yango moodle

What is the number of ground spoilers on each wing Seleccione una: a. 2. b. 3. c. 1.

The minimum tank fuel temperature prior to takeoff and inflight is? Seleccione una: a. -47 C. b. -45 C. c. -43 C.

Where is the Hydraulic pressure and quantity displayed on the NG aircraft? Seleccione una: a. Lower DU, Displayed by use of the MFD “SYS” switch. b. Lower DU selection of Display sourse of the mfds. c. Upper DU, just above the fuel quantity displays.

In Flight the Recirculation Fan operates with the switch in the AUTO position execpt: Seleccione una: a. When both packs are on unless either pack switch are selected to HIGH. b. When one pack is off. c. Anytime the forward outflow valve is open. d. When both pack switches are selector to AUTO.

What is the recommended turbulent penetration airspeed for the B737NG? Seleccione una: a. 280 Kts/0.76M. b. 280 Kts/0.72M. c. 280 Kts/0.78M.

On Take Off the Crew Alerts are inhibited: Seleccione una: a. From 80 kts to 400 feet RA, or 30 seconds after reaching 80 Kts whichever occurs first. b. From 84 kts to 400 feet RA or 30 seconds after reaching 84 kts whichever occurs first. c. From 60 Kts to 400 feet RA or 30 seconds after reaching 60 kts whichever occurs first.

At what cabin altitude is the Altitude Warning Horn automatically horn automatically activated? Seleccione una: a. 9,500 feet. b. 10,000 feet. c. 14,000 feet. d. 13,875 feet.

When does croos bus tie relay automatically open. Seleccione una: a. When on ILS approach with dual channel autopilot engaged when APP is armed. b. When on ILS approach with FD or autopilot couple at glide slope capture. c. When on ILS approach with single channel autopilot engaged when VOR/LOC is armed. d. When on ILS approach with FD or autopilot coupled at localizer capture.

What will cause the APU to automatically shut down? Seleccione una: a. Senses a fire. b. Low Oil Pressure; Fault; Overspeed; Fire; Fuel control unit failure. c. Overspeed; Maintenance; Fire; Battery switch off in flight. d. Fire; Pulling the Fire handle; silencing the bell.

The ENG FAIL alert is shown on wich dial? Seleccione una: a. N1. b. EGT. c. N2.

Either generator or the APU can power both transfer buses. In the event a power source fails, what is required for that transfer bus to be powered by the opposite transfer bus power source. Seleccione una: a. The battery switch must be ON. b. The BUS TRANS switch must be in the AUTO position. c. The generator switch must be OFF.

The high altitude landing switch when on: Seleccione una: a. Reprograms cabin altitude warning annunciation to 15.000 feet b. Reprograms cabin pressurization from high altitude to normal operation c. Reprograms cabin altitude warning annunciation from 10.000 to 14.000 feet. a. Reprograms cabin altitude warning annunciation to 15.000 feet. b. Reprograms cabin pressurization from high altitude to normal operation. c. Reprograms cabin altitude warning annunciation from 10.000 to 14.000 feet.

The maximum aircraft altitude for electrical use of the APU is? Seleccione una: a. 35.000Ft. b. 37.000Ft. c. 41.000Ft.

The OFF SCHED DESCENT light illuminates if: Seleccione una: a. The aircraft descanded before reaching the planed cruise altitude set in the FLT ALT indicator. b. The aircraft has climbed above the selected flight altitudes (as set in the FLT ALT indicator). c. The aircraft has temporarily leveled off before reaching the planed cruise altitude set in the FLT ALT indicator. d. The aircraft has landed before reaching the selected flight altitude set in the FLT ALT indicator.

The EEC provides: Seleccione una: a. Thrust lever inputs to automatically control forward and reverse thrust. b. A variable thrust climb feature once the thrust lever is set at the beginning of the climb. c. A vaiable thrust take-off and climb ance the thrust lever is set at the beginning of takeoof roll. d. A constant EGT and Fuel flow feature once the thrust lever is set at the beginning of the climb.

