boeing 737 NG familiarization

what are the zone in the aircraft. 100,200,300,400,500,600,700,800,. ,300,400,500,600,700,800,900. 100,200,300,400,600,700,800.

what are the models of B737NG. B737-300,B737-400,B737-500. B737-600,-B737-700,B737-800,B737-900. B737-100,B737-200.

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 (Nose) and F (Main Landing Gear). The main points are wing jacking points Eand D and forward body Jacking point F. The four auxiliary points are after body jacking Point D and three landing gear points E (Nose) and F (Main Landing Gear).

What is the body Fuselage station. A plane that is perpendicular to the fuselage centerline. A plane that is parallel to the fuselage centerline. A plane that is vertical to the fuselage centerline.

Where is located p6 and p18 panels. P6 is located behind the first officer’s seat P18 is located behind the captain’s seat. P6 is located forward the first officer’s seat P18 is located after the captain’s seat.

maximum angle of the nose steering is. 78 Degrees. 88 Degrees. 68 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 20 minutes of AC and DC power to systems Necessary to maintain safe flight. A minimum of 40 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 120v ac to 28v dc. Change 118v ac to 28v 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 on the after side of the fuselage, near the nose.

What is the function of the Static Inverter. Supplies a one phase, converter 28 vdc to 115 Vac output to the AC standby bus. Supplies a two phase, converter 28 vdc to 115 Vac output to the AC standby bus. Supplies a one phase, converter 115 vdc to 28Vac output to the AC standby bus.

What type of alert does the Fire and overheat detection system provide to alert the flight crew?. Visual and aural indications. visual indications. aural indications.

Where are located the APU remote control panel. Is in the right main wheel 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 center tank air to a level which does not support combustion. Removes oxygen in the center tank air to a level which support combustion. supplies oxygen in the center tank air to a level which does not support combustion.

How many fuel tanks are installed in the aircraft. There are 3 fuel tank: • Main tank 1 • Main tank 2 • Center tank. There are 2 fuel tank: • Main tank 1 • Main tank 2. 1 fuel tank center tank.

What is the function of the Fuel Spar valve battery. Makes sure that the engine fuel feed system always has power to close the engine fuel spar valve. Makes sure that the engines fuel feed system always has power to open 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 not prevent corrosion. Remove water from the low points of each tank to prevent corrosion. none.

During refueling procedures of the main tanks center tanks, the BLUE valve position lights come on. When the refueling shutoff valve solenoids have power. When the refueling shutoff valve solenoids has powers.

.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. There are 4 measuring sticks in the A/C their function is manually measure the quantity of fuel. There are 6 measuring sticks in the A/C their function is manually measure the quantity of fuel. there are 16 measuring stick.

Which are the three main Hydraulic Systems. System A, B, and STANBY Hidraulic Sys. System A, B, and battery.

What is the function of Power Transfer Unit (PTU). 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 autoslat system if system A is de-pressurized. Supplies alternative pressure to leading edge flaps and slats and autoslat system if system C is de-pressurized.

Where is the main cabin pressurization outflow valve located?. lower aft fuselage. above before fuselage.

Which zone in the B737-600/700 aircraft are temperature controlled by the Air Conditioning System?. Pack/Zone Temperature Controller. the fligth compartment and passenger cabin.

What is the function of the main gear torsion link. Prevent the inner shock strut from rotation in the outer shock strut. Prevent the not inner shock strut from rotation in the outer shock strut.

What does it mean when the GREEN, RED landing gear position lights come on and when all landing gear position lights are off?. the green landing gear and the auxiliary landing gear , the red landing gear position lights come on. When the landing gear is down and locked. The red landing gear position lights come on when the landing gear are not down and locked, not up and locked, or are in transition to up or down.

What is the function of Shimmy damper. Decreases vibration between the inner and outer cylinders during high speed taxi and heavy brake use. increase vibration between the inner and outer cylinders during high speed taxi and heavy brake use.

What brake system gets pressure to operate the brakes to stops wheel rotation before the landing gear retracts. The alternate brake system. the parking brake.

What are the sources of the Pneumatic system. Engine 1 bleed air system • Engine 2 bleed air system • Auxiliary power unit (APU) bleed air system • Pneumatic ground air connection. • Engine 2 bleed air system • Auxiliary power unit (APU) bleed air system • Pneumatic ground air connection. • Auxiliary power unit (APU) bleed air system • Pneumatic ground air connection.

What the stages of the engine is used to obtain the bleed air to the pneumatic system. Is from the 5th and 9th stages. Is from the 4th and 9th stages. Is from the 9th and 5th stages.

What is the meaning of EGT. Exhaust gas temperature. exhaust gear temeperature.

What are the incorrect conditions for which the ECU performs a protective shutdown of the APU. Low oil not pressure, high oil temperature or starter- generator filter clogged. Low oil pressure, high oil temperature or starter- generator filter clogged.

How many Thermocouples are installed in the APU. Two chromel/alumel thermocouples. one termocouples. three termocouples.

What are the primary flight control. Aileron (2) • Elevator (2) • Rudder. slat,flap,elevator. stabilizer vertical,ruder,stabilizer horizontal.

What are the secondary flight control. • Leading edge devices (12) • Trailing edge flaps (4) • Spoilers and speedbrakes (12) • Horizontal stabilizer. • ruder • slats • Spoilers and speedbrakes (12).

What is the purpose of flight spoilers. To assist the ailerons for roll control. to assist the slats. to assist the flaps.

How the horizontal Stabilizer is operated. the pilot use the stabilizer trim wheels on the control stand to manually move the forward aft cable drumps.the aft cable drum moves the gear box and jackscrew the moves the horizonta stabilizer. the pilot use the stabilizer not trim wheels on the control stand to manually move the forward aft cable drumps.the aft cable drum moves the gear box and jackscrew the moves the horizonta stabilizer. Manual operation & Electric operation.

How is operated the Leading edge flap and slat and the Trailing edge Flaps in a Standby condition. If system B is de-pressurized. The PTU is controlled by the PTU control valve. System A pressurizes the motor when the PTU control valve is open. System B supplies the fluid to the pump. If system C is de-pressurized. The PTU is controlled by the PTU control valve. System A pressurizes the motor when the PTU control valve is open. System C supplies the fluid to the pump. leading edge flap and slat they work hydraulically and trailing edge flaps works electrically.

what kind of engine are installed on the boeing 737-600/700/800/900. CFM56-6. CFM56-7. CFM56-5.

What is the purpose of engine fuel and control system. calculates the quantity of fuel necesary to make the commanded thurst. not calculates the quantity of fuel necesary to make the commanded thurst.

how many EEC are installed in the engine. one for each engine. two for each engine. three for each engine.

how many ignition exciters are in the engines. two ignition exciter for each engine. one ignition exciter for each engine.

what is the function of ignition exciters. supply power to the spark igniters.change 115v ac input to a dc voltaje of approximately 15,000 to 20,000 for the spark igniters is 14.5 to 16 joules. supply power to the spark igniters.change 120v ac input to a dc voltaje of approximately 15,000 to 20,000 for the spark igniters. supply power to the spark igniters.change 125v ac input to a dc voltaje of approximately 15,000 to 20,000 for the spark igniters.

where is obtained the air for HPTACC. sends HP 4th storage and 9 th storage air to the high pressure turbine. sends HP 5th stage and 9 th stage. sends HP 6th stage and 9 th stage.

where is obtained the air for LPTACC. sends fan discharge air to the low pressure turbine (LPT) case. sends fan charge air to the low pressure turbine (LPT) case.

what is the function of VBV. system lets a part of the low pressure compressor(LPC) discharge air go to the secondary airflow. system lets a part of the low pressure compressor(LPC) charge air go to the secondary airflow. let some LPC discharge air bypass the engine and mix with the fan discharge air.

what is the function of thrust lever resolver. change the mechanical forward and reverse thrust lever position to analog thrust lever position to analog thurst lever resolvers. dishange the mechanical forward and reverse thrust lever position to analog thrust lever position to analog thurst lever resolvers.

what is the function of thrust rever system. changes the direction of the fai air exhaust to help create reverse thurst. dishanges the direction of the fai air exhaust to help create reverse thurst.

what is the purpose of engine oil system. supplies oit to lubricated cool and clean the engine bearings and gears. supplies oit to not lubricated cool and clean the engine bearings and gears.

what engine rotor turn during start procedure. N2/ hihg pressure rotor. N1/ high pressure rotor.

where are located service door,entry door emergency door in the aircraft. The entry doors are on the left side of the airplane. The galley service doors are on the right side of the airplane. The emergency exit doors are above the wings on both sides of the airplane. supplies oit to lubricated cool and clean the engine bearings and gears. the entry door on the before side of the airplane,the emergency exit doors are above the wings on both sides of the airplane service doors service doors are near the systems they serve.

when the door warning system is activated. when the door is latched,it causes the P5 panel warning light to go off. when the door is latched,it causes the P7 panel warning light to go off. The door warning system gives the crew a visual indication when a door is not secure (NOT CLOSED).

what components are heated with elctrical power. air data probe,flight compartment window,water and waste system lines and drains. air data not probe,flight compartment window,water and waste system lines and drains.

what is the porpuse of the flight data recorder system. stores airplane parameters and system data for the last 25 hours of operation. stores airplane parameters and system data.

how much time the FDR store aircraft parameters and system data. 25 hours of operation. 20 hours of operation. 15hours of operation.

where is located the two master caution lights and the two marning lights. p7 glareshield panel. p4 center.

what is the purpose of common display system. show performance,navigation and engine information in many different formats on six displays unit in the flight compartment. show performance,navigations and engines information in many different formats on six displays unit in the flight compartment.

what is the function of the exterior lights. supply light for airplane identification direction and to aid in the safe operation of the airplane. suppies lights for airplane identification direction and to aid in the safe operation of the airplane.

what is the purpose of oxygen system. supply oxygen to the flight crew,cabin attendants and passenger. suppliesnot oxygen to the flight crew,cabin attendants and passenger.

what is the purpose of potable water tank. supplies potable water to the lavatories and galleys. supply not potable water to the lavatories. supply not potable water to the galleys.

where is located the water tank. is located at aft of the aft cargo compartment. is loccated at forward of the cargo compartment.

how many antenas de VHF system have. 3 antenas. 4 antenas. 2 antenas.

how much time store the above voice recorder system. the last 120 minutes of communication data in memory. the last 60 minutes of communication data in memory. the last 100 minutes of communication data in memory.

what is static air pressure. is the ambient air pressure around the airplane. is the ambient air not pressure around the airplane. is to measure Pitot and static air pressure. These pressures are used to calculate flight parameters such as airspeed and altitude.

what is pitot air pressure. is the air pressure on the pitot probe tube as a result of the forward motion of the aiplane. is the air not pressure on the pitot probe tube as a result of the forward motion of the aiplane.

What components are connected to N2 and N1 rotor. N2: high pressure compressor, high pressure turbine, accessory gearbox. N1: Low pressure turbine, Low pressure compressor, FAN. N1: high pressure compressor, high pressure turbine, accessory gearbox. N2: Low pressure turbine, Low pressure compressor, FAN.

What Kind of Bearing support the engine rotor`s and what kind of loads absorb. Ball bearings absorb the axial and the radial loads from the shafts. Roller bearings absorb only radial loads. Ball bearings not absorb the axial and the radial loads from the shafts. Roller bearings absorb only radial loads. Calculates the quantity of fuel necessary to make the commanded thrust.

Which are the adventages of the composite material. High strength • Corrosion resistant • Increased fatigue life • Light weight. aileron,flaps.

.What components are heated with bleed air. The wing thermal anti-ice and the engine inlet cowl thermal anti-ice systems use hot bleed air. The flaps thermal anti-ice and the engine inlet cowl thermal anti-ice systems use hot bleed ai.

What does it mean when the ON green light come on in the Window Heat control panel. four the green on lights give an indiccation of the status of window heat to the N1.and 2 windows.the lights come on when power is supplied to the related window. three the green on lights give an indiccation of the status of window heat to the N1.and 2 windows.the lights come on when power is supplied to the related window.

What is the function of Master Caution system. Provides a visual alert to the flight crew for incorrect airplane systems operation. Provides aural alert to the flight crew for incorrect airplane systems operation.

When the EEC can operate the ignition system in automatic mode. When the electronic engine control (EEC) sees a possible engine flameout condition. Where the electronic engine control (EEC) sees a possible engine flameout condition.

How is activated the Passenger Oxygen system automatically. Automatically by operation of a pressure switch (14000 feet cabin altitude). manual by operation of a pressure switch (12000 feet cabin altitude). Automatically by operation of a pressure switch (10000 feet cabin altitude).

Which system provides the water tank pressurization?. From the EPSUor the air compressor to pressurize the water tank. From the pneumatic system or the air compressor to pressurize the water tank. From the engine or the air compressor to pressurize the water tank.

Where is located the Water and Waste Indicator panel?. The water service panel is at the before section of the fuselage, bottom right side. aft attendant control panel. The water service panel is at the aft section of the fuselage, bottom left side.

What is the source that send speed and altitude parameters to the standby altimeter/airspeed indicator?. Pitot and alternate static ports. static ports. speed air.

Which computer contain the Instrument Landing System Function?. Multi-mode receiver (MMR). emergency power supply(EPSU). ADIRS.

Which display unit is used for the cabin crew to visualize the weather radar, TCAS, parameters?. Navigation Display (ND. primary flight display. second flight display.

What are the function of digital flight control system?. • Autopilot • Flight director • Altitude alert • Speed trim • Mach trim. • Autothrottle. slats flaps ailerons elevator.

What is the function of yaw damper?. Keeps the airplane inestable around the airplane yaw (vertical) axis. Keeps the airplane stable around the airplane yaw (vertical) axis.

What is the computer that control the autothrottle system?. flight warning computer. Flight Control Computer A (FCC). ECAM.

what are conditions that allow the yaw damper system to operate. the system hydraulic pressure is available,the FLT CTRL B switch must be ON. the system electric pressure is available,the FLT CTRL B switch must be ON.

Quiens son más pendejos del EMAI. 7.1. 7.2. Ambos.