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)

24
Q

Zero Fuel Gross Weight (lbs)

25
Empty Weight (Standard, lbs)
2933
26
USEFUL LOAD (Standard, lbs)
2267
27
Engine (Lycoming)
IO-540-C4B5
28
Rated Horsepower
250
29
Rated Speed (rpm)
2575
30
Bore (inches)
5-1/8
31
Stroke (inches)
4-3/8
32
Displacement (cubic inches)
541.5
33
Compression Ratio
8.5:1
34
Dry Weight (pounds)
402
35
Fuel Capacity (U.S. gal)
144* * 140 gallons usable
36
Fuel, Aviation Grade (octane)
91/96
37
Oil Capacity (U.S. qts, each eng)
12
38
Maximum Baggage (lbs) Forward Compartment
150
39
Maximum Baggage (lbs) Rear Compartment
150
40
With oxygen installed
105
41
Baggage Space (cubic ft) Forward Compartment
17.4
42
Baggage Space (cubic ft) Rear Compartment
23.2
43
Baggage Door Size (in) Forward Compartment
19.5 x 30.5
44
Baggage Door Size (in) Rear Compartment
30 x 31
45
Wing Span (ft)
37.2
46
Wing Area (sq ft)
207.56
47
Length (ft)
30.2
48
Height (ft)
10.3
49
Wing Loading (lbs per sq ft)
25.05
50
Power Loading (lbs per hp)
10.4
51
Propeller Diameter (maximum, in)
77
52
Wheel Base (ft)
7.5
53
Wheel Tread
11.3
54
Tire Pressure
Nose 27 Main 46
55
Tire Size
Nose (four ply rating) 600x6 Main (eight ply rating) 700x6