ATA 05-20, 34/44/46

What does ATA 05-00 cover?. Navigation systems only. Time Limits / Maintenance Checks, including conditional inspections due to special or unusual conditions. Cabin systemsD) Electronic Flight Bag (EFB).

What are Critical Design Configuration Control Limitations (CDCCL)?. Optional maintenance recommendations. Design features intended to preclude a fuel tank ignition source for the operational life of the airplane; they are mandatory and controlled by Special Federal Aviation Regulation (SFAR) 88. Only related to landing gear.

What are Airworthiness Limitation Instructions (ALIs)?. Optional inspection tasks. Mandatory inspection tasks related to fuel tank ignition source prevention that must be done to maintain the design level of safety. Cabin crew procedures.

is the purpose of a Transit Check?. Full heavy maintenance. Only Transit Checks. To assure continuous serviceability of a transiting aircraft; it is basically a “walk-around” inspection of interior and exterior for obviousdamage, leaks, proper operating equipment and required servicing.

Operators accumulating less than 100 flight hours/month/airplane should consider which type of maintenance program?. High Utilization Maintenance Program. Low Utilization Maintenance Program based on calendar time. No maintenance program.

Task intervals in the maintenance document are expressed in which units?. Only flight hours. Flight hours, cycles, or calendar time. Only calendar time.

What does ATA 06-10 cover?. Navigation. Principal Dimensions and Areas. Cabin systems.

What does ATA 06-20 cover?. Zone diagrams. Station diagrams (fuselage, wing, stabilizer, engine and nacelle) for maintenance practices. Access panels only.

What does ATA 06-30 cover?. Principal dimensions. Zones diagrams (Major es). Towing procedures.

What does ATA 07-11 cover?. Towing. Jacking the airplane (nose jacking and axle jacking). Parking.

What does ATA 08-12 cover?. Leveling. Periodic airplane weighing. Towing.

What does ATA 09-11 cover?. Towing the airplane. Taxiing. Parking.

13. hat does ATA 10-11 cover?. Towing. Leveling. Parking the airplane (normal parking and prolonged parking).

What does the Pitot-Static / Air Data Standby Instruments system provide?. Static and total air pressure information for air data systems and standby instruments. Only attitude data. Only radio altitude.

What is the Air Data Inertial Reference System (ADIRS)?. A) Only a weather radar system. B) Only a backup compass. C) The primary system that provides air data and inertial reference data to the airplane systems.

What is the primary unit that provides attitude and air data in normal operation?. A) Secondary Attitude Air Data Reference Unit (SAARU). B) Air Data Inertial Reference Unit (ADIRU). C) Standby Attitude Indicator only.

What is the Secondary Attitude Air Data Reference Unit (SAARU)?. A) The primary inertial reference unit. B) The secondary (backup). C) Only a temperature probe.

When the Captain Air Data/Attitude switch is in the ALTN (Alternate) position, what is the source for the Captain displays?. Full Air Data Inertial Reference Unit (ADIRU). Secondary Attitude Air Data Reference Unit (SAARU) for attitude and Secondary Attitude Air Data Reference Unit (SAARU). Flight Management Computing Function (FMCF).

In the ALTN (Alternate) position, which source remains for heading and track data?. Air Data Inertial Reference Unit (ADIRU). PSecondary Attitude Air Data Reference Unit pp. Cps) Global Positioning System (GPS).

What does the Localizer Antenna Switching do?. Switches between Weather Radar antennas. Changes the inputs between the Very High Frequency Omnidirectional Range (VOR) antenna and the localizer antennas. Controls Automatic Direction Finder (ADF) antennas.

Who controls the position of the localizer and glideslope antenna switches?. The Control Display Units (CDUs). The Flight Management Computing Function (FMCF). The Autopilot Flight Director Computers (AFDCs).

What are the three ways to tune the Multi-Mode Receivers (MMRs)?. Automatically by Airplane Information Management System (AIMS) cabinets, Manually by left/right/center Control Display Unit (CDU). Only by Global Positioning System (GPS). Only by Autopilot Flight Director Computer (AFDC).

Which Flight Management Computing Function (FMCF) normally auto-tunes the Instrument Landing System (ILS) receivers?. The left Airplane Information Management System (AIMS) Flight Management Computing Function (FMCF). The Secondary Attitude Air Data Reference Unit (SAARU). The Flight Management Computing Function (FMCF) of the right Airplane Information Management System (AIMS) cabinet.

In Alternate Tuning mode, who tunes the left and center Multi-Mode Receivers (MMRs)?. The right Control Display Unit (CDU). The left Control Display Unit (CDU). The center Control Display Unit (CDU).

. Is there an alternate tune function from the center Control Display Unit (CDU)?. Yes, for all receivers. No, there is no alternate tune function from the center Control Display Unit (CDU). Only for Distance Measuring Equipment (DME).

