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Multi > PA-34-200 Piper Seneca I > Flashcards

PA-34-200 Piper Seneca I Flashcards

1
Q

VS0

A

60 KIAS

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2
Q

VS1

A

66 KIAS

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3
Q

VFE

A

108 KIAS

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4
Q

VLO (up)

A

108 KIAS

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5
Q

VLO (down)

A

130 KIAS

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6
Q

VLE

A

130 KIAS

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7
Q

VMGE (manual gear extend)

A

87 KIAS

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8
Q

VA

A

126-115 KIAS

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9
Q

VNO

A

165 KIAS

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10
Q

VNE

A

188 KIAS

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11
Q

VR

A

74 KIAS

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12
Q

VX

A

78 KIAS

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13
Q

VY

A

92 KIAS

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14
Q

Vclimb

A

104 KIAS

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15
Q

VTP (traffic pattern)

A

100 KIAS

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16
Q

VREF

A

82 KIAS

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17
Q

VREF (short)

A

76 KIAS

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18
Q

VREF (no flap)

A

92 KIAS

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19
Q

Max X-wind component

A

13 KNOTS

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20
Q

VREF (single engine)

A

92 KIAS

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21
Q

VG

A

102 KIAS

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22
Q

VMC

A

70 KIAS

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23
Q

VYSE

A

92 KIAS

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24
Q

VXSE

A

86 KIAS

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25
Q

VSSE

A

92 KIAS

26
Q

V (window open)

A

130 KIAS

27
Q

V (manual gear extend)

A

87 KIAS

28
Q

Max weight in nose baggage compartment

A

100 lbs

29
Q

Max weight in aft baggage compartment

A

100 lbs

30
Q

Max weight in hat rack

A

No heavy objects

31
Q

What categories of operation is the aircraft certified for?

A

Normal category only

32
Q

Maximum positive load factor limit

A

+3.8G

33
Q

Maximum negative load factor limit

A

Not defined. No inverted flight maneuvers approved.

34
Q

Who is the engine manufacturer and what are the model numbers of the left and right engines?

A

Lycoming
IO-360-C1E6 (left)
LIO-360-C1E6 (right)

35
Q

Maximum horsepower of the engines

A

200 hp

36
Q

Maximum engine RPM

A

2700

37
Q

Minimum fuel grade

A

100LL

38
Q

Minimum voltage to start engine

A

11V

39
Q

Maximum continuous cranking time of the starter

A

30 seconds

40
Q

Minimum cool down time between engine starting attempts

A

3 min

41
Q

Max oil temp (red line)

A

245 deg

42
Q

Max CHT (red line)

A

475 deg

43
Q

Normal operating limit for CHT at takeoff power and continuous power

A

435 deg

44
Q

Normal operating limit for CHT at economy power and cruise

A

400 deg

45
Q

Alternator output (volts)

A

14 Volts

46
Q

Max alternator amps load

A

60 Amps

47
Q

Battery output (V)

A

12 Volts

48
Q

Airspeed indicator white arc (KIAS)

A

60-108 KIAS

49
Q

Airspeed indicator green arc

A

66-165 KIAS

50
Q

Airspeed indicator yellow arc

A

166-188 KIAS

51
Q

Airspeed indicator upper red line

A

188 KIAS

52
Q

Airspeed indicator lower red line

A

70 KIAS

53
Q

What does the lower red line on the airspeed indicator represent?

A

VMC

54
Q

Airspeed indicator blue radial line

A

92 KIAS

55
Q

Max oil capacity (per engine)

A

8 qts

56
Q

Min oil capacity (per engine)

A

Not in POH. 2 qts per Lycoming operator manual. 6 qts is normally recommended by most operators

57
Q

Total fuel capacity

A

98 Gal

58
Q

Total usable fuel

A

93 Gal

59
Q

Total unusable fuel

A

5 Gal

60
Q

Usable fuel per wing

A

46.5

61
Q

Unusable fuel per wing

A

2.5 Gal

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