Ryanair

What is the wingtip height of blended wing aircraft?

The operation of the overwing exit locks is dependent on:

Activated at 14,000 feet, the passenger oxygen masks drop down from the stowage:

When are the NO SMOKING signs illuminated?

The aircraft is on ground and the Flight Recorder Switch is on NORMAL:

What happens if you reject takeoff at 100 knots with Autobrakes in RTO?

What are the 737-800s maximum latitude certifications:

What is the minimum pavement width for a 180 degrees turn?

The aircraft is on the ground and the Flight Recorder Switch is in NORMAL:

The APU is capable of supplying bleed air conditioning packs:

ZONE TEMP amber light illumination for CONT CAB indicates:

The maximum differential pressure is:

Illumination of an amber COWL ANTI ICE light indicates:

When does the amber DUAL BLEED Light illuminate?

After normal engine start, what should be done if the DUAL BLEED light is illuminated:

Following an unpressurised takeoff, when is the first engine Bleed Switch positioned to ON?

Which systems use engine bleed air for operation?

What happens when the WING-BODY OVHT TEST Switch is pressed?

If all TEMPERATURE ZONE SELECTORS are positioned to OFF:

An illuminated BLEED TRIP OFF light indicates

In flight with both PACK switched in HIGH:

During single pack operation with TRIM AIR selected OFF:

During descent, the pressurization descent mode is activated when:

The amber DUAL BLEED light is illuminated before starting engines. What should you do?

What is the position of the isolation valve when the ISOLATION VALVE Switch is in AUTO?

A panel failure of the Flight Altitude (FLT ALT) Indicator may result in the following indication:

The position indicator of the outflow valves show the position of the valve:

Where are the bleed trip sensors installed?

The Recirculation Fan:

The ISOLATION VALVE switch is set to AUTO, both engine bleeds are ON and both pack switches are in AUTO. The isolation valve:

Illumination of the amber BLEED TRIP OFF light indicates what valve has automatically closed?

While making a no engine bleed air take off and an engine failure occurs, when should the bleed air switches be positioned to ON?

The wing-body overheat light comes on. What is the related master caution warning?

Refer to the Cabin/Flight Altitude placard. At cruise altitude FL290, the cabin altitude should read:

Cruising at FL370. The motorised Overboard Exhaust valve will open in flight if:

In the PACK fail non-normal procedure, the crew selects a warmer temperature in order to:

The ram air system deflector doors:

The amber OFF SCHEDULE DESCENT Light illuminates. What does that indicate?

What is the differential pressure the pressure controller maintains above 37,000 ft?

What is the primary source of conditioned air to the cockpit?

What systems need pneumatic power for operation?

Due to a malfunction you are required to return to the airport of departure. To avoid the OFF SCHED DESCENT warning, you reset the FLT ALT. What can you expect?

Warm air from the E&E bay is:

In MANUAL pressurization mode, the outflow valve is driven by?

A WING BODY OVERHEAT light indicates:

Which systems use engine bleed air for operation?

What is the position of the Engine Bleed Air Switches during the secure scan flow on the parking checklist:

The right primary pack control fails. The right pack:

The BLEED TRIP OFF light:

In the PACK TRIP OFF non-normal procedure, the crew selects a warmer temperature in order to:

A DUCT OVERHEAT light only cause:

The Cockpit Voice Recorder (CVR) can be erased:

What statement is correct about the flight crew oxygen mask in the EMERGENCY position:

When the passenger service unit (PSU) is activated, how long can it supply oxygen?

Emergency exit light can be activated from:

In AUTO, the FASTEN BELTS and RETURN TO SEAT signs:

Operation of the airstairs from the exterior panel with the switch to STANDBY:

The operation of the over-wing emergency exits depends on:

Where are the logo lights installed?

At what cabin altitude is the passenger oxygen system automatically activated?

Where do you read the flight crew oxygen pressure?

The Auto position of the Cockpit Voice Recorder (CVR) On/Auto switch:

If a landing is made with RTO selected:

The wing span is (-800):

When the PASS OXY ON Light is illuminated, what does this indicate?

The flight crew oxygen system uses auto pressure breathing masks / regulators with pressure breathing starting at:

Illumination of the PSEU fault light on the aft overhead panel will indicate:

The flight crew oxygen may be as high as:

What could cause the amber ANTISKID INOP Light to illuminate?

Extending the airstairs using the exterior system:

The ISFD is an emergency source of altitude, heading, attitude and airspeed. In case of total electrical failure it is powered by its own battery for:

The EMERGENCY EXIT LIGHTS Switch in the ARMED position:

The Flight Crew oxygen pressure can be:

The Cockpit Voice Recorder uses four independent channels to record flight deck audio for a maximum of:

The wing-span of the 737-800 is:

Do not attempt to make a turn away from an obstacle within:

For RVSM operation, the maximum allowable altitude display difference for sea level, between the Captain and F/Os on the ground is?

Pushing the ATTEND call switch:

Positioning the WING ANTI-ICE switch to ON in flight:

Dual angle-airflow sensors (alpha vanes) provide angle-of-attack information to the stall warning system, autothrottle, autopilot and autoslats are anti-iced:

When operating on standby power:

Which are not heated?

Positioning the ENG ANTI-ICE switch to ON in flight:

The aircraft experiences a loss of both engine driven generators. Which one is true?