What is the maximum differential pressure for the B737NG? Seleccione una: a. 9.1 PSI. b. 7.8 PSI. c. 8.35 PSI.

Serviceability of the tailskid cartridge is shown by Seleccione una: a. A Green and red decal b. Wear dimples c. A Green decal. a. A Green and red decal. b. Wear dimples. c. A Green decal.

The EGPWS provides alerts based on radio altitude and combinations of barometric altitude, airspeed, glide slope deviation, and airplane configuration for: Seleccione una: a. Excessive deviation below an ILS glide slope or altitude loss after take off or go-around. b. Unsafe terrain clearance when nt in the landing configuration. c. Any of the above. d. Excessive descent rate or excessive terrain clousure rate.

Why don’t the new generation aircraft have viewers to determine the position of the landing gear? Seleccione una: a. Because they have a complete set of independent Gear Position Indicators. b. Because downlocks are electrically operated through the hot battery bus. c. Because the gear operation is more reliable.

What component controls and monitors the B737NG APU? Seleccione una: a. ECU b. FCU c. FADEC. a. ECU. b. FCU. c. FADEC.

An A/T LIM indication when illuminated indicates: Seleccione una: a. The A/T is positioned at their normal operating limit as calculated by the FMC. b. The A/T LIM has been exeeded and manual inputs are now required for the affected engine(s). c. The A/T is using a degraded N1 thrust limit from the related EEC. d. The A/T computer is calcilating a N1 limit for the affected engine or engines.

On the ground or in flight with at least one engine running CONFIG is displayed if the center tank quantity is more than and the center tank pumps are producing no or low pressure. Seleccione una: a. 453 Kgs. b. 760 Kgs. c. 726 Kgs.

What is the APU starter duty cycle? Seleccione una: a. 2 consecutive aborted starts attempts, a 15 minute cooling period is required. b. 3 consecutive aborted starts attempts, a 15 minute cooling period is required. c. 3 consecutive aborted starts attempts, a 30 minute cooling period is required.

The ENG OVERHEAT light and: Seleccione una: a. MASTER CAUTION and OVHT/DET system annunciator illuminate. b. If both loops sense a fault with OVHT DET switch in the NORMAL position. MASTER CAUTION and OVHT/DET system annunciator lights illuminate. c. Illuminate if either fire loop senses a fire. d. MASTER CAUTION and OVT/DET system annunciator lights do not illuminate.

The Engine Fire Extinguisher system contains: Seleccione una: a. One bottles in each engine nacelle to either engine or APU. b. Four bottles in the main wheel well, two for each engine. c. Two bottles in the main wheel well to their respective engine and the APU. d. Two bottles in the main wheel well to both engines.

On the NG aircraft, the Outboard Landing Lights are now located Seleccione una: a. On the LEading edge of the Wing. b. They are on the same position as the 737CL. c. On the lower fuselaje, adjacent to the Ram Air Inlets.

Where are the Logo lights located on the New Generation aircraft? Seleccione una: a. The Logo lights have moved to the top of the horizontal stabilizer. b. The Logo lights have moved to the top of the fuselaje. c. The Logo lights have moved to the vertical Stabilizer.

The TOTAL Air Temperature provides independent temperature data to each ADIRU: Seleccione una: a. Data derived from the left ADIRU is used by the left IRS and the left FMC. b. Answer A. and B: are correct. c. Data derived from the right the right ADIRU is used by the left IRS and the right FMC. d. Data derived from the right ADIRU is used by the right the right IRS and the right FMC.

The Crossbleed Start Indication (X-BLD) is shown on which dial? Seleccione una: a. N2 b. N1 c. EGT. a. N2. b. N1. c. EGT.

The Alternate Flaps Position switch when selected to the UP position will: Seleccione una: a. Hydraulically retract the trailing edge flaps. b. Electrically retract the leading edge slats and flaps and trailing edge flaps. c. Electrically retract the trailing edge flaps. d. Hydraulically retract the leading edge flaps and slats and electrically retract the trailing edge flaps.

