Repaso Semana 2 Boeing 777

Which of the following is the left forward panel in the Boeing 777 flight deck?. P2. P3. P1.

The main instrument panels (P1 & P3) contain how many display units?. 2. 4. 6.

Which panel contains the Mode Control Panel (MCP), Electronic Flight Instrument System (EFIS) Control Panels, and Master Warning & Caution lights?. P5 Overhead Panel. P10 Control Stand. Glareshield Panels.

Note regarding the lower centre display unit on P2: It is identical to the other five display units. It only displays Engine Indication and Crew Alerting System (EICAS) data. It is reversed (top to bottom) from the other five display units.

The P10 Control Stand includes which of the following?. Radio Tuning Panels and Audio Control Panels. Air Data Inertial Reference System (ADIRS) controls. Speedbrake lever, Thrust levers, Flap lever, and Cursor Control Devices (CCD).

The P61 Overhead Maintenance Panel is primarily used by: Maintenance personnel. Cabin crew. Flight crew during normal operations.

The P18 panel is known as the: Forward Aisle Stand Panel. Overhead Circuit Breaker Panel. Maintenance Access Terminal (MAT) / Second Observer Panel.

Which of the following controls are located on the P13 and P14 Side Wall Panels?. Air Data Inertial Reference System (ADIRS) and Primary Flight Computers. Engine fire panel and transponder panel Page 2 | ATA 31 Boeing 777 Indicating/Recording Systems Quiz | FOR TRAINING PURPOSES ONLY. Shoulder heaters, outboard display brightness, and panel flood light brightness.

What is the primary purpose of the Systems Card Files?. To hold ARINC 429 bus interface cards for essential systems and ARINC 629 Signal Gateway (ASG) cards. To store flight data in solid-state memory. To display primary flight information.

What does ASG stand for?. Airplane Systems Gatewa. ARINC 629 Signal Gateway. ARINC Signal Generator.

How many systems card files are there on the airplane?. One. Four. Two.

Each systems card file contains how many power supply cards?. 2. 4. 3.

The Left Systems Card File (LSCF) contains how many ARINC 429 system cards?. 6. 8. 9.

The Right Systems Card File (RSCF) contains how many ARINC 429 system cards?. 9. 10. 8.

The ARINC 629 Signal Gateway (ASG) cards change data formats between which two standards?. ARINC 429 and ARINC 629. ARINC 629 and ARINC 717. ARINC 429 and ARINC 717.

Which cargo smoke detector connects directly to the ARINC 629 Signal Gateway (ASG) cards in the Left Systems Card File (LSCF)?. Aft cargo smoke detector. Both forward and aft. Forward cargo smoke detector.

The ARINC 629 Signal Gateway (ASG) cards are: Specific to left or right only. Not interchangeable. Interchangeable.

What is the primary purpose of the clocks?. To record flight data. To control display brightness. To give time reference to the flight crew.

The clocks can display which of the following data?. Only manual time and date. Only Universal Time Coordinated (UTC) from the Global Positioning System (GPS),elapsed time. Time and date set manually, Universal Time Coordinated (UTC) and date from the Airplane Information Management System (AIMS), elapsed time, and chronograph time.

Where are the clock switches located that control the chronograph function?. On the glareshield panel. On the P10 Control Stand. On the P5 Overhead Panel.

The Airplane Information Management System (AIMS) cabinets get Universal Time Coordinated (UTC) and date from: Manual crew input only. The multimode receivers (MMRs). The clocks themselves.

Do the Airplane Information Management System (AIMS) cabinets use the manually set clock time and date for any function?. Yes, for the Flight Data Recorder (FDR) only. Yes, for all timing functions. No, the AIMS cabinets do not use the clock time.

What is the purpose of the Flight Data Recorder System (FDRS)?. To display engine parameters to the crew. To generate aural warnings. To store airplane parameters and system data.

. How many hours of the most recent flight does the Flight Data Recorder (FDR) record?. 24 hours. 25 hours. 20 hours.

The Digital Flight Data Acquisition Function (DFDAF) is located in: The Flight Data Recorder (FDR) itself. The Quick Access Recorder (QAR). The Core Processor Module / Communications.

When does the Flight Data Recorder System (FDRS) operate?. Only during flight. Continuously whenever electrical power is available. During any engine start, while any engine is running.

The Flight Data Recorder (FDR) receives airplane parameters from the Digital Flight Data Acquisition Function (DFDAF) on which data buses?. ARINC 717. ARINC 629. ARINC 429.

Physical description of the Flight Data Recorder (FDR): It is made of stainless steel, weighs approximately ____ pounds, and is international orange in color. 14. 18. 16.

The Flight Data Recorder (FDR) case supplies protection for fire up to a temperature of: 500 °C for 1 hour. 800 °C for 2 hours. 1100 °C for 1/2 hour.

What is the purpose of the Underwater Locating Device (ULD)?. To power the Flight Data Recorder (FDR) underwater. To record underwater acoustic data. To make the Flight Data Recorder (FDR).

. The Underwater Locating Device (ULD) has an operational life of how many days underwater?. 30 days. 25 days. 7 days.

The Underwater Locating Device (ULD) sends out an acoustic pulse tone of: 25 kHz at 2 pulses per second. 37.5 kHz at one pulse per second. 50 kHz continuously.

The purpose of the Airplane Condition Monitoring System (ACMS) reports is to: Control the flight path. Analyze airplane performance, analyze trends. Display navigation data.

The Airplane Condition Monitoring Function (ACMF) is located in: Both Airplane Information Management System (AIMS) cabinets. The left Airplane Information Management System (AIMS) cabinet only. The right Airplane Information Management System (AIMS) cabinet only.

