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POH - Piper Aztec > Section I Specifications > Flashcards

Section I Specifications Flashcards

1
Q

PERFORMANCE

A

Performance figures are for airplanes equipped for cross-country transportation and flown at gross weight under standard conditions at sea level or stated altitude. Any changes in equipment may result in changes in performance.

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2
Q

Take-off Run (max effort, ft)

A

820

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3
Q

Take-off Distance Over 50-ft Barrier (max effort, ft)

A

1250

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4
Q

Accelerate-Stop Distance (ft)

A

2220

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5
Q

Minimum Controllable Single Engine Speed (mph)

A

80

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6
Q

Stalling Speed (gear down, flaps down 50”, power off, mph)

A

68

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7
Q

Stalling Speed (gear and flaps up, power off, mph)

A

74

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8
Q

Best Rate of Climb (ft per min)

A

1490

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9
Q

Best Rate of Climb Speed (mph)

A

120

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10
Q

Best Angle of Climb Speed (mph)

A

107

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11
Q

Single Engine Rate of Climb (ft per min)

A

240

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12
Q

Best Single Engine Rate of Climb Speed (mph)

A

102

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13
Q

Best Single Engine Angle of Climb Speed (mph)

A

97

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14
Q

Absolute Ceiling (ft)

A

21,100

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15
Q

Service Ceiling (ft)

A

19,800

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16
Q

Single Engine Absolute Ceiling (ft)

A

6,400

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17
Q

Single Engine Service Ceiling (ft)

A

5,000

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18
Q

Top Speed (mph)

A

216

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19
Q

Landing Roll (flaps down, max effort, ft)

A

850

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20
Q

Landing Distance Over 50-ft Barrier (flaps down, ft)

A

1620

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21
Q

Altitude Cruising Speeds (mph)
Altitude Cruising Range (No Reserve)
MP
Fuel Consumption (both engines, gph)

A

page 8 POH

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22
Q

Gross Weight (lbs)

A

5200

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23
Q

Maximum Landing Weight (lbs)

A

4940

24
Q

Zero Fuel Gross Weight (lbs)

A

4400

25
Q

Empty Weight (Standard, lbs)

A

2933

26
Q

USEFUL LOAD (Standard, lbs)

A

2267

27
Q

Engine (Lycoming)

A

IO-540-C4B5

28
Q

Rated Horsepower

A

250

29
Q

Rated Speed (rpm)

A

2575

30
Q

Bore (inches)

A

5-1/8

31
Q

Stroke (inches)

A

4-3/8

32
Q

Displacement (cubic inches)

A

541.5

33
Q

Compression Ratio

A

8.5:1

34
Q

Dry Weight (pounds)

A

402

35
Q

Fuel Capacity (U.S. gal)

A

144* * 140 gallons usable

36
Q

Fuel, Aviation Grade (octane)

A

91/96

37
Q

Oil Capacity (U.S. qts, each eng)

A

12

38
Q

Maximum Baggage (lbs) Forward Compartment

A

150

39
Q

Maximum Baggage (lbs) Rear Compartment

A

150

40
Q

With oxygen installed

A

105

41
Q

Baggage Space (cubic ft) Forward Compartment

A

17.4

42
Q

Baggage Space (cubic ft) Rear Compartment

A

23.2

43
Q

Baggage Door Size (in) Forward Compartment

A

19.5 x 30.5

44
Q

Baggage Door Size (in) Rear Compartment

A

30 x 31

45
Q

Wing Span (ft)

A

37.2

46
Q

Wing Area (sq ft)

A

207.56

47
Q

Length (ft)

A

30.2

48
Q

Height (ft)

A

10.3

49
Q

Wing Loading (lbs per sq ft)

A

25.05

50
Q

Power Loading (lbs per hp)

A

10.4

51
Q

Propeller Diameter (maximum, in)

A

77

52
Q

Wheel Base (ft)

A

7.5

53
Q

Wheel Tread

A

11.3

54
Q

Tire Pressure

A

Nose
27
Main
46

55
Q

Tire Size

A

Nose (four ply rating)
600x6
Main (eight ply rating)
700x6

POH - Piper Aztec (6 decks)

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