Limitations

Question 1

What is Max Ramp Weight?

Answer 1

18,078 pounds

8200 kg

Question 2

Max TO Weight

Answer 2

17,968 lbs

8,150 kg

Question 3

Max Landing weight

Answer 3

16,865 lbs

7,650 kg

Question 4

Max zero fuel weight

Answer 4

13,999 lbs

6,350

Question 5

V LO

V LE

Answer 5

250 KIAS

Question 6

V MC

For takeoff with takeoff flaps

Answer 6

97 KIAS

Question 7

V MC

For landing with landing flaps

No Icing Conditions

Answer 7

91 KIAS

Question 8

V MC

For landing with landing flaps in Icing Conditions

Answer 8

95 KIAS

Question 9

Operating Maneuvering Speed

V O

Answer 9

205 KIAS

Question 10

Max Flap Extended Speeds

V FE

Answer 10

Flap 1 180 KIAS

Flap 2 170 KIAS

Flap 3 170 KIAS

Flap full 160 KIAS

Question 11

Max Altitude for Flaps Extended

Answer 11

18,000 ft

Question 12

Max Tire Ground Speed

Answer 12

182 knots

Question 13

Runway slope

Type surface

Answer 13

-2% to +2%

Paved

Question 14

Load factor limit flaps up

Answer 14

3.00 g

Question 15

Load factor limit flaps down

Answer 15

1,2,3 and full

2.00 g

Question 16

Baggage Loading

Answer 16

LH forward cabinet - 44 lb (20kg)

Lab cabinet - 33 lb (15kg)

Aft baggage - 463 lb (210kg)

Forward baggage - 110 lb (50kg)

Refreshments - 71 lb (32kg)

Side stowage - 36 lb (16.5kg)

Question 17

Max takeoff and landing tailwind component

Answer 17

10 knots

Question 18

Max crosswind component allowed to apply static takeoff power

Answer 18

18 knots

Question 19

Hydraulic system accumulator pre-charge check interval

Answer 19

15 consecutive calendar days or before the next flight, whichever occurs last

Question 20

Stall warning and protection system must be tested

Answer 20

Prior to each flight

Question 21

What are the prohibitions associated with the use of the SVS?

Answer 21

Use of the SVS as primary information to base decisions and/or plan maneuvers, to navigate, or to avoid terrain, obstacles, or traffic is prohibited

Question 22

Minimum battery voltage for start

Answer 22

24V

Question 23

Minimum GPU voltage required for battery charging

Answer 23

27V

Question 24

Max generator load on ground

Answer 24

330 amps each

Question 25

Max generator load in flight

Answer 25

390 amps each

Question 26

Max useable fuel per tank

Answer 26

FAA 399.4 Gal (2,676 lbs) ANAC/EASA - 1,512 L (1,214 kg)

Question 27

Unusable fuel per tank

Answer 27

FAA - 3.75 US Gal (25.13 lbs) ANAC/EASA - 14 L (11kg)

Question 28

Max fuel capacity

Answer 28

FAA - 806.2 US Gal (5,401 lbs) ANAC/EASA - 3,052 L (2,450 Kg)

Question 29

Max fuel imbalance

Answer 29

FAA - 33 US Gal (220 lbs) ANAC/EASA - 125 L (100kg)

Question 30

Min fuel tank temperature

Answer 30

-37 C

Question 31

Max fuel tank temperature on the ground

Answer 31

52 C Can be exceeded up to 80 C in flight

Question 32

Position of fuel xfeed during takeoff and landing

Answer 32

OFF

Question 33

Max thrust operating limits

Answer 33

Max Thrust: 10 minutes Max ITT: 725 C N2: 101 % N1: 100 % Oil pressure: 45-160 Oil temperature: 10-132.2 C

Question 34

Takeoff operating limits:

Answer 34

Thrust: 5 minutes Max ITT: 700 N2: 101% N1: 100% Oil Pressure: 45-160 Oil Temperature: 10-132.2 C

Question 35

Max ITT for max continuous thrust and max climb thrust

Answer 35

680 C

Question 36

Ground idle operating limits

Answer 36

N2: 55.1% (OEI) 51.2% (AEO) Oil pressure: 25-160 Oil temperature: -40-132.2C

Question 37

Flight idle operating limits

Answer 37

N2: 55.1% Oil pressure 25-160

Question 38

Engine start operating limits

Answer 38

Time: 5 seconds ITT MAX: 765 C Oil Temperature: -40 C

Question 39

Transient operating limits 20 seconds

Answer 39

ITT: 765 N2: 103 N1: 102 Oil pressure: 0-20

Question 40

Transient limits 200 seconds

Answer 40

Max Oil Temperature 140.5

Question 41

Transient limits 400 seconds

Answer 41

Oil pressure 20-270

Question 42

Starter limit motoring attempt cool down times:

Answer 42

1st: 60 seconds 2nd: 60 seconds 3rd: 15 minutes 4th: 30 minutes

Question 43

Air conditioning

Answer 43

For operation on ground the GPU must be used or one engine must be turned on.

Question 44

Pressurization (PSI)

Answer 44

Max differential: 9.4 Max diff over pressure: 9.6 Max diff negative pressure: -0.3 Max diff T.O. + L. 0.2

Question 45

When must the crew activate the ice and rain protection system?

Answer 45

When icing conditions exist or are anticipated as per section 3 Normal Proceedures.

Question 46

Define “when icing conditions exist or are anticipated “.

Answer 46

1). Whenever the SAT on the ground or for takeoff, or TAT in flight, is 10C or below and visible moisture in any form is present. (Clouds, fig, vis 1 mi or less, ice, standing water or slush)

Question 47

Operating in icing conditions

Answer 47

Max altitude for T.O. + L: 10,000 ft Min. airspeed gear + flaps up: Wing and stabilizer anti-ice inhibited or armed 165 KIAS Wing and stabilizer anti-ice uninhibited 150 KIAS

Question 48

What I the limitation regarding contaminated aircraft surfaces?

Answer 48

Takeoff is prohibited with frost (polished or not), ice, snow or slush adhering to wings, control surfaces , engine inlets, or other control surfaces.

Question 49

In what environmental condition is flight prohibited?

Answer 49

Flight in freezing drizzle or freezing rain is prohibited. The pilot must immediately exit the freezing rain or freezing drizzle by changing altitude or course.

Question 50

What are the limitations regarding use of the autopilot in icing conditions?

Answer 50

Autopilot use is prohibited in the following conditions: 1) . Severe icing 2) . Unusual control force or control deflection, or unusually large control forces to move flight controls when the the autopilot is disconnected. 3) . Indications of frequent autopilot re-trimming during straight and level flight.

Question 51

When must the wing inspection light be operative?

Answer 51

Prior to flight into known or forecast icing conditions, at night.

Question 52

Autopilot/Yaw Damper Limitations

Answer 52

Min. Engagement Height (2 engine): 600 ft. Min. Engagement Height ( 1 engine): 1,000 ft. Min. Use Height (2 engine): 195 ft Min. Use Height (1 engine): 220 ft Altitude loss (maneuvering/cruise): 160 ft Yaw damper airspeed is limited to 180 KIAS if in icing conditions.