What does QAR stand for?. Quick Access Recorder. Quality Assurance Report. Quantitative Analysis Recorder.

. The Quick Access Recorder (QAR) records data from the Airplane Condition Monitoring Function (ACMF) onto: A solid-state memory card. Magnetic tape. An optical disk.

What are triggers in the context of the Airplane Condition Monitoring System (ACMS)?. Manual report buttons only. Physical switches on the overhead panel. Logic equations that detect conditions.

Airlines use which tool to program the Airplane Condition Monitoring System (ACMS) with custom features?. Maintenance Access Terminal (MAT) only. Control Display Unit (CDU). Ground Based Software Tool (GBST).

. What is the purpose of the Airplane Information Management System (AIMS)?. To only record flight data. To provide only aural warnings. To collect and calculate large quantities of data.

Which of the following systems are managed/supported by the Airplane Information Management System (AIMS)?. Only the Primary Display System (PDS). Only Flight Data Recorder System (FDRS) and Airplane Condition Monitoring System (ACMS). Primary Display System (PDS), Central Maintenance Computing System (CMCS), Airplane Condition Monitoring System (ACMS), Flight Data Recorder System (FDRS).

How many Airplane Information Management System (AIMS) cabinets does the airplane have?. One. Two. Three.

Each Airplane Information Management System (AIMS) cabinet contains: Two Input/Output Modules (IOMs) and two Core Processor Modules (CPMs). Six Display Units (DUs). Four Input/Output Modules (IOMs).

. What is the function of the Input/Output Module (IOM)?. To generate graphics for the displays. To record flight data. To transfer data between the software functions.

Which type of Core Processor Module (CPM) is found only in the left Airplane Information Management System (AIMS) cabinet?. Core Processor Module / Communications (CPM/Comm). Core Processor Module / Basic (CPM/Basic). Core Processor Module / (CPM/ACMF).

Which type of Core Processor Module (CPM) is found only in the right Airplane Information Management System (AIMS) cabinet?. Core Processor Module / Airplane Condition Monitoring Function (CPM/ACMF). Core Processor Module / Basic (CPM/Basic). Core Processor Module / Communications (CPM/Comm).

The software functions in the Core Processor Module / Graphics Generator (CPM/GG) include: Digital Flight Data Acquisition Function (DFDAF) and Quick Access Recorder Function (QARF). Airplane Condition Monitoring Function (ACMF) and Flight Management Computing Function (FMCF). Data Conversion Gateway Function (DCGF) and Primary Display Function (PDF).

The Airplane Information Management System (AIMS) also supplies the Data Conversion Gateway Function (DCGF), which: Is used only by the Flight Data Recorder (FDR). Is a software function that many airplane systems use. Controls the stick shakers.

What is the purpose of the Warning Electronics System (WES)?. To record flight parameters. To manage ARINC data buses. To supply indications.

How many Warning Electronic Units (WEUs) does the Warning Electronics System (WES) have?. One. Two. Three.

Each Warning Electronic Unit (WEU) has how many internal channels that do the same functions?. One. Three. Two.

Which of the following are functions performed by the Warning Electronics System (WES)?. Only stall warning and altitude alert. Only master warning light control. Master warning light control, alert aural control/amplification.

Outputs from the Warning Electronics System (WES) go to: Only the Airplane Information Management System (AIMS) cabinets. Only the master warning lights. Master warning lights, aural warning speakers, stick shaker actuators.

The Warning Electronics System (WES) amplifies alert aurals from which systems?. Only the Traffic Alert and Collision Avoidance System (TCAS). Only the Ground Proximity Warning System (GPWS. Traffic Alert and Collision Avoidance System (TCAS) computer, Ground Proximity Warning Computer (GPWC).

The Primary Display System (PDS) is part of: The Flight Data Recorder System (FDRS). The Airplane Information Management System (AIMS). The Warning Electronics System (WES).

How many identical display units (DUs) does the Primary Display System (PDS) use?. four. five. six.

The display units (DUs) are: ARINC D flat panel liquid crystal display (LCD) units. Electromechanical instruments. Cathode Ray Tube (CRT) displays.

Major components of the Airplane Information Management System (AIMS) Primary Display System (PDS) include: Only the six display units (DUs). Only the Electronic Flight Instrument System (EFIS) control panels. Six Display Units (DUs), two Electronic Flight Instrument System Control Panels (EFIS CPs).

What determines which types of display format show on a given display unit (DU)?. Only crew selection via the Display Select Panel (DSP). Only the instrument source select panels. Location of the display unit.

The Airplane Information Management System (AIMS) cabinets send information to the display units (DUs) on: ARINC 429 buses only. ARINC 629 buses only. High speed coax lines through four coax couplers.

Two Remote Light Sensors (RLSs) are located: On the overhead panel. Inside each display unit (DU). On the forward part of the glareshield.

The Primary Flight Display (PFD) gives the crew information on: Only navigation data. Only engine parameters. Attitude, critical parameters.

Three Control Display Units (CDUs) give alternate functions for: Only the Flight Management System. Only maintenance pages. Alternate Electronic Flight Instrument System Control Panel (EFIS CP).

The systems ARINC 629 buses supply most of the data to the Warning Electronics System (WES). The rest of the data comes from: Only ARINC 429 buses. Only analog signals. Discrete inputs.

Partitions in the Airplane Information Management System (AIMS) Core Processor Modules (CPMs) permit: Unlimited functions without separation. Only one function per Core Processor Module (CPM). Multiple functions.