Challenger 650 Limitations Flashcards

1
Q

Maximum Crosswind
Dry or Wet Runway

A

24kts

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2
Q

Maximum Crosswind
Contaminated Runway

A

Fair/Medium…..15kts
Poor…..10kts

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3
Q

Maximum Tailwind

A

10kts for takeoff or landing

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4
Q

Structural Weight Limitation
Ramp & Taxi

A

48,300 lbs

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5
Q

Structural Weight Limitation
Takeoff

A

48,200 lbs

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6
Q

Structural Weight Limitation
Landing

A

38,000 lbs

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7
Q

Maximum Certified Altitude
Operating

A

41,000 ft

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8
Q

Maximum Certified Altitude
Flaps Extended

A

15,500 ft

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9
Q

Maximum Airspeed (Vfe)
Flaps 20

A

231 kts

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10
Q

Maximum Airspeed (Vfe)
Flaps 30

A

197 kts

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11
Q

Maximum Airspeed (Vfe)
Flaps 45

A

189 kts

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12
Q

Turbulent Air Penetration Speed

A

280 kts/.75m

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13
Q

Maximum Landing Gear Extend Speed

A

250 kts/.70m

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14
Q

Maximum Pressurization Differential
Taxi and Takeoff

A

0.2 psi

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15
Q

Maximum Pressurization Differential
Landing

A

0.2 psi

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16
Q

APU Starter Operation

A

Three attempts in 1 hour

17
Q

APU Maximum Altitude for Start

A

20,000 ft

18
Q

APU Maximum Operating Altitude

A

20,000 ft

19
Q

APU Maximum Altitude for Bleed Air Use

A

15,000 ft

20
Q

APU Maximum Speed for Start and Operation

A

290 kias

21
Q

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

A

80 ft AGL

22
Q

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

A

160 ft AGL

23
Q

Autopilot Minimum Altitude
Visual or IAP to MDA

A

320 ft AGL

24
Q

Minimum Battery Voltage for Engine Start or APU Start

A

22V

25
Q

Maximum Fuel Quantity Pressure Fueling

A

20,000 lbs

26
Q

Maximum Fuel Imbalance
Taxi, Takeoff, Landing

A

400 lbs

27
Q

Maximum Fuel Imbalance
Inflight

A

800 lbs

28
Q

Engine Anti-Ice

A

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

29
Q

Engine and Wing Anti-Ice

A

Use in accordance with Operation of Anti-Ice System.

30
Q

Wing Anti-Ice

A

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

31
Q

Brakes Minimum Turn Time

A

15 minutes

32
Q

Aircraft Approach Category

A

Category C
(Category D if Approach speed is greater than 140kts)

33
Q

Takeoff Engine ITT

A

884 degrees C (5 minute transient limit)
900 degrees C (2 minutes out of 5 total transient)

34
Q

Maximum Takeoff ITT (OEI with APR operating)

A

928 degrees C (2 minutes out of 5 total transient)

35
Q

Minimum Engine oil pressure for Takeoff

A

45 psi

36
Q

Maximum Transient Engine 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.

37
Q

Continuous Ignition Usage

A
  1. Takeoff or landing on contaminated runways
  2. Takeoff with high crosswind
  3. Moderate or heavy intensity rain
  4. Moderate or heavier intensity turbulence
  5. In the vicinity of thunderstorms
38
Q

External Light Usage

A
  1. Do not illuminate RECOG TAXI LTS while aircraft is not moving.
  2. Do not illuminate the landing lights on the ground except for takeoff and landing.