Performance Questions

TODA is defined as:

ASDA is defined as:

V1 is defined as the:

VR is the speed at which:

V2 is the:

VMCG is the minimum control speed:

VMCA is the minimum speed at which directional control can be maintained:

Which relationship must always be maintained during takeoff?

VMCG must always be less than or equal to:

VS in the landing configuration is known as:

The climb gradient is defined as:

For a Class A aeroplane, the minimum second segment climb gradient with one engine inoperative is:

The second segment of the takeoff flight path begins at:

Rate of climb is:

The absolute ceiling is the altitude where:

The service ceiling is the altitude where maximum rate of climb drops to:

Specific range is defined as:

Long-range cruise (LRC) speed is typically:

A cost index of 0 in the FMS represents:

A high cost index in the FMS will result in:

Maximum endurance speed occurs at the speed for:

The screen height for landing distance for Class A aircraft is:

For a wet runway, the landing distance required must be factored by:

The dry runway landing distance factor for commercial operations is:

LDA stands for:

During a drift-down after engine failure above the OEI ceiling, the aircraft:

The net takeoff flight path is obtained by reducing the gross gradient by:

OEI stands for:

An increase in temperature above ISA will:

An increase in aerodrome pressure altitude will:

ISA temperature at sea level is:

The ISA temperature lapse rate in the troposphere is:

Density altitude is pressure altitude corrected for:

Runway contamination with standing water primarily affects performance by:

The minimum aquaplaning speed for a tyre on a wet runway is approximately:

Compacted snow on a runway will:

MTOW stands for:

MZFW is the maximum weight of the aircraft with no:

The structural limitation that MZFW primarily protects is:

MLW stands for:

The net takeoff flight path must clear all obstacles by at least:

The standard obstacle accountability area half-width for takeoff is:

A clearway may not exceed:

A stopway must be:

A balanced field length exists when:

VMU is the:

VREF is:

The regulated takeoff weight (RTOW) is the lowest of:

Increasing flap setting for takeoff will:

A headwind during takeoff will:

An uphill runway slope will:

A tailwind during landing will:

The screen height for takeoff with all engines operating is:

If an engine fails before V1, the pilot should:

If an engine fails at or after V1, the pilot should:

The first segment of the takeoff flight path ends when:

During the third segment of the takeoff flight path, the aircraft:

The minimum required gross climb gradient for the final takeoff segment (2-engine, OEI) is:

Best angle of climb speed (VX) gives the:

Best rate of climb speed (VY) gives the:

For a jet aircraft, maximum range speed occurs at the speed for:

Step climbing during cruise is used to:

The optimum cruise altitude for a jet increases as:

On a hot day compared to ISA, an aircraft will have:

High humidity will:

During a drift-down procedure, the recommended speed is:

The minimum obstacle clearance during a drift-down is:

If an obstacle cannot be cleared on the net takeoff flight path, the pilot may:

Viscous aquaplaning occurs:

Reverted rubber aquaplaning is caused by:

TORA is defined as:

The effect of a downhill runway slope on takeoff is:

If a flight requires a fuel load that would make TOW exceed MTOW, the pilot must:

The relationship between aircraft weights is:

A steep approach (5.5° glideslope) is sometimes used to:

Using reverse thrust for landing performance calculations in the EU is:

At the maximum range cruise speed, specific range is:

As aircraft weight decreases in cruise, the speed for maximum range:

After an engine failure during cruise, the pilot should first:

The obstacle accountability area widens if:

The effect of a tailwind on takeoff performance is:

VLO is the maximum speed for:

VLE is the maximum speed with:

VFE is the maximum speed for:

Reduced thrust takeoff (assumed temperature method) is used to:

When is a reduced thrust takeoff NOT permitted?

The initial climb-out speed for a twin-engine jet with one engine inoperative should not be less than:

Green dot speed on Airbus aircraft represents:

The buffet onset boundary limits the:

The 'coffin corner' refers to:

Autobrakes at a higher setting will:

The approach speed (VAPP) in turbulent conditions is typically:

Maximum taxi weight exceeds MTOW by the:

Anti-ice usage during takeoff affects performance by:

ISA standard pressure at sea level is:

A wet runway is defined as one where the surface is soaked but without:

A contaminated runway is one where more than what percentage is covered with water, slush, snow, or ice?

The ASD (Accelerate-Stop Distance) assumes engine failure at:

If an aircraft must land overweight in an emergency:

The net ceiling is the altitude where the net rate of climb equals: