Netjets Captain Exam Questions

Question 1

On a dry runway, your LDA (turbo jet aircraft) should be equal to

Answer 1

LD x 1.67

Question 2

on SID’s higher gradient are sometimes published with the altitude up to which they must be realised. Above that altitude

Answer 2

min gradient of 3.3% is applicable to to an altitude of 820 above the highest obstacle

Question 3

if landing on wet runway and the anti skid light illuminates, one should

Answer 3

disengage the system, use max reverse thrust and deploy the drag devices and apply gentle braking

Question 4

flashing red lights to an aircraft on ground means

Answer 4

taxi clear of landing area in use

Question 5

a flashing green light to an aircraft in flight means

Answer 5

return for landing

Question 6

at ISA -34 your pressure altitude

Answer 6

over reads

Question 7

long range cruise

Answer 7

is faster than max range

Question 8

a reduced climb max thrust uses

Answer 8

more trip fuel

Question 9

given airfield elevation of 1500ft, altimeter 1000 millibars, calculate pressure altitude

Answer 9

1890

Question 10

flight carries in lower than optimum altitude equals

Answer 10

less time, more fuel

Question 11

timing in hold above 14000 is

Answer 11

1m 30 seconds

Question 12

lightning is most likely to occur at temp of?

Answer 12

+5 to -5 OAT

Question 13

with engine failure at v1, it is possible to

Answer 13

continue to 35ft without exceeding the takeoff field length and stop without exceeding the take off field length

Question 14

the corrective action for dutch roll is?

Answer 14

use firm but gently aileron

Question 15

for the least trip fuel , climb at

Answer 15

best rate of climb

Question 16

when does net takeoff flight path end and enroute performance begin

Answer 16

1500ft

Question 17

first segment is

Answer 17

is from 35 ft point to the point where the gear is retracted

Question 18

second segment is

Answer 18

from the end of the 1st segment to gross height of at least 400 feet at constant v2

Question 19

final segment is

Answer 19

extends from the level off height to a q net height of 1500 or more with the flaps up and max continuous thrust

Question 20

how does weight affect descent point?

Answer 20

you must descend earlier with heavier plane

Question 21

there are 2 runways, on is 8000 ft and the other is 10000 ft long, with respect to second segment climb, which runway will allow for a greater 2nd segment perfomance

Answer 21

10000ft runway

Question 22

on a 3 degree glide path, oat -25oc. OM crossing height of 1760ft, the aircraft will indicate

Answer 22

1820ft

Question 23

in a swept wing, compared to a straight wing, the same amount of lift requires

Answer 23

a greater angle of incidence

Question 24

on a swept wing, the aircraft stress limit with flaps down compared to flaps up is

Answer 24

lower

Question 25

what is local qnh

Answer 25

regional alti setting

Question 26

qne is defined as

Answer 26

standard alti setting 2992 or 1013.2 mb

Question 27

a super stall is caused by?

Answer 27

nose up pitching moment compounded by wing wake which blanks out the high set elevator

Question 28

what is the best means for stopping on a runway?

Answer 28

brakes

Question 29

initially on a wet runway what is the most effective means for slowing down?

Answer 29

reverse thrusters and spoilers

Question 30

normal climb speed schedules are

Answer 30

compromise between enroute speeds and best rate speed

Question 31

as weight decreases, the indicated mach number for long range cruise will

Answer 31

decrease

Question 32

as altitude increases the differences between IAS and TAS

Answer 32

Increase

Question 33

approach gradient requirements take into consideration

Answer 33

engine failure performance

Question 34

if braking efficiency is proportional to the temp of the brakes, which is correct

Answer 34

braking can be degraded in large aircraft after long taxis

Question 35

v2 is defined as

Answer 35

1.2 Vs or 1.1 VMCA

Question 36

in bad weather, landing limits are a combination of

Answer 36

DA and RVR

Question 37

when landing on a wet runway , you should apply a 115% correction factor

Answer 37

always

Question 38

In a metar the sequence R28 11V16 decodes as

Answer 38

runway 28 RVR 1100 to 1600 meters

Question 39

if you have a tcas 2 RA would demand a

Answer 39

climb/descend

Question 40

final reserve is

Answer 40

fuel quantity which equals 15 mins flight at holding speed at 1500 ft and at actual weight

Question 41

which about the moca is right

Answer 41

the width of the moca corridor 10 nm

Question 42

what initial action should be carried out in case of bomb scare

Answer 42

inform atc and put bomb in most safe position

Question 43

an engine failure during flight with consequential damage in the surrounding structure, according to the OM part a is

Answer 43

an accident

Question 44

standard takeoff minima for a runway with REDL, but without runway centrelights is

Answer 44

250 m VIS/RVR

Question 45

forecast should be prepared within? before time of departure

Answer 45

3 hours

Question 46

an aircraft being overtaken, who has right of way?

Answer 46

plane being overtaken

Question 47

what is the normal radius of an MSA and obstacle clearance

Answer 47

25nm and 1000 ft

Question 48

what is the min auth rvr for a visual approach

Answer 48

800m

Question 49

lvp’s must be in place when rvr is less than ?

Answer 49

400 m

Question 50

takeoff alternate should be

Answer 50

one hour flight single engine with still air and ISA conditions

Question 51

sids are calculated for

Answer 51

all engines running

Question 52

climb gradient means

Answer 52

gradient = still air

Question 53

on a sid you have to be at 4000 ft at 4dme after the der, what would be your target speed

Answer 53

the best angle speed

Question 54

the gross climb gradient (2 engines) aeroplane for the second and fourth segments respectively are equal to

Answer 54

2.4 and 1.2

Question 55

a takeoff with more than normal takeoff flaps will result in

Answer 55

longer takeoff distance

Question 56

does the weight of a aircraft inflence vmca

Answer 56

vmca is inversely proportional to the aircraft mass