. What are the four Very High Frequency Omnidirectional Range (VOR) tune modes indicated on the Navigation Radio (NAV RADIO)page?. Auto-tune (A), Procedure (P) tune, Route (R) tune, and Manual (M). Only P and R. Only A and M.

What does the letter “M” after a Very High Frequency Omnidirectional Range (VOR) frequency indicate?. Maintenance mode. Manual tune: the crew has manually. Marker beacon.

. What is the valid frequency range for Very High Frequency Omnidirectional Range (VOR)?. 108.10 to 111.95 Mhz. 190 to 1750 kHz. 962 to 1215 MHz.

How is a Distance Measuring Equipment (DME) normally tuned?. By entering an L-band frequency directly. Only by Global Positioning System (GPS). By entering a Very High Frequency Omnidirectional Range (VOR).

Can the DELETE key be used to delete an existing Automatic Direction Finder (ADF) frequency?. Yes, always. No, the DELETE. Only from the center Control Display Unit (CDU).

How is the ANT (Antenna) mode selected on the Automatic Direction Finder (ADF)?. By entering the letter “A” after the frequency. By pressing a dedicated button. Automatically.

. What does the ANT (Antenna) mode of the Automatic Direction Finder (ADF) do?. Changes to Very High Frequency Omnidirectional Range (VOR). Uses only the sense antenna to receive station audio broadcasts. Uses both antennas.

How is the BFO (Beat Frequency Oscillator) mode selected?. By entering the letter “B” after the frequency. Automatically when Morse is presente. With a physical switch.

When does the Alternate Navigation Radio (ALTN NAV RADIO) page become available?. Only when the tune inputs from the Airplane Information Management System (AIMS) cabinets. When ALTN is selected on the Air Data switch. On the ground only.

Normally, where do the radio tune commands come from?. Always from the left Flight Management Computing Function (FMCF). From the right Flight Management Computing Function (FMCF). From the Air Data Inertial Reference Unit (ADIRU).

What are the selection criteria used by the Flight Management Computing Function (FMCF) to choose the best Distance MeasuringEquipment (DME)/Distance Measuring Equipment (DME) pair?. Distance only. Range (not farther than line-of-sight and not closer than 9 nautical miles (nm). Identifier only.

What does the Navigation (NAV) source switch on the Instrument Source Select Panel (ISSP) select?. The air data source. The attitude source only. The source of Navigation.

What are the three positions of the Flight Management Computer (FMC) Selector?. ON / OFF / AUTO. Normal / ALTN / OFF. Left (L), AUTO, and Right (R).

In the AUTO position of the Flight Management Computer (FMC) Selector, what happens when the active Flight Management Computing Function (FMCF) fails?. The other Flight Management Computing Function (FMCF) becomes active. There is no active Flight Management Computing Function (FMCF). The Control Display Unit (CDU) takes full control of Lateral Navigation (LNAV) and Vertical Navigation (VNAV).

When both Flight Management Computing Functions (FMCFs) fail, who supplies map data to the onside Navigation Display (ND)?. The Air Data Inertial Reference Unit (ADIRU). The onside Control Display Unit (CDU). The Secondary Attitude Air Data Reference Unit (SAARU).

When is the Cell Modem (CM) started?. Upon aircraft Weight On Wheels (WOW). Always in flight. Only when selected by the pilot.

What flight information does the Global Communications Suite (GCS) acquire through ARINC 429 connections?. Both ends. Only altitude. Latitude, Longitude, Heading, and Time.

What is the Electronic Flight Bag (EFB)?. An electronic system that provides flight crews with digital charts, manuals, performance calculations, and other operational information onDisplay Units (DUs) in the flight deck. Processes and manages the Electronic Flight Bag (EFB) applications, interfaces with airplane systems, and communicates with the DisplayUnit (DU).

What do the Captain and First Officer Air Data/Attitude switches on the Instrument Source Select Panels (ISSP) control?. The tuning of the Very High Frequency Omnidirectional Range (VOR) receivers. The source of attitude and air data displayed on the onside Primary Flight Display (PFD) and Navigation Display (ND).

When the Air Data/Attitude switch is in the NORMAL position, what is the source of attitude and air data for the Primary FlightDisplays (PFDs) and Navigation Displays (NDs)?. Secondary Attitude Air Data Reference Unit (SAARU). Air Data Inertial Reference Unit (ADIRU). Flight Management Computing Function (FMCF).

When the Captain Air Data/Attitude switch is in the ALTN (Alternate) position, what is the source for the Captain displays?. Secondary Attitude Air Data Reference Unit (SAARU) for attitude and Secondary Attitude Air Data Reference Unit (SAARU)single channel (right) for air data. Only Air Data Inertial Reference Unit (ADIRU) left channel.

