STEMME S6-RT Скачать руководство пользователя | Manualshive

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Date of Issue: 18. November 2011

Date of Rev.: . .

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This section of the Flight Manual contains a technical description of the aircraft
and its systems and equipment. There are also user notes for each system.

The description of installed non standard systems is given in section 9.

Additional explanations of the components and systems of the Stemme S6 RT
are given in the Maintenance Manual (Stemme Doc. No.: P500 006.000).

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Содержание S6-RT

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Страница 85: ... 3 00 0 3 2 0 40 96 0 0 00 4 B 6 6 4 7 3 0 7 7 4 0 0 0 3 5 3 2 B 7 3 9 1 6 E 0 80 6 D 09 0 3 2 0 40 6 7 3 0 3 0 7 3 0 3 0 L 1 0 M 3 5 21 00 1 9 0 ...

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Страница 87: ... 3 00 6 1 9 5 7 0 40 0 3 0 6 4 3 0 7 7 4 C 3 0 C 6 6 3 7 B 0 3 0 3 0 7 0 3 3 4 00 C 3 0 C D D 4 B 4 7 0 0 3 1 3 2 00 0 0 9 B 4 7 0 0 4 2 8 3 B H 4 ...

Страница 88: ... 3 00 6 4 3 0 B 4 7 3 0 7 7 4 C 3 0 C 4 0 4 7 0 0 3 1 3 2 00 0 0 9 0 4 7 0 0 4 1 3 B H 4 6 4 0 4 7 3 0 7 7 4 6 4 4 0 0 3 9 ...

Страница 89: ... 3 00 1 5 0 3 0 7 0 7 9 0 1 8 40 3 0 4 1 3 B H 4 6 0 0 7 3 0 7 7 4 1 5 0 2 0 7 0 B 16 3 1 K 3 B H 30 1 B H 1 3 B H C 3 0 C 5 0 4 4 7 B 1 2 3 3 0 0 0 9 0 6 4 4 7 3 0 7 7 4 ...

Страница 90: ...00 3 7 0 3 3 9 3 0 7 0 3 3 0 3 F G 3 3 6 B 1 2 3 4 4 0 0 0 7 0 0 3 0 0 B B 9 D 0 1 D 0 B D 0 7 6 6 0 0 0 0 0 3 0 6 0 7 4 4 7 0 0 0 B 2 0 0 B B 0 0 0 9 0 0 1 0 0 0 9 0 0 1 7 0 40 0 0 0 0 3 3 0 7 0 0 0 0 0 4 ...

Страница 91: ... 3 00 0 0 0 1 3 0 1 0 0 0 7 0 3 0 0 9 0 2 B 1 2 3 3 4 0 0 0 0 3 7 0 0 0 0 2 B H 0 4 3 B 1 2 4 4 0 0 0 2 4 3 1 0 0 0 7 0 2 0 40 6 0 0 0 0 9 0 3F 0 0 4 0 3 7 0 L 7 9 4 ...

Страница 92: ... 3 00 3 0 3 3 2 3 3 6 0 0 0 R R F B H 0 4 3 B 1 2 4 4 0 0 0 2 4 3 3 1 0 0 0 7 0 0 40 3 5 3 3 6 3 0 0 0 3 3 0 B H 3 5 9 0 5 3 3 8 59 D 2 3 6 3 1 3 7 6 2 1 F 1 4 0 0 0 0 0 H 1 1 3 3 3 0 0 3 3 3 7 0 ...

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Страница 97: ... 4 1 1 5 5 1 A 0 5 7 B 2 0 2 0 1 0 A 0 5 7 B 2 0 2 0 1 5 A 0 5 7 9 5 1 7 3 B 2 0 2 0 1 D 5 A 5 9 5 1 7 3 B 2 0 2 0 6 1 1 A 0 5 7 5 7 B 2 0 2 0 1 1 A 0 5 7 5 7 B 8 2 0 8 2 0 6 1 0 1 1 A 0 5 7 B 2 0 2 0 ...

Страница 98: ...1 E 9 1 4 9 6 9 1 1 0 7 E 01 1 1 4 1 A B 1 6 AE B 1 5 3F 1 41 4 8 0 C GH 6 2 1 4 8 0 C G 6 1 1 41 1 6 8 7 E 1 03 6 4 3 3F 6 2 4 2 2 5 0 7 4 1 1 H 1 6 4 6 2 2 1 2 6 9 2 4 9 3 4 1 4 1 D A 1 4 1 6 B 1 1 1 1 1 ...

Страница 99: ...1 D 1 6 1 6 1 6 6 1 5 6 1 4 6 1 4 6 6 I 2 J 6 6 1 6 J 6 1 J 6 6 4 6 1 6 1 1 1 6 1 6 22 1 6 1 6 4 6 1 1 4 1 6 1 6 6 3 6 A 1 2 6B 6 2 6 2 1 4 2 2 1 1 9 4 0 7 4 A 1 HB 2 1 H 3 1 8 2 I 6 3 1 6 2 1 3 1 6 1 2 1 6 2 9 1 2 1 6 ...

Страница 100: ...A B 6 2 1 5 7 H 2 2 6 1 2 1 6 1 6 9 1 4 6 6 6 6 6 5 0 6 6 6 6 6 5 0 6 1 2 6 4 1 4 1 2 6 1 6 6 0 9 1 1 2 9 9 1 2 6 2 1 1 1 3 6 1 1 6 I 6 4 6 4 6 2 6 6 1 6 1 6 0 8 1 6 1 49 4 6 1 1 49 6 4 4 6 6 1 1 6 6 1 6 3 6 4 ...

Страница 101: ... 4 1 1 4 1 49 6 1 1 6 1 4 1 I 6 1 6 4 1 2 6 1 9 4 2 4 2 6 6 6 A6 B 6 1 1 6 1 1 4 4 1 3 2 4 1 1 6 1 1 1 1 1 1 1 3 2 2 1 1 1 7 E 9 2 1 A 4 B ...

Страница 102: ... 4 1 1 6 2 6 A 1 29 B 4 1 1 6 26 1 6 61 3 4 6 1 26 1 3 2 2 6 H 7 1 2 6 1 6 1 6 2 7 2 4 6 2 2 A 6 J B 1 7 3 2 1 4 H 9 1 4 1 7 6 I 1 1 4 6 ...

