Interview Study questions

Question 1

what distance from aircraft, fuelling equipment and exposed public areas do you need when using idle thrust

Answer 1

30m

Question 2

what distance from aircraft, fuelling equipment and exposed public areas do you need when using breakaway thrust

Answer 2

46m

Question 3

what angel behind the exhaust needs to be clear at idle and breakaway thrust

Answer 3

15 degrees either side.

Question 4

PC24 dimensions

Answer 4

17m wing span
16.85m length
5.3m heigh

Question 5

How many air stair and cargo door indicators are there

Answer 5

6 air stair indicators (8 shoot bolts though)

9 indicators on the cargo door

Question 6

Aircraft weights
Max Ramp?
Max Takeoff?
Max Landing?
Max ZFW?

Answer 6

Max Ramp - 18400lbs
Max Takeoff - 18300lbs
Max Landing - 16900lbs
Max ZFW - 14220lbs

Question 7

What is Vmo and Mmo

Answer 7

290kts

0.74 Mach

Question 8

What speed and wake turbulence category is the the PC24 in?

Answer 8

Cat B speeds

Medium wake turbulence category

Question 9

When is TCAS II inhibited on takeoff and landing

Answer 9

Takeoff - below 1100ft radalt

Landing - below 900ft radalt

Question 10

What is the terminology for TCAS RA?

Answer 10

“TCAS RA”
“Clear of conflict returning to FL350”
“Clear of conflict FL350 resumed”

Question 11

What does the auto pilot pitch the aircraft to on GA when operating on 2 engines and OEI?

Answer 11

2 engines - 15 degrees pitch

1 engine - 9 degrees pitch

Question 12

What approach category can the PC24 fly?

Answer 12

Cat 1

Question 13

What altitude is the aircraft limited to without the Yaw Damper engaged?

Answer 13

30000ft

Must be engaged above this level

Question 14

What is the max floor and seat rail loading?

Answer 14

Floor - 100lbs/sq.ft. or 500kg/sq.m.

Seat rail - 670lbs/sq.ft. or 1000kg/sq.m.

Question 15

What is the max maneuvering speed at MTOW and 13000lbs?

Answer 15

18300lbs - 170kts

13000lbs - 140kts

Question 16

What are the rudder input limitations?

Answer 16

below 20000ft - 130 max deflection
above 20000ft - 125 max deflection
Below 45000ft - 130/125kts - 185kts (no more than 1/3 pedal input)
Below 45000ft - 185kts - 290kts (no more than 1/10 pedal input)

Question 17

What is the max tail wind component?

Answer 17

10kts

Question 18

What are the crosswind limitations

Answer 18

20kts demonstrated normal operations

17kts limitation with LH Bus, Rud Lim, DCPU1A Fail

Question 19

What is the max OAT for sea level takeoff?

Answer 19

+ 50 degrees

Question 20

What is the minimum and maximum operating temperature at 35000ft

Answer 20

Min - minus 65 degrees

Max - minus 33 degrees

Question 21

What engines do the PC24 have?

Answer 21

Williams International FJ44-4A QPM

Question 22

What is the thrust available and what is its limit?

Answer 22

Take-off thrust - 3420lbs, 855 ITT, 5 mins
Automatic Thrust Reserve - 3600, 10 min OEI or 5 min
MCT - 835 ITT

Question 23

What is the Aircraft Classification number (ACN)?

Answer 23

5