What is the highest priority source for Captain attitude and air data displays under non-normal conditions?. Air Data Inertial Reference Unit (ADIRU) right flight controls ARINC 629 bus (air data and attitude). Air Data Inertial Reference Unit (ADIRU) left flight controls ARINC 629 bus.

What does the Localizer Antenna Switch do?. Selects the Air Data Inertial Reference Unit (ADIRU) source. Switches between left and right Weather Radar (WXR) Receiver-Transmitters (RTs). Changes the inputs between the Very High Frequency Omnidirectional Range (VOR) antenna and the localizer antennas.

Between which antennas does the Glideslope (G/S) Antenna Switch change the receiver inputs?. Between Very High Frequency Omnidirectional Range (VOR) and localizer. Between the Glideslope (G/S) antenna in the nose radome and the Glideslope (G/S) track antenna on the aft nose gear doors.

. In Alternate Tuning mode (when Airplane Information Management System (AIMS) Flight Management Computing Function(FMCF) tuning functions fail), who tunes the left and center receivers?. The left Control Display Unit (CDU). The right Control Display Unit (CDU).

[ATA 06] Where is the airplane DATUM located?. 92.5 inches forward of the nose (perpendicular to the fuselage centerline). *.

[ATA 34] Which of the AIMS has the ACMS function?. Left AIMS Cabinets. *.

[ATA 34] Through which AIMS is communication to the FDR?. Left AIMS Cabinet. *.

[ATA 34] With which ARINC do the AIMS cabinets communicate?. ARINC 629. *.

[ATA 34] Which unit is responsible for the Master Caution?. Left AIMS Cabinet via CPM/GG. *.

[ATA 34] The DUs have two internal temperature sensors. The power supply shuts down the DU when it reaches: 110 degrees Celsius. *.

[ATA 34] When only one DU shows the EICAS display (Limited Mode), which 3 DSP switches are functional?. ENG, AIR and FUEL switches. *.

[ATA 34] What do the Graphics Generators (GG) do?. They receive reformatted PFD and ND data, convert it to video format and send it to the DUs. *.

[ATA 34] The Flight Compartment Printer receives data from the print driver partition of: The DCMF (Data Communication Management Function). *.

[ATA 34] What test is performed to verify defects on a CDU display?. The CDU special functions test. *.

[ATA 34] If 1 gyro and 2 accelerometers fail in the ADIRU, what happens?. Attitude is still displayed (5 gyros and 4 accelerometers remain; minimum = 4 of each). *.

[ATA 34] How do the Standby Air Data Modules (SADM) transmit data?. ARINC 429 bus. *.

[ATA 34] What air pressures do ADIRU and SAARU use to calculate airspeed?. Both pitot and static air pressures. *.

[ATA 34] Airspeed and attitude on standby instruments are calculated/supplied by: Airspeed → SADM (Standby Air Data Modules). Attitude → SAARU. *.

[ATA 34] If the left RA fails, highest priority for the Captain's PFD: Center Radio Altimeter transceiver. *.

[ATA 34] How long can the SAARU supply backup navigation if the ADIRU fails?. 3 minutes. *.

[ATA 34] During an ADF test from the MAT, the pointer goes to: Approximately 135° (test position). *.

[ATA 34] What shows on the PFD if RA NCD (non computer data) occurs?. RA display goes out of view. *.

[ATA 34] How is ILS data shown on the ND?. Mode selector to APP (Approach). *.

[ATA 34] When powering up the ADIRU from the flight deck switch, what happens?. NCD during alignment (6–15 min to complete). *.

[ATA 34] Which two Standby Instruments are interchangeable?. Standby Airspeed Indicator (SASI) and Standby Altimeter (SALT) — by program pins. *.

[ATA 46] The EFB EUs have two CPU cores that host which software?. Linux and Windows. *.

[ATA 34] What does the Standby Airspeed Indicator show on the ground and not moving?. 30 knots. *.

[ATA 34] Where is the Terrain Awareness display of the EGPWS shown?. Only on the ND (Navigation Display). *.

[ATA 34] How many Radio Altimeters are on the airplane?. 3 (Left, Center and Right). *.

[ATA 06] How many jack points does the airplane have?. 3 primary and 5 auxiliary. *.

[ATA 09] What is the minimum distance to maintain when towing the aircraft?. 10 feet. *.

[ATA 20] Where are the Approved Standard Maintenance Practices for placards?. AMM Chapter 20 – Standard Practices – Airframe. *.

[ATA 11] In which AMM chapter are the Placards found?. Chapter 11. *.

[ATA 06] What are the 6 fuselage manufacturing sections?. Section 41, 43, 44, 46, 47 and 48. *.

[ATA 06] Which section is NOT pressurized?. 48. *.

[ATA 34] The FMCF of the right AIMS cabinet is in the: CPM (BASIC) — Core Processor Module (Basic). *.