Страница 103: ...1 1 4 29 1 2 49 1 J 1 H 1 4 1 1 6 2 1 0 7 E 1 4 1 1 4 1 A B 1 6 AE B 1 5 3F 1 41 4 8 0 C GH 6 2 1 4 8 0 C G 6 1 1 41 1 6 0 7 9 2 1 9 2 9 1 9 1 49 9 9 9 J 1 1 11 49 2 1 4 11 4 1 2 9 1 2 9 1 1 4 1 4 1 9 6 2 1 2 4 1 1 1 9 4 A B ...

Страница 104: ...6 2 1 2 1 4 1 AE 9 6 6 HB 6 1 1 3 3F J 1 2 4 9 1 4 1 4 3 3F 55D 2 5 2 1 6 3 3F 6 1 A 2 6 6 1 2 B 49 55 8 7 E 4 19 6 H 6 2 2 1 1 4 1 0 7 6 1 6 1 2 1 6 1 4 1 A 1 B A 1 B 1 1 3 3F A 6 29 2B 1 9 1 6 4 6 1 2 49 55 8 35 ...

Страница 105: ... 3F 1 2 41 1 A 6 29 2B 1 2 3 3F 4 5 6 55 3 6 1 3 3F E 35 A 6 1 6 6 J 9 B 5 3 1 4 6 1 2 A B 1 1 6 1 1 1 6 1 0 7 03 2 1 6 6 1 A B 1 3 3F 1 4 4 1 49 1 1 1 2 E 9 2 1 8 6 3 6 22 1 3 6 3 3 3 1 3 6 9 1 2 3 3 3F 4 5 3 3 1 5 F 7 ...

Страница 106: ... 4 1 3 6 3 3 1 3 3 A 10 1K 0 B 3 2 J 55 1 3 3F 6 9 6 6 1 2 7 2 1 1 2 0 3 2 1 9 6 0 A 7 B 6 9 1 9 6 E 1 5 3 1 3 2 1 1 1 1 0 AJ 4B L 2 1 1 1 1 6 1 9 6 6 5 3 6 6 9 1 9 3 6 6 C 0 C 6 C 0 C ...

Страница 107: ...1 B 41 3 3F 1 9 1 9 2 1 1 41 5 3 3F 41 9 1 41 1 1 1 2 3 3F 2 9 1 6 1 9 1 1 1 1 1 5 1 7 5 3 9 9 1 1 1 1 6 3 3F 6 1 1 1 8 1 1 3 3F 1 4 1 3 2 1 9 9 0 5 6 0 0 4 4 5 1 3 3F A B 6 AE 4B 3 3F 8 0 C G A3 3F 1 1 2 B 1 2 1 1 4 1 1 6 8 0 C G 10 1 2 9 1 4 ...

Страница 108: ... 4 1 1 41 4 4 4 1 7 1 4 1 6 41 4 1 1 4 A B 8 0 C G 6 6 AE B 4 11 1 1 1 2 2 6 2 8 0 C G 3 3F 1 6 1 8 0 6 AE 4B A B 1 6 4 1 9 3 2 6 1 1 6 1 1 1 2 3 2 11 6 11 1 2 1 1 6 1 ...

Страница 109: ... 4 1 3 3 3F 4 1 4 1 9 8 3 3 3F 1 4 5D 3 3F 1 2 9 1 1 5D 3 3F 2 A 1 B M 3 3 2 0 3 2 4 4 6 3 3F 1 A B 3 3F 1 A B 9 0 5 3 4 4 3 2 1 3 3F J E 1 3 3F J 5 1 7 5 A B 3 2 6 6 AE B 9 6 9 3 1 9 6 ...

Страница 110: ...1 4 1 1 A 03 1 1 6 2 1 3 2 6 03 3 3F 4 3 5 5 1 7 5 A B 5 1 1 37 3 3F 1 6 3 3F 6 1 2 3 5 3 6 A 0 B 5 3 9 3 6 3 3F 8 1 3 3F 1 J 4 1 1 1 0 3 3F A 4 6 B 1 5 1 7 3 3F J 9 1 1 41 4 1 3 3F 1 1 2 5 1 7 3 3F 1 1 1 0 0 A 1 1B 5 2 3 3F 9 ...

Страница 111: ...5 3 3F 9 1 N5 7 N3 1 4 3 3F 9 1 1 4 11 3 3F 9 1 1 4 8 3 3F 9 1 N5 7 N3 1 4 N 5 3 3F 9 1 1 4 2 3 3F 9 1 1 4 6 AE 4B 3 3F 6 4 1 3 3F 6 A 1 49 2 1B 6 7 A B 3 3F 1 0 3 3 3F 6 AE 4B 0 0 3 J 3 3F9 J A B 6 4 E 6 4 4 3 4 35 1 5 3 A 9 1 B 1 ...

Страница 112: ... 4 1 1 11 1 3 3F 1 3 1 4 1 3 A 9 9 11 9 9 2 9 6 B 8 5 1 7 5 A 1B 6 AE 4B 3 3F 1 1 3 3F 9 1 1 1 1 5 5 1 7 3 3F A B ...

Страница 113: ...7 H 1 1 1 4 1 1 8 7 1 1 4 1 1 5 2 0 2 0 H 1 1 9 4 1 1 4 7 1 1 1 5 1 1 3 1 1 2 0 2 0 7 1 2 0 19 1 1 4 1 4 1 9 1 1 1 1 1 1 9 41 4 4 1 4 1 4 1 1 4 1 1 1 1 A6 0 3 B 1 1 6 1 A 1 B 4 4 49 6 4 1 49 1 1J 2 4 6 2 4 1 6 1 9 1J 1 2 ...

Страница 114: ... 3 6 A 4 B 2 E 2 6 AE 4B 6 3 3 3F 1 6 1 4 6 3 1 1 6 3 3F 6 1 6 3 3F 1 6 7 1 3 3F 1 2 A B 49 6 2 8 O 4 3 3F 6 7 A B P 4 A 0 B9 3 3F 3 3F 1 6 9 C A C B 0 C 4 3 4 2 3 3F 9 C A C B 0 C A 4 6 4 2B 3 4 2 3 3F 2 4 1 1 H ...

Страница 115: ... 4 1 3 2 4 1 A Q L 0 L3B 4 6 A R L 0 L3B 5 1 A Q L 0 L3B A 6 A R L 0 L3B 5 3 3F 35 6 3 A B A B9 B 7 1 4 1 6 1 9 6 2 8 3 3F 1 9 6 1 4 6 3 3F 2 9 1 6 7 3 3F9 4 6 3 2 4 A 1 9 3 4 B 7 2 G 9 4 2 4 1 3 6 1 6 ...

