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Limitations Flashcards

Know the limitations for the XL & XLS

1
Q

45 minute IFR reserve fuel

A

XLS. 1037

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2
Q

Minimum fuel for Release

A

XLS. 1935

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3
Q

Hot Spare fuel

A

3800

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4
Q

Emergency fuel

A

900

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5
Q

Minimum Runway length or Release and when you need an ops review

A

3800
Width 50
Dry less than 4500
Wet, contaminated, or DAAP less than 5000

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6
Q

Crosswind

A

24
Contaminated
Width 150 or greater 15
Width 149 or less. 10

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7
Q

Tailwind

A

10 kts

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8
Q

Max Ramp & Taxi weight

A

XLS. 20,400

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9
Q

Max Takeoff

A

XLS. 20,200

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10
Q

Max Landing Waights

A

18,700

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11
Q

Zero Fuel Waight

A

XLS. 15,100

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12
Q

Max Operating Altitudes

A

45,000

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13
Q

Max Takeoff and Landing Alt

A

14,000

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14
Q

Vmo

A

305

Blow 8,000 ft 260

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15
Q

Mmo

A

.75

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16
Q

Turbulent air penetration

A

180

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17
Q

Max Landing gear operating airspeed

A

Down 250

Up. 200

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18
Q

Max tire ground

A

165

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19
Q

Vfe 7°, 15°,& 35°

A

200
200
175

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20
Q

Minimum airspeed for sustained flight in icing

A

160

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21
Q

Vmca. Flaps 7°, 15°, & 35°

A

7° 90
15° 90
35° 92

22
Q

Vmcg

23
Q

Pressurization max differential

24
Q

Pressurization pressure relief valve opening

25
Q

max passenger

A

7 plus 3 lap children seats 3,4, & 10

26
Q

APU starter limitation

A

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

27
Q

APU limitations

A

Start. 20,000 ft
Max operating alt. 30,000 ft
Do not operate
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

28
Q

Autopilot minimum altitudes

A

En route. 1,000
Approach without vertical guidance. 300
ILS Approach. 180

29
Q

Battery limitations for engine start

A

Three start attempts per hour

Generator assisted start 1/3 of a start

30
Q

Minimum voltage for battery start

31
Q

Max GPU voltage

32
Q

Max GPU load

33
Q

Max engine generator load on ground

A

250A up to 4 minutes

34
Q

Max engine generator load in flight

35
Q

Max APU generator load on ground

36
Q

Max APU generator load inflight

37
Q

Fuel total quantity

38
Q

Max Fuel imbalance

A

400 normal

800 emergency

39
Q

Pilot & Static heat limitation

A

2 minutes on the ground unless in icing condition

40
Q

Tail boot limitations

A

Airspeed greater than 150 -35° C

Airspeed less than 150 -40° C

41
Q

Approach Category

A

Cat B

For approaches greater than 120 use Cat C

42
Q

Engine Limitations. N1%

A

100% Takeoff Thrust & max continuous Thrust

102% transient

43
Q

Engine Limitations N2%

A

Takeoff thrust in Max continuous thrust XLS 102.8%

Ground idol minimum XLS 49.3%

Flight idle minimum XLS. 53.2%

Transient. XLS 104%

44
Q

Engine Limitations max ITT

A

Takeoff thrust XLS. 740

Starting. XLS 740

Transient. XLS. 780

45
Q

Takeoff thrust limit

A

AEO 5 minutes

OEI. 10 minutes

46
Q

Oil limitations pressure

A

Take off thrust and Max continuous thrust
XLS. 45-160

Ground idol & Flight idol. XLS 25-160

Transient 20 second. 0

Transient 400 second XLS. 20-250

47
Q

OIL limitation temp

A

Takeoff thrust and Max continuous thrust 10-121.1

Ground and flight idle. -40-121.1

Starting. -40

Transient 400 second XLS 135

48
Q

Max oil consumption

A

XLS 1qt per 8 hours

49
Q

Oil type

A

Turbo oil 2380

50
Q

Starter Limitations

A

Maximum of 3 engine start attempts with 90 second interval May be made in any 30 minute period After the 3rd attempt a 30 minute cooldown period must be applied

51
Q

Thrust Reverser limitations

A

Rest 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

XLS (18 decks)

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