REPASO 1

WHERE ARE THE LATITUDE AND LONGITUDE INCLINOMETERS LOCATED?. IN THE RH MAIN WHEEL WELL. IN THE MEC. IN THE NOSE WHEEL WELL.

WHAT COMPONENTS CAN BE LOCATED NEAREST TO STATION 92.5 ?. RADOME. E6 RACK. FWD ENTRY DOOR.

WHEN WORKING WITH ESDS EQUIPMENT, WICH IS A SAFETY PRECAUTION TO BE OBSERVED?. A GROUNDED WRIST-STRAP MUST BE WORN WHEN HANDLING ANY ESDS EQUIPMENT. EXTERNAL POWER MUST BE REMOVED FROM THE AIRPLANE BEFORE HANDLING ANY ESDS EQUIPMENT. THE ESDS POWER CIRCUIT BREAKERS MUST BE TRIPPED BEFORE HANDLING ANY ESDS EQUIPMENT.

THE ARINC 636 SYSTEM IS A DIGITAL DATA TRANSFER SYSTEM VIA WHICH OF THE FOLLOWING?. FIBRE OPTIC CABLING. A PAIR OF TWISTED WIRES AND TERMINATION RESISTORS. E-CORE DATA COMMS CABLING.

WHICH OF THE FOLLOWING STATEMENT IS CORRECT? SECTION 48 OF THE 777 FUSELAGE: HAS 30 FOOT PLUG ADDED FOR THE 777-ER VARIANTS. HAS COMPOSITE MATERIAL MANUFACTURED FLOOR BEAMS FOR WEIGHT SAVING. IS UN-PRESSURISED IN FLIGHT.

WHERE IS THE HF ANNTENA LOCATED?. ON THE LEADING EDGE ON THE FIN. ON THE WING TIP. ON THE FUSELAGE CENTER LINE.

WHAT IS THE NAME OF MANUAL USED BY THE FLIGHT CREW TO OBTAIN 8 DIGIT CODES FOR AIRPLANE FAULTS?. RAMP MAINTENANCE MANUAL. FAULT REPORTING MANUAL. AIRCRAFT MAINTENANCE MANUAL.

WHAT COMPONENTS CAN BE FOUND ON THE P18 DECK PANEL?. THE THROTTLE CUADRANT. THE FIRE HANDLES. THE MAT.

WHICH OF THE FOLLOWING STATEMENT IS CORRECT? THE DISPATCH DEVIATION GUIDE: IS USED TO RECORD AND REPORT NON AIRWORTHINESS FAULT. LIST THE ALTERNATIVE LANDING AIRFIELD FOR DIVERSIONS. CONTAINS THE MEL AND ACCEPTABLE FAULT DISPATCH PROCEDURES.

WHICH OF THE FOLLOWING MANUALS WILL SUPPLY CDCCL INFORMATION?. MPD. IPC. TSM.

Station Numbers, Buttock lines and Water lines are measured in units of which of the following?. Centimetres. Metres. inches.

Where can the E10 rack holding the APU battery and charger be located?. Aft of the Bulk Cargo door station 1937. In the passenger compartment above the aft galley LBL 388. Aft of the Rear Cargo Door station 110.

What connects LRUs to the ARINC 629 data buses?. Cable Termination Resistors. Current Mode Couplers. ASG (ARINC Signal Gateway) Cards.

Where are the OPAS (Overhead Panel ARINC 629 System) card files found?. On the E3 rack in the MEC. On the P61 Maintenance Panel. In the P84 and P85 System card files in the MEC.

What is the name of manual used by the Flight Crew to obtain 8 digit codes for airplane faults?. Ramp Maintenance Manual. Fault Reporting Manual. . Aircraft Maintenance Manual.

Which of the following statements is correct? The Dispatch Deviation Guide: Is used to record and report non airworthiness faults. List the alternative landing airfields for diversions. Contains the MEL and acceptable fault dispatch procedures.

which two standby instruments are interchangeable?. stanby altimeter & stanby airspeed indicator. Stanby Attitude indicator & stanby airspeed indicator. Stanby Attitude indicator & stanby altimeter.

What are Pressure(s) used by ADIRU and SAARU to calculate airspeed?. Pitot Air Pressure. Static Air Pressure. Both Pitot and Static Aire Pressure.

How long the SAARU Can Supply backup navigation function if ADIRU Failed?. 10 minute. 30 minute. 3 minute.

Air speed and Attitude indicated on stanby instruments are calculated by. SADMs. ADIRU. SAARU.

Where is the Terrain Awareness Display for EGPWS Shown?. On the ND Only. Both the PFD and ND. On the PFD Only.

What is indicated on Stanby Airspeed indicator when aircraft on ground moving: 0 knots. 50 knots. 30 knots.

What tunes the VOR receivers Automatically?. CDUs. Radio Tuning Panel. AIMS Cabinets.

What happens if one gyro and two accelerometers fail in the ADIRU. Attitude will not be displayed by the ADIRU. Heading output is lost from the ADIRU. A Status message is Displayed.

what make the bottom TCAS Antenna Omni directional?. The system is always omni directional. Nothing. the system can only utilise the upper fuselage antenna. The PSEU Supplies a gear not up signal.

What happens when the air data inertial reference unit (ADIRU) Is initially turned in from the fligth deck switch?. A Self test is carried out for 30 sec only. the heading flag is removed before the self test is initiated. Attitude Data is available after 30 secs.

How does the Automatic Direction finder receiver get tuning data?. Using the VOR/ADF Switch on the EFIS Control panel. manually from the Control Display Unit. Automatically from the FMCF and AIMS.

Where does AIMS receive its time from?. Captain Clock. ELMS. MMRs.

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.

What test would you do to check for defects in CDU Display ?. The CDU Configuration test. The CDU Reset and bite test. The CDU Special function test.

On the B777 aircraft the FMCF In the rigth AIMS Cabinete is in the. CMP (COM). CPM (BASIC). CPM (ACMF).

If Both FMCFs Fail, how is the ALTN Navigation data to the ND. Only the Center CDU supplies data to the left ND. The left CDU sends data to both NDs. The Onside CDU Supplies the data to the NDs.

what is the main hardware components of the onboard network sistem (ONS). Aircraft information management system (AIMS). Network file server (NFS). Local area network (lan).

The EFB EUs have two PCU Core, hosting what software?. Android & Window. Window only. Linux & Window.

where can you find a list of all LSAP (loadable software aircraft parts). Internal confg. system config. Load mode.

From where can maintenance staff access the eXTV System?. maintenance access terminal(MAT). Passenger in-seat Display. Crew Terminal.