Страница 116: ... 4 1 5 7 1 6 2 3 6 6 1 A 6 3 0 0 1 A EDB 2 E 2 5 3 6 5 E 2 6 E F 5 2 3 3F 6 2 6 9 3 3 3F9 5 0 3 B 5 0 5 1 2 5 7 1 2 E 2 3 3 6 4 2 5 1 5 3F 0 5 7 3 2 4 6 8 3 2 05 6 ...

Страница 117: ...3 3F 6 2 Q 9 1 6 05 Q 6 1 9 2 B 2 6 3 3F 1 4 G9 1J 1 1 1 A B 1 4 3 5 1 2 2 6 8 7 5 1 6 1 1 1 4 4 7 1 1 4 A 1 B 55 3 1 3 1 1 3 E 2 1 3 3F 3 3F A B 3 3F 9 9 3 3 3F9 5 0 1 5 6 4 4 O A 1 B 4 8 1 6 A 4 1 1 4 2 B ...

Страница 118: ... 4 1 A 4 6 4 2B 5 A 3B 3 A 9 9 11 9 9 2 9 6 B 3 4 35 A 9 9 B 1 3 1 3 3F 2 E 2 5 6 14 2 3 3F 1 4 6 8 7 6 6 1 1 1 2 1 1 2 H 5 5 7 D E 2 3 3F 6 1 6 9 C 1 1 4 55 A 6 1 9 1 3 B 8 7 5 1 6 1 1 1 4 4 ...

Страница 119: ... 4 1 7 1 1 4 A 1 B 55 3 1 3 1 1 0 0 1 3 3F 6 A 1 B 3 3F 1 9 C A C B 0 C 9 9 3 3 3F9 1 6 A 4 1 4 B 8 2 5 2 1 2 03 2 4 6 2 0 2 0 9 D 6 E 0 3 0 7 1 4 1 1 1 4 1 0 7 1 1 1 4 1 1 ...

Страница 120: ... 6 1 1 1 1 1 1 1 1J 1 H 3 1 A B 3 37 F 5 5 C D 6E 3 37 A F 5 5 C D 6 E 4 1 4 A B 5 1 7 3 A B 1 4 4 1 1 1 3 2 0 2 0 3 3F 1 9 1 3 3F 1 9 3 5 1 7 4 1 3 3F 1 1 1 1 1 1 2 0 2 0 49 P 3 1 2 4 0 3 E 1 6 9 3 3 5 3 A1 B P 1 1 R ...

Страница 121: ... 4 1 0 0 0 0 7 6 1 6 5 1 2 3 0 1 4 2 6 1 P 1 1 R N3 N 5 1 1 3 6 3 1 9 1 9 1 0 3 4 9 4 1J 6 A B 2 1 6 6 4 6 4 4 6 4 A6 B 1 6 6 1 6 2 4 2 6 1 6 4 2 6 4 1 4 9 1 1 4 2 4 1 4 19 6 2 2 4 2 1 ...

Страница 122: ... 4 1 4 2 4 2 0 0 2 1 6 1 7 6 A4 6 5 B 1 49 1 6 1 8 0 2 6 1 4 1 1 4 1 4 2 19 1 9 2 4 1 6 5 2 4 4 1 9 A 2 1 B 2 4 2 7 1 6 6 A4 6 5 B 6 1 6 1 1 4 1 0 2 3 5 1 3 2 0 8 2 0 1 6 1 3 Q L 0 L3 6 ...

Страница 123: ... 8 4 1 6 5 9 6 6 1 4 3 6 35 8 35 N 0 5 7 6 N 5 8 7 6 1 1 1 6 6 1 1 4 7 E 1 6 5 9 6 2 6 N 0 5 7 1 4 0 2 8 7 6 6 1 1 19 5 5 6 1 1 4 8 7 A6 1 B 1 1 1 1 ...

Страница 124: ... 4 1 0 7 6 4 4 6 6 1 7 9 1 8 0 9 1 1 2 0 A 8 B 1 0 8 A6 2 0 0 2 B 6 6 6 9 6 7 8 1 3 3 3F 1 6 1 4 6 3 1 1 3 6 4 7 3 3F 3 3F 1 6 9 C A C B 0 C 49 3 4 8 3 2 4 1 A Q L 0 L3B 4 6 A R L 0 L3B ...

Страница 125: ... 4 1 5 1 A Q L 0 L3B G 5 6 A R L 0 L3B 1 5 0 5 7 9 6 9 6 1 6 B 1 4 E B 1 9 E 9 7 1 4 1 6 1 9 6 2 7 1 1 6 4 A 1 B 4 6 4 1 0 A 1 B 7 1 A 0 B 6 1 2 0 2 0 1 6 4 9 1 3 3F 1 9 6 1 4 6 3 3F 1 6 7 3 3F 4 6 3 3F ...

Страница 126: ... 4 1 3 3F 3 2 4 A 1 9 2 3 4 7 2 G 9 4 2 4 8 1 3 A 6 2 6 35 B 6 4 0 4 2 19 1 1 2 1 4 1 1 1 4 6 6 9 1 0 7 1 1 4 1 1 0 7 2 1 1 9 6 1 6 1 1 2 1 1 2 1 6 ...

Страница 127: ... 4 1 0 4 3 5 1 6 2 1 5 5 A 1 1 B 2 1 1 0 5 7 3 6 4 4 6 5 1 7 A B 3 3F 5 3F A B 1 1 H P 8 5 1 6 A 4 1 1 4 2 B 2 1 4 7 2 1 4 1 1 1 6 1 9 2 1 1 1 4 6 5 03 1 6 1 6 9 2 4 2 E 2 3 4 1 6 ...

Страница 128: ... 4 1 7 1 1 4 6 6 N5 7 6 9 1 1 4 1 0 4 6 4 4 1 5 5 A 1 1 B 2 1 1 0 5 7 3 6 4 4 6 5 1 7 A B 3 3F 5 3F A B 1 1 H P 8 1 6 A 4 1 1 4 2 9 B 2 5 3F9 1 1 4 5 3F 4 1 1 N3 1 5 A 1 1 6 6 1 B ...

Страница 129: ... 1 6 6 6 2 1 1 1 6 9 1 1H 6 2 4 6 11 2 6 1 03 6 1 2 1 1 1 1 1 6 5 5 4 6 5 03 1 6 E 2 3 4 1 6 0 7 2 1 1 9 6 1 6 1 1 14 4 4 2 1 1 1 S 1 6 2 A R B 6 6 6 A B S 1 1 1 1 1 7 4 4 6 2 1 1 2 4 3 1 5 3F 7 2 1 2 4 6 03 19 03 4 1 ...

