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Phenom 100 Study Guide 2015 recurrent > P100 - LIMITATIONS > Flashcards

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

A

139 Kts

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

A

5

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
Q

Activate ALL AVAILABLE ice protection systems?

A

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
Q

Activate the ENGINE ice protection system?

A

If SAT (TAT in flight) is between 5C and 10C with visible moisture:

ENG 1/2 - ON
Stab - OFF
WSHLD - OFF

27
Q

Minimum Temperature for Wing/Stabilizer Deice System Operation

A

-40C

28
Q

Minimum Airspeed (AEO, Flap ZERO and Gear UP)

A

160 KIAS

29
Q

Max Differential Pressure
Max Differential Overpressure
Max Differential Negative Pressure
Maximum Differential Pressure for Takeoff and Landing

A

Max press 8.3
Max diff 8.6
Max Neg -0.4
Max TO/Land 0.2

30
Q

Maximum generator load on Ground

A

250 Amps each

31
Q

Minimum Autopilot engagement height:

Single Engine

Dual Engine

A

Single engine 1000 ft

Dual engine 500 ft

32
Q

When must Fuel Transfer Button be pushed out?

A

During Takeoff, Landing , Maneuvers, and Turbulence

33
Q

Min Fuel temperature

Max Fuel temperature on ground

Max Fuel temperature in flight

A

Min temp -37C

Max on ground 52C

Max in flight 80C

34
Q

Maximum imbalance

A

220 lbs

35
Q

Max usable quantity per tank

Unusable quantity per tank

A

Max usable 1403 lbs

Unusable 22 lbs

36
Q

Max Ramp
Max Takeoff
Max Landing
Max Zero Fuel

A

Max Ramp 10626 lbs
Max Takeoff 10582 lbs
Max Landing 9877 lbs
Max Zero Fuel 8885 lbs

37
Q

Minimum Autopilot use height

A

195 ft

38
Q

Operational Limits:

Maximum

A 
TL @ 10mins
Max ITT @ 845
N1 @ 100
N2 @ 100.4
OIL PRES @ NA
OIL TEMP @ NA
39
Q

Operational Limits:

Takeoff

A 
TL @ 5mins
Max ITT @ 830
N1 @ 100
N2 @ 100.4
OIL PRES @ 170
OIL TEMP @ 14-130
40
Q

Operational Limits:

Max Continuous/Climb

A 
TL @ NA (Although not for continued use)
Max ITT @ 830
N1 @ 100
N2 @ 100.4
OIL PRES @ 170
OIL TEMP @ 14-130
41
Q

Operational Limits:

Starting

A 
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
Q

Operational Limits:

Transient 1 and 2

A 
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
Q

What is the limitation regarding contaminated aircraft surfaces

A

Takeoff is prohibited with frost, ice, snow or slush adhering to wings, control surfaces, engine inlets, or other critical surfaces.

44
Q

In what environmental condition is flight prohibited?

A

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
Q

What are the limitations regarding use of the Autopilot in icing conditions.

A

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

Phenom 100 Study Guide 2015 recurrent (9 decks)

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