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
max passenger
7 plus 3 lap children seats 3,4, & 10
26
APU starter limitation
3 start attempts with 90 seconds cooling between each attempt in any 30 minute period
27
APU limitations
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
Autopilot minimum altitudes
En route. 1,000 Approach without vertical guidance. 300 ILS Approach. 180
29
Battery limitations for engine start
Three start attempts per hour | Generator assisted start 1/3 of a start
30
Minimum voltage for battery start
24V
31
Max GPU voltage
28V
32
Max GPU load
1,000A
33
Max engine generator load on ground
250A up to 4 minutes
34
Max engine generator load in flight
300A
35
Max APU generator load on ground
200A
36
Max APU generator load inflight
230A
37
Fuel total quantity
6790
38
Max Fuel imbalance
400 normal | 800 emergency
39
Pilot & Static heat limitation
2 minutes on the ground unless in icing condition
40
Tail boot limitations
Airspeed greater than 150 -35° C | Airspeed less than 150 -40° C
41
Approach Category
Cat B | For approaches greater than 120 use Cat C
42
Engine Limitations. N1%
100% Takeoff Thrust & max continuous Thrust 102% transient
43
Engine Limitations N2%
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
Engine Limitations max ITT
Takeoff thrust XLS. 740 Starting. XLS 740 Transient. XLS. 780
45
Takeoff thrust limit
AEO 5 minutes | OEI. 10 minutes
46
Oil limitations pressure
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
OIL limitation temp
Takeoff thrust and Max continuous thrust 10-121.1 Ground and flight idle. -40-121.1 Starting. -40 Transient 400 second XLS 135
48
Max oil consumption
XLS 1qt per 8 hours
49
Oil type
Turbo oil 2380
50
Starter Limitations
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
Thrust Reverser limitations
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