Страница 130: ... 4 55 8 7 5 1 6 1 1 1 4 4 4 1 A 0 B 19 D 6 E A 6 5 7 B 8 7 N5 7 0 5 7 2 4 03 1 6 4 5 1 7 3 A B 3 3F 1 9 3 1 6 6 6 55 8 7 5 1 6 1 1 1 4 4 7 03 19 6 1 4 2 1 03 1 2 N3 6 6 1 1 9 03 6 6 2 3 1 5 3F 4 1 A 0 B 19 ...

Страница 131: ... 4 1 D 6 E A 6 N5 7 B 5 1 7 3 A B 3 3F 1 9 8 7 N5 7 N 0 5 7 2 4 03 1 6 4 3 1 6 0 0 7 2 1 1 9 6 1 6 1 1 2 1 1 2 1 6 6 0 1 5 5 A 1 1 B 2 1 1 6 9 0 5 7 5 1 7 A B 3 3F 5 3F A B 1 1 H ...

Страница 132: ... 4 1 P 2 1 4 7 2 1 4 1 1 1 6 1 9 2 1 1 1 4 6 5 03 1 6 1 6 9 2 4 2 E 2 3 4 1 6 8 1 R 1 1 7 1 1 4 6 6 N5 7 6 9 1 1 4 1 6 5 6 5 2 3 1 5 3F 4 ED 0 1 3 11 1 E 2 49 2 2 ...

Страница 133: ... 8 4 1 5 3 5 2 E 2 1 6 1 3 Q L 0 L 3 3 0 0 6 6 6 6 AE 4B 8 3 6 35 35 1 3 3 3 4 A 9 9 B ...

Страница 134: ...1 1 1 4 6 6 5 5 1 1 2 0 2 0 2 0 2 0 2 0 2 0 2 0 2 0 2 0 2 0 2 0 2 0 8 2 0 2 0 2 0 8 2 0 8 2 0 2 0 2 0 2 0 6 4 2 1 6 1 1 4 1 6 4 6 1 A B 1 4 4 1 1 4 1 6 4 6 1 1 1 4 6 1 6 4 S L 0 S L3 4 6 1 1 6 9 1 1 1 1 1 1 4 1 4 1 4 49 2 6 1 6 10 6 1 4 1 19 4 6 1 6 ...

Страница 135: ...7 1 1 1 1 6 1 1 1 1 6 1 03 1 6 4 9 6 1 1 1 1 1 2 1 1 4 2 0 2 0 1 1 1 6 1 A GB 1 1 6 1 A GB 1 2 6 2 1 1 1 4 9 1 6 9 1 1 1 5 6 4 0 4 6 1 6 1 1 5 6 5 5 03 1 4 4 1 1 4 1 5 5 3 66 4 5 1 I 1 4 1 03I 4 6 1 7 1 6 5 2 0 2 0 6 0 5 7 ...

Страница 136: ... 1 03I 4 6 1 1 1 19 1 1 3 1 4 2 0 2 0 4 2 0 2 0 2 0 2 0 6 5 5 6 1 1 9 6 1 3 3 1 4 4 1 1 6 D 4 4 4 4 14 1 1 1 1 1 6 1 03 1 1 4 1 1 1 1 6 1 1 1 6 1 2 0 2 0 6 1 4 6 1 1 2 4 1 1 1 1 1 6 1 1 1 1 1 1 6 D 4 6 1 11 4 6 2 11 6 1 6 0 4 6 6 1 2 0 2 0 ...

Страница 137: ... 4 1 3 1 3 9 F 5 5 7 9 4 1 1 1 1 1 9 41 4 4 1 4 1 4 1 1 1 0 1 4 6 1 03 6 1 1 6 1 4 1 1 1 1 1 9 1 4 4 1 1 1 1 1 1 2 1 1 4 2 0 2 0 1 1 1 6 1 A GB 1 1 6 1 A GB ...

Страница 138: ... 4 1 1 1 9 9 1 1 1 1 1 9 1 4 8 7 1 2 039 1 4 4 1 0 7 03 1 2 03 1 ...

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Страница 146: ...0 4 4 4 1 8 00 0 8 0 0 8 00 10 A A A ...

Страница 147: ...4 5 6 07 07 7 107 8 8 9 C 2 6 3 98 D 4 8 62 E 6 6 0 00 1 8 9 C F 698 D 4 8 62 E 6 6 0 1 9 9 C6 3 98 6 8 62 E 0 6 6 0 0 0 11 9 8 9 C 2 6 3 98 6 8 F66G B 6 6 1 0 0 0 9 9 C F 698 6 8 F66G B 6 6 0 1 0 1 1 C F 98 5 D 4 8 62 E 6 6 0 1 ...

Страница 148: ...5 H 4 4 4 4 6 6 6 3 8 4 4 8 4 3 6 5 5 6 3 B 2 F8 3 4 5 6 07 07 7 107 9 9 C6 3 98 62 E 0 6 6 0 0 0 11 9 8 9 C 2 6 3 98 F66G B 6 6 1 0 0 0 9 9 C F 698 F66G B 6 6 0 1 0 1 1 8 9 C 2 6 3 98 62 E 6 6 1 0 0 0 ...

Страница 149: ... 1 8 00 0 8 0 0 8 00 10 4 2 6G 6 6 3 8 4 4 4 4 8 7 4 7 8 ...

Страница 150: ... 1 8 8 8 F66 21 2 D 9 2 6 3 9 I 5 5 I 5 5 1G 8 6 3 B 2 68 2 2 2 5 2 4 4 7 D 2 4 J 8 4 8 8 4 2 1G D 2 D 2 4 ...

Страница 151: ... 9 8 8 0 55 5 5 0 0 10 5 0 5 0 5 5 00 5 0 5 0 5 5 0 5 5 0 0 0 005 5 50 5 5 5 5 5 0 5 5 0 5 0 5 0 5 0 0 0 0 0 0 005 0 50 5 0 5 5 0 5 00 0 0 5 5 5 0 5 0 5 5 0 5 0 ...

Страница 152: ... 7 D 9 F 69 6 3 8 I 5 5 6 7 2 7 D 9 F 9 6 3 5 5 7 A 6 0 6 F66 21 2 D 9 2 6 3 9 6 3 B 7 I 5 5 ...

