Prefect Limitations

Question 1

V MO (max Operating Speed)

Answer 1

238 Kts

Question 2

M MO (max Mach number)

Answer 2

0.45

Question 3

V LOE (max speed landing gear operation extend)

Answer 3

182 kts

Question 4

V LE (max Speed landing gear extended)

Answer 4

182 kts

Question 5

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

Answer 5

164 kts

Question 6

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

Answer 6

143 kts

Question 7

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

Answer 7

151 kts

Question 8

V LOR (max speed landing gear operation retract)

Answer 8

137 kts

Question 9

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

Answer 9

114 kts

Question 10

Sever turbulence airspeed recommended

Answer 10

140 - 180 kts

Question 11

Max airspeed to apply REV during landing

Answer 11

80 kts

Question 12

Min airspeed for use of REV during landing

Answer 12

40 kts

Question 13

T/O and landing crosswind component max

Answer 13

25 kts

Question 14

Max speed to open canopy

Answer 14

110 kts

Question 15

Max speed with canopy open

Answer 15

120 kts

Question 16

Max T/O AUM

Answer 16

1515 kg

Question 17

Max landing AUM

Answer 17

1515 kg

Question 18

Max Aerobatics AUM

Answer 18

1440 kg

Question 19

Max Zero Fuel AUM

Answer 19

1370 kg

Question 20

Min flying AUM

Answer 20

1170 kg

Question 21

Max baggage compartment mass

Answer 21

50 kg

Question 22

Max nose up when FUEL TANK selector in Emergency Transfer

Answer 22

15 degrees

Question 23

Max nose down when FUEL TANK selector in Emergency Transfer

Answer 23

10 degrees

Question 24

Aerobatic max +ve g

Answer 24

+6 g

Question 25

Aerobatic max -ve g

Answer 25

-4 g

Question 26

Utility max +ve g

Answer 26

+4.4 g

Question 27

Utility max -ve g

Answer 27

-1.7 g

Question 28

Flaps down max +ve g

Answer 28

+3.8 g

Question 29

Flaps down min g

Answer 29

+0 g

Question 30

Icing limitation

Answer 30

Flight into known icing conditions is prohibited

Question 31

Max OAT

Answer 31

ISA + 23°C

Question 32

Min OAT

Answer 32

-54°C

Question 33

Reduced power - OAT operation limitation. Min OAT

Answer 33

ISA -15°C

Question 34

Fuel must contain FSII at

Answer 34

below +4°C

Question 35

Min battery V for engine start

Answer 35

24V

Question 36

Start attempt durations (attempt 1, 2 & 3)

Answer 36

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

Question 37

Max Transient TRQ (10 sec)

Answer 37

115%

Question 38

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

Answer 38

111%

Question 39

Max continuous TRQ

Answer 39

92%

Question 40

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

Answer 40

927°C

Question 41

Max transient TOT (6 sec over 810°C)

Answer 41

899°C

Question 42

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

Answer 42

810°C

Question 43

Max continuous TOT

Answer 43

752°C

Question 44

Max continuous N2 speed

Answer 44

2130 RPM N2

Question 45

Max N2 for static ground ops with crosswind >10 kts

Answer 45

1850 RPM N2

Question 46

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

Answer 46

1523-1786 RPM N2

Question 47

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

Answer 47

106% N1

Question 48

Max continuous N1

Answer 48

105% N1

Question 49

Max transient oil pressure (cold weather/engine start)

Answer 49

150 psi

Question 50

Max oil pressure

Answer 50

130 psi

Question 51

Min oil pressure at N1 >94%

Answer 51

``` 120 psi 105 psi (BETA RANGE) ```

Question 52

Min oil pressure at N1 85-94%

Answer 52

``` 90 psi 75 psi (BETA RANGE) ```

Question 53

Min oil pressure at N1 <85%

Answer 53

``` 50 psi 35 psi (BETA RANGE) ```

Question 54

Max oil temp at TRQ <40%

Answer 54

107°C

Question 55

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

Answer 55

107°C

Question 56

Max continuous temp at TRQ >40%

Answer 56

82°C

Question 57

Min oil temp

Answer 57

0°C

Question 58

Min oil before starting

Answer 58

-40°C

Question 59

Total fuel capacity

Answer 59

282.7 kg

Question 60

LH collector tank capacity

Answer 60

16.8 kg

Question 61

Unusable fuel LH wing

Answer 61

6.3 kg

Question 62

Unusable fuel RH wing

Answer 62

1.4 kg

Question 63

Usable fuel

Answer 63

275 kg

Question 64

Max tank asymmetry

Answer 64

45.3 kg

Question 65

Max fuel in each wing for aerobatics

Answer 65

115 kg

Question 66

Max fuel pressure

Answer 66

25 psi

Question 67

Min fuel pressure

Answer 67

12 psi

Question 68

Engine Power

Answer 68

450 SHP

Question 69

Desire oil temp range

Answer 69

54-82 °C

Question 70

Normal operating oil pressure

Answer 70

90-130 psi