Phenom 300 Limitations Flashcards

1
Q

Maximum Ramp Weight (MRW)

A

18497lb

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2
Q

Maximum Takeoff Weight (MTOW)

A

18387lb

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3
Q

Maximum Landing Weight (MLW)

A

17042lb

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4
Q

Maximum Zero Fuel Weight (MZFW)

A

14220lb

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5
Q

Baggage Loading LH Forward Cabinet

A

44lb

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6
Q

Baggage Loading Lavatory Cabinet

A

33lb

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7
Q

Baggage Loading Aft Baggage Compartment

A

463lb

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8
Q

Baggage Loading Forward Baggage Compartment

A

110lb

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9
Q

Baggage Loading Refreshment Center

A

71lb

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10
Q

Maximum Takeoff and Landing Tailwind

A

10kt

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11
Q

Minimum Voltage for Engine Start

A

24V

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12
Q

Minimum GPU Voltage for battery charging

A

27V

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13
Q

Maximum Generator Load

A

On Ground: 330A Each
In Flight: 390A Each

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14
Q

Maximum usable quantity fuel per tank

A

2676.6lb

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15
Q

Unusable quantity fuel per tank

A

25.13lb

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16
Q

Fuel tank temperature

A

Minimum: -37C
Maximum: 52C
In flight: 80C

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17
Q

Crossfeed valve operation

A

Feed knob must be set to OFF during takeoff and landing

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18
Q

Motoring Limitations

A

Motoring Number: 1
Cool down time: 60 seconds
Motoring Number: 2
Cool down time: 60 seconds
Motoring Number: 3
Cool down time: 15 minutes
Motoring Number: 4
Could down time: 30 minutes

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19
Q

Maximum Takeoff and Landing Altitude

A

10000 ft in icing
14000 ft otherwise
Above 8300 ft gotta wear a mask up to 25000 ft

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20
Q

Maximum Altitude for Operations

A

AEO - 45000 ft
OEI - 15000 ft

21
Q

Minimum Temperature for Landing

A

-38 C

22
Q

Minimum Airspeed in Icing

A

WINGSTAB INHB (flap and gear up) 165 KIAS
WINGSTAB ARM (flap and gear up) 165 KIAS
WINGSTAB ON (flap and gear up) 150 KIAS

23
Q

For air conditioning system operation on ground

A

the GPU must be used or one engine generator must be turned on

24
Q

Maximum Cabin Differential Pressure

A

9.4 psi

25
Q

Maximum Cabin Differential Overpressure

A

9.6 psi

26
Q

Maximum Cabin Differential Negative Pressure

A

-0.3 psi

27
Q

Maximum Cabin Differential for Takeoff and Landing

A

0.2 psi

28
Q

VLO

A

250 kts

29
Q

VLE

A

250 kts

30
Q

VFE

A

Flaps 1: 180 kts
Flaps 2: 170 kts
Flaps 3: 170 kts
Flaps full: 160 kts

31
Q

Maximum Altitude for Flaps Extended

A

18000 ft

32
Q

Maximum Tailwind for Steep Approach Mode

A

5 kts

33
Q

AP Minimum Engagement Height (all engines)

A

600 ft AGL

34
Q

AP Minimum Engagement Height (one engine)

A

1000 ft AGL

35
Q

AP Minimum Use Height (all engines)

A

195 ft AGL

36
Q

AP Minimum Use Height (one engine)

A

220 ft AGl

37
Q

Altitude Loss (maneuvering/cruise)

A

160 ft

38
Q

Maximum Crosswind Takeoff

A

Dry Runway
Static: 18
Rolling: 25 kts
Wet/Contaminated Runway
Runway<150’: 10
Runway>150’: 15

39
Q

Maximum Crosswind Landing

A

28 kts

40
Q

Turbulent air penetration speed VRA/MRA

A

232/.65

41
Q

Maneuvering airspeed VA

A

205

42
Q

Maximum tire ground airspeed

A

182

43
Q

Minimum Airspeed in Icing (yaw damper off)

A

180

44
Q

Minimum Control Speed VMC

A

Takeoff 97
Landing (no icing conditions) 91
Landing (icing conditions) 95

45
Q

Battery temperature limit starting w/out a GPU

A

-18 c

46
Q

Vmo/Mmo

A

320/.78

47
Q

IFR Fuel Reserve

A

1121 lbs

48
Q

Engine Temp Limitations

A