Which part of the engine is heated by engine anti-ice system? Seleccione una: a. Pt2 probes. b. The bullet. c. Fan blades. d. Engine cowl lip. a. Pt2 probes. b. The bullet. c. Fan blades. d. Engine cowl lip.

Illumination of the CONT CAB ZONE TEMP light: Seleccione una: a. The control cabin air mix valves drive to full cold. b. Nothing happens automatically with DUCT OVERHEAT, refer to QRH. c. Idicates duct temperatures overheat or failure of the flight deck primary and stanby temperature control. d. The cargo compartment air mix valves drive to full hot. a. The control cabin air mix valves drive to full cold. b. Nothing happens automatically with DUCT OVERHEAT, refer to QRH. c. Idicates duct temperatures overheat or failure of the flight deck primary and stanby temperature control. d. The cargo compartment air mix valves drive to full hot.

The AC standby Bus normally powerd by: Seleccione una: a. Transfer Bus 1. b. Transfer Bus 2. c. Main Bus 2. d. Main Bus 1.

The STAB OUT OF TRIM light operates: Seleccione una: a. Only when the autopilot is engaged. b. Only when the stabilizer trim failed. c. Only when the speed trim system is activated. d. Anytime it senses additional trim is needed.

The EEC becomes energized anytime the engine accelerates Seleccione una: a. N1 more than 18%. b. N1 more than 20%. c. N2 more than 15%.

In which position must the Disengage bar be placed to allow AP engagement? Seleccione una: a. CWS. b. UP. c. CMD.

What is the maximum differential pressure for take off & LDG on the B737NG? Seleccione una: a. 0.200 PSI b. 0.175 PSI c. 0.125 PSI. a. 0.200 PSI. b. 0.175 PSI. c. 0.125 PSI.

The dimensions of the B737 -700 are Seleccione una: a. Wingspan 35.79m, Length 33.60m. b. Wingspan 36.79m, Length 33,50m. c. Wingspan 37.80m, Length 32,60m.

The TAI Green (thermal Anti-Ice Indication) is shown in which dial?. a. EGT. b. N1. c. N2.

Where are the REVERSER Lights ? Seleccione una: a. Glareshield. b. Aft Overhead Panel. c. Overhead Panel.

What is the maximum takeoff and landing altitude for the B737NG? Seleccione una: a. 15000FT b. 13500FT c. 14000FT. a. 15000FT. b. 13500FT. c. 14000FT.

What will happen on the on the new generation aircraft if a tire is flailing while the gear retract? Seleccione una: The gear with a flailing tire will not retract. The tire will be fully braked before it enters the Wheel well. The maing landing gear weel has a sensor that detects flailing tires.

The conditions for speed trim operation are: Seleccione una: All answer is correct. Most frequently during takeoffs and go-around. Autopilot not engaged, Sensing of trim requiremnt. Airspeed 100 KIAS-Mach 0.5, 10 seconds after takeoff, 5 seconds after release of trim switches.

In MANUAL pressurization mode the outflow valve is driven by Seleccione una: A motor supplied from DC bus 1. A motor supplied from the DC standby bus. A motor supplied from DC bus 2.

The New Generation Aircraft is designed to be fueled through the wing tanks with gravity Seleccione una: TRUE. FALSE.

The TRIP RESET switch resets BLEED TRIP OFF, PACK TRIP OFF, DUCT OVERHEAT AND WING BODY OVERHEAT lights. Seleccione una: FALSO. VERDADERO.

The automatic flight system (AFS) consists of: Seleccione una: AFDS; A/T; MCP; FMC. AFDS; A/T. AFDS; A/T; MCP.

If aileron pressure ir released the A/P rolls the wings level when the bank angel is: Seleccione una: 5 degrees or lees. 10 degrees os lees. 6 degrees or less. 15 degrees or lees.

