Limitations

Question 1

Max Ramp/Taxi Weight

Answer 1

48,300 lbs

Question 2

Max Takeoff Weight

Answer 2

48,200 lbs

Question 3

Max Landing Weight

Answer 3

38,000 lbs

Question 4

Max Crosswind (TO/LD)

Answer 4

Dry/Wet - 24 knots
Contaminated Fair - 15
Contaminated Poor - 10

Question 5

Max Tailwind

Answer 5

10 knots

Question 6

Max Zero Fuel Weight

Answer 6

32,000 lbs

Question 7

Max Baggage Compartment Weight

Answer 7

900 lbs

Question 8

Max Operating Altitude

Answer 8

FL410

Question 9

Max Flap Extend Altitude

Answer 9

15,500’

Question 10

Max Gear Ext Altitude

Answer 10

20,000’

Question 11

Max TO/LD Altitude

Answer 11

10,000’

Question 12

Minimum Altitudes for the AutoPilot

Answer 12

ILS/LPV: 80’

Precision with 3.5-4.5 deg GS angel: 160’

Non-Precision/Visual: 320’

Question 13

Vfe

Answer 13

Flaps 20 - 231 knots
Flaps 30 - 197 knots
Flaps 45 - 189 knots

Question 14

Max Land Gear EXT speed (V LE)

Answer 14

250 / 0.70 M

Question 15

Max Land Gear Operating speed

Answer 15

197 knots / 0.60 M

Question 16

Turbulent Air Penetration Speed

Answer 16

280 / 0.75 M

Question 17

Min Climb Speed above FL180

Answer 17

250 / 0.72 M

Question 18

Max cruise speed in RVSM

Answer 18

0.83M

Question 19

Minimum Flap Va

Answer 19

Flaps 0 - Ref+40
Flaps 20 - Ref+30
Flaps 30 - Ref+20
Flaps 45 - Ref+10

Question 20

APU Starter Limitation

Answer 20

3 attempts in 1 hour

Question 21

APU Max Airspeed

Answer 21

290 knots

Question 22

APU Max Altitude for Start and Operations

Answer 22

20,000’

Question 23

Can you use the APU for single-engine in-flight restarts?

Answer 23

No

Question 24

Max Altitude for Bleed Air from APU

Answer 24

15,000’

Question 25

Max Fuel Imbalance

Answer 25

Ground - 400 lbs
Air - 800 lbs

Question 26

Max Fuel Capacity

Answer 26

20,000 lbs

Question 27

When does fuel from the Aux tank begin to flow into the wing tanks?

Answer 27

When Wing Tanks are < 93%

Question 28

Minimum Fuel Temperature for TO

Answer 28

5 deg C (fuel filter)

Question 29

Brake turn time limitation

Answer 29

15 minutes

Question 30

Min oil pressure for TO

Answer 30

45 psi

Question 31

Max transient oil pressure after cold start

Answer 31

156 psi (130 psi idle - 10 min max)

Question 32

What conditions require the use of CONT IGN (5)

Answer 32

TOLD on contaminated runways

TO in XW greater than 10 knots

MOD+ rain

MOD+ turbulence

VCTS

Question 33

Max ITT for Takeoff

Answer 33

884 (5 mins)

900 (2 min/5 total transient)

Question 34

Max ITT with MAX TO (OEI with APR)

Answer 34

899 (5 min)

928 (2 min/5 total transient)

Question 35

Minimum Voltage for engine start or APU

Answer 35

22V

Question 36

With IGN ARM’d and START pressed: (3)

Answer 36

Starter Control Valve (in associated Engine) - Opens

10th stage L, R, ISOL - OPEN

Start Light Illuminates

Question 37

Min PSIs for Starts (Starter CV limitation)

Answer 37

APU - 40 psi

External Air - 45 psi

Cross Bleed - 60 psi

Question 38

If the Engine Cowl or Wing A/I systems are ON, close __________ for TOLD

Answer 38

Bleed Air 10th Stage Valves

Question 39

If Type II, III or IV has been applied, select WING A/I to _____ just prior to TO thrust

Answer 39

NORM

Question 40

What category of approach is the 650 certified for?

Answer 40

Cat C

Question 41

External lights red limitations? (2)

Answer 41

Do not illuminate the landing lights while on the ground EXCEPT for takeoff and landing.

Do not illuminate recog taxi lights while the aircraft is not moving.

Question 42

Min oil psi for engine start?

Answer 42

> 25 psi = stable engine start

Question 43

Engine starter limitations:

Answer 43

Three consecutive engine start cycles with five minute cooling between additional cycles.

Start cycle time limited to 60 seconds.

Max ITT prior to all starts is 120°C.

Do not use a starter if N2 exceeds 55%

Question 44

Anti-Ice limitations for takeoff/landing? (2)

Answer 44

If the cowl or wing A/I system is ON, close bleed air 10th stage valves for takeoff and landing.

If II, III or IV fluids have been applied select NORM just prior to takeoff thrust.

Question 45

PROBE heat limitation?

Answer 45

Limit heat on the ground to 2 minutes when TAT is greater than or equal to 15°C