power. When the refueling shuton valve solenoids have power.
How many fuel measuring stick are installed in the aircraft and what is the function? There are 8 measuring sticks in the A/C their function is manually measure the quantity of fuel. nine are 9 measuring sticks in the D/C their function is manually measure the quantity of fuel There are 3 measuring sticks in the A/C their function is manually measure the quantity of fue .
Which are the three main Hydraulic Systems? System A, D, and C System B, C, and D (Auxiliary) System A, B, and C (Auxiliary).
What is the function of Power Transfer Unit (PTU)? Supply alternative pressure to leading edge flaps and slats and autoslat system if system C is de-pressurized. Supplies alternative pressure to leading edge flaps and slats and autoslat system if system B is de-pressurized. Supplies alternative pressure to leading edge flaps and slats and manual system if system A is despressurized. .
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