KH 737

what is the first officers instrument panel. P1 panel. P2 panel. P3 panel. P7 panel.

Which main circuit braker panels are behind the first officer and capitain on panels: P6 and P18 panels. P6 and P8 panels. P18 and P6 panels. P18 panel.

Which are the three main jack points on the aircraft?. Wing jacking points A and B and nose jacking point C. Wing jacking points A and B and aft body jacking point C. Wing jacking point A body jacking point B and nose jacking point C. Wing jacking points A and C and aft body jacking point B.

Where is located the external power panel?. On the right side of the fuselage at near the nose. On the nose wheel well at near the nose. On the left side of the fuselage at near the stabilizer. AFT on the right side of the fuselage at near the APU.

What is the purpose of Nitrogen Generation System?. Allow oxygen in the center tank. Removes oxygen in the center tank. Removes nitrogen in the wing tanks. Filter oxygen in the center tank.

What is the purpose of the engine Fuel Spar Valve Battery?. Make sure that the engine 1 always has power to close the fuel spar valve. Make sure that the engine fuel system always has power to close spar valve. Make sure that the engine fuel feed system always has power. Make sure that the engine fuel system always has power to open spar valve.

What is the purpose of Scavenge Ejector Pumps?. Controls water from the high points of each tank to prevent corrosion. Removes water from the low points of each tank to prevent corrosion. Removes water from the low points of wing tanks to prevent corrosion. Remove water from the low points of center tank to prevent corrosion.

The primary flight control system has these components: Aileron (2) Stabilizers (2) and Rudder. Flaps and Elevator (2) and Rudder. Aileron (2) Elevator (2) and Rudder. Spoilers (2) Elevator (2) and Rudder.

The nose wheel steering system supplies: Ground directional control of the airplane. Extension and retraction systems extend and retract the landing gear. Flight directional control of the airplane. Support the aircraft on ground.

Which are the zones that Air Conditioner system controls the temperature?. The flight comparment and the passenger cabin. The pasenger cabin and cargo comparment. The AFT cargo comparment and FWD cargo comparment. The flight comparment and the cargo comparment.

How many thermocuples are on the APU exahaust section?. One chromel/alumel. Ten chromel/alumel. Three chromel/alumel. Two chromel/alumel.

When the Electronic Engine Control (EEC) operate automatically the engine ignition systems during operation?. Continuous operation. N1 at climb power. When sees a possible engine flameout condition. When sees a possible engine burnout condition.

The ignition exiters change the 115v ace input to: ac voltage of approximately 5000 to 10000v for spark igniter. dc voltage of approximately 15000 to 20000v for spark igniter. ac voltage of approximately 15000 to 20000v for spark igniter. dc voltage of approximately 5000 to 10000v for spark igniter.

There are 12 BVB that let some Low Pressure Compressor discharge air bypass the engine and mix with the fan dischrge. LPC stall during deceleration. LPC stall during fast aceleration. LPC stall during cold weather. LPC stall during hot weather.

What is the purpose of thrust reverse (T/R) system?. Increases the velocity of the exaust gases. Increases engine thrust. Changes the direction of the fan air exhaust to help create reverse thrust. Changes the acceleration of the fan air bleed to help create reverse thrust.

The engine oil system supplies oil to: Lubricate and cool and clean the accesory gear box. Lubricate and cool and claean the engine fan case. Lubricate and cool and claean the engine bearings and gears. Lubricate and cool and claean the engine rotors and compressor.

AOA sensor TAT probe and Pitot probes are heated by: Electrical power. Mechanical power. Bleed air. Pneumatic system.

What is the purpose of the airplane exterior lights?. Supply light for safety takeoff and landing. Supply light for maintenance operation ground support and flight. Supply light for airplane identification direction and to aid in the safe. Supply light for safety takeoff and landing, cabin crew lights and emergency lights.

The water heating system supplies hot water to: Water tank. The lavatory hot water faucet. Water tank and sinks. The lavatory hot water toilet.

Where is located the water quantity indicator?. At the attendant panel. At water tank. At cockpit. P2 panel secundary engine display.

Where is located the waste quantity indicator?. At cockpit. At the attendant panel. At water tank. At waste water tank.

Two master caurion lights and two system master caution annunciator are located?. P9 control panel. P6 load panel. P7 glareshield. P8 center pedestal.

The doors warning system give the visual indicator when?. The doors are closed and latched. The doors are not secure or not larched. The doors are open and latched. The doors are close and secured.

What is the purpose of the oxygen system?. To provide oxygen for the passenger only from takeoff to landing. To provide oxygen for crew and passenger only from takeoff to landing. To provide oxygen for the crew and passenger when required. To provide oxygen for the crew and passenger when the plane is on ground.

During a start or motor procedure the engine staring system uses pneumatic powe to turn: Engines N1 rotor. Engines accesory gearbox. Engines N2 rotor. Engines N1 and N2 rotor at the same time.

What is the purpose of flight spoilers?. Assist the elevator for pitch control. Assist the ailerons for roll control. Assist the ailerons for yaw control. Assist the ailerons for pich control.

The pitot static system provides?. Air temperature. Air density amd velocity. Measure pitot and static air pressure. Degrees of the aircraft angle.

How many VHF comunications antennas has B737-600-700-800-900?. 2. 4. 3. 1.

The engine fuel flow indicatot is showed at. P5. P2. P8. P7.

The autopilot mode is a function of?. Yaw Damper System (YDS). Auto Throttle System (ATS). Digital Fligth Control System. Display Fligth Computer System.

When you move the steering wheel full travel how many degrres maxumum can be turning the nose wheels?. 98. 68. 78. 75.

Which system provides the tank pressurization?. The hydraulic or the air compressor. The electric system or the air compressor. The pneumatic system or the air compressor. The electric pump from the main water tank.

What are the adventages of the composite?. Lightweight and econimic. Corrosion resistant and icreased fatigue life and lightweight. Economic and durable. Economic and hard properties.

Where is the main cabin pressurization outflow valve located?. Lower FWD fuselage. Near to the nose. Lower AFT fuselage. Lower nose landig gear.

What is the computer that control Autrothrottle System?. Engine Control Unit (ECU). Flight Managment Computer (FMC). Flight Control Computer (FCC). Flight Control Unit (FCU).

What are the engines stages used to obtain the bleed air to the pneumatic system?. The stages 5th and 9th from HPC. The stages 4th and 9th from HPC. The stages 5th and 9th from LPC. The stages 4th and 9th from LPC.

What kind of bearing support the engine rotors and what kind of loads absorb?. Ball bearing: absorb radial and axial loads Roller bearing: absorb only radial loads. Ball bearing absorb only radial loads Roller bearings support the engine rotors and absorb both radial and axial loads. Ball bearing: absorb only axial loads Roller bearing: absorb radial and axial loads. Ball bearing: absorb radial loads only Roller bearing: absorb axial loads only.

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

How many ignition exciters are in the engines?. Two for each engine. Two for all engines. One for each engine. One for all engines.

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 C is de-pressurized. Supplies alternative pressure to leading edge flaps and slats and autoslat system if system B is pressurized. Supplies alternative pressure to leading edge flaps and slats and autoslat system if system B is over-pressurized.

What does it mean when the ON green light come on in the Window Heat control panel?. Three the green on lights give an indiccation of the status of window heat to the N1 and 2 windows the ligths come on when the power is supplied to the related window. Four the green on lights give an indiccation of the status of window heat to the N1 and 2 windows the ligths come on when the power is supplied to the related window. Three the red on lights give an indiccation of the status of window heat to the No 1 and 2 windows the ligths come on when the power is supplied to the related window. Three the red on lights give an indiccation of the status of window cold to the No 1 and 2 windows the ligths come on when the power is supplied to the related window.

What is the purpose of common display system?. Show performance, navegation and engine information in many different formats on six displays unit in the flight comparment. Show performance, navegations and engines information in many different formats on six displays unit in the flight comparment. Show performance, navegation and engine information in many different formats on five displays unit in the flight comparment. Show performance, navegation and engine information in many different formats on five displays unit in the flight comparment.

What is the purpose of Tail Skid?. Controls the brake system to prevent skids diring brake application. Protects the stabilizer bulkhead and fuselage structure when the main landing gear shocks are extended and the airplane rotates during takeoff. Protects the stabilizer bulkhead and fuselage structure when the nose landing gear shocks are extended and the airplane rotates during takeoff. Controls the brake system to prevent skids diring brake application during takeoff or landing.

What is the source that send speed and altitude parameter to the standby/airspeed indicator?. Capitan pitot probe and FO static port. First officer pitot prove and static port. The auxiliary pitot probe and the alternate static port. The emergency static port of the nose radom radar.

What is the function of ignition exciters?. Supply power to the spark ignited changing the 115 v AC to DC voltage. They regulate the timing of the spark ignition process. They conver mechanical energy into electrical energy. Supply power to the spark ignited changing the 115 v DC to AC voltage.

Where is obtained the air for LPTACC?. From stage 1 from LPC. Sends fan discharge air to the low pressure turbine (LPT) case. It is obtained from the engine's high-pressure air system. Sends fan discharge air to the high pressure turbine (HPT) case.

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. The system hydraulic pressure is available, the FLT CTRL B switch must be OFF. The system pneumatic pressure is available, the FLT CTRL B switch must be ON.

What is the function of GCU?. The GCUs monitor the system to control and protect the IDGs. The GCUs monitor the system to control and protect the Engines. The GCUs monitor the system to control and protect the EEC. The GCUs monitor the system to control and protect the Igniters of spark.

Where are located the engine and APU fire control panel?. APU fire control panel P8. And P28 for ground panel. APU fire control panel P5. And P38 for ground panel. APU fire control panel P7. And P38 for ground panel. APU fire control panel P5. And P27 for ground panel.

Where is located the refueling panel?. Lower right wing. Upper right wing. Lower left wing. Left AFT wing.

What is the function of FQIS?. The fuel quantity indicating system (FQIS) shows fuel weight of the main tanks and the center tank on the common display system (CDS) and the P15 refuel panel. The fuel quantity indicating system (FQIS) shows fuel weight of the main tanks and the center tank on the common display system (CDS) and the P13 refuel panel.

What are the main hydraulic system?. The main hydraulic systems are A and B. System A has most of its components on the left side of the airplane and system B on the right side. The main hydraulic systems are A and B and stand by. System A has most of its components on the left side of the airplane and system B on the right side. The main hydraulic system is A. System A has most of its components on the left side of the airplane and system stand by on the right side.

What is a body station, buttock line and body water line?. Water line is a plane perpendicular to the BBL. Water line is a plane parallel to the BBL.

What is the function of the main gear torsion link?. Prevent the inner shock strut from rotation in the outer shock strut. Prevent the outer shock strut from rotation in the inner shock strut.

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

Where is located the MCP ?. In the grarlishield P7 panel. In the P8 panel. Mode Control Panel. P18 panel.

What is the computer that control the autothrottle system??. DFC Display Flight Computer. EEC. Flight computer control A.