Страница 153: ... 0 2 0 9 2 4 4 J 8 4 8 8 8 4 1G 4 D D 4 ...

Страница 154: ... B 4 4 4 0 D 9 F 69 6 3 0 5 5 F 0 F F 0 4 4 7 4 H 4 1 4 7 8 8 D 7 4 F 4 F 7 4 4 8 4 I 1 0 I 4 2 7 7 0 I 00 55 1 7 0 I 0 5 ...

Страница 155: ... during Weighing 6 3 6 3 1 Logsheet for Report of Empty Mass and CG Location 6 5 6 4 1 Mass Moments and Useful Load 6 9 6 4 2 Calculation of Proper Loading for Flight 6 10 6 5 1 Equipment List 6 13 ...

Страница 156: ...ll approved equipment for this aircraft equipment list is given in chapter 6 5 The weight empty CG location and empty mass moment for the aircraft are determined during the pre delivery inspection This data is then noted in the logsheet for report of the empty mass and the CG location chapter 6 3 1 Repeat the weighing of the aircraft in the intervals required by law generally every 4 years The emp...

Страница 157: ... P500 006 000 Installed equipment according to the current equipment list No loose ballast Aircraft dry including operating fluids Brake fluid Amount of engine oil 0 5 0 8 US gal 2 3 liters Coolant 0 63 0 66 US gal 2 4 2 5 liters Unusable fuel 0 55 US gal 2 1 liters 0 3 US gal 1 liter optional The aircraft s empty mass and empty CG location are determined using the following method Every wheel of ...

Страница 158: ...ence points are projected vertically down onto the ground from the root leading edge of the left and right wings This generates a vertical plane The connecting line between the two reference points is the reference line From this reference line the distance to the front landing gear distance b and main landing gear distance a is measured See Illustration 6 1 Aircraft alignment during weighing The ...

Страница 159: ...s in equipment are made then new empty mass and empty CG location can be determined through calculations If the cause of the changes is NOT precisely known for example when making repairs the aircraft must be weighted again The following logsheet describes the chronological changes in the aircraft s empty mass and CG location The logsheet can be reused for subsequent reports These changes might be...

Страница 160: ...to the aircraft structure and or equipment Registration No Serial No Sheet No 0 0 Current Empty Mass Cleared by Authorized Personnel Con No Date Description of action taken Mass lbs Lever to RP ft Moment ft lb 1 Weighing at delivery ...

Страница 161: ...data determine the corresponding mass moments by using Diagram 6 4 1 Mass Moments and useful load Loading diagram or calculate the mass moments Keep the negative value of the lever in mind if a location is infront of the RP Use seperate columns in row 2 for the left and right seat in table 6 4 2 Calculation of the proper loading for flight 3 Determine the load carried in the rear baggage compartme...

Страница 162: ...calculate the total mass and total moment from row 4 and row 7 of the table Place these values in row 8 This represents the aircraft in its T O configuration with fuel The constant mass moment from row 5 as result of retraction of landing gear must NOT be considered here Due to displacement of C G forward with maximum fuel load the critical case to be checked is with landing gear extended most for...

Страница 163: ...9 Revision Date of Issue 18 November 2011 Date of Rev 1 e g Step 2 e g Step 6 e g Step 3 ...

Страница 164: ... right 3 Rear Baggage Compartment Lever 5 5741 ft 4 Operating Mass and Total Mass Moment without Fuel Sum 1 through 3 5 Displacement of Mass Moment due to retraction of landing gear 152 14 ft lb 6 CG Location in RP in behind RP Allowed 454 5 6 7 Fuel load Useable Fuel 0 744kg l Lever 0 3642 ft mean value see Diagram 6 4 1 8 Total Operating Mass and Total Mass Moment with Fuel Sum 4 and 7 9 CG Loca...

Страница 165: ... When calculating the CG position without including the change of fuel mass during flight the CG must be within the following limits 454 78 5 9 5 6 7 5 69 behind RP 78 9 6 7 9 ...

Страница 166: ...t must be performed in correspondence with the Maintenance Manual The given equipment list contains the following information for a better overview The column Con No includes a continuing number and a character for specification with the meaning I Instruments A Avionics M Miscellaneous Equipment Items The columns Mass and Lever give the mass and the effective lever relative to the reference plane ...

Страница 167: ...443 I 4 Compass Airpath C2400 I 5 Variometer Winter 5STVM5 2 I 6 Soaring Computer incl Electr Variometer LX Navigation LX 166 I 7 CDI Garmin Gl 106A I 8 MAP Gauge UMA Instr I 9 Oil Pressure Gauge UMA Instr I 10 Oil Temp Gauge UMA Instr I 11 CHT Gauge left right UMA Instr I 12 Ammeter UMA Instr I 13 Voltmeter UMA Instr I 14 FuelGauge right left UMA Instr I 15 Tachometer Rotax I 16 Trim Indicator I ...

Страница 168: ... 0 0 Con No Description Manu facturer Type Spec No Inst Mass lbs Lever ft or I 24 I 25 I 26 I 27 I 28 I 29 I 30 I 31 I 32 I 33 I 34 I 35 I 36 I 37 I 38 I 39 I 40 I 41 I 42 I 43 I 44 I 45 I 46 ...

Страница 169: ... A 1 COM NAV GPS Garmin GNS 430W A 2 Electronic Flight Information Sys Dynon EFIS D 10A A 3 Transponder Garmin GTX 330 A 4 Audio Panel Garmin GMA 340 A 5 Radio Becker AR 4201 VHF A 6 Transponder Becker BXP 6401 2 Mode S A 7 GPS Garmin GPSMAP 695 A 8 Intercom PS Eng PM 1000 A 9 A 10 A 11 A 12 A 13 A 14 A 15 A 16 A 17 A 18 A 19 A 20 A 21 A 22 A 23 A 24 ...

Страница 170: ...w Tail Clutch Tost E22 not applicable for S6 RT M 5 Tow Bar STEMME not applicable for S6 RT M 6 Release Mechanics STEMME not applicable for S6 RT M 7 Rear view Mirror left STEMME not applicable for S6 RT M 8 Rear view System Camera Display STEMME not applicable for S6 RT M 9 Solar Panel STEMME M 10 M 11 M 12 M 13 M 14 M 15 M 16 M 17 M 18 M 19 M 20 M 21 M 22 M 23 ...

