SOPs exam

Welcome to your SOPs - Exam

When is the missed approach altitude set on a Non Precision Approach?

500ft AAL (Top of the amber band)

1000ft AAL (Top of the white band)

Once overhead the FAF

It is never set

When on the Approach and below 1000 ft AAL, the RVR falls below the applicable minimum, may the approach be continued?

FALSE

Only if the RVR is expected to Improve

True, but only on a cat 2/3 approach

TRUE

When setting airspeed bugs with no operative FMC, what is the default weight?

45,000 kgs

50,000 kgs

65,317 kgs

32,000 kgs

With more than 453kgs in the centre tank, the Captain may elect to leave the center tank pump switches off until

the AFTER TAKE-OFF checklist

3000ft agl

the selection of FLAPS UP

Passing FL100

Which Statement is correct in regard to performing the Engine Crossbleed Start (RYR) Supplementary Procedure?

The pushback must be complete with the parking brake set, the tug disconnected, and ATC clearance is obtained.

The ground crew must be aware and clear you for a crossbleed start before or during the pushback, there is no need to notify ATC.

When advancing the thrust lever to increase the duct pressure, you may need to provide additional thrust if you have decided to keep the PACK switches on.

There is no need to check the area behind the aircraft is clear as the anti-collision light is on.

When should the "ENGINE + WING" Anti-Ice setting be used on the OPT for takeoff performance calculations?

When you select WING ANTI-ICE ON before takeoff, even if you are not expecting to re-select it ON until after passing the MSA

When the OAT is +10 degrees Celsius or less and visible moisture is present

When you are expecting to select WING ANTI-ICE ON after liftoff but before reaching the MSA

When the OAT is +3 degrees Celsius or less and visible moisture is present

What is the Engine starter duty cycle limit?

1 minute

2 minutes

1 minute and 30 seconds

3 minutes

During any Go-Around when is ATC called if required?

After autopilot engagement

After 400 ft

After calling "SPEED CHECKS, FLAPS UP"

During the D.A.L.T.A setup for a circling approach, when setting the range rings for the approach and landing, the pilot should set 10 NM range ring and 4/5 NM ( VMC/IMC) range ring from the approach runway and…

4.2 NM ring from the landing runway.

4.2 NM including abeam radial from the landing runway.

4.2 NM ring from the opposite runway.

4.2 NM including abeam radial from the landing runway.

If your destination and alternate become unsuitable, once you have found a suitable alternate the fuel required is:

the final reserve fuel

the fuel from your present position to the new alternate + 5%

the fuel from your present position to the new alternate plus the final reserve fuel

During the before taxi procedure in icing conditions, engine anti-ice is selected ON. The COWL VALVE OPEN light on engine no. 1 illuminates bright, and stays illuminated bright. Choose one of the following actions.

This is normal, and indicates that the cowl valve is fully open.

Shut down the engine and contact maintrol.

Engine anti-ice is not available on the affected engine, position the switch to OFF and resume normal operations.

Position the APU BLEED air switch to OFF and increase thrust slightly, up to a maximum of 30 % N1.

Who is responsible to call "FLAPS 15" when the position is indicated on the flap position indicator?

The Pilot Monitoring after positioning ENGINE START switches to CONT and checking RECA

The Pilot Flying when responding to the landing checklist items.

There is no need to check if flap 15 is indicating correctly.

The Pilot Flying when requesting "GEAR DOWN".

When can both GEN1 and GEN2 be selected ON and the APU off during the engine start procedure?

Only when engines are confirmed stable by the PM and the GEN OFF BUS lights are illuminated and the tug and tow bar has been disconnected and the by-pass pin has been removed.

Once both engines are confirmed stable by the PM and the GEN OFF BUS lights are illuminated.

GEN2 after engine 2 is stabilized and GEN1 after engine 1 is stable.

Once the parking brake is set and during the before takeoff checklist

What criteria must be met to allow selection of V/S with flaps extended on departure?

A SID speed restriction results in delaying the flap retraction schedule

At any time when he climb rate needs to be reduced in order to comply with Ryanair policy on V/S when approaching stop altitude.

