Performance 2

The engine failure during take-off run results in:

• an increased acceleration.

• a shorter take-off run.

• a long ground roll.

• a higher V1.

With a downward sloping runway:

• V1 will increase.

• V1 will decrease.

• VR will increase.

• VR will decrease.

When descending below the optimum altitude for a jet aeroplane at the long range cruise speed:

• Mach number decreases

• TAS increases.

• Mach number remains constant.

• Mach number increases.

During a glide at constant Mach number, the pitch angle of the aeroplane will:

• increase at first and decrease later on.

• increase.

• decrease.

• remain constant.

During certification flight testing of a transport aeroplane, the distances measured from brake release to the 35 feet point are equal to: 1547m with all engines running 1720m with failure of critical engine at V1, with all other things remaining unchanged The take-off distance adopted for the certification file is:

• 1547m

• 1720m

• 1779m

• 1978m

V1 for a balanced-field is calculated when:

• the take-off mass is field-length limited by the stopway to produce the maximum take-off mass.

• the speed is equal to V2.

• the take-off mass is field-length limited by the clearway to produce the maximum take-off mass.

• the acceleration/stop distance available is equal to the take-off distance available.

A jet aircraft's maximum altitude on a transcontinental flight with a full traffic load is usually limited by:

• its certification maximum altitude.

• its pressurisation maximum altitude.

• the altitude at which low and high-speed buffet will occur.

• thrust limits.

If the airworthiness documents do not specify a correction for landing on a wet runway; the landing distance must be increased by:

• 0.2

• 0.05

• 0.1

• 0.15

For a jet aeroplane in a level flight, cruising at VMD. If the mass is decreased:

• the minimum drag decreases and lAS decreases.

• the minimum drag decreases and lAS increases.

• the minimum drag remains the same and lAS decreases.

• the minimum drag remains the same and lAS remains the same.

If the value of the balanced V1 is found to be lower than VMCG, which of the following is correct?

• The ASDR will become greater than the one engine out take-off distance.

• The one engine out take-off distance will become greater than the ASDR.

• The VMCG will be lowered to V1.

• V1 must be increased to at least the value of VMCG.