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Which inertial reference system data is displayed on the cockpit displays and instruments during normal operation?. Pitch and roll attitude, magnetic heading, vertical speed. True heading, vertical speed, inertial altitude, pitch and roll attitude. Computed airspeed, inertial altitude, magnetic heading pitch and roll attitude.

The normal way to disconnect the autopilot is …?. By opening the correspondent circuit breaker. By pressing the yaw damper test switch. By pressing one of the disconnect switch at the control wheels.

The autopilot rudder servos: Are used for turn coordination. Are only used in multichannel approach and rollout. Do not backdrive the rudder pedals.

The vor can be tuned…. The vor frequency is constant, that means it is not necessary to be tuned. Only manually from the vor control panel. Manually from the vor control panel or automatically from the fmc.

Which mode control position(s) allow manual tuning of the dme?. Vor or ils. Vor or plan. Map or plan.

The máximum authority of rudder with yaw damper is…. Depends if the fcc yaw axis is engaged. +/-3 with one yaw damper channel active or +/- 6 with both channels active. +/- 6 set fixed independent of yaw damper modules active .

Which inertial reference system data is displayed on the cockpit displays and instruments during normal operations?. Pitch and roll attitude, magnetic heading, vertical speed. True heading, vertical speed, inertial altitude, pitch and roll attitude. Computed airspeed, inertial altitude, magnetic heading, pitch and roll attitude.

The right iru is being used in its backup att mode, for this mode to be effective, what information must the crew enter periodically?. Heading. Windspeed & direction. Present position.

The weather radar antenna stabilization is controlled from… : The weather radar transceiver. The weather raddar control panel. The efis control panel.

Which statement concerning the power supply for the irus is correct?. Backup Power is from the main battery, backup power is limited to 5 minutes for the right iru. Backup Power is from the main battery. Backup power is limited to 5 minutes. Backup power is from the irs battery units. Backup power is limited to 5 minutes for the center and right iru.

The new feature of egpws is… : The information shown depends on geographical data base. The information shown depends on weather conditions. The information shown depends on navigational aids.

Instruments landing system (ils) is turned: Instruments landing system (ils) control panel. Multimode receiver (mmr) control panel. Automatically in map or plan.

Where is the g/s director element located?. In the g/s antenna assembly. In the nose radome assembly. On the forward bulkhead.

Where does the right dme interrogator receive autotune frequency from?. Right flight control computer (fcc). Left control display unit (cdu). Left flight management computer (fmc).

The align Lights on the irs control panel (Irmp) are flashing. What could be the possible fault?. At the end of the alignment time latitude and longitude were not entered. The airplane is fliying over 82 latitude. This is normal.

The vor deviation and to/from data is calculated by… : The ehsi. The efis symbol generators. The rdmis.

To engage ap in single channel, how many fccs are required. One. Two. Three.

An a/t disengage switch pressed will produce… : A/t disc light, sound, master caution light, autothrot disc message. The fccs disengage. An automatic reléase of a/t arm switch to off position at mcp.

How is the flight crew notified about the capabilities to perform an autoland?. This conditioning is shown on the asa. By means of the a/p ámbar light on the discrete annunciator panel. By means of a caution message on the upper eicas.

After the auto pilot disc and warnings light are actívated, they are extinguished by… : Presising cancel switch at the eicas system. Pushing either a/p disengage switch. Moving the disengage bar to off on the mcp.

The irs test is performed…. Pressing any iru front panel test switch all three irus will be in test. Automatically by the cross talk between irus during alignement. By the irus test switches or the yaw damper test switch on the p61 panel.

The thrust target from tms is showed on… : On fmcs/ cdu. Standby engine indicator with the selector in auto. On upper eicas display. N1 indication.

Fmcs. Failure of captain’s cdu. What happen to the fmcs?. The remaining cdu automatically controls both fmcs. The complete system is inoperative. Left fmc activity is stopped (standby mode).

The L iru information is shown on…. Captain’s eadi, ehsi, vsi and f/o’s rdmi. F/o’s eadi, ehsi, vsi and rdmi. Captain’s eadi, ehsi, vsi and rdmi.

In Which instrument(s) can you find localizer & glideslope information?. Captain & first officer hsis only. Captain & first officer adis only. Captain & first officer adis, hsis, and the standby attitude indicator (or isfd).

What is the purpose of the g/s director element?. To alter the g/s radiation antenna patterns such that the ils receivers have maximum g/s sensitivity. To alter the g/s radiation antenna patterns such that the ils receivers have minimum g/s sensitivity. To alter the g/s radiation antenna patterns such that the ils receivers have mínimum g/s spurious.

What about tcas is true?. The top antenna is rotated by a sinchro motor 115vac. Resolution advisor is seen on eadi. An ra (resolution advisor) is developed when an intruder is detected 2500feet avobe its flight level.

In Which of the following positions the efis control panel provides dme tuning automatically?. Map. Vor. ils.

Enhanced. the wx radar tranceiver (with pws). Can detect clear air turbulences in high altitude. Can detect windshear during landing only. Can detect windshear during take off and landing.

During touch Down the mcdp… : Will perform a power up auto test and data record. I. Will actívate the auto test mode in progress. Will reset to zero the irs residual gnd speed.

Where is the weather radar transceiver located?. At main equipment center rack E-8. At the after equipment center rack E-6. An the forward equipment center.

.When the autothrottle functions will be engaged?. The a/t arm switch must be in arm position and a mode has been selected on the afcs mcp. The autopilot must be in off condition. The autothrottle computer must be in off condition.

How many fcc does the afds have?. 3 fcc. 1 fcc. 2 fcc.

.Which are the conditions for multichannel engage?. At the moment that the app is selected on the mcp. After app. Selected loc and g/s captured and radio alt 1500 feet or below. When g/s is captured with no power fault.

What is the meaning of the vnav mode of the thrust management system (tms). Autothrottle modes are selected by the flight control computer (fcc). Vnav is an autopilot mode and has no effect to the tms. Autothrottle and thrust limit modes are selected by the flight management computer (fmc).

Where are the ils antennas located?. Behind the radome. Under the fuselage. In the top of the vertical stabilizer.

The afds go-around mode is enabled, it will be activated… : Only when the a/t switch is in off at the mcp. By pressing at leasted one go around switch at the thrust levers while in flight. Pressing the spd switch at the mcp.

What does land 3 means in asa?. There is triple redundancy of power sources, engaged fccs, sensors and servos, (fail operational). There is at least dual redundancy of engaged fccs (fail passive). A fail operational level will not be achieved.

How Can the marker system be tested?. Pressing the test switch on the overhead panel. All marker lights illuminate together. Pressing the test switch on the Left vor receiver. The marker lights illuminate sequencially for 10 seconds. Pressing the test switch on the Left vor receiver. All marker lights illuminate together for 10 seconds.

The ils system can be tested using… : A switch located on the p-5 overhead panel. A switch located on the ils control panel. A switch located on the p-61 maintance panel.