Quiz 2

[ATA31]The flight compartment printer receives data and sends status and error information back to which AIMS function/systems?. ACMS(Airplane Communication Monitoring Function). DCMF(Data Communication Management Function). CMCS(Central Maintenance Computing System).

[ATA24]GE 90. Where can you add oil to the IDG?. Through an access door in the thrust reverser 6:00 position. Through a panel on the right fan cowl at 6:00 position. The left fan duct cowl must be completely opened.

[ATA24]GE 90. How is the backup generator oil cooled?. Fan air only. Eng oil only. Fan air or 2.5 bleed air.

[ATA24]What does the white AVAIL in the external power switches on the P5 panel indicate?. Good power quality at the power source. The split system breaker is closed. External power is powering the aircraft.

[ATA24]If normal power is lost & the RAT generator is in operation, what buses are powered?. Cap & F/O’s Flt instruments buses through TRU C1 & C2. Left/Right XFR & Left/Right Utility buses. Cap & F/O’s Flt instruments buses through TRU L & R.

[ATA24]Which ELMS power panel is unique to the Boeing 777 freighter?. P330. P400. P300.

[ATA24]What does control the CCB’s & TTB’s?. IDG GCU’s. Backup Generator Converter. EEU’s.

[ATA31]The left AMIS cabinet sends AFDAF data to the FDR on: An ARINC 429 function. An ARINC 629 function. An ARINC 717 function.

[ATA31]Where to the Capt & F/O’s clocks get their UTC from?. ADIRS UTC Function. ELMS UTC Function. AIMS UTC Function.

[ATA31]If the PFD, a fail conditions occurs, what happened on display?. The system automatically switches to a backup source. The last know value remains in view and a flag is shown. The information is removed and flag comes into view.

[ATA31]Which AIMS LRM’s provide the calculation for the Primary display system?. CPM/GG. CPM/ACMF. CPM/Comm.

[ATA31]Which of the AIMS cabinet has the ACMF(Airplane Condition Monitoring Function). Only the left. Left and Right. Only the right.

[ATA31]When only one DU shows the EICAS display, EICAS is said to be in what mode?. Alternate mode. Limited mode. Secondary mode.

[ATA31]Advisory message are: Amber in colour and left justified with the first space blank. Red in colour and at the top of the display. Amber in colour and have an associated owl sound.

[ATA31]How many of the CPM/GG are supplying data to the flight deck DU’s in the operation?. 2. 4. 3.

[ATA31]Which unit makes the Master Caution Light On the signal?. WEU1 and WEU2. CPM/GG in AIMS. EICAS computers.

[ATA31]The normal source of the data sent to the FDR from the DFDAF?. Randomly of left or right AIMS cabinets. The left AIMS cabinet only. The right AIMS cabinet only.

[ATA24]PW 4000. Where can you add oil to the IDG?. Through an access door in the thrust reverser at 6:00 position. Through a panel on the right fan cowl at 6:00 position. The left fan duct cowl must be completely opened.

[ATA24]When does the backup generator converter perform an auto. After engine start. Once every 72 hours. Upon landing.

[ATA24]What are the three power source during a normal auto land?. L IDG, R IDG & APU GEN. L IDG, R IDG & RAT GEN. L IDG, R IDG & RATE BUG.

[ATA31]Which displays give a graphic representation of aircraft system?. Status page. Maintenance pages. Synoptic pages.

[ATA31]To which databuses do the area signal gateway cards connect?. System ARINC 629 databuses. ARINC 429 databuses. Flight system ARINC 629 databuses.

[ATA31]What do the ASG cards located in the system card files execute?. Perform ARINC 429-629 convesion. Perform the air supply function. Supply power to the card file.

[ATA31]Which of the following statements about the underwater locating device is correct?. The ULD has a alkaline battery with a 6 year life. The ULD has a replacable battery with a life of 10 years. The ULD has a lithium battery, which if unactivated, lasts for 6 years.

[ATA29]Which components control the fault lights related to the hydraulic system?. ELMS. AIMS. HYDIM Cards.

[ATA29]What controls the Air Drive Pumps (ADP) to increase pump output for autoslat operation?. Flap Slat Contro Unit (FSCU). Logic Speed Contro Unit (LSCU). HYDIM Card.

[ATA29]GE 90. Which of the following statements is true about the engine drive pimp (EDP)?. The depressurization solenoid is not part of de EDP. When the depressurization solenoid is energized, the pump pressure output goes to the hydraulic system. When the EDP is switched OFF, the depressurization solenoid gets electrical power.

[ATA29]How is an Air Driven Pump (ADP) overspeed condition reset?. By performing the appropriate maintenance access terminal (MAT) test. By switching the pump switch to OFF and back to ON position. By operating of reset switch on the Logic Speed Control Unit (LSCU).