CL-30 Limitations

Question 0

Cabin Differential Pressure Limits

Answer 0

Air………………………… -.5 to 9.4 psi

Landing………………… -.5 to 1.0 psi

Taxi………………………… -.5 to .1 psi

Question 1

Generator Load Limits

Answer 1

2 or 3 generators operating………………….400 amps

1 generator operating (on ground)…………400 amps

1 generator (in flight)…………………………….500 amps

Transient limit (5 minutes)………………………600 amps

Question 2

V mo

M mo

Answer 2

Up to 8000 ft ………………………. 300 kts

8000 ft to 29475 ft ………………..320 kts

Above 29475 ft ……………………… .83m

Question 3

V mcg

Answer 3

111 kts

Question 4

Maneuvering Load Factors

Answer 4

Flaps up …………………… 2.6g to -1.0g

Flaps down …………………. 2.0g to -0g

Question 5

APU Maximum Altitudes

• Operation
• Generator
• Bleed Air

Answer 5

Operation …………………….. 37,000 ft

Generator …………………….. 30,000 ft

Bleed Air ………………………. 20,000 ft

Question 6

APU Starter Cooling Times

Answer 6

Start Attempts Cooling Time

1 ............................................... 1 min
2 ............................................... 1 min
3 ............................................. 20 min
4 ............................................... 1 min
5 ............................................. 40 min

Question 7

V’LE

V’LO

  - Retraction
  - Extension

Answer 7

V’LE …………………………. 250 kts

V’LO Ret…………………… 200 kts
Ext……………………. 250 kts

Question 8

V’RA

V’FE

Answer 8

V’RA …………………………. 265 kts or .75 m

V’FE
Flaps 10 or 20 …………………… 210 kts
Flaps 30 …………………………… 175 kts

Question 9

Spoilers

Answer 9

Do not extend spoilers below:

                Approach + 8 kts
                500 ft  AGL

Do not select flight spoilers to EMER except during an
emergency or as required by procedure.

Question 10

Maximum useable fuel

   - Single Point
   - Over Wing

Answer 10

Per Tank Total

Single Point ………………. 7075 lbs 14,150 lbs

Over Wing ………………… 6500 lbs 13,000 lbs

Question 11

Approved Fuels

Answer 11

Jet A
Jet A1
Jet B
JP 4
JP 5
JP 8

Question 12

Maximum depth of Water or Slush

Takeoff / Landing

Answer 12

Takeoff ………………….. .25”

Landing ………………… .5”

Question 13

Autopilot Minimum Use Height

Answer 13

Climb, Enroute, Descent ……………………………. 700 ft AGL

Visual and Non Precision Approaches ………… 200 ft AGL

Precision Approaches (GS 3.5d or less) ............. 80 ft AGL
                                     (GS 3.6d - 4.4d) ............ 160 ft AGL

Question 14

Required Equipment for RVSM

Answer 14

Autopilot
Altitude Alerting System
Altitude Encoding Transponder
2 Air Data Computers

Question 15

Maximum Ramp Weight

Answer 15

39,000 lbs

Question 16

Maximum Landing Weight

Answer 16

33,750 lbs

Question 17

Thrust Reversers

Answer 17

• Use only on paved surfaces
• Do not use in flight
• Do not use to backup aircraft
• Do not use on touch & go’s
• Reverse thrust above idle is prohibited below 40 kts

Question 18

Runways

Answer 18

• Paved runways only
• Maximum slope +/- 2%
• 4000 ft long (company limitation)
• 70 ft wide (company limitation)

Question 19

Maximum Gear Extension Altitude

Answer 19

18,000 ft

Question 20

V’1mcg

Answer 20

116 kts

Question 21

Auto flight

Answer 21

• Do not intentionally overpower the autopilot

- Maximum altitude with the yaw damper off is 31,000 ft

Question 22

Maximum depth of wet snow

Takeoff / Landing

Answer 22

Takeoff ………………… .5”

Landing ……………….. 1”

Question 23

V’mca

Answer 23

Flaps 10 …………….106 kts

Flaps 20 …………… 102 kts

Question 24

Maximum Takeoff Weight

Answer 24

38,850 lbs

Question 25

Maximum Fuel Imbalance

Answer 25

Fuel onboard Max imbalance < 4700 lbs ..................................... 600 lbs 4700 lbs - 10,000 lbs ................... 450 lbs 10,000 lbs - 13,700 lbs ................ 315 lbs > 13,700 lbs ................................... 250 lbs

