JAAAppendices

032

Technical Realization: LPLUS 2002

JAA Appendices, Subject: 032 Page Edition:12-2002 1

Table Of Contents

032-915 A 3032-1014 A rev. 05.05.2003 (separate issued paper)032-2211 A 4032-2219 A 5032-2929 A 6032-3589 A 7032-3590 A, 3591 A 8032-4732 A 9032-4733 A 10032-4743 A 11032-4744 A 12032-6569 A, 6570 A, 6571 A, 6572 A, 6573 A, 6590 A 13032-6574 A, 6575 A, 6577 A, 11661 A 14032-6576 A, 6578 A, 6580 A 15032-6579 A, 6581 A, 6582 A, 6583 A 16032-6584 A, 6585 A 17032-6586 A 18032-6587 A, 6588 A 19

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032-915 A

JAA Appendices, Subject: 032 Page Edition:12-2002 3

032-2211 A

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032-2219 A

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032-2929 A

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032-3589 A

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032-3590 A, 3591 A

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0 32-4732 A

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032-4733 A

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032-4743 A

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032-4744 A

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032-6569 A, 6570 A, 6571 A, 6572 A, 6573 A, 6590 A

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032-6574 A, 6575 A, 6577 A, 11661 A

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032-6576 A, 6578 A, 6580 A

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032-6579 A, 6581 A, 6582 A, 6583 A

4. CRUISE4. 1 Requirements

The aeroplane may not be assumed to be flying above the altitude at which a rate of climb of 300 ft/minute is attained.

The net gradient of descent, in the event of engine failure, is the gross gradient +0,5%.

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032-6584 A, 6585 A

CIVIL AVIATION AUTHORITYFLIGHT PLANNING & MONITORING

DATA SHEET SEP 1

Figure 2.2 RECOMMENDED CRUISE POWER SETTINGS

TABLE 2.2.320° C LEAN

23.0 IN. HG (OR FULL THROTTLE) @ 2300 RPMOf Peak EGT CRUISE LEAN MIXTURE 3400 Ibs. Press.

Alt.IOAT Man.

Press.Fuel Flow Air Speed

Feet °C °F IN. HG PPH GPH KIAS KTASISA - 20° C(ISA - 36° F)

0 2000 4000 6000 8000

10,000 12,000 14,000 16.000

-3 -7

-11 -15 -18 -23 -17 -31 -35

26 20 13

6 -1 -9

-16 -23 -31

23.0 23.0 23.0 23.0 22.4 20.7 19.2 17.8 16.4

67.6 69.7 72.1 74.4 73.8 68.4 63.8 60.0 56.3

11.3 11.6 12.0 12.4 12.3 11.4 10.6 10.0

9.4

152 152 153 153 150 143 135 127 117

144 149 154 158

160 157 153 148 141

Standard Day (ISA)

0 2000 4000 6000 8000

10,000 12,000 14,000 16.000

17 13

9 5 2

-3 -7

-11 -15

62 56 49 42 35 27 20 13

5

23.0 23.0 23.0 23.0 22.4 20.7 19.2 17.8 16.4

65.4 67.4 69.4 71.7 71.1 66.2 61.8 58.5 55.3

10.9 11.2 11.6 12.0 11.9 11.0 10.3

9.8 9.2

147 147 148 148 145 137 129 120 109

145 149 154 159 160 157 152 146 137

ISA + 20° C(ISA + 36° F)

0 2000

4000 6000 8000

10,000 12,000 14,000 16,000

37 33 29 25 22 17 13

9 -

98 92 85 78 71 63 56 48

-

23.0 23.0 23.0 23.0 22.4 20.7 19.2 17.8

-

63.2 65.1 67.1 69.0 68.5 64.0 60.0 57.1

-

10.5 10.9 11.2 11.5 11.4 10.7 10.0

9.5 -

142 143 143 142 140 132 123 113

-

145 149 154 158 160 156 151 142

-

NOTES: 1. Full throttle manifold pressure settings are approximate.

2. Shaded area represents Operation with full throttle. 3. Fuel flows are to be used for flight planning only and will vary from aeroplane to aeroplane. Lean using the EGT.

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032-6586 A

CIVIL AVIATION AUTHORITYFLIGHT PLANNING & MONITORING

DATA SHEET SEP 1

Figure 2.3 ECONOMY CRUISE POWER SETTINGSTABLE 2.3.1

20° C LEAN

21.0 IN. HG (OR FULL THROTTLE) @ 2100 RPMOf Peak EGT CRUISE LEAN MIXTURE 3400 Ibs. Press.

Alt.IOAT Man.

Press.Fuel Flow

Air Speed

Feet °C °F IN. HG PPH GPH KIAS KTASISA - 20° C(ISA - 36° F)

0 2000 4000 6000 8000

10,000 12,000 14,000 16.000

-4 -8

-11 -15 -19 -23 -27 -31 -35

25 18 12

5 -2 -9

-17 -24 -32

21.0 21.0 21.0 21.0 21.0 20.8 19.3 17.9 16.5

52.7 54.0 55.4 56.9 58.9 60.1 56.7 54.5 52.2

8.8 9.0 9.2 9.5 9.8

10.0 9.5 9.1 8.7

126 128 130 131 132 132 123 113

95

120 125 130 136 141 144 139 132 114

Standard Day (ISA)

0 2000 4000 6000 8000

10,000 12,000 14,000 16.000

16 12

9 5 1

-3 -7

-11 -

61 54 48 41 34 27 19 12

-

21.0 21.0 21.0 21.0 21.0 20.8 19.3 17.9

-

51.8 53.1 54.4 55.7 57.3 58.5 55.6 53.5

-

8.6 8.9 9.1 9.3 9.6 9.8 9.3

8.9 -

120123 124125126126116103

118 124 129 134 140 143 137 125

- ISA + 20° C(ISA + 36° F)

0 2000

4000 6000 8000

10,000 12,000 14,000 16,000

36 32 29 25 21 17 13

- -

97 90 83 77 70 63 55

- -

21.0 21.0 21.0 21.0 21.0 20.8 19.3

- -

50.8 52.1 53.4 54.7 55.9 56.8 54.5

- -

8.65 8.7 8.9 9.1 9.3 9.5 9.1

- -

114 116 118 119 120 119 108

- -

115 121 127 132 137 141 131

- -

NOTES: 1. Full throttle manifold pressure settings are approximate.

2. Shaded area represents Operation with full throttle. 3. Fuel flows are to be used for flight planning only and will vary from

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aeroplane to aeroplane. Lean using the EGT.

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032-6587 A, 6588 A

CIVIL AVIATION AUTHORITYFLIGHT PLANNING & MONITORING

DATA SHEET SEP 1

4. RANGE PROFILEThe graph at Figure 2.4 (page 9) provides a simple and rapid means of determining the still air range (nautical air miles) for the sample aeroplane. An example of the use of the graph is shown.Note that the figures make allowance for the taxi, run-up and 45 minutes reserve fuel.

Figure 2. 4 RANGE

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