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Command Training > Ch.2 Memory Items > Flashcards

Ch.2 Memory Items Flashcards

1
Q

Wingspan (without extended wingtips).

A

21.44m

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2
Q

Wingspan (with extended wingtips)

A

22.75m

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3
Q

Flaps extended speed Vfe, may only be extended:

A
  • on ground
  • as required for take off
  • low altitude holding
  • approach & landing
  • up to a max altitude of 14,000ft
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4
Q

Flaps extended speed Vfe 7 or 15.

A

175 KIAS

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5
Q

Flaps extended speed Vfe 20.

A

165 KIAS

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6
Q

Flaps extended speed Vfe 35.

A

140 KIAS

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7
Q

Max landing gear retraction speed VLOR.

A

150 KIAS

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8
Q

Max landing gear extension speed VLOE.

A

200 KIAS

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9
Q

Max landing gear emergency extension speed VLOEE.

A

200 KIAS.

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10
Q

Max landing gear extended speed VLE.

A

200 KIAS.

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11
Q

Minimum control speed SF340A.

A

103 KIAS (Flaps 20& 35).

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12
Q

Minimum control speed SF340B.

A

106 KIAS (flaps 20 & 35).

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13
Q

Minimum control speed SF340WT.

A

103 KIAS (flaps 20 & 35).

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14
Q

Max operating speed VMO.

A
  • 250 KIAS up to approx 16,000ft.

- Above this VMO decreases as indicated by the VMO pointer to approx 210 KIAS at 25,000ft.

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15
Q

Max manoeuvring speed VA.

A

180 KIAS.

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16
Q

Max rough air penetration speed VRA.

A
  • 190 KIAS up to 21,000ft.

- Above this, reduce speed as indicated by VMO pointer minus 30 KTS.

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17
Q

Max tailwind takeoff.

A

10 KTS.

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18
Q

Max landing tailwind.

A

15 KTS.

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19
Q

Max operating altitude.

A

25,000ft.

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20
Q

Max crosswind.

A

35 KTS.

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21
Q

Autopilot operations not authorised:

A
  • Below 50ft AGL during approach.
  • Below 100ft AGL for non coupled approach.
  • Below 200ft AGL during take off or go around.
  • Below 500ft AGL during cruise.
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22
Q

Yaw damper operation is not authorised for:

A
  • Take off
  • Go around
  • Landing
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23
Q

When holding in icing conditions what flap setting must be used?

A

Flap 0.

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24
Q

Landing flap must be set by what radio height?

A

300ft radio height.

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25
Q

Fire protection duration for SF340WT.

A
  • 60 minutes (2 bottles).
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26
Q

Fire protection duration for SF340B/ A.

A

35 minutes.

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27
Q

SF340B/ WT Max taxi weight.

A

13,290kg.

28
Q

SF340B/ WT Max take off weight.

A

13,155kg.

29
Q

SF340B/ WT Max landing weight.

A

12,930kg.

30
Q

SF340B/ WT Max zero fuel weight.

A

12,020kg.

31
Q

SF340A Max taxi weight.

A

12,840kg.

32
Q

SF340A Max take off weight.

A

12,700kg.

33
Q

SF340A Max landing weight.

A

12,340kg.

34
Q

SF340A Max zero fuel weight.

A

11,660kg.

35
Q

Max cabin diff pressure in flight.

A

7.5 PSI.

36
Q

Max cabin diff pressure landing.

A

0.3 PSI.

37
Q

Cabin pressure warning alarm.

A

7.5 PSI.

38
Q

Cabin altitude cabin press warning.

A

10,000ft.

39
Q

DC generators max voltage.

A

29v.

40
Q

Normal load per DC generator.

A

400A.

41
Q

Max load DC generators.

A

600A for 5 minutes.

42
Q

Main batteries normal voltage.

A

24v.

43
Q

External power GPU max voltage.

A

29.5v.

44
Q

External power battery cart max voltage.

A

29.5v.

45
Q

Amperage requirement engine start max.

A

1600A.

46
Q

Min fuel in each tank for take off.

A

135kg.

47
Q

Max imbalance between fuel tanks.

A

90kg.

48
Q

Low level fuel light illuminates at:

A

135kg.

49
Q

Total quantity of usable fuel is:

A

2542kg.

50
Q

Windshield heating time in normal before switching to high:

A

7 minutes.

51
Q

Time from switching standby pitot on until full ice protection is obtained:

A

5 minutes.

52
Q

Windshield wipers in low position max KIAS:

A

130 kts.

53
Q

Windshield wipers in high position max KIAS:

A

160 kts.

54
Q

Max difference between two airspeed indicators.

A

8 KIAS.

55
Q

Number of brake applications on fully charged brake accumulators:

A

11.

56
Q

Max speed for use of brakes with anti skid system off or inoperative:

A

40 kts.

57
Q

SF340B take off power + APR or go around power:

A

107 TRQ 940 ITT (max 5 minutes)

107 TRA 950 ITT (max 2 minutes)

1396 PROP RPM

58
Q

SF340B take off power:

A

100 TRQ 917 ITT (max 5 min)

100 TRQ 927 ITT (max 2 min)

1396 PROP RPM

59
Q

SF340B max continuous OEI:

A

100 TRQ 944 ITT

1396/PROP RPM

60
Q

SF340B transient except take off (max 12 seconds):

A

112 TRQ 965 ITT

1572 PROP RPM

61
Q

SF340B max engine start ITT:

A

965 degrees.

62
Q

SF340B limitations for motoring start:

A
  • Max Ng for motoring 26%
  • Min stabilised Ng prior to condition lever start 17%
  • Min Ng prior to tailwind start 20%
63
Q

SF340A take off power:

A

108 TRQ 930 ITT (max 5 min)

1396 PROP RPM

64
Q

SF340A max continuous OEI:

A

100 TRQ 917 ITT

1396 PROP RPM

65
Q

SF340A transient except take off (max 12 sec):

A

118 TRQ 960 ITT

1572 PROP RPM

66
Q

SF340A engine start ITT:

A

960 degrees.

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