Prefect limitations Aug 21 Flashcards

1
Q

VMO (Max Operating Speed)

A

238

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2
Q

MMO (Max operating Mach Number

A

0.45MN

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3
Q

V LOE (Max speed landing gear oppression extend)

A

182

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4
Q

V LE (Max speed landing gear extend)

A

182

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5
Q

VO (Aerobatic) (Max manoeuvre speed up to 1440kg AUM)

A

164

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6
Q

VO (Utility) (Max manoeuvre speed 1440 to 1515 kg AUM)

A

143

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7
Q

VFE - T/O (Max speed flaps extended at take off position)

A

151

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8
Q

V LOR (Max speed landing gear operation retract)

A

137

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9
Q

VFE (Max speed flaps extended beyond take off position)

A

114

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10
Q

Power lever must not be retarded below __ during flight

A

Flight Idle

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11
Q

Max airspeed to apply reverse thrust during landing

A

80

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12
Q

Min airspeed for use of Reverse thrust during landing

A

40

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13
Q

Take off and landing cross wind component limitations

1) Take off and landing ___
2) maximum crosswind for break release take off __
3) flaps should be up in crosswinds grater than __

A

25
20
20

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14
Q

Recommended cruise airspeed during severe turbulence?

A

140-180

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15
Q

Max opening speed of the canopy in flight

A

110

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16
Q

Max speed with canopy open in flight

A

120

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17
Q

Max take off AUM

A

1515

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18
Q

Max landing AUM

A

1515

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19
Q

Max aerobatics AUM

A

1440

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20
Q

Max zero fuel AUM

A

1370

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21
Q

Min flying AUM

A

1170

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22
Q

Max baggage compartment Mass

A

50kg

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23
Q

Pitch attitude limitations, when fuel tank selector in emergency transfer
Max nose up ___
Max nose down ___

A

15

10

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24
Q

Aerobatic (<1440kg) max G limits

A

-4 to +6

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25
Q

Utility (<1515) G limits

A

-1.7 to +4.4

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26
Q

Flaps down max positive G

Flaps down min G

A

+3.8

0

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27
Q

Max OAT on the ground

A

+38c

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28
Q

Max OAT

A

ISA + 23c

29
Q

Min OAT

A

-54c

30
Q

Reduced power - OAT operating limitation minimum

A

ISA - 15c

31
Q

OAT <4c in visible rain or moisture

A

P/S Heat - On

Comp intake - Both

32
Q

What must fuel contain when OAT is below 4c

A

FSII

33
Q

Min battery voltage for engine start

A

24v

34
Q

Max transient TRQ (10 Seconds)

A

115%

35
Q

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

A

111%

36
Q

Max continuous TRQ

A

92%

37
Q

Max engine start TOT

A

927c (10 seconds over 810c)

38
Q

Max transient TOT

A

899c (6 seconds over 810c)

39
Q

Max T/O power TOT

A

810 (5 min at T/O, cumulative per sortie)

40
Q

Max continuous TOT

A

752c

41
Q

Taxi and landing might limitation

OAT > +38c =

A

Max 40 minutes (min 30 mins cool time)

42
Q

Max transient limit (Propeller RPM)

A

2233 N2 (15 seconds max above 2130 N2)

43
Q

Max continuous speed of propeller RPM

A

2132

44
Q

Max static ground ops propeller RPM

A

1850 N2

45
Q

N2 must not be allowed to stabilise within the ___

A

N2 speed avoidance range

46
Q

The N2 speed avoidance range is

A

Stabilised for longer than 1 second between 1523 and 1786 RPM with more than 20% TRQ

47
Q

Speed avoidance range applied in both

A

Forward and reverse thrust

48
Q

Accumulated time spent in the N2 speed avoidance range must be recorded in __

A

The engine logbook

49
Q

Gas generator RPM

Max transient N1
Max continuous N1

A

106% N1 (max 15 sec >105%)

105% N1

50
Q
Oil pressure 
Max transient (cold weather / engine start)
A

150 PSI

51
Q

Oil Pressure max

A

130 PSI

52
Q

Oil pressure min at an N1 greater than 94%

A

120

105 (Beta)

53
Q

Oil pressure min at N1 85% to 94%

A
90 PSI
75 PSI (Beta)
54
Q

Oil pressure N1 <85%

A
50 PSI
35 PSI (Beta)
55
Q

Oil temperature max limit at TRQ <40%

A

107c

56
Q

Oil temperature Max transient TRQ >40% (5min)

A

107c

57
Q

Oil temperature at max continuous TRQ >40%

A

82c

58
Q

Min oil temperature

A

0c

59
Q

Min oil temperature before starting

A

-40c

60
Q

Total Fuel Capacity

A

282.7kg

61
Q

LH collector tank capacity

A

16.8kg

62
Q

Unusable fuel left wing

A

6.3kg

63
Q

Unusable fuel right wing

A

1.4kg

64
Q

Usable fuel

A

275kg

65
Q

Max tank asymmetry

A

45.3kg

66
Q

Max fuel in each wing for aerobatics

A

115kg

67
Q

Max fuel pressure

A

25 PSI

68
Q

Min fuel pressure

A

12 PSI