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Ground School > Limitations > Flashcards

Limitations Flashcards

1
Q

Altitude limit

A

FL100 (10,000ft)

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2
Q

Max Take-off AUM

A

1515kg

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3
Q

Max Landing AUM

A

1515kg

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4
Q

Max Aerobatics AUM

A

1440kg

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5
Q

Max Zero Fuel AUM

A

1370kg

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6
Q

Max Baggage Compartment Mass

A

50kg

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7
Q

Max Nose Up when FUEL TANK Selector is in EMERGENCY TRANSFER

A

15 degrees

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8
Q

Max Nose Down when FUEL TANK Selector is in EMERGENCY TRANSFER

A

10 degrees

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9
Q

Aerobatic max positive g

A

+6g

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10
Q

Aerobatic max negative g

A

-4g

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11
Q

Utility max positive g

A

+4.4g

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12
Q

Utility max negative g

A

-1.7g

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13
Q

Flaps down max positive g

A

+3.8g

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14
Q

Flaps down min g

A

+0g

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15
Q

At what AUM is ac cleared for aerobatics?

A

1440kg

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16
Q

What is the CofG limit for Aerobatics?

A

2732mm aft of datum

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17
Q

What must be selected on the Fuel Selector when conducting Aerobatics or Spinning?

A

Fuel Selector LEFT

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18
Q

When conducting Aerobatics or spinning, Fuel Transfer pump ON or OFF?

A

OFF

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19
Q

When conducting Aerobatics or Spinning, what is the max fuel in either wing tank?

A

115kg

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20
Q

What is the max time allowed in a pitch attitude in excess of 45 degrees Nose Up or Down?

A

30 secs

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21
Q

What is the max time allowed in inverted flight?

A

30 secs

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22
Q

What is the max time allowed when in a wing down or knife edge flight?

A

30 secs

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23
Q

What is the max number of spins allowed?

A

8

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24
Q

After flying in an restricted attitude, what must you do?

A

Return to erect positive g flight and pitch attitude of less that +/- 45 degrees for at least the time spent in the restricted attitude.

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25
Q

Are you allowed to spin with flaps extended?

A

Nope

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26
Q

What must you do if Oil Pressure drops below 35 psi during a restricted attitude?

A

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

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27
Q

What will happen to TRQ indications if a restricted attitude causes a sudden drop in oil pressure?

A

They will be affected…

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28
Q

What are the restricted attitudes?

A

Pitch attitude 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).

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29
Q

What must you do if, after flying inverted, the oil pressure fails to rise to normal levels?

A

Land and troubleshoot the inverted oil system.

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30
Q

With airspeed in excess of VO, what is prohibited?

A

Full or abrupt deflection of the control surfaces.

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31
Q

What is V MO?

A

Max Operating Speed

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32
Q

What speed is V MO?

A

238 KIAS

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33
Q

Limits for V MO?

A

Never exceed

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34
Q

What is M MO?

A

Max operating mach number

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35
Q

What speed is M MO?

A

0.45MN

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36
Q

Limits for M MO?

A

Never exceed

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37
Q

What is V LOE?

A

Max speed landing gear operation extend

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38
Q

What speed is V LOE?

A

182 KIAS

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39
Q

Limits for V LOE?

A

Do not exceed during gear extension

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40
Q

What is V LE?

A

Max speed landing gear extended

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41
Q

What speed is V LE?

A

182 KIAS

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42
Q

Limits for V LE?

A

Do not exceed with gear extended

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43
Q

What is V O (Aerobatic)?

A

Max manoeuvre speed up to 1440kg AUM

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44
Q

What speed is V O (Aerobatic)?

A

164 KIAS

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45
Q

Limits for V O (Aerobatic)?

A

Do not apply max control deflection above this speed

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46
Q

What is V O (Utility)?

A

Max manoeuvre speed 1440 to 1515kg AUM

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47
Q

What speed is V O (Utility)?

A

143 KIAS

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48
Q

Limits for V O (Utility)?

A

Do not apply max control deflection above this speed

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49
Q

What is V FE-T/O?

A

Max speed flaps extended at take-off position

50
Q

What speed is V FE-T/O?

A

151 KIAS

51
Q

Limits for V FE-T/O?

A

Do not exceed with flaps at TAKE-OFF

52
Q

What is V LOR?

A

Max speed landing gear operation retract

53
Q

What speed is V LOR?

A

137 KIAS

54
Q

Limits for V LOR?

A

Do not exceed during gear retractions

55
Q

What is V FE?

A

Max speed flaps extended beyond take-off position

56
Q

What speed is V FE?

A

114 KIAS

57
Q

Limits for V FE?

A

Do no exceed with flaps beyond TAKE-OFF

58
Q

What must you NOT do with the POWER lever during flight?

A

POWER lever MUST NOT be retarded BELOW FI

59
Q

Max airspeed to apply REVerse Thrust during landing?

A

80 KIAS

60
Q

Min airspeed to apply REVerse Thrust during landing?

A

40 KIAS

61
Q

Max Crosswind for Take-off & Landing?

A

25 kts

62
Q

Maximum crosswind for brake-release take-off?

A

20 kts

63
Q

With a crosswind greater than 20kts, what should you do with the Flaps?

A

Flaps should be UP (CAUTION).

64
Q

What is the recommended cruise speed (Severe Turbulence Airspeed)?