A SID speed restriction results in delaying the flap retraction schedule and the aircraft has accelerated to the assigned speed restriction and the climb rate needs to be reduced in order to comply with Ryanair policy on V/S when approaching stop altitude and AFDS is engaged above MFRA.

Never

What is the volcanic ash cloud encounter recovery?

Select reciprocal heading and engage HDG SEL Select lower altitude and engage LVL CHG Disengage AT and close thrust levers

Select lower altitude and engage LVL CHG Disengage AT and close thrust levers

Select reciprocal heading and engage HDG SEL Disengage AT and close thrust levers

Select lower altitude and engage VS at 1000ft/min

In descent when setting QNH what is the correct PF call?

SET QNH____, STANDBY ALTIMETER SET

SET QNH____, PASSING____ DESCENDING ___FEET

SET QNH____, PASSING____ DESCENDING ___FEET, ___ FLAGS, STANDBY INSTRUMENTS SET

SET QNH____, PASSING____ DESCENDING ___FEET, ___ FLAGS, STANDBY ALTIMETER SET

Correct Mark 4.00 out of 4.00 Not flaggedFlag question Question text Selection of the autopilot Control Wheel Steering is recommended for operation in severe turbulence. Choose the most appropriate answer.

False, never use CWS.

True, but DO NOT use the ALT HOLD mode.

True, and use the ALT HOLD mode.

What considerations should be evaluated before attempting to re-engage the A/P?

Assure that the aircraft is following the FD commands, is in trim about all axes and that there is no pressure on the control column/wheel.

Correct Assure the aircraft is in level flight and speed is above 220 kts.

Assure the aircraft is in level flight and the A/T is ON.

Assure the aircraft is above the MSA and the A/T is OFF.

A Window Heat ON light is extinguished and the associated WINDOW HEAT switch is ON. To check if it has failed you should

Confirm Window Heat switches are ON and position the Window Heat Test switch to OVHT. An extinguished ON light indicates that window heat has failed.

Confirm Window Heat switches are ON and press Master Caution RECALL. A MASTER CAUTION, AIR COND and extinguished ON light indicates that window heat has failed.

Confirm Window Heat switches are ON. An extinguished ON light indicates that window heat has failed.

Confirm Window Heat switches are ON and position the Window Heat Test switch to PWR. An extinguished ON light indicates that window heat has failed.

What is the correct AFDS re-engagement sequence?

PF calls for the desired Roll/Pitch modes on the MCP, assures that the aircraft is following the FD commands, is in trim about all axes and that there is no pressure on the controls. Then engages the A/P and the A/T.

PF engages the A/P by pressing CWS on the MCP, then selects the desired Roll/Pitch modes and engages the A/T.

PM engages the A/P and the A/T to reduce workload. Then the PF selects the desired Roll/Pitch modes on the MCP.

When should progress page 4/4 be selected with reference to approach procedures and what is the purpose of this operation?

Should be selected once cleared for an approach with the purpose of monitoring lateral and vertical deviation.

Should be selected on completion of the approach checks with the purpose of monitoring lateral and vertical deviation.

Should be selected once cleared for an approach with the purpose of monitoring only ANP/RNP.

Should be selected descending through MSA with the purpose of monitoring cross track error, vertical deviation and ANP/RNP.

What is the minimum fuel tank temperature for CSFF relief?

at or above -16

no limit

After De-Icing or Anti-icing the aircraft, Assumed Temperature Reduced Thrust (ATRT):

Is not permitted

After De-Icing or Anti-icing the aircraft, Assumed Temperature Reduced Thrust (ATRT):

Is permitted provided the runway surface is not contaminated

When the MDA is 900ft AAL or higher on a non-precision approach the crew should

Set the MAA at 2000ft AAL

Set the MAA at 1300ft

Set the MAA when ALT ACQ is annunciated

If the MAA is higher than 1300ft, set the MAA in the MCP Altitude window when the aircraft is 300ft above MDA/DA to avoid inadvertent ALT ACQ.

The aircraft may be operated safely up to

FL410 in any configuration

the optimum altitude indicated in the FMC

the maximum altitude indicated in the FMC

the LIDO indicated altitude

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