AOPP

With respect to a take off with reduced thrust, which of the following is true:

Assuming that the aeroplane takes off at the maximum permitted take off weight when using an increased V2 procedure, the effect on the aeroplane’s performance will be that:

The expected V1 for take off is 130 kt. If the V1 is changed to 135 kt and the weight remains the same, then:

The minimum required distance for take off is:

Take Off information is as follows – ASSUME NO OBSTACLES:  TODA 1850m  ASDA 1850m  OAT 25 C  PH 2000 ft  Slope 0%  Wind + 10 head  Flaps 15º  Rwy Wet  Bleeds ON  Tyres 225 mph The maximum take off weight in kg is closest to:

Which of the following is true:

Take Off information is as follows:  Obstacle – 2,250 ft amsl @ 4,000m from brakes release, on runway centre line  TORA 2300m  ASDA 2300m  OAT 30 C  PH 2000 ft  Slope 1% Up  Wind + 10 head  Flaps 5º  Rwy Wet  Bleeds OFF  Tyres 210 mph The maximum take off weight in kg is closest to:

Which of the following is true:

Take Off information is as follows – ASSUME NO OBSTACLES:  TORA 1650m  ASDA 1650m  OAT 25 C  PH 2000 ft  Slope 1% Down  Wind 0  Flaps 15º  Rwy Wet  Bleeds ON  Tyres 225 mph The maximum take off weight in kg is closest to:

Take Off information is as follows:  Obstacle – 4,400 ft amsl @ 3,000m from brakes release, on runway centre line  TORA 1800m  ASDA 1800m  OAT 35 C  PH 4000 ft  Slope 0%  Wind + 10 head  Flaps 15º  Rwy Wet  Bleeds OFF  Tyres 225 mph The maximum take off weight in kg is closest to: