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Phenom 100 Study Guide 2015 recurrent > P300 Limitations > Flashcards

P300 Limitations Flashcards

1
Q

Aircraft Weights

Max Ramp,
Max Takeoff,
Max Landing,
Max Zero Fuel

A

MRW 18497
MTOW 18387
MLW 17042
MZFW 14220

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2
Q

MAX Landing Gear Extension (VLO)

A

250 kts

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3
Q

Max speed at which the airplane can be flown with Landing Gear extended and locked. (VLE)

A

250 kts

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4
Q

Min Control Speed (VMC) for takeoff (takeoff flaps).

A

97 kts

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5
Q

VMC Landing - No Icing Conditions

A

91 kts

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6
Q

VMC Landing - Icing Conditions

A

95 kts

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7
Q

Operating Maneuvering Speed (Vo)

A

205 kts

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8
Q

Max Flaps Extended Speed.

Flap 1,2,3,FF

A

F1 - 180 kts, F2 - 170 kts, F3 - 170 kts, FF - 160 kts

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9
Q

Max altitude with flaps extended.

A

18,000 ft

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10
Q

Max Tire Groundspeed

A

182 kts

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11
Q

Runway Slope:

Type of runway surface:

A

-2 to +2 percent

Paved

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12
Q

Load Factor Limit with Flaps UP

A

3.00 g

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13
Q

Load Factor Limit with Flaps DOWN (1,2,3, FF)

A

2.00 g

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14
Q

Baggage Loading:

Forward,
LH Forward,
Side Facing Divan,
Refreshment Center,
LAV Cabinet,
AFT Baggage
A

FB 110
LH CAB 44
Side Divan 36
Refreshment 71
LAV 33
AFT 463

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15
Q

Max takeoff and landing tailwind

Max Crosswind component to apply static takeoff power

A

10 kt tailwind

18 kt crosswind

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16
Q

Hydraulic system pre-charge check interval

A

15 consecutive calendar days or before next flight, which ever occurs last

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17
Q

Stall Warning and Protection System must be tested:

A

Prior to each flight

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18
Q

Prohibitions associated with the use of the SVS

A

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

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19
Q

Min battery voltage for engine start

A

24 V

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20
Q

Min GPU voltage required for battery charging

A

27 V

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21
Q

Max generator load on Ground

A

330 Amps each

22
Q

Max generator load in Flight

A

390 Amps each

23
Q

Max usable fuel quantity per tank

A

2676 lbs

24
Q

Unusable fuel quantity per tank

A

25.13 lbs

25
Q

Max fuel capacity

A

5401 lbs

26
Q

Max permitted imbalance between tanks

A

220 lbs

27
Q

Min fuel tank temperature

A

-37 C

28
Q

Max fuel temperature on ground

A

52 C

note: Max fuel temp can be exceeded up to 80 C in flight

29
Q

Position of XFEED knob during Takeoff and Landing

A

OFF

30
Q

Operating Limits MAX Thrust

A

TL 10 min
Max ITT 725
N1 100
N2 101
Oil Press 45 to 160
Oil Temp 10 to 132.2

31
Q

Operating Limits Takeoff

A

TL 5 min
ITT 700
N1 100
N2 101
Oil Press 45 to 160
Oil Temp 10 to 132.2

32
Q

Operating Limit Max Continuous

A

TL na
ITT 680
N1 100
N2 101
Oil Press 45 to 160
Oil Temp 10 to 132.2

33
Q

Operating Limit Max Climb

A

TL na
ITT 680
N1 100
N2 101
Oil Press 45 to 160
Oil Temp 10 to 132.2

34
Q

Operating Limit Ground Idle

A

TL na
ITT na
N1 -
N2 min 55.1 (OEI)
51.2 (AEO)
Oil Press 25 to 160
Oil Temp. -40 to 132.2

35
Q

Operating Limit Flight Idle

A

TL na
ITT na
N1 -
N2 55.1
Oil Press 25 to 160
Oil Temp -

36
Q

Operating Limit Starting

A

TL 5 sec
ITT 765
N1 -
N2 -
Oil Press -
Oil Temp -40 min

37
Q

Operating Limits Transient 20 Seconds

A

TL 20 sec
ITT 765
N1 102
N2 103
Oil Press 0-20
Oil Temp -

38
Q

Operating Limits Transient 200 Seconds

A

TL 200 seconds
ITT -
N1 -
N2 -
Oil Press -
Oil Temp 140.5 max

39
Q

Operating Limits Transient 400 Seconds

A

TL -
N1 -
N2 -
Oil Press 20-270
Oil Temp -

40
Q

Starter Limits

A

1st 60 sec
2nd 60 sec
3rd 15 min
4th 30 min

Note: After fourth sequential motoring, cycle may be repeated following a 30 minute cool-down period.

41
Q

Air Conditioning operation on the ground

A

GPU must be used or ONE engine generator must be turned on.

42
Q

Pressurization:

Max Diff,
Max Diff Overpressure,
Max Negative Pressure,
Max Diff for TO and Landing

A

Max Diff 9.4 psi
Max Over 9.6 psi
Max Neg -0.3 psi
Max TO/Land 0.2 psi

43
Q

Ice and Rain Protection

When must the crew activate the Ice Protection System

A

When icing conditions exist or are anticipated. As per Section 3, Normal Procedures

44
Q

Operation in Icing Conditions:

Max TO and Land Altitude

Min Airspeed (flap and gear up):
Wing and Stab Anti-Ice inhibited
Wing and Stab Anti-Ice armed
Wing and Stab Anti-Ice Uninhibited

A

10000 ft

165 kias
165 kias
150 kias

45
Q

Wing Inspection Light

When must the Wing Inspection Light be operative

A

Prior to flight into known or forecast Icing conditions at night.

46
Q

Auto Pilot / Yaw Damper

Min Engagement Height (Dual Engine)

(Single Engine)

A

600 ft AGL

1000 ft AGL

47
Q

Auto Pilot / Yaw Damper

Min Use Height (Dual Engine)

Min Use Height (Single Engine)

A

195 ft AGL

220 ft AGL

48
Q

Autopilot / Yaw Damper

Altitude Loss (maneuvering / cruise)

Yaw Damper OFF is limited to XXX kts if in Icing conditions.

A

160 ft

180 kias

49
Q

Define: When icing conditions exist or are anticipated

A

SAT on ground or takeoff or TAT in flight is 10C or below and visible moisture in any form is present (clouds, fog, vis 1 mile or less, rain, snow, sleet or ice crystals)

SAT on ground 10C or below and ramps, taxiways are contaminated with snow, ice, standing water, or slush

50
Q

What is the limitation regarding contaminated surfaces

A

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

51
Q

In what environmental condition is flight prohibited

A

Freezing rain or drizzle

Pilot must immediately exit the freezing rain or freeze drizzle conditions by changing altitude or course

52
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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