Question 26

V'MCL

Answer 26

Flaps 10 ............ 108 kts Flaps 20 ............ 106 kts Flaps 30 ............ 102 kts

Question 27

Maximum depth of dry snow | Takeoff / Landing

Answer 27

Takeoff ................... 2" Landing .................. 3"

Question 28

Maximum Zero Fuel Weight

Answer 28

27,200 lbs

Question 29

Jet A temperature limits

Answer 29

-30c thru 50c For temps > or = 45c - Minimum fuel for takeoff is 2800 lbs - < 2000 lbs of fuel (1000 lbs per side), do not operate engines for more than 30 minutes

Question 30

Minimum fuel for a "Go Around"

Answer 30

500 lbs per side

Question 31

Maximum Takeoff / Landing Pressure Altitude

Answer 31

10,000 ft

Question 32

Maximum Tailwind Component

Answer 32

10 kts

Question 33

Maximum Tire Speed

Answer 33

182 kts

Question 34

Maximum altitude for flap deployment

Answer 34

18,000 ft

Question 35

Maximum operating altitude

Answer 35

45,000 ft

Question 36

Minimum Flight Weight

Answer 36

23,100 lbs

Question 37

Minimum battery temperature for takeoff

Answer 37

-20c

Question 38

Air Source Selector

Answer 38

Do not select the Air Source switch to "TRIM AIR ONLY" while aircraft is on the ground.

Question 39

Engine Starts

Answer 39

- 3 consecutive starts followed by 15 minutes of cooling | - Engine must be motored for 30 seconds after aborted start

Question 40

Crew and passenger oxygen masks

Answer 40

- Not approved for use above 40,000 ft cabin altitude. | - Prolonged use of passenger masks above 25,000 ft cabin altitude not recommended.

Question 41

Wing Anti Ice (ground)

Answer 41

On for takeoff when temperature is 5c or below and visible moisture is present, or when surface snow, ice, water or slush is present.

Question 42

Standby Instrument / Standby Compass

Answer 42

- Standby instrument can not be used for localizer back course approaches - Left and right windshield heat must be selected OFF while the standby compass is being read

Question 43

Wing Anti Ice (flight)

Answer 43

Selected ON when temperature is 10c thru -40c and visible moisture is present. Selected ON if "ICE DETECTED" CAS illuminates For N530FX and newer; airspeed below 210 kts

Question 44

APU Anti ice / De-ice procedures

Answer 44

Do not operate APU during de-icing

Question 45

Wing Anti Ice with Type II and Type IV Anti Ice fluids

Answer 45

If required the wing anti ice must be selected "ON" just prior to throttle advance for takeoff.

Question 46

Engine Anti Ice (flight)

Answer 46

Selected "ON" when temperature is 10c thru -40c and visible moisture is present. Selected "ON" when "ICE DETECTED" CAS illuminates.

Question 47

Engine Anti Ice (ground)

Answer 47

Selected "ON" when temperature is 10c or below and visible moisture is present, or when surface snow, ice, water or slush is present

Question 48

Minimum bulk fuel temperature for takeoff.

Answer 48

-30c

Question 49

Maximum bulk fuel temperature for takeoff.

Answer 49

50c

Question 50

Maximum altitude when using Jet B or JP 4 fuels.

Answer 50

16,000 ft

Question 51

Maximum speed and altitude APU can be started.

Answer 51

30,000 ft and 285 kts

Question 52

Maximum demonstrated crosswind. | Takeoff / Landing

Answer 52

Takeoff ....................... 28 kts Landing ...................... 24 kts

Question 53

Wingspan

Answer 53

63' 10"

Question 54

Aircraft length

Answer 54

68' 8"

Question 55

Aircraft height

Answer 55

20 ft

Question 56

Minimum pavement width for 180 degree turn

Answer 56

58 ft

Question 57

Engine type

Answer 57

HTF-7000

Question 58

Maximum altitude for Left engine start on ground

Answer 58

9000 ft

Question 59

Maximum altitude for APU start on ground

Answer 59

14,000 ft

Question 60

Maximum single point refueling / de-fueling pressure

Answer 60

Refueling ...................... 55 psi De-fueling .................... -8 psi