Limitations - RED Items Flashcards

Know the limitations for the XL & XLS

1
Q

Hot Spare Fuel

A

4500 lbs

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2
Q

Inclement Weather Fuel

A

4500 lbs

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3
Q

Minimum Runway length for release and when you need an ops review:

A
  • 3800 Minimum

Ops Review When:

  • Contaminated less than 5000
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4
Q

Minimum Runway Width

A

60’ | 75’ if WET or T/R credit used

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5
Q

Crosswind Limits

A
  • Dry or Wet: 24
  • Contaminated
    • Width 150 or greater: 15
    • Width 149 or less: 10
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6
Q

Tailwind Limit

A

10 kts

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7
Q

Max Ramp & Taxi weight

A

20,400 lbs

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8
Q

Max Takeoff Weight

A

20,200 lbs

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9
Q

Max Landing Weight

A

18,700 lbs

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10
Q

Zero Fuel Weight

A

15,100 lbs

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11
Q

Max Operating Altitude

A

45,000’

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12
Q

Max Takeoff and Landing Alt

A

14,000’

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13
Q

Vmo

A
  • 305 kts
  • 260 kts below 8,000 ft
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14
Q

Mmo

A

M .75

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15
Q

Turbulent air penetration speed

A

180 kts

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16
Q

Max Landing gear operating airspeed

A
  • Down: 250 kts
  • Up: 200 kts
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17
Q

Max tire ground

A

165 kts

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18
Q

Vfe 7°, 15° & 35°

A
  • 7°: 200 kts
  • 15°: 200 kts
  • 35°: 175 kts
19
Q

Minimum airspeed for sustained flight in icing

A

160 kts

20
Q

APU starter limitation

A

3 start attempts in any 30 minute period with 90 seconds cooling between each attempt.

21
Q

Max altitude to start APU:

A

20,000’

22
Q

Max altitude to operate the APU:

A

30,000’

23
Q

Do not operate APU when:

A
  • When aircraft is unattended
  • During ground de/anti-icing procedures
  • If APU TEST has failed
  • Do not attempt to start the APU after dual Gen failure
  • Following any APU Shutdown do not attempt restart until 30 sec after APU is at 0% rpm
24
Q

Autopilot minimum altitudes

A
  • En route. 1,000
  • Approach without vertical guidance. 300
  • ILS Approach. 180
25
Q

Battery limitations for engine start

A
  • Three start attempts per hour
  • Generator assisted start = 1/3 of a start
26
Q

Minimum voltage for battery start

A

24V

27
Q

Max GPU Voltage

A

28V

28
Q

Max GPU load

A

1,000A

29
Q

Max engine generator load on ground

A

250A up to 4 minutes

30
Q

Max engine generator load in flight

A

300A

31
Q

Max APU generator load on ground

A

200A

32
Q

Max APU generator load inflight

A

230A

33
Q

Fuel total quantity

A

6,790 lbs

1,006 gallons

34
Q

Max Fuel Imbalance

A
  • Normal: 400 lbs
  • Emergency: 800 lbs
35
Q

Pitot & Static heat limitation

A

2 minutes on the ground unless in icing condition

36
Q

Tail boot limitations

A
  • Airspeed greater than 150: -35° C
  • Airspeed less than 150: -40° C
37
Q

Approach Category

A

Cat B. For approaches greater than 120 use Cat C

38
Q

Engine Limitations max ITT

A
  • Takeoff thrust: 740
  • Starting: 740
  • Transient: 780 (20 secs)

[ITT >670 deg for >7 seconds will require engine inspection, per AFM]

39
Q

Takeoff thrust limit

A
  • AEO - 5 minutes
  • OEI - 10 minutes
40
Q

Max oil consumption

A

1 qt per 8 hours

41
Q

Starter Limitations

A
  • Maximum of 3 engine start attempts in a 30 minute period with a 90 second rest in between.
  • After the 3rd attempt a 30 minute cooldown period must be applied
42
Q

Thrust Reverser limitations

A
  • Thrust reverser must be idle before 60 kts
  • Deployment is limited to 3 minutes in any 10 minute period
  • When APU is operating do not use reverse thrust longer than 30 seconds
  • Do not use reverse thrust when conducting touch and goes
  • Do not use reverse thrust to back the aircraft
43
Q

Emergency Fuel

A

900 lbs