Страница 171: ...ember 2011 Date of Rev 0 0 Serial No Reg No Date Con No Description Manu facturer Type Spec No Inst Mass lbs Lever ft or M 24 M 25 M 26 M 27 M 28 M 29 M 30 M 31 M 32 M 33 PPPPPPPPP PPPPP PPPPP Clearance Installed Equipment List Date ...

Страница 172: ...Pedals 7 7 7 6 1 Layout of the Instrument Panel 7 13 7 6 2 Control Elements of the Instrument Panel 7 15 7 7 1 Nose Gear and Steering 7 17 7 7 2 Main Gear and Brakes 7 17 7 7 3 Landing Gear Doors 7 18 7 7 4 Hydraulic Actuation 7 18 7 7 5 Operation and Electrical system of retractable Landing Gear 7 18 7 7 6 Procedures after Emergency Extension of the Landing Gear 7 20 7 10 1 Canopy 7 24 7 10 2 Ent...

Страница 173: ...m 7 36 7 11 8 Load Transmission and Transmissions 7 37 7 12 1 Design of the Fuel System 7 39 7 12 2 Control Elements and Gauges in the Cockpit 7 40 7 12 3 Circuit Logic and Operation of the Fuel Pumps 7 40 7 12 4 Measurement of the Amount of Fuel 7 42 7 13 1 Power Supply and Battery System 7 43 7 13 2 Ignition System 7 43 7 13 3 Electrical Circuits 7 43 7 13 4 Electrical Consumers and Circuit Brea...

Страница 174: ...contains a technical description of the aircraft and its systems and equipment There are also user notes for each system The description of installed non standard systems is given in section 9 Additional explanations of the components and systems of the Stemme S6 RT are given in the Maintenance Manual Stemme Doc No P500 006 000 ...

Страница 175: ...ne inner wing left and right outer wings and two winglets An integral tank for fuel is located in the forward area of the right inner wing an optional second tank can be installed in the left inner wing The airbrakes are located in the inner section of the outer wing The wing spars of all wing sections are made completely of carbon fiber composites The wing shells are made of CFC sandwich elements...

Страница 176: ...matic Design CFC Sandwich 2 part Aileron across the span of the outer wing Mounting Inner aileron 9 joints and 1 control connector each Outer aileron 7 joints and 1 control connector each Axial fixations near the control connectors Operation Operated with control rods Aileron differential realized by parted ailerons Outer ailerons deflect more than inner ailerons Flap deflection is also overlayed ...

Страница 177: ...d to the rudder pedals The steerable nose wheel is operated by control cables Design CFC Sandwich Mounting 6 joints and 1 control connector each Operation Operated with push rods flap deflection is effective across whole wing span inner wing and outer wing The flaps are set by using the flap lever with detents Setting indicator is located near the flap lever The flap deflection is overlaid over th...

Страница 178: ... be locked properly after they have been adjusted The rudder pedals are unlocked by pulling the black handle forward of the control stick 7 2 8 To move the pedals forward pull the handle and push onto the pedals with your feet Keep the handle pulled until the pedals have reached the position you want Afterwards release the handle and lock the pedals 7 2 8 To move the pedals rearward pull them back...

Страница 179: ...located at the inner section of the outer wing Design Airbrake designed as aluminum section sealing plates made of CFC placed at top ends of airbrakes Mounting 2 rotational shafts in each airbrake box Operation Operated with control rods the airbrakes lock at the wing joint The airbrakes are operated by moving the blue airbrake lever ...

Страница 180: ...ore detailed descriptions of each element are given in each relevant section of this Flight Manual as well as in the Maintenance Manual For operation instructions of the installed equipment refer to the Maintenance Manual of the STEMME S6 S6 RT STEMME Doc No P500 006 000 and to the operation manuals of the manufacturer provided for the installed equipment ...

Страница 181: ...7 10 Revision Date of Issue 18 November 2011 Date of Rev 6 2 2 8 3 2 1 4 5 2 6 7 8 9 10 11 12 13 1 ...

Страница 182: ... clamping 7 Canopy Jettison Red handle on top of the forward center console below the instrument panel 8 Cowl Flaps Lever Black handle on top of the forward center console below Canopy Jettison handle to operate the inlets and outlets of the engine cowling The lever is unlocked by pushing a push button and locked again by releasing the button 9 Rudder Pedals One pair for each seat in the foot area...

Страница 183: ... Valve Red rotary handle on the rear center console at the upper canopy frame behind head position of the pilot 15 Handle bar for Emergency Extend Black pull handle next to fuel valve pulling of the handle opens the hydraulic valve for emergency extend by bowden cable 14 15 ...

Страница 184: ... November 2011 Date of Rev 111111111111111111111111111111111 The illustration shows the layout and position of the most important control elements and instruments on the instrument panel in the standard configuration 6 9 S N IIIIII ...

Страница 185: ...ctronic Variometer 21 Voltmeter 8 Control Knob Canopy Ventilation 22 Oil Pressure Gauge 9 Trim Indicator 23 Cylinder Head Temperature right 10 Compass 24 Fuel Gauge right Tank 11 Audio Panel Garmin 25 Ammeter 12 COM NAV GPS Garmin 26 Engine Hours Meter 13 Transponder Garmin 27 opt 12 V Socket 14 Tachometer of Engine Announciator panel on the instrument panel L1 Low Fuel Caution Light yellow L5 Int...

Страница 186: ...Bus A17 COM Radio A9 Ldg Gear Power The following illustration shows the layout of the additional control elements of the instrument panel in the standard configuration 6 Control elements of the instrument panel 1 Master Switch Batt and Switch for Engine Bus Eng 5 Fuel Pressure Difference Gauge 2 Landing Gear Lever 6 TCU Isolation Switch red safety switch 3 Control Unit for Propeller Pitch 7 Main ...

Страница 187: ...er 2011 Date of Rev Circuit breakers switches of the instrument panel S1 Auxiliary Fuel Pump S5 POS Lights S2 Fuel Transfer Pump for optional left tank S6 Landing Light S3 Instrument Light S7 Avionics Master Switch S4 Anti Collision Light ...

Страница 188: ...a hydraulic actuator connected to the nose gear drag strut In the fully extended position the drag strut locks by its overcenter locking and additional spring independent from hydraulic pressure 7 The struts of the main landing gear are welded tubes which are stiff to torque They are connected to the central steel tube framework of the midsection of the fuselage via retraction kinematic The elasti...

