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Phenom300 > Limitations > Flashcards

Limitations Flashcards

1
Q

What is Max Ramp Weight?

A

18,078 pounds

8200 kg

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2
Q

Max TO Weight

A

17,968 lbs

8,150 kg

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3
Q

Max Landing weight

A

16,865 lbs

7,650 kg

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4
Q

Max zero fuel weight

A

13,999 lbs

6,350

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5
Q

V LO

V LE

A

250 KIAS

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6
Q

V MC

For takeoff with takeoff flaps

A

97 KIAS

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7
Q

V MC

For landing with landing flaps

No Icing Conditions

A

91 KIAS

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8
Q

V MC

For landing with landing flaps in Icing Conditions

A

95 KIAS

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9
Q

Operating Maneuvering Speed

V O

A

205 KIAS

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10
Q

Max Flap Extended Speeds

V FE

A

Flap 1 180 KIAS

Flap 2 170 KIAS

Flap 3 170 KIAS

Flap full 160 KIAS

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11
Q

Max Altitude for Flaps Extended

A

18,000 ft

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12
Q

Max Tire Ground Speed

A

182 knots

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13
Q

Runway slope

Type surface

A

-2% to +2%

Paved

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14
Q

Load factor limit flaps up

A

3.00 g

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15
Q

Load factor limit flaps down

A

1,2,3 and full

2.00 g

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16
Q

Baggage Loading

A

LH forward cabinet - 44 lb (20kg)

Lab cabinet - 33 lb (15kg)

Aft baggage - 463 lb (210kg)

Forward baggage - 110 lb (50kg)

Refreshments - 71 lb (32kg)

Side stowage - 36 lb (16.5kg)

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17
Q

Max takeoff and landing tailwind component

A

10 knots

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18
Q

Max crosswind component allowed to apply static takeoff power

A

18 knots

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19
Q

Hydraulic system accumulator pre-charge check interval

A

15 consecutive calendar days or before the next flight, whichever occurs last

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20
Q

Stall warning and protection system must be tested

A

Prior to each flight

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21
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

22
Q

Minimum battery voltage for start

A

24V

23
Q

Minimum GPU voltage required for battery charging

A

27V

24
Q

Max generator load on ground

A

330 amps each

25
Q

Max generator load in flight

A

390 amps each

26
Q

Max useable fuel per tank

A

FAA 399.4 Gal (2,676 lbs)

ANAC/EASA - 1,512 L (1,214 kg)

27
Q

Unusable fuel per tank

A

FAA - 3.75 US Gal (25.13 lbs)

ANAC/EASA - 14 L (11kg)

28
Q

Max fuel capacity

A

FAA - 806.2 US Gal (5,401 lbs)

ANAC/EASA - 3,052 L (2,450 Kg)

29
Q

Max fuel imbalance

A

FAA - 33 US Gal (220 lbs)

ANAC/EASA - 125 L (100kg)

30
Q

Min fuel tank temperature

A

-37 C

31
Q

Max fuel tank temperature on the ground

A

52 C

Can be exceeded up to 80 C in flight

32
Q

Position of fuel xfeed during takeoff and landing

A

OFF

33
Q

Max thrust operating limits

A

Max Thrust: 10 minutes

Max ITT: 725 C

N2: 101 %

N1: 100 %

Oil pressure: 45-160

Oil temperature: 10-132.2 C

34
Q

Takeoff operating limits:

A

Thrust: 5 minutes

Max ITT: 700

N2: 101%

N1: 100%

Oil Pressure: 45-160

Oil Temperature: 10-132.2 C

35
Q

Max ITT for max continuous thrust and max climb thrust

A

680 C

36
Q

Ground idle operating limits

A

N2: 55.1% (OEI)
51.2% (AEO)

Oil pressure: 25-160

Oil temperature: -40-132.2C

37
Q

Flight idle operating limits

A

N2: 55.1%

Oil pressure 25-160

38
Q

Engine start operating limits

A

Time: 5 seconds

ITT MAX: 765 C

Oil Temperature: -40 C

39
Q

Transient operating limits 20 seconds

A

ITT: 765

N2: 103

N1: 102

Oil pressure: 0-20

40
Q

Transient limits 200 seconds

A

Max Oil Temperature 140.5

41
Q

Transient limits 400 seconds

A

Oil pressure 20-270

42
Q

Starter limit motoring attempt cool down times:

A

1st: 60 seconds
2nd: 60 seconds
3rd: 15 minutes
4th: 30 minutes

43
Q

Air conditioning

A

For operation on ground the GPU must be used or one engine must be turned on.

44
Q

Pressurization (PSI)

A

Max differential: 9.4

Max diff over pressure: 9.6

Max diff negative pressure: -0.3

Max diff T.O. + L. 0.2

45
Q

When must the crew activate the ice and rain protection system?

A

When icing conditions exist or are anticipated as per section 3 Normal Proceedures.

46
Q

Define “when icing conditions exist or are anticipated “.

A

1). Whenever the SAT on the ground or for takeoff, or TAT in flight, is 10C or below and visible moisture in any form is present. (Clouds, fig, vis 1 mi or less, ice, standing water or slush)

47
Q

Operating in icing conditions

A

Max altitude for T.O. + L: 10,000 ft

Min. airspeed gear + flaps up:

Wing and stabilizer anti-ice inhibited or armed 165 KIAS

Wing and stabilizer anti-ice uninhibited
150 KIAS

48
Q

What I the limitation regarding contaminated aircraft surfaces?

A

Takeoff is prohibited with frost (polished or not), ice, snow or slush adhering to wings, control surfaces , engine inlets, or other control surfaces.

49
Q

In what environmental condition is flight prohibited?

A

Flight in freezing drizzle or freezing rain is prohibited.

The pilot must immediately exit the freezing rain or freezing drizzle by changing altitude or course.

50
Q

What are the limitations regarding use of the autopilot in icing conditions?

A

Autopilot use is prohibited in the following conditions:

1) . Severe icing
2) . Unusual control force or control deflection, or unusually large control forces to move flight controls when the the autopilot is disconnected.
3) . Indications of frequent autopilot re-trimming during straight and level flight.

51
Q

When must the wing inspection light be operative?

A

Prior to flight into known or forecast icing conditions, at night.

52
Q

Autopilot/Yaw Damper Limitations

A

Min. Engagement Height (2 engine): 600 ft.

Min. Engagement Height ( 1 engine): 1,000 ft.

Min. Use Height (2 engine): 195 ft

Min. Use Height (1 engine): 220 ft

Altitude loss (maneuvering/cruise): 160 ft

Yaw damper airspeed is limited to 180 KIAS if in icing conditions.

Phenom300 (3 decks)

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