P100 - LIMITATIONS Flashcards

1
Q

What is the maximum GPU voltage required for battery charging?

A

27 V

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2
Q

What is the minimum battery voltage required for Start?

A

24 V

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3
Q

What are the prohibitions associated with the use of the SVS?

A

Use of the SVS as primary information to base decisions and/or plan maneuvers, to navigate, or to avoid terrain, obstacles, or traffic is prohibited.

Prohibited - decisions, plan maneuvers, navigate, terrain, obstacles, traffic

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4
Q

Max generator Load may be exceeded up to 300A when?

A

In-Flight below 34,000 ft

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5
Q

When must the Stall Warning Protection Systems be tested?

A

Prior to Each flight

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6
Q

When should the Hydraulic System pre charge pressure be checked?

A

At each 15 consecutive calendar days or before next flight, whichever occurs last.

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7
Q

Max Takeoff and Landing tailwind component

A

10 Kts

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8
Q

Baggage Loading

A

Forward Baggage - 66
RH Forward Cabinet - 55
LH Aft Cabinet - 33
Aft Baggage Compartment - 353

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9
Q

For air conditioning system operation in ground

A

GPU must be used or both generators must be turned ON

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10
Q

Runway slope

Type of runway surface

A

-2% to +2%

Paved

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11
Q

What is the normal maximum speed at which the airplane can be flown with the Landing Gear extended and locked (Vle)

A

275 KIAS

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12
Q

In the event of Emergency Descent, at which speed can Landing Gear be extended?

A

250 KIAS

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13
Q

What is the normal maximum speed at which the Landing Gear can be safely extended and retracted (Vlo)

A

180 KIAS

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14
Q

What is the Minimum Control Speed (Vmc) for takeoff

A

97 KIAS

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15
Q

What is the Minimum Control Speed (Vmc) for landing with NO ICING CONDITIONS

A

86 KIAS

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16
Q

What is the Minimum Control Speed (Vmc) for landing with ICING CONDITIONS

A

97 KIAS

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17
Q

What is the Operating Maneuvering Speed Vo

A

186 KIAS

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18
Q

Maximum Altitude for Flap extended:

Yaw Damper Operative

Yaw Damper not Operative

A

15,000 ft

12,000 ft

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19
Q

When must the yaw damper be engaged?

A

Above 25,000 and above 250 KIAS

20
Q

Flap Extended Speed (Vfe)

Flaps 1, 2, 3, Full

A

Flaps 1 - 200 KIAS
Flaps 2 - 160 KIAS
Flaps 3 - 160 KIAS
FULL. - 145 KIAS

21
Q

Max Tire Ground Speed

22
Q

Load Factor Limit with Flaps UP

Load Factor Limit with Flaps Down (1, 2, 3, Full)

A
  1. 27 g

2. 0 g

23
Q

Max number of Adult Passengers in standard seating configuration

24
Q

Cool-down time between engine starter motoring?

A

60 seconds
60 seconds
15 minutes
30 minutes

Wait an additional 30 min before restarting the sequence

25
Activate ALL AVAILABLE ice protection systems?
At first sign of ice formation or if SAT (TAT in flight) is below 5C with visible moisture WSHLD 1/2 - ON ENG 1/2 - ON Stab - ON
26
Activate the ENGINE ice protection system?
If SAT (TAT in flight) is between 5C and 10C with visible moisture: ENG 1/2 - ON Stab - OFF WSHLD - OFF
27
Minimum Temperature for Wing/Stabilizer Deice System Operation
-40C
28
Minimum Airspeed (AEO, Flap ZERO and Gear UP)
160 KIAS
29
Max Differential Pressure Max Differential Overpressure Max Differential Negative Pressure Maximum Differential Pressure for Takeoff and Landing
Max press 8.3 Max diff 8.6 Max Neg -0.4 Max TO/Land 0.2
30
Maximum generator load on Ground
250 Amps each
31
Minimum Autopilot engagement height: Single Engine Dual Engine
Single engine 1000 ft Dual engine 500 ft
32
When must Fuel Transfer Button be pushed out?
During Takeoff, Landing , Maneuvers, and Turbulence
33
Min Fuel temperature Max Fuel temperature on ground Max Fuel temperature in flight
Min temp -37C Max on ground 52C Max in flight 80C
34
Maximum imbalance
220 lbs
35
Max usable quantity per tank Unusable quantity per tank
Max usable 1403 lbs Unusable 22 lbs
36
Max Ramp Max Takeoff Max Landing Max Zero Fuel
Max Ramp 10626 lbs Max Takeoff 10582 lbs Max Landing 9877 lbs Max Zero Fuel 8885 lbs
37
Minimum Autopilot use height
195 ft
38
Operational Limits: | Maximum
``` TL @ 10mins Max ITT @ 845 N1 @ 100 N2 @ 100.4 OIL PRES @ NA OIL TEMP @ NA ```
39
Operational Limits: | Takeoff
``` TL @ 5mins Max ITT @ 830 N1 @ 100 N2 @ 100.4 OIL PRES @ 170 OIL TEMP @ 14-130 ```
40
Operational Limits: | Max Continuous/Climb
``` TL @ NA (Although not for continued use) Max ITT @ 830 N1 @ 100 N2 @ 100.4 OIL PRES @ 170 OIL TEMP @ 14-130 ```
41
Operational Limits: | Starting
``` TL @ NA Max ITT @ 830 but may be exceeded upto 5secs (892/950depending on pre/post mod) N1 @ NA N2 @ NA OIL PRES 0-270 OIL TEMP 0-40 ```
42
Operational Limits: | Transient 1 and 2
``` TRANS 1 TL @ 20secs Max ITT @ 830 N1 @ 101 N2 @ 102 OIL PRES @ May be exceeded unto 250psig during 500secs.... OIL TEMP @ NA ``` ``` TRANS 2 TL @ 90secs Max ITT @ NA N1 @ NA N2 @ NA OIL PRES @ May be exceeded unto 250psig during 500secs OIL TEMP @ 130-141 ```
43
What is the limitation regarding contaminated aircraft surfaces
Takeoff is prohibited with frost, ice, snow or slush adhering to wings, control surfaces, engine inlets, or other critical surfaces.
44
In what environmental condition is flight prohibited?
Intentional flight in freezing drizzle or freezing rain is prohibited The pilot must immediately exit the freezing rain or freezing drizzle conditions by changing altitude or course.
45
What are the limitations regarding use of the Autopilot in icing conditions.
Autopilot use is prohibited in the following conditions: Severe Icing Unusual control force or control deflection, or unusually large control forces to move flight controls when autopilot is disconnected Indications of frequent autopilot re-trimming during straight and level flight