A

140 to 180 KIAS

65
Q

Max canopy opening speed?

A

110kts

66
Q

Max Speed with canopy open?

A

120kts

67
Q

Can the canopy ever be open or unlocked during flight?

A

No, only in emergency conditions.

68
Q

Can you ever fly into icing conditions?

A

NO. Flight into known icing conditions is prohibited.

69
Q

What is OAT?

A

Outside Air Temperature

70
Q

What is the max (on the ground) OAT?

A

+38°C

71
Q

What is the Max OAT?

A

ISA +23°C

72
Q

What is the Min OAT?

A

-54°C

73
Q

What is the Reduced Power Min OAT?

A

ISA -15°C

74
Q

IN OAT <4°C in visible moisture or rain, what must you do?

A

P/S HEAT: ON

COMP INTAKE: BOTH

75
Q

At what OAT must fuel contain FSII?

A

Below +4°C

76
Q

What is the max duration Taxy & Landing lights can be used for during OAT >+38°C?

A

Max 40 mins (min 30 mins cool time)

77
Q

What is the Min battery voltage for engine start?

A

24V

78
Q

What is Engine Start Limitations for consecutive start attempts?

A

Start Attempt 1: Starter ON for 30 sec -> Cooling Down for 1 min.
Start Attempt 2: Starter ON for 30 sec -> Cooling Down for 1 min.
Start Attempt 3: Starter ON for 30 sec -> Cooling Down for 30 mins.

79
Q

What is the Max Transient TRQ? (Duration and %)

A

10 Sec. 115%.

80
Q

What is the Max T/O Power TRQ? (Duration and %)

A

5 min at T/O. Cumulative per sortie. 111%.

81
Q

What is the Max Continuous TRQ?

A

92%

82
Q

What is TOT?

A

Turbine Outlet Temperature

83
Q

What is the Max Engine Start TOT?

A

927°C (10 sec over 810°C)

84
Q

What is the Max Transient TOT?

A

899°C (6 sec over 810°C)

85
Q

What is the Max T/O Power TOT?

A

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

86
Q

What is the Max Continuous TOT?

A

752°C

87
Q

What is N2?

A

Propeller RPM

88
Q

What is N1?

A

Gas Generator RPM

89
Q

What is the Max Transient limit for N2?

A

2233 N2 (15 sec max above 2132 N2)

90
Q

What is the Max Continuous Speed for N2?

A

2132 N2

91
Q

What is the Max Static Ground Ops with Crosswind component >10kts for N2?

A

1850 N2 (This is relevant to the Propeller Overspeed Governor Check)

92
Q

What is the N2 Speed Avoidance Range?

A

N2 stabilized for longer than 1 sec between 1523 RPM and 1786 RPM with more than 20% TRQ

93
Q

When does the N2 Speed Avoidance Range Apply?

A

Forward and reverse thrust

94
Q

Where must the Accumulated time spent in the N2 Speed Avoidance Range be recorded?

A

In the Engine Logbook.

95
Q

What is the Max Transient N1?

A

106% N1 (max 15 sec >105% N1)

96
Q

What is the Max Continuous N1?

A

105% N1

97
Q

What is the Max Transient (cold weather/engine start) Oil Pressure?

A

150 psi

98
Q

What is the Max Oil Pressure?

A

130 psi

99
Q

How much does the Min Oil pressure decrease above 5000ft pressure altitude?

A

2 psi for each 1000ft above 5000ft (pressure altitude). to a max reduction of 20 psi.

100
Q

What is the min Oil pressure at N1 >94%

A

120 psi (Beta: 105 psi)

101
Q

What is the min Oil pressure at N1 85% - 94%?

A

90 psi (Beta: 75 psi)

102
Q

What i the min Oil pressure at N1 <85%?

A

50 psi (Beta: 5 psi)

103
Q

What is the Max Oil Temperature limit at TRQ <40%?

A

107°C

104
Q

What is the Max Transient Oil Temperature at TRQ >40 % (5 min)

A

107°C

105
Q

What is the Max Continuous Oil Temperature at TRQ >40%

A

82°C

106
Q

What is the Min Oil Temp?

A

0°C

107
Q

What is the Min Oil Temp before starting?

A

-40°C

108
Q

What is the Total Fuel Capacity?

A

282.7kg

109
Q

What is the LH Collector Tank Capacity?

A

16.8kg

110
Q

What is the Unusable Fuel Left Wing?

A

6.3kg

111
Q

What is the Unusable Fuel Right Wing?

A

1.4kg

112
Q

What is the Usable Fuel?

A

275.0kg

113
Q

What is the Max Tank Asymetry?

A

45.3kg

114
Q

What is the Max Fuel in each wing for Aerobatics?

A

115.0kg

115
Q

What is the Max Fuel Pressure?

A

25 psi

116
Q

Wat is the Min Fuel Pressure?

A

12 psi

117
Q

What is the ESI?

A

Electronic Standby Indicator

118
Q

What are the ESI Limitations?

A

Flight in IMC is not permitted with a:
Amber Battery Symbol (less than 30 mins power remaining)
Amber or Red X displayed over Battery Symbol
CAL DUE message by the battery symbol

119
Q

What must you shout before turning the battery on?

A

“POWER ON”

120
Q

What must you check before carrying out the flap functional test?

A

That there are no obstructions below the flap.

Ground School (3 decks)

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