La maximum flight operational Altitude of the B737NG is Seleccione una: 41000 Ft. 37000 Ft. 42000 Ft.

The Air Data Inertial Reference Unit ADIRU, is limited to operate from Seleccione una: 82 North, 82 South. 80 North, 80 South. 82 North, 60 South.

The autopilot can not be engaged for take off below? Seleccione una: 400 Feet. 200 Feet. 600 Feet.

What is indicated by the IMBAL light on the #1 or #2 Fuel Quantity Indicator? Seleccione una: The is more than 907 Kgs difference between the main tank quantities. There is more than 453 Kgs difference between the main tank quantities. There is less than 453 Kgs difference between the main tank quantities.

Which APU annunciator light will not cause an automatic shutdown of the APU? Seleccione una: OVERSPEED. LOW OIL PRESSURE. FAULT. MAINT.

The maximum difference on the ground between the captain & FO altimeters at 8000Ft is? Seleccione una: 75 feet. 50 feet. 60 feet.

The Landing Gear Tranfer Unit provides for gear retraction when: Seleccione una: Airborne, No.1 engine RPM drops below a limit value, either mIN Lnding gear is not up. Airborne, No.2 engine RPM drops below a limit value, either main landing gear is not up. Airborne, No.2 engine fail, LANDING GEAR lever is positined UP. Airborne, No.1 engine RPM drops below a limit value Hydraulic System B fail.

Illumination of the PSEU light on the aft overhead panel will actívate the MASTER CAUTION system Seleccione una: TRUE. FALSE.

When are the GPWS windshear warnings available? Seleccione una: Below 1500 feet AGL. Below 800 feet AGL. Below 2500 feet AGL.

How do you connect the external Service Interphone to the Service Interphone System? Seleccione una: By selecting Service Interphone Switch to On position. Automatically by connecting any headset or hand Microphone into a jack. It is always connected.

When EEC is in Hard Alternate mode, what parameters are used to control engine thrust? Seleccione una: The EEC reverts to an alternate mode thrust schedule predetermined by the manufacturer. There is a standard performance table to recalculate EEC parameters according to flight condition. Parameters are drawn from ADC to be calculated by FMC.

While on the ground, what is indicated by the TR UNIT light being illuminated on the AC and DC Metering Panel? Seleccione una: Any TR unit has failed. The only souse of power is the Battery. No answer is correct.

What is the maximum takeoff altitude on NG aircraft? Seleccione una: 13.500’. 14.000’. 10.000’.

What causes the ENG FAIL alert to display on the engine EGT indicator? Seleccione una: Engine start lever in idle and operating below sustained idle (less than 50% N2). Engine start lever in idle and operating below sustained idle (less than 40% N2). Engine start lever in idle and operating below sustained idle (less than 60% N2).

When will the Dual Bleed light illuminate on the Air Systems Panel? Seleccione una: When the APU Bleed Air Valve is open and either engine N°1 Bleed Air Switch is ON or engine N°2 Bleed Air Switch is ON with the Isolation Valve is Open. When the APU Bleed Air Valve is closed and either engine N°1 Bleed Air Switch is ON or engine N°2 Bleed Air Switch is ON with the Isolation Valve is Open. When the APU Bleed Air Valve is closed and either engine N°1 Bleed Air Switch is ON or engine N°2 Bleed Air Switch is ON with the Isolation Valve is closed.

What is indicated by the illumination of the ENGINE CONTROL light on the Engine Panel? Seleccione una: A fault is detected in the system and the aircraft is not able to be dispatched. A fault is detected in the normal system and the system is in the alternate mode. No answer is correct.

What occurs when the Engine Bleed Air Switch is selected to the ON position? Seleccione una: Opens the Engine Bleed Air Valve when the respective engine is operating. Closes the Engine Bleed Air Valve when the respective engine is operating. Dual Bleed light illuminate if the APU Bleed Air Valve is closed.

Which igniter works on battery power? Seleccione una: Right ignitor. It is powered by the AC Standby Bus which is powered by the battery when the battery is the only power. Left ignitor. It is powered by the AC Standby Bus which is powered by the battery when the battery is the only power. No answer is correct.

If all AC power is lost, for how long does right IRS remain on? Seleccione una: 5 minutes. 10 minutes. 15 minutes.

What LE devices are not Skew protected ? Seleccione una: 1 and 8. 2 and 7. All are skew protected.

What is the maximum operating altitude for the APU while supplying both bleed air and electrical power to the aircraft? Seleccione una: 10000 ft. 41000 ft. 17000 ft.

How Much Rudder and Nose Wheel deflection is controlled by full rudder pedal input? Seleccione una: 7° on Nose Wheel and 29° on Rudder. 9° on Nose Wheel and 27° on Rudder. 5° on Nose Wheel and 30° on Rudder.

What is indicated by the COWL VALVE OPEN light being illuminated Dim on the Engine Anti-ice Panel? Seleccione una: Related Engine Cowl Anti-ice Valve is open (switch on). Related Engine Cowl Anti-ice Valve is in transit (switch on). All the answers are correct.

What hydraulic system normally powers the auto-slat operation? Seleccione una: Hydraulic System B. Hydraulic System A. Hydraulic System Standby.

What is indicated by the DC FAIL light being illuminated on the IRS Panel? Seleccione una: The DC power source for the related IRS is not normal. The AC power source for the related IRS is not normal. The stanby power source for the related IRS is not normal.

What occurs by moving and holding alternate flap position switch to the up position? Seleccione una: Only trailing edge flaps retract. Only leading edge flaps retract. Both LE Flaps and TE flaps are electrically retracted.

What is indicated by the LOW QUANTITY light on Flight control panel indicate? Seleccione una: Low Standby Hydraulic system quantity. (Approx 50 % Full). Low standby Hydraulic system quantity (Approximately 22% Full). Low Quantity in Hydraulic system in general (Averaging 70%).

What is the the highest altitude recommended for starting the APU on battery power only. Seleccione una: 25000 feet. 20000 feet. 41000 feet.

When EEC is operating in soft alternate mode, what parameters are used to control engine thrust? Seleccione una: Last valid flight conditions sensed which allow the mode change to occur without an immediate change. Values preset for ISA conditions according to flight altitude that allow for better engine protection. Degraded FMC N1 precalculated parameters.

When the Mach Trim System is automatically engaged? Seleccione una: At speeds above Mach 0.615. At speeds below Mach 0.615. At speeds above Mach 0.655.

How many hours does the FDR Records? Seleccione una: The last 25 hours. The last 30 hours. The last 120 minutes.

What is the normal cabin differential pressure when flying above 37.000 ft? Seleccione una: 8.35 psid. 7.80 psid. 7.45psid.

If the Audio Control Panel is operating in the degraded mode, how do you make PA´s and communicate on the interphone system? Seleccione una: Only the service interphone handset works because it bypasses the Audio Control Panel. Through the Audio Control Panel. All the answers are correct.

What is indicated by ON DC light on IRS Panel? Seleccione una: IRS on DC Power and performing alignment Self Test. Only dc buses available for IRSs. DC power is powering IRS and corresponding ADIRUs.

When is LOW QUANTITY LIGHT on Flight Control Panel Armed? Seleccione una: Light is always armed. Light is armed only when Standby hydraulic system is operating. Light is armed when hydraulic system B is below a fixed value.

When will the radio altitude display on the Primary Flight Display? Seleccione una: Below 2500 feet AGL. Below 2000 feet AGL. Below 1500 feet AGL.

How long can a start cycle take for the APU? Seleccione una: 120 Seconds. 180 seconds. 135 seconds.

What causes the DRIVE light on the Generator Drive and Standby Power Panel to illuminate? Seleccione una: When low oil pressure is sensed in the IDG. When the IDG is connected to the Transfer Bus. When over speed is sensed in the IDG.

