chris 1

A pilot should always continue the take-off after engine failure at V1

Runway contamination will cause V1 to increase

For a balance field, selecting a lower V1 from ideal will cause the field required to increase due to a higher TODR

For a balance field, selecting a higher V1 from ideal will cause the field required to decrease due to a lower TODR

4000m

6000m

7000m

5500m

1500ft above the take off surface to 1500ft above the landing surface

1500ft above the take off surface to 1000ft above the landing aerodrome level

From the start of level flight to the end of level flight

50ft ablve the take off surface to 1500ft above the landing aerodrome level

Vx

maximum specific range

maximum glide endurance

maximum cruise endurance

Aircraft operating closer to Vmo/Mmo

Fuel flow will increase

Total drag will increase

All of the above

Vef,Vr,Vmu,V2

V1,Vmcg,Vmbe,Vlof

Vmcg,Vlof,Vmu,V2

V1,Vef,Vr,Vmu

500ft

800ft

1500ft

3000ft

Descent at the same angle with the same time in the descent but at a faster speed

required a faster speed to achive the same descent angle as the lighter aircraft

descent steeper, at a faster speed with a greater rate of descent

descend at a steeper angle at a faster speed at the same rate of descent

increased LDR and decreased Landing Climb Limited LM

increased LDR and increased Landing Climb Limited LM

decreased LDR and decreased Landing Climb Limited LM

decreased LDR and increased Landing Climb Limited LM

Target Vmo initial before switching to maintain Mmo

Extend spoiler, flaps and gears to create more parasite drag to assist with descent

add more power in order to descent at a faster speed

Target Mmo initial and apply speed brakes

decreased take-off mass, increased pressure altitude, increase temperature

increased pressure altitude, increased outside air temperature, increase take off mass

increased outside air temperature, decreased pressure altitude, decreased flap setting

decreased take-off mass, increased density, increased flap setting

1.2 Vs for all turbojets

1.2 Vsr for all turboprops and 1.15 Vsr for all turbojets

1.08 Vsr for 4 engine turboprops and 1.13 Vsr for 2 and 3 engine turboprops

1.15 Vs for all aeroplanes

i: remain constant

ii: decrease

i: remain constant

ii: increase

i: increase

ii: decrease

i: increase

ii: remain constant

High density, headwind and upslope

low density, tailwind and downslope

low density, headwind and downslope

high density, tailwind and upslope

Both decrease

both increase

Vx increase while Vy constant

Vx constant while Vy decrease

it is dark

the runway is wet

obstacles are present close to the end of the runway

the runway is contaminated

Increase

Decrease

No change

Increase then decrease

In the event of anti-skid inoperative V1 has to be increased

an increased in runway contamination will result in higher reduction V1

For balanced field, selecting a lower V1 from idea will cause the field required to increase higher ASDR

For a balanced field, selecting a higher V1 from ideal will cause the field required to increase a higher ASDR

156

148

132

136

Vx, maximum cruise range, Vmd

Maximum cruise range, Vx, Vmd

Vx, Vmd, maximum cruise endurance

Vx, maximum cruise range, glide endurance

increase of aircraft mass

decrease of aircraft mass

tailwind

headwind