737机型习题

737机型习 题 快递公司问题件快递公司问题件货款处理关于圆的周长面积重点题型关于解方程组的题及答案关于南海问题 ATA21 Air Conditioning 1. The air conditioning system controls __________ of the airplane. A the exterior environment B the interior environment C the anti-ice system D the oxygen system 2. The air conditioning system for flight crew, passengers, and _______ . A engine B air conditioning accessory unit C cabin temperature controller D equipment 3. Air conditioning sub-systems are _______ , Pressurization, Equipment cooling, Heating, Cooling and Temperature control. A Distribution B Pack cooling temperature C Electronic equipment D Air conditioning accessory unit 4. These _______ panel let you control the air conditioning system. A electronic equipment compartment B passengers compartment C flight compartment D nose compartment 5. _______, air conditioning accessory unit and cabin pressure controllers in the EE compartment control the functions of the air conditioning system. A Cabin temperature controller B Auxiliary power unit C Electronic display unit D Common display system 6. The cabin temperature controller controls _______ , flight compartment temperature and passenger cabin temperature of the air conditioning system. A Pack cooling temperature B The bleed air temperature C The exhaust temperature D The landing gear cabin temperature 7. _______ is the interface for the airplane operational logic and the air system. A Cabin pressure controllers B Passenger pressure controllers C Air conditioning accessory unit D Air conditioning system 8. The cabin pressure controllers control the cabin _______ function of the air conditioning system. A temperature B heating C pressure D cooling 9. These flight compartment panels on the _______ forward overhead panel let you control the air conditioning subsystem. A p5 B p2 C p1 D p4 10. _______ , Passenger cabin temperature, Temperature indication and selection, Duct overheat indication and Air mix valve position indication controls and indications are on the cabin temperature panel. A Water indication B Oil indication C Fuel indication D Control cabin temperature control 11. The equipment cooling fans switch is on _______ . A the cabin cooling panel B the equipment cooling panel C the cabin temperature panel D the air conditioning/bleed air controls panel 12. The distribution system has _______ , Recirculation fan, Ground conditioned air connection in the distribution compartment. A Distribution B Electronic equipment C Main distribution manifold D Water indication 13. The equipment cooling system has components in _______ , the forward equipment compartment and the flight compartment. A the nose compartment B the passenger compartment C the EE compartment D the galley 14. The _______ air conditioning packs are in the air conditioning compartment. A 1 B 3 C 5 D 2 15. The air conditioning compartment are on the left and right sides of keel beam in _______. A the wing-to-body area B the head-to-body area C the landing gear cabin D the left area 16. These are the primary parts of the air conditioning system that have an effect on the supply of _______ or the recirculation of conditioned air. A hot air B fresh air C cool air D common air 17. The left and right flow control systems provide the ______ quantity of fresh air. A different B good C distinguished D same 18. _______ changes when airplane conditions change. A hot air B cool air C fresh air D common air 19. This part of the A/C system removes _______ as necessary and controls the temperature of the fresh air before it goes into the air distribution part of the air conditioning system. A water B oil C fuel D pressured air 20. The control for the right makes sure that it supplies air at a temperature that gives the necessary cooling for _______. A the flight compartment B the EE compartment C the nose compartment D the passengers compartment KEY: B D A C A A C C A D B C C D A B D C A D ATA22 Digital Flight Control System 1. The digital flight control system does these functions of _______ , flight director, altitude alert, speed trim, mach trim. A height director B speed director C autopilot D climb director 2. The FCCs get inputs from several systems such as __________ and the flight management computer and sends commands to the aileron and elevator actuators. A APU B ADIRU C CDS D DEU 3. There are two autopilots, autopilot A from FCC A and autopilot B from FCC B. When you engage an autopilot from _______ , the autopilot controls the airplane attitude. A MCP B AGB C IDG D EEC 4. The FCCs get inputs from several systems and send flight director commands to _______ to provide guidance for the pilots. A EEC B IDG C AGB D CDS 5. When the MCP flight director switches are on, _______ shows on the common display system. A autopilot B flight director C altitude alert D speed trim 6. _______ can use the flight director commands to control the attitude of the airplane. A Flight crew B Flight attendant C Passengers D Maintenance personnel 7. As the airplane approaches or flies away from _______ selected altitude, an alert occurs. A IDG B DEU C MCP D CDS KEY: C B A D B A C ATA24 Electrical Power 1. The electrical power system has automatic and manual _______ features. A control B operation C play D perform 2. Electrical power has these subsystems: Generator drive, AC generator, _______, External power, AC electrical load distribution. A AGB B ASG C DC generator D BPCU 3. The electrical power system makes