SOPs exam

Welcome to your SOPs - Exam

During the post flight procedures who annunciates "Doors to manual and crosscheck"?

CPT

What is the Engine starter duty cycle limit?

1 minute and 30 seconds

2 minutes

1 minute

3 minutes

During the climb as PM you see a FMC scratchpad message:

Only the PM is required to acknowledge the message as this is not PF's area of responsibility

Both pilots must acknowledge the message before it is cleared

This message must be cleared immediately to allow subsequent messages to be displayed

The message may be ignored until reaching top of climb as this is a critical phase of flight

During Fuel Balancing with fuel in the center tank what should the position of the center tank fuel pumps and crossfeed selector be?

Right centre tank fuel pump On and crossfeed selector OPEN

Right centre tank fuel pump ON and crossfeed selector CLOSED

Both center tank fuel pumps Off and crosfeed selector OPEN

Left center tank fuel pump ON and crossfeed selector OPEN

Which statement is correct If an engine failure occurs during a NO ENGINE BLEED TAKEOFF?

Do not position the engine BLEED switches ON until reaching 1500 ft or until obstacle clearance height has been attained.

Do not position the engine BLEED switches ON until reaching 3000 ft or until obstacle clearance height has been attained.

Do not position the engine BLEED switches ON until reaching 1000 ft or until obstacle clearance height has been attained.

Do not position the engine BLEED switches ON until reaching 400 ft or until obstacle clearance height has been attained.

Inexperienced co-pilots or a co-pilot newly converted onto type shall not conduct the landing when specific weather conditions are experienced. Choose the most appropriate description.

When the crosswind is in excess of 15kt during normal operations or when the crosswind is more than 2/3rds limiting value, whichever is greater

When the crosswind is in excess of 15kts during normal operations regardless of runway limitations and conditions

When the crosswind is in excess of 22kts during normal operations with suitable runway limitations and conditions

When the crosswind is in excess of 15kt during normal operations or when the crosswind is more than 2/3rds limiting value, whichever is lower

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.

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

Shut down the engine and contact maintrol.

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

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

Can an enroute alternate be considered at the planning stage that is within a NFZ?

A techlog entry must be made.

Visually inspect the engines and if nothing found, no action required.

No action required.

Verbally tell the engineer at the next suitable location.

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 the Boeing OPT is unavailable on both EFBs, what should crews do?

Download the required RTOWs to the FDF and prepare a paper load sheet.

Delete the OPT application and re-install it.

Contact Operations

Under which conditions do we select GEN 1 and 2 ON and the APU OFF during the engine start procedure?

When at least one engine is stable.

When one engine is stable and the pushback has been complete.

When both engines are stable provided there are no additional defects and there is no requirement to perform a NO ENGINE BLEED takeoff.

When both engines are stable and the parking brake has been set.

What is the correct AFDS re-engagement sequence?

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.

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.

Which statement is correct regarding the ‘Cabin Crew Standby’ call during an RTO?

The purpose of the call is to inform cabin crew to resume normal procedures.

This is part of the On Ground Emergency procedure and is mandatory during a Rejected Takeoff.

This is mandatory during a Rejected Takeoff to prompt cabin crew to interrupt all the procedures.

Cabin crew will follow established procedures following an RTO. ‘Cabin Crew Standby’ call at this point could interrupt these procedures

What is the three step escalation process for protecting minimum reserve fuel?

Request EAT – PAN PAN call – MAYDAY FUEL call

MINIMUM FUEL – Request EAT – MAYDAY FUEL call

MINIMUM FUEL – PAN PAN call – MAYDAY FUEL call

Request EAT – MINIMUM FUEL – MAYDAY FUEL call

What range ring must be entered for the landing runway in the fix page on the RWxx point when planning a circle to land?

4.2

Who submits the EFL flight information at the end of each sector?

CPT

What is the correct method to calculate OPT performance for take-off in gusty headwind conditions?

Enter wind direction and full gust value only. Check that crosswind is within limits and continue with the calculation.

Enter wind direction and steady wind value. Complete the performance calculation.

Enter wind direction and full gust value to check that crosswind is within limits. Then enter the steady wind direction (without gust value) to complete the performance calculation.

Enter wind direction and steady wind value plus half of the gust value and complete the performance calculation.

What is the diversion distance (maximum distance from an adequate aerodrome for two-engined aeroplanes without an ETOPS approval) for the RYR B737-800?

396 nm

416 nm

427 nm

none of the above

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

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

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

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.

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

Which of the following statements is true regarding the Isolated Pack Operation during Engine Start supplementary procedure?

This considers one Pack switch position set to AUTO if there is a delay after both engines start before the air system is re-configured.

This considers the Isolation valve switch position set to CLOSE to allow ONE Pack Switch to be selected to HIGH mode. This is to improve air quality when the cabin is very warm.

This considers the Isolation valve switch position set to CLOSE to allow BOTH Pack Switch to be selected to HIGH mode. This is to improve air quality when the cabin is very warm.

This considers the Isolation Valve switch position set to CLOSE and the Right PACK switch position set to AUTO after No.2 Engine has stabilized after Engine Start. This is to improve cabin air quality between starting the first and second engine.

During Fuel Balancing with fuel in the center tank what should the position of the center tank fuel pumps and crossfeed selector be?

Right centre tank fuel pump On and crossfeed selector OPEN

Right centre tank fuel pump ON and crossfeed selector CLOSED

Both center tank fuel pumps Off and crosfeed selector OPEN

Left center tank fuel pump ON and crossfeed selector OPEN

What should the pressurisation FLT ALT window be set to during the Preflight procedure?

Optimum cruise altitude (or ATC capped level, if lower)

Current step climb level corresponding with MCP and FMC

LIDO final planned level

Filed level or lower if performance limited or level capped.

During Flight Deck Safety Inspection, what is the FIRST item to be checked in the Techlog?

It is the Captain's responsibility to check the techlog.

Verify Techlog registration agrees with aircraft registration.

Verify the door code.

Can an enroute alternate be considered at the planning stage that is within a NFZ?

Yes

When can flight crew inhibit RAAS?

Airline policy (airfield brief) prohibits the RAAS for the intended airport or the runway.

NOTAM applies to the intended runway.

All of the other answers are correct

Airport is not in the GPWS database.

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