PA-34-200 Piper Seneca I

Question 1

VS0

Answer 1

60 KIAS

Question 2

VS1

Answer 2

66 KIAS

Question 3

VFE

Answer 3

108 KIAS

Question 4

VLO (up)

Answer 4

108 KIAS

Question 5

VLO (down)

Answer 5

130 KIAS

Question 6

VLE

Answer 6

130 KIAS

Question 7

VMGE (manual gear extend)

Answer 7

87 KIAS

Question 8

VA

Answer 8

126-115 KIAS

Question 9

VNO

Answer 9

165 KIAS

Question 10

VNE

Answer 10

188 KIAS

Question 11

VR

Answer 11

74 KIAS

Question 12

VX

Answer 12

78 KIAS

Question 13

VY

Answer 13

92 KIAS

Question 14

Vclimb

Answer 14

104 KIAS

Question 15

VTP (traffic pattern)

Answer 15

100 KIAS

Question 16

VREF

Answer 16

82 KIAS

Question 17

VREF (short)

Answer 17

76 KIAS

Question 18

VREF (no flap)

Answer 18

92 KIAS

Question 19

Max X-wind component

Answer 19

13 KNOTS

Question 20

VREF (single engine)

Answer 20

92 KIAS

Question 21

VG

Answer 21

102 KIAS

Question 22

VMC

Answer 22

70 KIAS

Question 23

VYSE

Answer 23

92 KIAS

Question 24

VXSE

Answer 24

86 KIAS

Question 25

VSSE

Answer 25

92 KIAS

Question 26

V (window open)

Answer 26

130 KIAS

Question 27

V (manual gear extend)

Answer 27

87 KIAS

Question 28

Max weight in nose baggage compartment

Answer 28

100 lbs

Question 29

Max weight in aft baggage compartment

Answer 29

100 lbs

Question 30

Max weight in hat rack

Answer 30

No heavy objects

Question 31

What categories of operation is the aircraft certified for?

Answer 31

Normal category only

Question 32

Maximum positive load factor limit

Answer 32

+3.8G

Question 33

Maximum negative load factor limit

Answer 33

Not defined. No inverted flight maneuvers approved.

Question 34

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

Answer 34

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

Question 35

Maximum horsepower of the engines

Answer 35

200 hp

Question 36

Maximum engine RPM

Answer 36

2700

Question 37

Minimum fuel grade

Answer 37

100LL

Question 38

Minimum voltage to start engine

Answer 38

11V

Question 39

Maximum continuous cranking time of the starter

Answer 39

30 seconds

Question 40

Minimum cool down time between engine starting attempts

Answer 40

3 min

Question 41

Max oil temp (red line)

Answer 41

245 deg

Question 42

Max CHT (red line)

Answer 42

475 deg

Question 43

Normal operating limit for CHT at takeoff power and continuous power

Answer 43

435 deg

Question 44

Normal operating limit for CHT at economy power and cruise

Answer 44

400 deg

Question 45

Alternator output (volts)

Answer 45

14 Volts

Question 46

Max alternator amps load

Answer 46

60 Amps

Question 47

Battery output (V)

Answer 47

12 Volts

Question 48

Airspeed indicator white arc (KIAS)

Answer 48

60-108 KIAS

Question 49

Airspeed indicator green arc

Answer 49

66-165 KIAS

Question 50

Airspeed indicator yellow arc

Answer 50

166-188 KIAS

Question 51

Airspeed indicator upper red line

Answer 51

188 KIAS

Question 52

Airspeed indicator lower red line

Answer 52

70 KIAS

Question 53

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

Answer 53

VMC

Question 54

Airspeed indicator blue radial line

Answer 54

92 KIAS

Question 55

Max oil capacity (per engine)

Answer 55

8 qts

Question 56

Min oil capacity (per engine)

Answer 56

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

Question 57

Total fuel capacity

Answer 57

98 Gal

Question 58

Total usable fuel

Answer 58

93 Gal

Question 59

Total unusable fuel

Answer 59

5 Gal

Question 60

Usable fuel per wing

Answer 60

46.5

Question 61

Unusable fuel per wing

Answer 61

2.5 Gal