All window heat is selected ON. The green window heat ON light for the Right Side Window extinguishes. The likely reason is:

The R ELEV PITOT Light is illuminated and PROBE HEAT switches are ON. What does this indicate?

The window heat PWR TEST:

The wing anti-ice system provides bleed air to:

The alpha vanes provide angle-of-attack information to the stall warning system, auto throttle, auto pilot, auto slats and are anti-iced:

Which window(s) are heated with the LEFT FWD WINDOW HEAT switch ON?

What is the maximum airspeed limit according MEL, when WINDOW HEAT is inoperative for window nr 4?

Refer to the thermal anti-ice (TAI) CDS indication. TAI is shown above each N1 indicator:

Wing anti-ice

To receive NAV and ADF voice and range audio:

Antenna switching from tail antenna to nose antenna occurs when:

When the Audio System is operating in the degraded mode:

On the ground, for primary ATC communication:

In degraded mode, what are the combinations for transmission and reception at the degraded station?

Pushing VHF TEST switch on the radio tuning panel:

When the Captains audio control panel is operating in degraded mode:

The Automatic Flight System (AFS) consists of:

The Air Data Inertial Reference System (ADIRS) produces the following flight data:

During AUTO LAND, at which radio altitude should the flare mode be engaged?

When control wheel pressure is released during CWS roll operation, the aircraft will roll wings level when the bank angle is:

What is the latest altitude (AGL) CMD that can be selected on the second autopilot to execute a dual channel A/P approach?

Which is the correct mode on the FMA? Condition: After takeoff, A/P engaged, before flaps up. (Thrust: Roll: Pitch)

How many independent Flight Control Computers (FCCs) are there in the Autopilot Director System (AFDS)?

Normally, N1 limits and target N1 values are provided to the A/T by the:

During an ILS approach below 1,000 feet Radio Altitude, a BELOW G/S alert occurs. To cancel the alert:

Which A/T modes permit manual thrust changes without A/T interference?

Which mode must be armed before the second autopilot can be selected during a dual channel A/P approach?

In normal operation, what provides the A/T system with N1 limit values?

Under speed limiting (flashing A) appears:

Which of the following occurs when a TO/GA switch is pressed once below 2000 feet radio altitude for an automatic go-around from an ILS channel A/P approach and FLARE armed?

What happens with the IAS/MACH display on the MCP if SPD INTV switch is pushed during VNAV operation:

At what altitude will both A/Ps automatically disengage if FLARE is not armed during an ILS dual channel approach:

What pitch mode is annunciated in the FMA after takeoff when the autopilot is first engaged in CMD?

Two independent radio altimeters provide radio altitude to the respective FCCs. With one radio altimeter inoperative:

LNAV will automatically disengage:

After a normal take-off, what pitch command can you expect from the F/D?

If the autopilot ALT HOLD mode is manually overridden with control column pressure, which of the following occurs?

The autopilot disengages if FLARE mode is not armed by:

After lift-off, the A/T remains in THR HLD until:

With VNAV engaged, the AFDS pitch and A/T modes are commanded by the:

The TR Unit light will illuminate in flight if:

Which bus supplies electrical power to the auxiliary battery charger:

Normal DC indications are:

One basic principle of operation for the 737 electrical system is:

When AC power is not available, the main battery energizes the hot battery and:

If ON DC on left IRS mode selector unit comes ON steady it means:

How are the Engine Bleed Air valves powered?

During primary charge cycle operation, battry voltage can be as high as:

With the STANDBY POWER switch in the AUTO position, loss of both engine driven generators and APU generator will result in that AC standby bus is powered by battery through static inverter, and DC standby bus is powered by battery…

A take off is performed with the APU powering both transfer buses:

On the ground, with the BATTERY switch OFF and STANDBY POWER Switch in BAT, the switched hot battery bus is:

Blue illumination of APU GEN OFF BUS means:

The ELEC light will illuminate in flight if:

The left IRS is electrically powered from:

The cross bus tie relay automatically opens at glide slope capture to:

Electrical power to start the APU comes from:

Illumination of the BAT DISCHARGE light indicates:

Illumination of the STANDBY POWER OFF lights indicates:

When the STANDBY POWER Switch is OFF:

As part of the preflight procedure, you are about to test the STALL warning. For this to be possible, an AC source must have powered the Aircraft for a minimum of approximately:

If the APU is the only source of electrical power:

The TRs (Transformer rectifier) converts:

Galley busses are powered from:

The AC Standby Bus is powered by:

With normal power source on the buses, placing the battery switch to OFF will remove power from:

The right IRS is electrically powered from:

Illumination of the GND POWER AVAILABLE light indicates:

Moving the battery switch to OFF automatically shuts down the APU:

The blue APU GEN BUS light will illuminate:

The GROUND POWER AVAILABLE light will extinguish when:

Switching the CAB/UTIL switch OFF removes all 115v AC from the gally busses and:

Illumination of the STANDBY POWER OFF lights indicates:

The cross bus tie relay:

When the aircraft batteries are the only source of power:

For ground service, a ground service switch is placed:

On the ground, the TR UNIT amber light illuminates if:

The APU may be used as a pneumatic source up to:

Once the thrust reverse auto-stow circuit is activated:

During battery start, when does the EEC start to operate?

During engine start, the maximum time allowance for EGT indication after start lever is moved to idle is:

If a crossfeed start is required during in flight starting, the X-BLEED START indication will be displayed above:

During a normal engine start:

When the EEC is not powered, following engine indications are displayed directly from the engine sensors: