b737-800

What is required to keep the mask harness inflated?. Nothing. Keep the red release levers locked in position. Release the red release levers. Keep the red release levers squeezed.

If the A hydraulic system fails in addition to a failure of the B system, the Accumulator Isolation Valve opens. This valve will then allow the accumulator pressure to operate the brakes as long as the accumulator pressure remains available Accumulator pressure operates the brakes as a last resort. The Brake Pressure gauge in the cockpit will indicate when____the accumulator is depleted. 1000. 500. 1200. 1500.

Which is the normal inflight position for the Landing Gear Lever?. ON. UP. DOWN. OFF.

RTO or Landing Autobrakes are Disarmed by: All of these. Advancing either or both Thrust levers after touchdown. Moving the Speed Brake Handle to the Down detent. Positioning the Autobrake select switch to OFF or Applying manual brakes.

What is the preflight position of the Normal/100% Selector on the crew oxygen masks?. Pushed in to the 100% oxygen position. Pulled out to the 0% oxygen position. Pulled out to the 100% oxygen position. Pushed in to the 0% oxygen position.

The EGT display changes from white to amber if the maximum continuous EGT is exceeded for more than___. two minutes. five minutes. 30 seconds. three minutes.

Autobrakes_______available when Alternate brakes are operating. ARE. ARE NOT.

Normally - during flight - the gear are locked in the up position and all Landing Gear Position Indicating lights are____. IN. OUT.

At what cabin altitude will the PSU door solenoids be automatically activated?. 13000. 12500. 15000. 14000.

The______Stage bleed air will augment the 5th stage bleed air, whenever the 5th stage air is not sufficient, such as during low thrust settings. 11th. 9th. 15th. 13th.

The EEC is electrically powered from the Transfer Buses until approximately______ N2 on engine start. 20%. 15%. 13%. 25%.

If the RTO is initiated at speeds over 90 knots, the AUTOBRAKE RTO MODE_____. will apply full braking action. will not apply full braking action.

The starter is_____operated. hydraulically. electrically. pneumatically.

The Gear Down Lock Viewer for the main gear is located on the cabin floor beneath the carpeting and a cover plate, and is adjacent to the_______aft of the overwing exit doors. 4th passenger window. 2nd passenger window. 3rd passenger window. last passenger window.

When the RTO mode is armed, the_____light should illuminate for 1 to 2 seconds, while a system self test is performed. red lever. green lever. OVERRIDE TRIGGER. AUTOBRAKE DISARM.

What is the maximum operating speed (in knots) with the Landing Gear extended?. 320. 300. 280. 350.

The Landing Gear Lever should be in the OFF position for manual gear extension. TRUE. FALSE.

Where is the BRAKE pressure gauge?. On the Cantain's Instrument Panel. On the First Officer's Instrument Panel. Inst above the brake handle. On the Navigator's Instrument Panel.

What is the maximum nosewheel turning angle that can be commanded by the rudder pedals?. 7 degrees. 78 degrees. 10 degrees. 17 degrees.

A_____light (between the PMC switches) illuminates whenever the engines should be in the high idle mode - but at least one engine is operating in low idle. HI IDLE. LO IDLE INOP. LOW IDLE. HI IDLE INOP.

According to this CBT, should the passenger oxygen masks be used when there is smoke in the cabin?. NO. YES.

Where is the switch located in the cockpit that allows the flight crew to manually activate the solenoids to open all PSU doors?. Right side of the fuselage. Left side of the fuselage. Forward overhead panel. Aft overhead panel.

Once activated, can an oxygen generating canister be shut off?. NO. YES.

The large fan and large amount of fan airflow - makes this a_____engine. triple axial. fuel inefficient. powerful. High Bypass.

How many continuous flow masks can be connected to a cabin P.O.B.?. TWO. ONE.

The Rejected Takeoff mode (TO) can only be selected with these conditions satisfied: The aircraft must be on the ground and wheel speed must be less than 60 knots. Thrust levers must be at idle. Antiskid must be on and ABS set to the RTO mode. All of these.

While the switch is held to the USED position, the display shows_____. fuel used since last reset. fuel used since level off. Fuel used on last 3 flights. Fuel used in center tank only.

After the gear are retracted for a minimum of 10 seconds, the pilot will move the Landing Gear Lever to the______position to remove hydraulic pressure from the landing gear system. OFF. ON.

The PSU doors are released by_____. manual levers. electrical activation. pneumatic pressure. hydraulic pressure.

The Thrust Reversers are operated_______. mechanically. hydraulically. electrically. preumatically.

If the RTO is initiated at speeds between 60 - 90 knots, the AUTOBRAKING______, and the AUTOBRAKE DISARM light will come on. does not initiate. initiates.

Normally - during flight - the gear are locked in the up position and all Landing Gear Position Indicating lights are_____. OUT. IN.

Where can you find the minimum crew oxygen bottle pressure for dispatch?. In Section 1 of the flight manual. In Section 15 of the flight manual. In Section 2 of the filght manual. In Section 17 of the flight manual.

Can the Parking Brake be set or released by either pilot?. YES. NO.

When engine reverse thrust is selected, an______REV appears above the N1 digital display box while the reverser is in transit. AMBER. RED. GREEN. BLUE.

Are the observer's masks located in a stowage box like the flight crew's masks?. no. yes.

Is hydraulic pressure needed to hold the nosegear in the retract position?. no. yes.

A red warning light illuminates when the engine limit is exceeded, and____. remains on until reset by maintenance. extinguishes after flaps are up and RPM is normal. extinguishes after 5 seconds. remains on until the RPM is reduced within limits.

Where is the crew oxygen bottle located?. Tail Compartment. Forward cargo compartment - right side. Aft cargo compartment - left side. Flight Deck.

According to this CBT, should the passenger oxygen masks be used when there is smoke in the cabin?___. NO. YES.

TAl displays in____if the cowl anti-ice valve is not in the position commanded by the cowl anti-ice switch. blue. green. amber. red.

Where is the light switch for the Nose Gear Viewer or Main Gear Viewer?. The light switch is located on the far right side of the overhead panel. The light switch is located on the far left side of the overhead panel. On the First Officer's Instrument Panel. On the Captain's Instrument Panel.

If - due to a malfunction - the Landing Gear Lever remains locked down after takeoff the pilot can pull the_______to release the Landing Gear Lever Lock - and then raise the Lever to the UP position. OVERRIDE TRIGGER. UPLOCK HOOK. HORN CUTOUT. ANTISKID/AUTOBRAKE CONTROL UNIT.

During takeoff, failures of________will cause the A/T to disengage. valid N1 limit signals from the FMC. the crew to advance the throttles.

When VNAV is engaged, the aircraft will automatically level off at the altitude displayed in_______or the FMC altitude - whichever is reached first. the Radio Altitude. The MCP altitude display.