AOPP

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

If the actual take off weight is determined to be lower than any performance limiting take off weight, then a reduced thrust take off may be considered

When conducting a reduced thrust take off, the aeroplane must be climbed at V2

Vmcg is checked using the assumed temperature method

A reduced thrust take off must be used when noise abatement procedures are in force

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 take off run required will be increased and the second segment climb performance will be improved

The take off run required will not be affected and the second segment climb performance will be reduced

The take off distance run required will be reduced and the second segment climb performance will be reduced

The emergency distance required will be reduced and the second segment climb performance will be improved

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 TODR would decrease

The ASDR would decrease

There would be no change in ASDR or TODR

The TODR would increase

The minimum required distance for take off is:

The greater of (a), (b) & (c) above

The ASDR with engine failure at V1

The AEO take off distance factored by 1.15

The take off distance with an engine failure at V1

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:

64,000 kg

74,250 kg

68,000 kg

76,200 kg

Which of the following is true:

Runway slopes down – decreases take off ground run

Runway slopes up – decreases take off ground run

Runway slopes down – increases take off distance required

Runway slopes up – decreases take off distance required

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:

68,000 kg

64,500 kg

69,500 kg

72,500 kg

Which of the following is true:

Runway slopes down – decreases take off ground run

Runway slopes up – decreases take off ground run

Runway slopes down – increases take off distance required

Runway slopes up – decreases take off distance required

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:

59,000 kg

74,250 kg

63,000 kg

76,200 kg

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:

52,000 kg

64,500 kg

60,500 kg

72,500 kg

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