POH 4.1 General Information Flashcards

1
Q

POH.4.1.1 Powerplant

A
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2
Q

Righ Engine (continental)

A

LTSIO-360-E or LTSIO-360-EB

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3
Q

Left Engine (Continental)

A

TSIO-360-E or TSIO-360-EB

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4
Q

Rated Horsepower (sea level)

A

200

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5
Q

Rated Horsepower (12,000 ft)

A

215

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6
Q

Rated Speed (rpm)

A

2575

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7
Q

Max Manifold Pressure (in. Hg.)

A

40

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8
Q

Compression Ratio

A

7.5:1

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9
Q

POH.4.1.2 Fuel and Oil

A
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10
Q

AVGAS ONLY
FUEL (Total)

A

128 US GAL

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11
Q

(Usable)

A

123 US GAL

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12
Q

MAX OIL

A

8 US Quarts

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13
Q

MIN OIL

A

6 US Quarts

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14
Q

POH.4.1.3 Baggage Area

A
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15
Q

Maximum Baggage (lbs) Forward Compartment

A

100

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16
Q

Maximum Baggage (lbs) Rear Compartment

A

100

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17
Q

POH.4.1.4 Dimensions

A
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18
Q

Wingspan (ft)

A

38.9

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19
Q

Wing Area (sq ft)

A

208.7

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20
Q

Length (ft)

A

28.5

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21
Q

Height (ft)

A

9.9

22
Q

Wing Loading (lbs per sq ft)

A

22

23
Q

Power Loading (lbs per hp) (sea level)

A

11.4

24
Q

Power Loading (lbs per hp) (12,000 ft)

A

10.6

25
Q

Propeller Diameter (in.)

A

76

26
Q

Turn Radius (ft)

A

33.2

27
Q

Gross Weight (lb)

A

4570

28
Q

Take off Run, flaps up, sea level (ft)

A

1100

29
Q

Takeoff Distance Over 50-ft Obstacle, flaps up, sea level

A

1460’

30
Q

Takeoff Run (f) short field effort, flaps 25º

A

900

31
Q

Takeoff Distance Over 50-ft Barrier (ft) (short field effort, 25º)

A

1240

32
Q

Rate of Climb, sea level (ft per min)

A

1340

33
Q

Rate of Climb, sea level, single engine (ft per min)

A

225

34
Q

Service Ceiling (ft)

A

25000’**

35
Q

Service Ceiling, engine out (ft

A

13400

36
Q

Absolute Ceiling (ft

A

25000**

37
Q

Absolute Ceiling, engine out (ft)

A

14800

38
Q

STANDARD FUEL CAPACITY

A
39
Q

Range at best power mixture (mi)
75% power, 16,000 ft
With 45 min. reserve

A

626

40
Q

No reserve

A

742

41
Q

55% power, 16,000 ft
With 45 min. reserve

A

701

42
Q

No reserve

A

830

43
Q

*4570 lbs Maximum Takeoff Weight; 4342 lbs Maximum Landing Weight **Maximum Operating Altitude

A
44
Q

Stalling Speed, gear and flaps down, power off (kts)

A

60

45
Q

Stalling Speed, gear down and flaps up. power off (kts)

A

66

46
Q

Fuel Consumption, 75% power, both engines (gph)

A

23.6

47
Q

Fuel Consumption, 65% power, both engines (gph)

A

20.5

48
Q

Landing Roll (flaps down) (ft)

A

1380*

49
Q

Landing Over 50-ft Barrier (flaps down) (short field effort) (ft)

A

2090*

50
Q

*4342 lb G.W., Maximum Landing Weight

A