Darkparadise

(ATA34) When either DME interrogator transmits, it sends out a suppression pulse to?. The ATC transponder and TCAS computer. The RA transceiver and ATC transceiver. The MMR and TCAS computer.

(ATA34) Airspeed and altitude Indicated on the standby Instrument are calculated by. SADM's. ADIRU. SAARU.

(ATA46) The EFB EU's have two CPU cores, hosting what software?. Android and Windows. Linux and Windows. Windows only.

(ATA34) Where is the Terrain Awareness display EGPWS shown. On both the PFD and ND. On the ND only. On the PFD only.

(ATA34) What is indicator on standby airspeed indicator when aircraft on ground and not moving. 0 Knots. 50 Knots. 30 Knots.

(ATA34) What is the purpose of the ATC program switching module. To set off the Unique 24-Fit Identification code the airplane. To allow for bite checking of the ACT system. To select alternate ACT • trasmstanding after a failure his occurred.

(ATA34) How does the standby Air data Modules transmit data. ARINC 626 bus. ARINC 517 bus. ARINC 429 bus.

(ATA34) What is the minimum speed to engage the Autopilot. 50 Knots. 80 Knots. 70 Knots.

(ATA44) Where is accessed to do ECS test?. Through the Crew Terminal Main Menu. Through the Crew Terminal Left Menu. Through the Crew Terminal Right Menu.

(ATA44) When is the cellular model (CM) Startes. After take-off. Upton aircraft weight on wheels. At aircraft power-up.

(ATA34) If both FMCF'S fail, how is the ALTN navigation data to the ND's supplied. The onside CDU supplies the data the ND. Only the center CDU supplies data to the left ND. The left CDU send data to both ND S.

(ATA22) The AFDC's have an inhibit that prevents the engagement of the autopilot during. the approach and landing. The takeoff roll and immediately after it. The cruise phase of the flight.

(ATA34) How do you clear a message from the CDU scratchpad. Push clear (CLR) key on the CDU. Push the Backspace LSK CDU on the CDU. Push the DEL and EXE Key.

(ATA46) Where can you find a list of all LSAP (Loadable Software Aircraft Part) Stored in the EFB maintenance. SYSTEM CONFIG. INTERNAL CONFIG. LOAD MODE.

(ATA34) How many antennas and transceivers has RA systems. 2 transceivers and 3 antennas. 4 antenna and 2 transceivers. 6 antennas and 3 transceivers.

(ATA22) With the FMC selector switch in the "L" position the active TMCF is. Left but won't change to the right TMCF if Left fails. Radomly selected to the Left or Right on power up. Left but will change to the right MCF in the Left fails.

(ATA34) Where are the ILS antennas?. Radome Only. Radome, Aft NG door and Upper fuselage. Radome, Vertical Stabilizer tip, AFT NLG.

(ATA34) How does the ground proximity terrain awareness function determine if a there is a terrain conflict?. Latitude and Longitude Only. Course Altitude and Speed. Airplane latitud, longitude, heading and barometric altitud.

(ATA46) What is the main hardware component of the onboard network system (ONS). Local Aerea Network (LAN). Network file server (NFS). Aircraft Information management system (AIMS).

(ATA22) the airplane is in cruise and has no faults. How many back drive actuators engage when the pilot engages the autopilot?. 6. 2. 3.

(ATA34) What source of radio Altimeter data has the highest priority to be used for the Captain's PFD if the left RA unit fails. Captain's Radio Altimeter Data will be lost. Center Radio Altimeter Transceiver. RA display goes out of view.

(ATA34) The pitot-static get static air pressure from. Static port on pitot probe. Static port on engine cowl. Flush static port on the fuselage.

(ATA22) If a fluorescent light in the mode control panel is degraded. The CMP microprocessor fails. An EICAS condition message is displayed. Maintenance memo is generated.

(ATA34) During an ADF test from the MAT, the poiter goes to. 135. 180. 0.

(ATA46) During initial power up it is observer that the EFB DU is flashing and showing the Self-test page intermittly for about a minute. What action would you take. Replace the Display as it has failed and perform a new P-Bit test. This is normal and maybe cancelled by pressing the MENU Bezel key. Reload the Operational Software into L EFB EU.

(ATA34) What happens if a single Channel fails on a MD&T card?. A maintenance message isgeneraed. All flight deck annunciators fail. Status message is generated.

(ATA34) What is the maximum the free of the TILT on the WXR antenna?. +/- 37 degree. +/- 25 degree. +/- 15 degree.

(ATA22) What happens when the autopilot switch is pressed if there are no faults. The AFDC are connected, then 2 will work. The CPM are connected, then 2 will work. The AFDC are connected, then 3 will work.

(ATA34) What happens if one gyro and two accelerometers fail in the ADIRU. Altitud will not be Displayed by the ADIRU. Status message is display. Heading output is lost from the ADIRU.

(ATA34) Where the ILS screen is displayed?. In the ND. In the PFD. Both EICAS screen.

(ATA22) The thrust limit mode and thrust limit are displayed on the. EICAS. ND. PDF.

(ATA34) The FMC calculated airplane position using three different sources of data -U+ what are the three different sources. Inertial position from the LADIQU, NAV radio position GPS position. GPS position last calculated position and initial reference position. Inertial position from sources the ADIRU'S SARRU position and last know position.

(ATA22) How many back drive actuators must be engaged for LAND3 announcement the Primary Flight Display?. 4. 6. 3.

(ATA22) At what radio altitud do the rudder pedal back drive actuators engage during approach. 1000 feet. 400 feet. 1500 feet.

(ATA34) The page shows the acting NAV DATA BASE. The IDENT Page. The RTE Page. The Post INIT Page.

(ATA22) What signals do the A/T arm switches on the MCP supply. Creab angel protection during Autoland. Autothrottle arm to the CPM Comm. Trim Enable Logic EEC.

(ATA34) What does the weather radar receiver-transmitter receiver pitch why B and roll data. To Stabilizer the antenna in flight. To quable auto ignition during flare. To calculate if the aircraft is Flaying towards a storm.

(ATA34) How do the ACT transponders get altitude data?. From the Air Data Inertial Reference Unite (ADIRU) through the AIMS cabinet. Directly from the CADS systems. Frome RA ALT through the FD system.

(ATA34) How long the SAARU can supply backup navigation function if ADIRU falled. 3 minutes. 30 minutes. 10 minutes.

(ATA34) Where is the CDU test done?. Maintenance page in MAT. CSCP control panel. Left CDU.

(ATA44) From where can maintenance staff access the eXTV system?. Maintenance Access Terminal (MAT). Passenger in-seat dispaly. Crew terminal.

(ATA34) What are mode of Weather radar (XWR)?. Altitud VOR mode, Centered MAP mode, Expanded MAP mode and Altitud Approach mode. Centered VOR mode, Altitud Approach mode. Expanded Approach mode, Expanded VOR mode, Centered MAP mode and Expanded MAP mode.

(ATA22) If a control wheel actuator fails during Autoland, the force limit of the remaining actuator is. Two times as high. Not affected. Half the force limit of a single actuator.

(ATA22) Engaging the A/P when back angle 5 degrees or lees whit the F/D off will activate. HDG hold only. TRK hold will turn to amber colour. HDG hold or TRK hold.

(ATA34) What air pressure(s) used by ADIRU and SAARU to calculate airspeed. Static air pressure. Both pitot and static air pressure. Pitot air pressure.

(ATA34) What will be shown on PDF if RA NCD occurs. RA display goes out of view. Yellow RA flag. Yellow NCD flag.

(ATA34) How is due auto tunning archived?. NAV receiver interfacing. AIMS interfacing. ELMS interfacing.

(ATA34) Which two Standby Instrument are interchangeable. Standby Altitud Indicator and Standby Altimeter. Standby Altitud Indicator and Standby Airspeed Indicator. Standby Altimeter and Standby airspeed Indicator.

(ATA22) What is the bac angle limit below 200ft. 30 degrees. 8 degrees. 15 degrees.

(ATA34) Which GPWS mode alerts the pilot thar the airplane is in windshear. Mode 3. All modes. Mode 7.

(ATA34) The Weather Radar Receiver transmitter gets pitch and roll data from which of the following?. The ADIRU. The AIMS cabinets. The WRX Suppression Computers.

(ATA34) How in the VOR autotuning mode?. Through ELMS. Through AIMS. Through DME.

(ATA22) Where is the autopilot controller?. MCP PANEL. MMR PANEL. AIMS PANEL.

(ATA34) If both FMCF's fall, how is the ALTN navigation data to the ND's supplied. The left CDU send data to both ND 's. The onside CDU supplies data the ND'S. Only the center CDU supplies data to the left ND.

(ATA34) If the ADIRUS fails where is the information received from. Automatically select the FPA backup mode. Automatically select the SAARU backup mode. Automaticall select the APP back up mode.

(ATA34) On the 777 aircraft the FMCF in the right AIMS cabinet is in the. CPM (ACMF). CPM (COMM). CPM (BASIC).

(ATA22) How many microprocessors does the MCP have?. 2. 3. 1.

(ATA34) The ATC antennas are interchangeable whit which other antennas was?. The ADF antennas. The VOR antennas. The DME antennas.

(ATA34) What color are the ADF parters on the ND. Yellow. White. Cyan.

(ATA22) Each AFDC computer consist of. 3 microprocessor and all the three command the back drive actuator. 3 microprocessor and only 2 them are used for back drive commands. 2 microprocessor a, one for each set of back drive actuatos.

(ATA34) Which GPS data is displayed on the ND?. Latitud Indication and GPWS system message. Terrain Awareness display, GPWS system message and GPWS alert message. GPWS Warnig messages, Altitude indication and Airspeed indication.

(ATA34) Where does AIMS receive its time from. ELMS. Captain Clock. MMR'S.

(ATA 22) The ILS antenna swtching discrete is generated by the: CPM BASIC in AIMS cabinet. Autopilot Flight Director Computer. Control Display Unit.

(ATA 22) Which of these statements is true: AUTOTHROTTLE DISC memo message show when the TMCS detects a manual disengagen. AUTOTHROTTLE DISC caution occurs when the TMCS detects an automatic disengagen. AUTOTHROTTLE DISC warning occurs when the TMCS detects an automatic disengagen.

(ATA 34) What makes the bottom TCAS antenna Omni directional?. The system is always Omni directional. Nothing, the system Can only utilize the upper fuselage antennas. The PSEU supplies a gear not up signal.

(ATA 34) What happens when the Air Data Inertial Reference Unit (ADIRU) is initially turned on from the flight deck switch?. A self test is carried out for 30 sec only. The heading flag is removed before the self test is initiated. Altitude data is available after 30 secs.

ATA 34) How does the Automatic Direction finder receiver get tuning data?. Using the VOR/ADF switches on the EFIS control panel. Manually from the Control Display Unit. Automatically from the FMCF of AIMS.

(ATA 34) How do you display ILS data on the ND?. Turn the mode selector to VOR. Turn the mode selector to APP. Select the RAD. NAV page on the CDU.

ATA 34) What test would you do to check for defects in a CDU display?. The CDU configuration test. The CDU reset and bite test. The CDU special functions test.

ATA 34) Which changes occurs on the standby attitude indicator, when "B/ CRS" (back course) is selected?. The localizer deviation bar goes out of view and the glideslope deviation bar reverses polarity. The localizer deviation bar reverses polarity and the glideslope deviation bar goes out of view. The localizer and glideslope deviation bars deviation bars go out view.

ATA 34) If the alternate V/MMO switch is in the "ALTN" position them the: The Air Data & Inertial Reference Units (ADIRU) adjust the Vmo/Mmo curve to compensate for a flight with the landing gear down. The Air Data & Inertial Reference Units (ADIRU) use the alternate static ports as input in order calculate the Vmo/Mmo curve, for normal flight. The Air Data & Inertial Reference Units (ADIRU) use the alternate pitot probe and static ports input in order to calculate the Vmo/Mmo curve for a flight with flaps/slats down.

(ATA 34) Are the TCAS antennas top and bottom interchangeable?. Both antennas are interchangeable. B777 only has top antenna installed. Never. Because bottom antenna is Omni directional.

(ATA 34) PWS ( Predictive wind sheer) uses landing gear control lever discrete info for?. Takeoff/Approach alert logic. For AIR/GND purposes. Approach alert logic only.

(ATA 34) After SADM replacement, what kind of software does it need to be loaded with?. OPS software. FMC NAV data base. It is not software loadable.