CL-30 Limitations Flashcards

0
Q

Cabin Differential Pressure Limits

A

Air………………………… -.5 to 9.4 psi

Landing………………… -.5 to 1.0 psi

Taxi………………………… -.5 to .1 psi

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1
Q

Generator Load Limits

A

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

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2
Q

V mo

M mo

A

Up to 8000 ft ………………………. 300 kts

8000 ft to 29475 ft ………………..320 kts

Above 29475 ft ……………………… .83m

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3
Q

V mcg

A

111 kts

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4
Q

Maneuvering Load Factors

A

Flaps up …………………… 2.6g to -1.0g

Flaps down …………………. 2.0g to -0g

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5
Q

APU Maximum Altitudes

  • Operation
  • Generator
  • Bleed Air
A

Operation …………………….. 37,000 ft

Generator …………………….. 30,000 ft

Bleed Air ………………………. 20,000 ft

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6
Q

APU Starter Cooling Times

A

Start Attempts Cooling Time

1 ............................................... 1 min
2 ............................................... 1 min
3 ............................................. 20 min
4 ............................................... 1 min
5 ............................................. 40 min
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7
Q

V’LE

V’LO

  - Retraction
  - Extension
A

V’LE …………………………. 250 kts

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

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8
Q

V’RA

V’FE

A

V’RA …………………………. 265 kts or .75 m

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

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9
Q

Spoilers

A

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.

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10
Q

Maximum useable fuel

   - Single Point
   - Over Wing
A

Per Tank Total

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

Over Wing ………………… 6500 lbs 13,000 lbs

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11
Q

Approved Fuels

A
Jet A
Jet A1
Jet B
JP 4
JP 5
JP 8
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12
Q

Maximum depth of Water or Slush

Takeoff / Landing

A

Takeoff ………………….. .25”

Landing ………………… .5”

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13
Q

Autopilot Minimum Use Height

A

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
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14
Q

Required Equipment for RVSM

A

Autopilot
Altitude Alerting System
Altitude Encoding Transponder
2 Air Data Computers

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15
Q

Maximum Ramp Weight

A

39,000 lbs

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16
Q

Maximum Landing Weight

A

33,750 lbs

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17
Q

Thrust Reversers

A
  • 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
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18
Q

Runways

A
  • Paved runways only
  • Maximum slope +/- 2%
  • 4000 ft long (company limitation)
  • 70 ft wide (company limitation)
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19
Q

Maximum Gear Extension Altitude

A

18,000 ft

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20
Q

V’1mcg

A

116 kts

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21
Q

Auto flight

A
  • Do not intentionally overpower the autopilot

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

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22
Q

Maximum depth of wet snow

Takeoff / Landing

A

Takeoff ………………… .5”

Landing ……………….. 1”

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23
Q

V’mca

A

Flaps 10 …………….106 kts

Flaps 20 …………… 102 kts

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24
Q

Maximum Takeoff Weight

A

38,850 lbs

25
Q

Maximum Fuel Imbalance

A

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

26
Q

V’MCL

A

Flaps 10 ………… 108 kts

Flaps 20 ………… 106 kts

Flaps 30 ………… 102 kts

27
Q

Maximum depth of dry snow

Takeoff / Landing

A

Takeoff ………………. 2”

Landing ……………… 3”

28
Q

Maximum Zero Fuel Weight

A

27,200 lbs

29
Q

Jet A temperature limits

A

-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

30
Q

Minimum fuel for a “Go Around”

A

500 lbs per side

31
Q

Maximum Takeoff / Landing Pressure Altitude

A

10,000 ft

32
Q

Maximum Tailwind Component

A

10 kts

33
Q

Maximum Tire Speed

A

182 kts

34
Q

Maximum altitude for flap deployment

A

18,000 ft

35
Q

Maximum operating altitude

A

45,000 ft

36
Q

Minimum Flight Weight

A

23,100 lbs

37
Q

Minimum battery temperature for takeoff

A

-20c

38
Q

Air Source Selector

A

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

39
Q

Engine Starts

A
  • 3 consecutive starts followed by 15 minutes of cooling

- Engine must be motored for 30 seconds after aborted start

40
Q

Crew and passenger oxygen masks

A
  • Not approved for use above 40,000 ft cabin altitude.

- Prolonged use of passenger masks above 25,000 ft cabin altitude not recommended.

41
Q

Wing Anti Ice (ground)

A

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

42
Q

Standby Instrument / Standby Compass

A
  • 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
43
Q

Wing Anti Ice (flight)

A

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

44
Q

APU Anti ice / De-ice procedures

A

Do not operate APU during de-icing

45
Q

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

A

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

46
Q

Engine Anti Ice (flight)

A

Selected “ON” when temperature is 10c thru -40c and visible moisture is present.

Selected “ON” when “ICE DETECTED” CAS illuminates.

47
Q

Engine Anti Ice (ground)

A

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

48
Q

Minimum bulk fuel temperature for takeoff.

A

-30c

49
Q

Maximum bulk fuel temperature for takeoff.

A

50c

50
Q

Maximum altitude when using Jet B or JP 4 fuels.

A

16,000 ft

51
Q

Maximum speed and altitude APU can be started.

A

30,000 ft and 285 kts

52
Q

Maximum demonstrated crosswind.

Takeoff / Landing

A

Takeoff ………………….. 28 kts

Landing …………………. 24 kts

53
Q

Wingspan

A

63’ 10”

54
Q

Aircraft length

A

68’ 8”

55
Q

Aircraft height

A

20 ft

56
Q

Minimum pavement width for 180 degree turn

A

58 ft

57
Q

Engine type

A

HTF-7000

58
Q

Maximum altitude for Left engine start on ground

A

9000 ft

59
Q

Maximum altitude for APU start on ground

A

14,000 ft

60
Q

Maximum single point refueling / de-fueling pressure

A

Refueling …………………. 55 psi

De-fueling ……………….. -8 psi