Страница 189: ... kinematical to the nose landing gear leg by hinge kinematic In the rear section of the center fuselage steel frame the hydraulic drive unit is installed The unit consists of the electrically powered hydraulic pump including controller for the pressurization of the complete hydraulic system and a pressure reservoir for emergency extension of the main and nose landing gear The pressure reservoir is...

Страница 190: ...g gear can be described as follows The final position for all landing gear legs is monitored separately for each landing gear leg by micro switches for positions UP and DOWN With master switch ON the hydraulic system pressure is kept at 90 bar 1305 psi 8 by pressure switches if necessary by pumping up For control of status of each landing gear leg including respective door three indication lights ...

Страница 191: ...Flight Manual Supplement This sub section gives a short description of the system for emergency extension of the retractable landing gear and describes the required procedures after an emergency extension on ground Pulling the handle bar for the emergency extension of the landing gear releases the valve for emergency extend VEE by a bowden cable The valve opens the pressure reservoir to the hydrau...

Страница 192: ...tion push backward after landing on ground 2 Swing lever for release of VEE backward in normal position 3 Fix securing clamp of bowden cable to VEE lever 4 Set landing gear lever to DOWN position EXTEND 5 Activate master switch Batt and wait until hydraulic system pressure 90 bar 1305 psi 8 is reached and hydraulic pump deactivates automatically For further information refer to the Maintenance Man...

Страница 193: ... and can be moved to the desired position Pay attention to even move of left and right rail to avoid wedge of adjustment After adjustment lock the rails in the nearest position Also the slope of the backrest can be adjusted This allows the backrest to be positioned by placing a small lever in one of several detents near the mounting of the seat belts Every seat is equipped with a four point safety...

Страница 194: ...r section of the fuselage A maximum load of 44 lbs 20 kg may be loaded into the compartment It can be loaded through a forward opening door at the top of the fuselage The locks are engaged with quick closing push buttons at the rear of the door 6 Do NOT place rigid or sharp objects in the baggage compartment without strapping them down Also pay attention to increase of minimum cockpit load refer t...

Страница 195: ...eft and right side of the cockpit frame At the rear it is also locked by a rear canopy hook This so called Roeger hook hook is designed to hold the rear of the canopy down at the beginning of the canopy jettison procedure and causes it to rotate upwards and be torn away 0 6 For canopy jettison ONLY pull the canopy jettison handle The rear canopy hook Roeger hook MUST remain engaged 6 Disconnect th...

Страница 196: ...The air for the cabin ventilation flows from the free airflow beneath propeller spinner into two air inlets From there it is lead into a centralized air distribution system where the airflow splits to the separate vents The canopy vents are located near the canopy hinge They are operated with a Bowden cable installed at the center top of the instrument panel Each seat for the pilot and copilot has...

Страница 197: ...the midsection of the fuselage with the engine suspension connecting it to the steel tube framework There the engine causes low noise emissions for the cabin and the aircraft s surroundings Specifications of the ROTAX 914 F2 Max T O Power MTOP 113 HP 84 5 kW at 5800 RPM max 5 min Max Continuous Power MCP 98 HP 73 4 kW at 5500 RPM Engine Displacement 73 9 in 3 1211 cm 3 Transmission Ratio of Engine...

Страница 198: ...Spinner with baseplate and commutator ring or with commutator ring and starter disk The propeller pitch is continuously adjustable from the T O setting to the cruise setting or glider setting depending on the mode of operation A direct current motor is controlled by the automatic propeller control unit which selects the corresponding propeller pitch according to the power setting and airspeed The ...

Страница 199: ...ion set the left flip switch to MANU and then set the right flip switch to HIGH RPM T O setting The propeller reaches the final pitch after 90 s After the propeller has moved out of the glide setting a green indication light will go ON and the propeller starts to windmill and after restart of the engine set the left flip switch to AUTO and the right flip switch to STOP Now select the desired prope...

Страница 200: ...ad to stone chippings on the propeller blades Due to this perform engine runs only on appropriate surfaces Also always follow the procedures described in chapters 3 and 4 The throttle is located on the center console between the seats It is equipped with a forward detent for 100 power maximum continuous power MCP and a forward stop for 115 power maximum takeoff power MTOP A spring pulls the thrott...

Страница 201: ...stion mixture is enriched in the starter carburetor with additional fuel This is needed for a cold start of the engine The starter carburetor is only operational if the throttle is set to IDLE 6 Only use the choke briefly when performing a cold start Before T O it must be set to the CLOSED position again 4 6 During the daily check check to see if the starter carburetor reaches the stop position Al...

Страница 202: ...llations of the control unit and the engine RPM might occur Avoid the range between 100 115 engine power and move through it quickly when the throttle is set To avoid damage to the engine the MAP is reduced when the engine RPM is too high or when the inducted air is too warm To monitor the turbo control unit use the red MAP warning light and the yellow TCU caution light When turning ON the electri...

Страница 203: ...fire gives a clear warning signal by a red warning light in combination with an acoustic alarm signal For fire detection 2 thermal sensors are mounted on the outside of the engine fire wall above the carburetors and another 2 sensors are mounted on the left and right containment of the fire wall outlet and exhaust shaft The system is designed fail safe that means a possible cable break to the sens...

Страница 204: ...elage between the wings Depending on the value of the operating temperature of the engine the position of the gill outlet and of the cowl flaps can be adjusted with a bowden cable Operation of the cowl flaps The cowl flaps of the inlets and outlets are manually operated with a self locking black T handle at the center console below the instrument panel If the handle is positioned fully forward thi...

Страница 205: ...ocated at the bottom of the central steel tube framework It is supplied with ram air through the lower center NACA cooling inlet 3 The filling hole 3 for the expansion tank 1 is located on top of the expansion tank 1 It is covered with a lid which closes the hole in a pressure resistant manner This is where the cooling system is filled and refilled if necessary 4 2 8 The overflow bottle 4 is locat...

Страница 206: ...ngine is warm The engine cooling system is pressurized There is a severe risk of being burnt by boiling splash water 6 When refilling coolant in the overflow reservoir and tightening the cap afterwards make sure that the plugged vent hose remains untwisted 4 6 The system has an overpressure valve Because of this coolant needed in the overflow bottle 4 can NOT be refilled at the expansion tank 1 To...

Страница 207: ...3 The main oil pump transports the oil from the oil tank through separate oil cooler and oil filter to the lubricating points Escaping oil is returned through the crank case The turbo charger is supplied through a separate oil pipe by the main oil pump There the oil is suctioned by a separate pump and returned directly to the oil tank At the flange of the oil pump a temperature sensor is installed...

