IR - DA42 Flashcards

1
Q

DA42
Stalling speeds (max weight)

A

V(S0) - 62kt
V(S1) - 66kt

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2
Q

DA42
V(X)

A

90kt

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3
Q

DA42
V(Y)

A

90kt

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4
Q

DA42
V(YSE)

A

85kt - BLUE LINE
= V(SSE) minimum control speed for training

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5
Q

DA42
V(MCA)

A

76kt (per Stapleford)

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6
Q

DA42
V(R)

A

80kt

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7
Q

DA42
Operating speed range in ice

A

118 - 156 kt

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8
Q

DA42
V(FE) - approach & landing

A

Approach - 133kt
Landing - 113kt

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9
Q

DA42
V(LE)

A

188kt
Extension AND extended

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10
Q

DA42
V(LOR)

A

152kt
Retraction speed

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11
Q

DA42
V(REF)

A

84kt (86kt flapless)

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12
Q

DA42
V(NO)

A

151kt

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13
Q

DA42
V(NE)

A

188kt

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14
Q

DA42
MTOM

A

1900kg

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15
Q

DA42
MLM

A

1805kg

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16
Q

DA42
MZFM

17
Q

DA42
Empty mass

18
Q

DA42
Max baggage
- Nose
- Cockpit
- Rear extension

A

Nose: 30kg
Cockpit: 45kg
Rear extension: 18kg

19
Q

DA42
When does landing gear warner go off

A

Landing gear retracted and:
- Flaps in LDG position; or
- Power < 20%

20
Q

DA42
Maximum load factor

21
Q

DA42
Max crosswind component

A

20kt Stapleford
(25kt pilots handbook)

22
Q

DA42
Fuel types

A

Jet-A, Jet-A1 and some others

23
Q

DA42
Total fuel useable (and total)

A

50 USG useable
[51 USG total]

24
Q

DA42
Typical fuel flow rate

25
Q

DA42
Max difference between fuel content in L and R tanks

26
Q

DA42
Fuel delivery method

A

Direct injection from common rail to each of the 4 cylinders.

27
Q

DA42
Autopilot operation speed limits

28
Q

DA42
Autopilot operation height limits

A

200ft AGL in approach and departure
800ft AGL other phases

29
Q

DA42
Critical Engine on DA42

30
Q

DA42
Max starter time

A

10 seconds

31
Q

DA42
Engines
- # cylinders
- # stroke
- sump type

A

4 cylinder
4 stroke
Wet sump

32
Q

DA42
Feathering rpm limit

A

Switching off engine master feathers the engine, but only if rpm is above 1300rpm.

33
Q

Minimum En-route Altitude vs
Minimum Safe Altitude

A

MEA is min alt between two fixes ensuring terrain clearance and navaid coverage.
MSA is a more general term that allows you to determine an altitude for a phase of the flight to ensure terrain clearance.

34
Q

DA42
Electrical system

35
Q

DA42
Backup batteries

A

30 minute backup for the ECU only
12V, 7.2 Ah batteries under each seat

36
Q

DA42
Main battery voltage

A

24V, 13.6 Ah

37
Q

Conditions conducive to windshear

A

Thunderstorms, Cb

38
Q

DA42 anti-icing systems
[Labelled de-ice incorrectly!]

A

Pitot heat
Static heat
Windscreen (fluid)
Wing leading edge (fluid)
Propeller (fluid)

39
Q

DA42
Landing gear operation

A

Hydraulic with electric pump