CL-650S AOM Limitations Flashcards

1
Q

Max Crosswind Dry or Wet Runway

A

24 kts

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2
Q

Max Crosswind Contaminated Runway Condition Fair/Medium

A

15 kts

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3
Q

Max Crosswind Contaminated Runway Condition Poor

A

10 kts

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4
Q

Max Tailwind Takeoff or Landing

A

10 kts

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5
Q

Max Ramp and Taxi Weight

A

48300 lbs

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6
Q

Max Takeoff Weight

A

48200 lbs

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7
Q

Max Landing Weight

A

38000 lbs

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8
Q

Max Operating Altitude

A

41000 ft

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9
Q

Max Flaps Extended Altitude

A

15500 ft

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10
Q

Max Airspeed Flaps 20

A

231 kts

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11
Q

Max Airspeed Flaps 30

A

197 kts

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12
Q

Max Airspeed Flaps 45

A

189 kts

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13
Q

Max Landing Gear Extended Speed

A

250/.70 M

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14
Q

Max Landing Gear Operating Speed

A

197/.60 M

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15
Q

Turbulent Air Penetration Speed

A

280/.75 M

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16
Q

Max Differential Pressure Taxi, Takeoff, Landing

A

0.2 psi

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17
Q

APU Starter Operation

A

3 attempts in 1 hour

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18
Q

APU Max Altitude for Start

A

20000 ft

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19
Q

APU Max Operating Altitude

A

20000 ft

20
Q

APU Max Altitude for Bleed Air Use

A

15000 ft

21
Q

APU Max Speed for Start and Operations

A

290 kts

22
Q

Autopilot Minimum Altitude After Takeoff

A

320 ft AGL

23
Q

Autopilot Minimum Altitude Category I ILS or LPV (GS < 3.5 degrees)

A

80 ft AGL

24
Q

Autopilot Minimum Altitude Precision Approach (GS >3.5 and <4.5)

A

160 ft AGL

25
Q

Autopilot Minimum Altitude Visual or IAP to MDA

A

320 ft AGL

26
Q

Minimum Battery Voltage for Engine Start or APU Start

A

22 V

27
Q

RECOG Taxi Lights

A

Do not illuminate while aircraft is not moving (Does not apply w/ LED bulbs)

28
Q

Landing Lights

A

Do not illuminate on the ground except for takeoff or landing (Does not apply w/ LED bulbs)

29
Q

Max Total Fuel Quantity

A

20000 lbs

30
Q

Max Fuel Imbalance Taxi, Takeoff, Landing

A

400 lbs

31
Q

Max Fuel Imbalance Inflight

A

800 lbs

32
Q

Engine Ice and Rain Protection

Anti-Ice On Takeoff and Land-No APU

A
  • Use in accordance with 4.6.4

- If engine cowl or wing anti-ice systems are selected On, close bleed air 10th stage valves for takeoff and landing

33
Q

Wing Ice and Rain Protection

(Deicing Required)

A
  • Use in accordance with 4.6.4

- If Type II, III, or IV fluids have been applied, select Norm just prior to takeoff thrust

34
Q

Minimum Brakes Turn Time

A

15 min

35
Q

Approach Category

A

Category C

If operational requirements dictate approach airspeed faster than 140 kts, use Category D minima

36
Q

Max ITT Takeoff

A

884 (5 minutes)

900 (2 minutes out of the 5 total transient)

37
Q

Max ITT Takeoff (OEI with APR operating)

A

928 (2 minutes out of the 5 total transient)

38
Q

Minimum Oil Pressure Takeoff

A

45 psi

39
Q

Max Transient Oil Pressure After Cold Start

A

156 psi (130 psi idle, 10 minute max)

-Operate engine at idle until oil pressure returns to normal range

40
Q

Continuous Ignition On

A
  • Takeoff or Landing on Contaminated Runways
  • Takeoff with High Crosswind (>10 kts)
  • Moderate or heavier intensity rain
  • Moderate or heavier intensity turbulence
  • In the vicinity of thunderstorms
41
Q

Icing Conditions

A
  • ICE displayed on EICAS
  • 10C and below with visible moisture or visibility less than 1 mile
  • Operating on contaminated surfaces
42
Q

Anti-Ice On Ground

OAT 10C or below Icing Conditions

A

L and R Cowl On

43
Q

Anti-Ice On Ground

OAT 5C or below Icing Conditions

A
  • L and R Cowl On

- Wing Norm

44
Q

Anti-Ice Flight Below 22000

TAT 10C or below Icing Conditions

A
  • L and R Cowl On

- Wing Norm

45
Q

Anti-Ice Flight 22000 and Above

TAT 10C or below, Icing Conditions, and Ice Detector failed

A

-L and R Cowl On
-Wing Norm
(*unless SAT is -40C or below)

46
Q

Anti-Ice On Ground

OAT 5C any conditions

A

-Wing Norm

Anytime temp 5C or below regardless conditions select Wing Norm during taxi and selected off for takeoff

47
Q

Wing Anti-Ice

Below 22000 and TAT 10C or below, No Icing Conditions

A

Select Wing Anti-Ice on prior to extending flaps for approach
(may be selected off when Wing Heat L/R indicators turn green)