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Prefect ESK > Limitations > Flashcards

Limitations Flashcards

1
Q

Max operating speed ‘Vmo’?

A

238 KIAS

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2
Q

Max operating Mach number ‘Mmo’?

A

0.45MN

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3
Q

Max speed landing gear operation extend ‘VLOE’?

A

182 KIAS

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4
Q

Max speed landing gear extended ‘Vle’?

A

182 KIAS

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5
Q

Max manoeuvre speed aerobatic ‘Vo’?

A

164 KIAS

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6
Q

Max manoeuvre speed utility ‘Vo’ ?

A

143 KIAS

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7
Q

Max speed flaps extended at take-off position ‘Vfe-T/O’?

A

151 KIAS

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8
Q

Max speed landing gear operation retract ‘Vlor’?

A

137 KIAS

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9
Q

Max speed flaps extended beyond take-off position ‘Vfe’?

A

114 KIAS

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10
Q

Max airspeed to apply REVerse Thrust during landing?

A

80 KIAS

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11
Q

Min airspeed to apply REVerse Thrust during landing?

A

40 KIAS

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12
Q

What is the Take-off & Landing crosswind component limitation speed?

A

25 kts

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13
Q

Maximum crosswind for brake-release take-off?

A

20 kts

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14
Q

What speed should flaps be UP in crosswinds greater than?

A

20 kts

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15
Q

Recommended cruise airspeed in Severe Turbulence?

A

140 to 180 KIAS

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16
Q

Max canopy opening speed?

A

110 KIAS

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17
Q

Max speed with canopy open?

A

120 KIAS

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18
Q

When can the canopy be opened in flight?

A

Emergency conditions only

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19
Q

Max Take-off AUM?

A

1515 kg

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20
Q

Max Landing AUM?

A

1515 kg

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21
Q

Max Aerobatics AUM?

A

1440 kg

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22
Q

Max Zero Fuel AUM?

A

1370 kg

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23
Q

Min Flying AUM?

A

1170 kg

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24
Q

Max Baggage Compartment Mass?

A

50 kg

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25
Q

What is the Max Nose Up when the FUEL TANK selector in EMERGENCY TRANSFER?

A

15 Degrees

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26
Q

What is the Max Nose DOWN when the FUEL TANK selector in EMERGENCY TRANSFER?

A

10 Degrees

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27
Q

Aerobatic max positive g limit?

A

+6g

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28
Q

Aerobatic max negative g limit?

A

-4g

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29
Q

Utility max positive g limit?

A

+4.4g

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30
Q

Utility max negative g limit?

A

-1.7g

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31
Q

Flaps down max positive g?

A

+3.8g

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32
Q

Flaps down max negative g?

A

+0g

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33
Q

For aerobatics and spinning the C of G no more than?

A

2732mm aft of datum

34
Q

For aerobatics and spinning fuel selector must be set to?

A

LEFT

35
Q

For aerobatics and spinning Fuel Transfer Pump must…?

A

Not be operating

36
Q

For aerobatics and spinning the Max fuel in either wing tank should not be more than?

A

115 kg

37
Q

For aerobatics and spinning there is a max time of 30 secs for:

A

Pitch attitudes in excess of 45 Degrees nose Up or Down
Inverted Flight
Wing down or knife edge flight (Balanced turns are not considered wing down flight)

38
Q

During aerobatics and spinning if the oil pressure drops below 35 psi what actions should you take?

A

Immediately return to normal erect attitude and select POWER Lever to FI

39
Q

Is flight into known icing conditions prohibited?

A

It is prohibited

40
Q

Max OAT on the ground?

A

+38 C

41
Q

Max OAT?

A

ISA +23 C

42
Q

Min OAT?

A

-54 C

43
Q

Reduced Power Min OAT?

A

ISA -15 C

44
Q

What aircraft settings are required when OAT <4 C in visible moisture of rain?

A

P/S HEAT
COMP Intake

45
Q

For aircraft cold weather operating limitations what must fuel contain and what temperature?

A

FSII & below +4 C

46
Q

Taxy & Landing Lights Limitation?

A

If OAT > +38 C there is a max of 40 mins and a min 30 mins cool time

47
Q

Min battery voltage for engine start?

A

24V

48
Q

What are the engine start attempt limitations?

A

1 attempt - Starter 30 Sec - Cool down 1 min
2 attempt - Starter 30 Sec - Cool down 1 min
3 attempt - Starter 30 Sec - Cool down 30 mins

49
Q

Max Transient TRQ?

A

10 Sec - 115%

50
Q

Max T/O Power TRQ? (5 min at T/O) (cumulative per sortie)

A

111%

51
Q

Max continuous TRQ?

A

92%

52
Q

Max Engine Start TOT? (10 sec over 810 C)

A

927 C

53
Q

Max Transient TOT? (6 sec over 810 C)

A

899 C

54
Q

Max T/O Power TOT? (5 min at T/O) (cumulative per sortie)

A

810 C

55
Q

Max Continuous TOT?

A

752 C

56
Q

Max Transient Limit? ( 15 sec max above 2200)

A

2233 N2

57
Q

Max Continuous Speed? (Propeller Limitations)

A

2200 N2

58
Q

Max Static Ground Ops with Crosswind component >10 kts (This is relevant to the Propeller Overspeed Governor Check)

A

1850 N2`

59
Q

Speed Avoidance Range (Propeller Limitations)

A

1523 - 1786 N2

60
Q

Max Transient N1? (max 15 sec > 105% N1)

A

106% N1

61
Q

Max Continuous N1?

A

105% N1

62
Q

Max Transient? (cold weather / engine start) (Oil Pressure Limitations)

A

150 psi - Beta Range

63
Q

Max? (Oil Pressure Limitations)

A

130 psi

63
Q

Min at N1… 85% to 94%? (Oil Pressure Limitations)

A

90 psi -75 psi

64
Q

Min at N1… > 94%? (Oil Pressure Limitations)

A

120 psi - 105 psi

65
Q

Min at N1… <85%? (Oil Pressure Limitations)

A

50 psi - 35 psi

65
Q

Max limit at TRQ ….. <40%? Oil Temp

A

107 C

66
Q

Max Transient at TRQ > 40%? (5 min) (Oil Temp)

A

107 C

67
Q

Max Continuous at TRQ > 40% (Oil Temp)

A

82 C

68
Q

Min Temp (Oil Temp Limitations)

A

0 C

69
Q

Min Temp Before Starting (Oil Pressure Limitations)

A

-40 C

70
Q

Total Fuel Capacity?

A

282.7 kg

71
Q

LH Collector Tank Capacity?

A

16.8 kg

72
Q

Unusable Fuel Left Wing?

A

6.3 kg

73
Q

Unusable Fuel Right Wing?

A

1.4 kg

74
Q

Usable Fuel?

A

275.0 kg

75
Q

Max Tank Asymmetry?

A

45.3 kg

76
Q

Max Fuel in each wing for Aerobatics?

A

115.0 kg

77
Q

Max Fuel Pressure?

A

25 psi

78
Q

Min Fuel Pressure?

A

12 psi

79
Q

Approximately how long is a normal start cycle before the starter disengages
at 58% N1?

A

15 Seconds

80
Q

Bearing the above in mind, what is the maximum time you should BLOW
an engine if the TOT is above 150°C prior to start?

A

Does not exceed 30 seconds

Prefect ESK (4 decks)

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