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Phenom 300 > Limitations > Flashcards

Limitations Flashcards

1
Q

Vlo / Vle

A

250 KIAS

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2
Q

Takeoff Vmc

A

97 KIAS

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3
Q

Landing Vmc (No icing)

A

91 KIAS

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4
Q

Landing Vmc (icing)

A

95 KIAS

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5
Q

Mmo

A

0.78M

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6
Q

Vo

A

205 KIAS

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7
Q

Vfe Flaps 1

A

180 KIAS

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8
Q

Vfe Flaps 2&3

A

170 KIAS

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9
Q

Vfe Flaps FULL

A

160 KIAS

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10
Q

Maximum Tire Speed

A

182 KT

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11
Q

Min Mach for SAT -56C to -60C

A

0.40M

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12
Q

Min Mach for SAT -61C to -65C

A

0.55M

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13
Q

Min Mach for SAT -66C to -70C

A

0.67M

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14
Q

Max Ramp Weight (Pre-mod)

A

18,078

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15
Q

Max Takeoff Weight (Pre-mod)

A

17,968

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16
Q

Max Landing Weight (Pre-mod)

A

16,865

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17
Q

Max Zero Fuel Weight (Pre-mod)

A

13,999

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18
Q

Max Ramp Weight (Post-mod)

A

18,497

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19
Q

Max Takeoff Weight (Post-mod)

A

18,387

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20
Q

Max Landing Weight (Post-mod)

A

17,042

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21
Q

Max Zero Fuel Weight (Post-mod)

A

14,220

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22
Q

Min Battery Voltage for start

A

24V

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23
Q

Min GPU Voltage for Batt Charge

A

27V

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24
Q

Generator Load on Ground

A

330A Each

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25
Q

Generator Load in Flight

A

390A Each

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26
Q

Maximum Fuel Capacity

A

5401 Lbs

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27
Q

Maximum Usable Fuel Capacity

A

5,352 lbs

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28
Q

Max Usable Fuel per tank

A

2,676 lbs

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29
Q

Unusable Fuel per tank

A

24.2 lbs

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30
Q

Max fuel imbalance

A

220 lbs

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31
Q

Minimum Fuel Temp

A

-37C

32
Q

Max Fuel Temp (Ground)

A

52C

33
Q

Max Fuel Temp (Flight)

A

80C

34
Q

Crossfeed Operation

A

OFF for Takeoff/Landing

35
Q

Inop Jet Pump Unusable Increase

A

44lbs

36
Q

Max differential Pressure

A

9.4 psid

37
Q

Max differential Overpressure

A

9.6 psid

38
Q

Max differential T/L

A

0.2 psid

39
Q

Max negative differential

A

-0.3 psid

40
Q

(ICING Conditions)

Max T/O & Landing PA

A

10,000 ft

41
Q

(ICING Conditions)

Max Cruise Alt OEI

A

15,000 ft

42
Q

(ICING Conditions)

Min Temp for landing

A

-38C

43
Q

(ICING Conditions)

Min Airspeed WHSAIS Inhibited

A

165 KIAS

44
Q

(ICING Conditions)

Min Airspeed WHSAIS Un-Inhibited

A

150 KIAS

45
Q

Starter Limits

A

Motoring Number Cool-Down Time
1 1 minute
2 1 minute
3 15 minutes
4 30 minutes

46
Q

Starting ITT (5 sec)

A

765C

47
Q

Max ITT (10 Min SE in ICE)

A

725C

48
Q

Takeoff ITT (5 min)

A

700C

49
Q

Max Continuous ITT

A

680C

50
Q

Transient ITT (20 sec)

A

765C

51
Q

Max N1 (10 min SE in ICE)

A

100%

52
Q

Takeoff N1 (5 min)

A

100%

53
Q

Max Continuous N1

A

100%

54
Q

Transient N1 (20 sec)

A

102%

55
Q

Max N2 (5 min SE in ICE)

A

101%

56
Q

Takeoff N2 (5 min)

A

101%

57
Q

Max Continuous N2

A

101%

58
Q

Min Ground Idle N2

A

55.1%

59
Q

Transient N2 (20 sec)

A

103%

60
Q

Forward Baggage Compartment Weight Limit

A

110lb

61
Q

Aft Baggage Compartment Weight Limit

A

463 lbs

62
Q

Forward Baggage Compartment Load Limit

A

22.1 lb/sq ft

63
Q

Aft baggage Load limit

A

70 lb/sq ft

64
Q

Autopilot

Minimum Engage Height (2 ENG)

A

600 ft AGL

65
Q

Autopilot

Minimum Engage Height (1 ENG)

A

1000 ft AGL

66
Q

Autopilot

Minimum Use Height (2 ENG)

A

195 ft AGL

67
Q

Autopilot

Minimum Use Height (1 ENG)

A

220 ft AGL

68
Q

Max Cruise Altitude

A

45,000 ft

69
Q

Max ALT for Flap Extended

A

18,000 ft

70
Q

Max ALT for T/O & Landing

A

14,000 ft PA

71
Q

Load Factors Flaps 0

A

3.00g

72
Q

Load Factors Flaps 1,2,3,Full

A

2.00g

73
Q

Runway Slope

A

+2.0%, -2.0%

74
Q

Max Tailwind Component

A

10 kts

75
Q

Max Crosswind for static T/O

A

18 kts

76
Q

Min Temp for T/O & Landing

A

-40C

77
Q

Max ISA Deviation

A

ISA+35C

Phenom 300 (2 decks)

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