and supplies AC and DC power to _______. A APU B Engine1 and Engine2 C Landing gear D Airplane 4. A standby AC and DC system gives _______ power. A normal B emergency C normal and emergency D special 5. The electrical power system has _______ main AC power sources and 1 standby power sources. A 2 B 4 C 6 D 8 6. The IDGs and APU starter-generator supply a _______, 115/200 volts at 400Hz. A 3 phase B 2 phase C 1 phase D DC 7. The AC power system design prevents _______ to the same load at the same time. A one source B two sources C three sources D four sources 8. The static inverter supplies a _______, 115V AC output to the AC standby bus. A 4 phase B 3 phase C 2 phase D 1 phase 9. Three transformer rectifier units change 115V ac to _______ dc. A 10V B 18V C 28V D 35V 10. The GCUs monitor the system to _______ the IDGs. A control and protect B control C protect D operate 11. _______ protects the airplane from external power whose quality is out of limits. A AGB B IDG C GCU D BPCU 12. _______ automatically removes loads to prevent an overload of an AC power source. A System logic B Subsystem logic C Part logic D AC logic 13. DC bus 1 usually receives power from TRU _______. A 2 B 1 C A+B D 3 14. The hot battery bus usually receives power from _______. A main battery B main battery charger C main battery or main battery charger D main battery and main battery charger KEY: A C D C B A B D C A D A B C ATA25 Equipment/Furnishings 1. The captain and first officer seats provide adjustable seats for _______. A flight crew B passengers C captain D first officer 2. _______ lock mechanism sets fore and aft movement on the seat tracks. A track B seat track C spring-loaded track D seat height 3. The seat height lock mechanism control _______. A seat height B seat attitude C seat back D A+B+C 4. The track lock mechanism controls _______. A seat fore B seat fore and aft C seat aft D seat left and right 5. Turn the knob to move the armrest ______. A up B down C up and down D up or down 6. The seat folds to _______ wall when not in use. A flight compartment B passenger compartment C EEC D nose compartment KEY: A C A B D A ATA26 Fire Protection 1. The fire protection systems monitor fire, pneumatic duct leaks, overheat, _______. A smoke B dust C water D ice 2. The airplane has these fire extinguishing systems: Engine, _______, Lavatory. A flight compartment B passenger compartment C EEC D APU 3. The fire alarms provide visual and aural indication to the flight crew about a fire in any of these systems: Engine 1 , Engine 2 , _______ . A Lavatory B APU C EEC D Passenger compartment 4. When there is a fire in the main wheel well, the compartment onerheat detection controller provides a ground for _______. A one red FIRE WARN lights and the bell B lights C bell D two red FIRE WARN lights and the bell KEY: A D B D ATA27 Flight Controls 1. The flight controls keep _______ at the necessary attitude during flight. A the airplane B the aileron C the elevator D the rudder 2. The primary flight control system moves the airplane about _______ axes. A 1 B 2 C 3 D 4 3. The secondary flight control system improve the _______ and handling properties of the airplane. A power B lift C speed D altitude 4. The aileron control wheels move cables that give input to _______ . A the aileron feel and centering unit B the accessory gear box C the power control unit D the auxiliary power unit 5. The _______ move the aileron wing cables and the ailerons. A ABG B APU C FCC D PCU 6. The actuators move the flight spoilers to assist the ailerons for _______ control. A pitch B roll C yaw D A+B+C 7. The elevator control columns move cables that give input to _______ . A the aileron feel and centering unit B the rudder feel and centering unit C the elevator feel and centering unit D A+B+C 8. The speedbrake lever move cables that control _______ . A the spoiler mixer B the rudder mixer C the elevator mixer D the aileron mixer 9. The stabilizer trim wheels move cables that give an input to _______ . A the gear box B the accessory gear box C the aileron D the rudder KEY : A C B A D B C A A ATA28 Fuel System 1. The fuel system supplies fuel to engines and _______ . A APU B AGB C FCC D CDS 2. The fuel tanks store _______ for use by engines and the APU. A oil B water C fuel D power 3. _______ add fuel to each tank. A The fuel storage B The pressure fueling system C The engine fuel feed D The APU fuel feed 4. The fueling station is on _______ . A the right wing B the left wing C the leading edge of the wing D the trailing edge of the wing 5. Each main tank has _____ boost pumps. A 1 B 5 C 3 D 2 6. The center tank boost pumps supply fuel at a higher _______ than the pumps in the main tanks. A speed B pressure C feed D temperature 7. _______ is in the left wing. A Center tank B Main tank 2 C Main tank 1 D A+B+C 8. _______ fuel temperature shows on the fuel control panel. A Main tank 1 B Main tank 2 C Center tank D A+B+C KEY: A C B A D B C A ATA29 Hydraulic Power 1. There are _______ independent hydraulic systems that supply hydraulic power for user systems. A 3 B 2 C 1 D 4 2. The main and auxiliary hydraulic systems supply pressurized _______ to airplane systems. A oil B fuel C fluid D water 3. System A has most of its components on _______ of the airplane. A the right side B the left side C all sides D forward part 4. The auxiliary hydraulic systems are the standby hydraulic system and _______ system. A PTU B APU