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Prefect Limitations > Prefect Limitations > Flashcards

Prefect Limitations Flashcards

1
Q

V MO (max Operating Speed)

A

238 Kts

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2
Q

M MO (max Mach number)

A

0.45

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3
Q

V LOE (max speed landing gear operation extend)

A

182 kts

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4
Q

V LE (max Speed landing gear extended)

A

182 kts

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5
Q

V O Aerobatic (max manoeuvre speed up to 1440kg)

A

164 kts

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6
Q

V O Utility (max manoeuvre speed 1440 - 1515kg)

A

143 kts

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7
Q

V FE-T/O (max speed flaps extended to T/O)

A

151 kts

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8
Q

V LOR (max speed landing gear operation retract)

A

137 kts

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9
Q

V FE (max speed flaps extended beyond T/O position)

A

114 kts

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10
Q

Sever turbulence airspeed recommended

A

140 - 180 kts

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11
Q

Max airspeed to apply REV during landing

A

80 kts

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12
Q

Min airspeed for use of REV during landing

A

40 kts

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13
Q

T/O and landing crosswind component max

A

25 kts

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14
Q

Max speed to open canopy

A

110 kts

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15
Q

Max speed with canopy open

A

120 kts

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16
Q

Max T/O AUM

A

1515 kg

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17
Q

Max landing AUM

A

1515 kg

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18
Q

Max Aerobatics AUM

A

1440 kg

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19
Q

Max Zero Fuel AUM

A

1370 kg

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20
Q

Min flying AUM

A

1170 kg

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21
Q

Max baggage compartment mass

A

50 kg

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22
Q

Max nose up when FUEL TANK selector in Emergency Transfer

A

15 degrees

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23
Q

Max nose down when FUEL TANK selector in Emergency Transfer

A

10 degrees

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24
Q

Aerobatic max +ve g

A

+6 g

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25
Q

Aerobatic max -ve g

A

-4 g

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26
Q

Utility max +ve g

A

+4.4 g

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27
Q

Utility max -ve g

A

-1.7 g

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28
Q

Flaps down max +ve g

A

+3.8 g

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29
Q

Flaps down min g

A

+0 g

30
Q

Icing limitation

A

Flight into known icing conditions is prohibited

31
Q

Max OAT

A

ISA + 23°C

32
Q

Min OAT

A

-54°C

33
Q

Reduced power - OAT operation limitation. Min OAT

A

ISA -15°C

34
Q

Fuel must contain FSII at

A

below +4°C

35
Q

Min battery V for engine start

A

24V

36
Q

Start attempt durations (attempt 1, 2 & 3)

A

1:
Starter ON: 30 sec
Cooling down: 1 min

2:
Starter ON: 30 sec
Cooling down: 1 min

3:
Starter ON: 30 sec
Cooling down: 30 min

37
Q

Max Transient TRQ (10 sec)

A

115%

38
Q

Max T/O Power TRQ (5min at T/O)

A

111%

39
Q

Max continuous TRQ

A

92%

40
Q

Max engine start TOT (10 sec over 810°C)

A

927°C

41
Q

Max transient TOT (6 sec over 810°C)

A

899°C

42
Q

Max T/O power TOT (5 min at T/O)

A

810°C

43
Q

Max continuous TOT

A

752°C

44
Q

Max continuous N2 speed

A

2130 RPM N2

45
Q

Max N2 for static ground ops with crosswind >10 kts

A

1850 RPM N2

46
Q

N2 speed avoidance range (must not be allowed to stabilize in for longer than 1 second)

A

1523-1786 RPM N2

47
Q

Max transient N1 (max 15 sec > 105% N1)

A

106% N1

48
Q

Max continuous N1

A

105% N1

49
Q

Max transient oil pressure (cold weather/engine start)

A

150 psi

50
Q

Max oil pressure

A

130 psi

51
Q

Min oil pressure at N1 >94%

A 
120 psi 
105 psi (BETA RANGE)
52
Q

Min oil pressure at N1 85-94%

A 
90 psi
75 psi (BETA RANGE)
53
Q

Min oil pressure at N1 <85%

A 
50 psi
35 psi (BETA RANGE)
54
Q

Max oil temp at TRQ <40%

A

107°C

55
Q

Max oil temp at TRQ >40% (5 min)

A

107°C

56
Q

Max continuous temp at TRQ >40%

A

82°C

57
Q

Min oil temp

A

0°C

58
Q

Min oil before starting

A

-40°C

59
Q

Total fuel capacity

A

282.7 kg

60
Q

LH collector tank capacity

A

16.8 kg

61
Q

Unusable fuel LH wing

A

6.3 kg

62
Q

Unusable fuel RH wing

A

1.4 kg

63
Q

Usable fuel

A

275 kg

64
Q

Max tank asymmetry

A

45.3 kg

65
Q

Max fuel in each wing for aerobatics

A

115 kg

66
Q

Max fuel pressure

A

25 psi

67
Q

Min fuel pressure

A

12 psi

68
Q

Engine Power

A

450 SHP

69
Q

Desire oil temp range

A

54-82 °C

70
Q

Normal operating oil pressure

A

90-130 psi

Prefect Limitations (1 decks)

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