Can one transfer bus be powered by the APU and the other by External Power? Seleccione una: No. Yes. No answer is correct.

What significant equipment operates in the Air System when the only source of power is the battery? Seleccione una: All the answers are correct. Manual pressurization control, Altitude warning horn and Pack lights. Air conditioning Pack Valves, Bleed Trip Off Lights.

During a normal APU shutdown cycle, what does the illumination of the FAULT light indicate? Seleccione una: The APU Fuel Shutoff Valve has not closed after 30 seconds. The APU Fuel Shutoff Valve is in transit. No answer is correct.

When does the source off light illuminates? Seleccione una: When transfer bus is not energized form selected power source. When transfer bus is energized by power source but generator not online. When generator is online but bus is not yet energized.

How many minutes does it take to align an IRS? Seleccione una: a. 5 to 17 minutes, depending on airplane latitude. b. 8 to 10 minutes depending or airplane location. c. 5 minutes because GPS signals quick align airplane position.

What is indicated by the three landing gear indicator lights on the aft overhead panel? Seleccione una: a. Actual landing gear position, replacing landing gear visors. b. Landing gear positions, as indicated by the landing gear position lights on the landing gear panel. c. Works as a backup in case landing gear indicator lights are inoperative.

On upper display panel, when will low alert in fuel quantity indicator be indicated? Seleccione una: a. Whenever respective wing tank has less than 906 KG (2000 lbs) of fuel. b. Whenever respective wing tank has less than 680KG (1500 lbs) of fuel. c. Whenever respective wing tank has less than 226 KG (500 lbs) of fuel.

When will config alert on Upper Display Unit appear? Seleccione una: a. When either engine is running and center tank pump switches are off. b. When either engine is running but not all main wing fuel tanks are on. c. When not enough fuel pressure is delivered to fuel inlet.

When is the IMBAL alert inhibited on the fuel quantity indicator? Seleccione una: a. When the airplane is on the ground or when the fuel LOW alert is displayed on the same main tank. b. When the airplane is on the air or when the fuel LOW alert is displayed on the same main tank. c. All the answers are correct.

Does the EEC provide overspeed protection for N1 or N2 in both the normal and alternate modes? Seleccione una: a. Yes, protection is always available. b. No, protection is only in normal mode. c. No, protection is only in alternate mode.

On IRS panel what is indicated by the align light (Steady) Seleccione una: a. IRS alignment modem, Initial ATT and Shutdown mode is processing. b. IRS alignment information invalid. c. IRS in Disagreement with GPS position.

When will the IDG Automatically disconnect? Seleccione una: a. When a high oil temperature is sensed in the IDG b. When an overcurrent or overtorque condition is sensed c. When oil pressure has dropped below limits. a. When a high oil temperature is sensed in the IDG. b. When an overcurrent or overtorque condition is sensed. c. When oil pressure has dropped below limits.

What does moving “ALTERNATE FLAPS” Switch to “ARM” accomplish?. a. Closes TE Flap Bypass valve. b. Activates stby pump. c. Arms alternate flap position switch. d. All of the above.

What causes a Zone Temp Light on FWD CAB or AFT CAB Selector? Seleccione una: a. Duct temperature overheat. b. Zone Temperature too cold. c. Zone Temperature too hot.

What is the maximum cabin differential pressure on NG Aircraft? Seleccione una: a. 9.1 psid. b. 8.65 psid. c. 7.8 psid.

Can you regain IRS heading information after IRS is lost inflight? Seleccione una: a. Yes, after selectin ATT following manual realignment procedures using compass heading information. b. No, until aircraft is in ground and realigned. c. No, there is no ATT selection and realignment procedures.

What is the max altitude APU can support both generators? Seleccione una: a. 41.000’. b. 37.000’. c. 17.000’.

When does the mach trim begin to operate Seleccione una: a. At .615 M. b. At .715 M. c. At .605 M.

The Ground Conditioned air is Plugged Directly into the Seleccione una: a. Mix manifold. b. Left pack. c. Right pack.