C AGB D CDU 5. If system B is depressurized, _______ system is a hydraulic motor-pump assembly that supplies alternative pressure to leading edge flaps and slats and autosat system. A APU B AGB C CDU D PTU KEY: A C B A D ATA30 Ice and Rain Protection 1. The ice and rain protection system keeps _______ from airplane parts. A ice B water C fog D A+B+C 2. The wing thermal anti-ice and the engine inlet cowl thermal anti-ice systems use _______ prevent ice. A hot APU bleed air B wiper C hot engine bleed air D A+B+C 3. The air data probes use _______ to prevent ice. A hot APU bleed air B electric heat C hot engine bleed air D wiper 4. Flight deck window use _______ to prevent ice formation and fog on the windows. A electric heat B hot APU bleed air C hot engine bleed air D wiper 5. The water and waste lines and drains use _______ to prevent ice. A hot APU bleed air B hot engine bleed air C wiper D electric heat 6. The controls and indications for the ice and rain protection systems are in the flight compartment on the _______ forward overhead panel. A P4 B P5 C P6 D P3 7. There are _______ WTAI in engine solenoid valves on the top of the engine compressor case. A 1 B 3 C 2 D 4 KEY: A C B A D B C ATA31 Flight Data Recorder System 1. The flight data recorder system stores airplane parameters and system data for the last _____ hours of operation. A 25 B 24 C 22 D 15 2. The flight data recorder system gets and stores airplane parameters from _______ . A airplane systems B airplane sensors C airplane systems and sensors D airplane 3. The flight data recorder system protects the data from _______ . A heat B heat and water C water D crash 4. The flight data acquisition unit processes analog, digital, and discrete signals from _______ . A many sensors and systems B many sensors C many systems D many modules 5. The flight data recorder system sensors send data about the position of the flight surfaces and controls to _______ . A FDR B FDU C ACMS D FDAU 6. The FDR is a fire and crash resistant _______ . A LED B LRU C FDAU D QAR KEY: A C B A D B ATA32 Landing Gear 1. The landing gear structural components hold the _______ of the airplane while the airplane is on the ground. A weight B speed C altitude D attitude 2. _______ supplies the ground directional control of the airplane. A The main landing gear B The nose landing gear C The nose wheel steering system D The main wheel 3. _______ downlock pin installs in the NLG downlock pin hole. A The main landing gear B The nose landing gear C The main wheel D The nose wheel KEY: A C B ATA33 Lights 1. There are _______ light systems on the airplane. A 6 B 5 C 4 D 3 2. There are _______ types of flight compartment lights. A 2 B 4 C 6 D 8 3. _______ supply light for specific tasks A The instrument and panel lights B The flight crew lights C The miscellaneous lights D The master dim and test 4. There are ______ lights in the flight crew lights. A 4 B 5 C 6 D 7 5. _______ system controls the light for the system annunciator and indicator lights. A The instrument and panel lights B The miscellaneous lights C The flight crew lights D The master dim and test 6. There are _______ types of panel lights in the flight compartment. A 3 B 4 C 5 D 6 7. Light plates supply the background light for ______ in the flight compartment. A the switches B the push-buttons C the panels D the indrections 8. Electrical power for the instrument and panel lights comes from the ____ ac transfer buses 1 or 2. A 28V B 22V C 220V D 110V KEY: A C B A D B C A ATA34 Flight Management Computer System 1. The flight crew uses the flight management computer system to _______ for a flight. A enter route and vertical performance flight plan data B enter route performance flight plan data C enter vertical performance flight plan data D enter flight plan data 2. With ACARS, _______ can receive flight plan data from a ground station and can send flight status information to a ground station. A FCC B FDU C FMC D FDAU 3. A navigation data base is in _______ memory. A FCC B FMC C FDAU D CDU 4. The FMC calculates the airplane _______ during the flight. A position B speed C attitude D altitude 5. _______ shows target speeds and altitude. A CDU B FMC C FCC D CDS 6. The FMCs receive data from _______ to calculate navigation and performance data. A airplane systems B other airplane systems C other systems D other airplane and other systems 7. The FMC _______ format is ARINC 429 digital data and analog discretes. A input data B output data C input and output data D recording data KEY: A C B A D B C ATA35 Oxygen 1. _______ supply oxygen to the flight crew and cabin attendants and passengers. A The oxygen system B The digital flight control system C The fuel system D The flight data recorder system 2. _______ is independent of the other oxygen system. A The passenger oxygen system B The fuel system C The flight crew oxygen system D The flight data recorder system 3. The passenger oxygen system uses _______ oxygen generators. A physical B chemical C stored D pressurized 4. The flight crew oxygen system supplies the flight crew with _______ pressure gaseous oxygen. A low B high C middle D on 5. The flight crew oxygen system’s components are in _______ . A the flight compartment B the passenger compartment C the nose compartment D the EE compartment 6. A mechanical pressure gage on the oxygen cylinder shows the cylinder _______ . A speed B pressure C station D A+B+C KEY: A C B A D B