Страница 208: ...drive which is located in the nose of the A C The drive shaft of the front drive is screwed to the propeller hub The drive is a belt drive model STEMME 050 251 which is encased in cast magnesium The gear belt discs are made of aluminum and have a transmission ratio of i 1 100 The drive suspension is screwed onto the load transmission frame drive frame with elastomer elements It transmits the prope...

Страница 209: ...e The engine shaft flange is connected to the long shaft with a spline shaft connector which allows for axial motion of the long shaft A flexible disk on each side of the long shaft compensates angle errors and angular motion In case of a failure of the long shaft it is contained in a protective tunnel made of aramid fiber composites This contains the shaft and sharp fragments in case of shaft rup...

Страница 210: ...uselage through quick connectors The fuel flows from the quick connectors to the fuel pumps main fuel pump and auxiliary fuel pump From there it continues to the fuel valve in the cockpit and then to the pressure regulator in front of the carburetors A return pipe leads from the pressure regulator through a quick connector back to the feeder compartment Optionally an additional integral tank can b...

Страница 211: ...age engine 8 at the switch panel of the instrument panel settings ON and OFF 8 8 Indication light for remaining fuel less than 1 3 1 9 US gal 5 7 l in feeder compartment Status indicator is goes ON if the auxiliary fuel pump is running On the instrument panel shows the amount of fuel in the left and right integral tanks 8 On the instrument panel shows the current fuel flow to the engine For basic ...

Страница 212: ...7 41 Revision Date of Issue 18 November 2011 Date of Rev 6 ...

Страница 213: ...k from becoming overfilled If the amount of fuel in the right is below 2 3 3 4 of its maximum capacity or below the level the fuel sensor could sense the transfer of fuel begins automatically if this is activated The transfer of fuel can be interrupted at any time by hand independent of the amount of fuel in the right tank by operating the fuel transfer pump switch 7 The amount of fuel in each tan...

Страница 214: ... Two independent charging coils are mounted on the crankshaft case Each coil supplies one of the two independent ignition circuits The electrical energy is stored in the capacitors of the electronic modules At the ignition point 2 of the 4 external probes discharge the capacitors through the primary coils of the dual ignition transformers The order of ignition is 1 4 2 3 The electrical system is d...

Страница 215: ...d is located on the control board in the engine compartment at the rear of the fire wall Circuit Circuit Breaker A Fuse A Isolation Switch A Main Bus Engine Bus 10 Master Circuit Breaker 50 Circuit Breaker for the Alternator 50 Stall Warning 2 Electrical Trim 5 Propeller Pitch Control 5 Voltmeter 2 External Alternator 5 Instrument Lighting 5 Position Lights 10 Anti Collision Light 5 Landing Light ...

Страница 216: ... the manufacturers of the installed equipment Internal Generator Bus Main Fuel Pump 5 Fuel Circulation Pump 3 Feed In 15 Internal Generator Caution Light 1 TCU 3 In the following chapter the different settings of important control elements of the electrical system are explained also refer to the chapter 7 6 for instrument panel layout 7 8 6 Separates all power sources from the main bus 8 6 Engine ...

Страница 217: ...he switch to the UP position Avionics Master Switch Activates the avionics bus It is designed as a 20A circuit breaker Auxiliary Fuel Pump The auxiliary fuel pump is turned ON and OFF with this switch when needed The aux fuel pump runs at the same time as the main fuel pump If the switch is set to ON then the green indication light on the announciator panel will go ON Fuel Transfer Pump Activates ...

Страница 218: ...ator falls below the battery voltage failure of the external alternator 3 Indication lights for state of Landing Gear one for each leg Light GREEN if gear leg is OUT and LOCKED Light RED if gear leg moves IN or OUT Light ORANGE landing gear leg s OUT and LOCKED but hydraulic pump still ON final system pressure not reached Light OFF if gear leg is in final IN position or system powerless CB master ...

Страница 219: ...s lead to the center of the wing There they need to be connected to the adapters of the mid section of the fuselage From there the lines are lead to the rear side of the instrument panel All tubes of the pressure system in the forward area of the cockpit are equipped with filters against moisture and dust The assignment of the pressure ports of different instruments standard instruments and option...

Страница 220: ...the airspeed drops to less than 1 1 times the stall speed at any flap setting then stall horn will sound The horn is installed in the instrument panel The stall warning system is designed as a small wind vane with a trigger switch It is mounted at the leading edge of the left wing near the wing joint ...

Страница 221: ... 0 1 02 3 0 4 5 ...

Страница 222: ... 0 1 2 0 2 6 0 0 0 5 0 0 2 5 ...

Страница 223: ... 7 8 9 0 5 7 8 7 8 15 4 7 8 0 0 2 0 0 1 2 5 0 0 0 0 5 5 5 2 ...

Страница 224: ... 1 2 2 00 0 1 00 00 2 00 0 0 2 2 0 0 0 2 0 0 2 0 2 1 2 2 0 2 0 2 0 0 0 2 7 8 A ...

Страница 225: ... 5 0 0 B 9 9 2 0 0 2 0 0 1 0 5 0 0 0 2 0 C 2 9 0 7 D 8 7C 8 9 E 4916 0 2 2 0 3 0 F GH 0 0 2 0 3 0 F G 00 2 0 0 9 9 0 0 0 5 0 0 0 5 0 4 0 0 5 0 7 0 8 0 0 0 0 1 0 0 0 0 0 1 0 00 ...

Страница 226: ... 0 76 0 8 5 0 2 0 1 0 0 A 00 A 0 6 0 5 0 7 8 0 1 7 0 0 8 5 0 0 0 7 5 5 8 0 9 2 00 0 5 1 2 2 00 1 1 6 0 0 0 0 2 0 0 7 5 0 8 0 4 ...

Страница 227: ...I 0 5 0 A 0 0 00 0 0 2 2 0 0 0 5 0 5 2 5 00 5 71 8 2 9 0 0 2 0 5 0 9 0 0 5 0 2 2 5 2 7 0 5 8 0 0 A 0 ...

Страница 228: ... 0 5 2 6 0 1 7 8 0 2 5 5 0 0 7 0 8 2 0 0 2 0 0 0 1 0 5 0 0 7 8 2 0 2 0 2 2 1 2 5 0 0 7 2 2 0 0 85 0 6 0 0 0 2 0 0 1 2 0 2 2 ...

Страница 229: ...3 C 2 2 7 0 8 5 0 1 0 4 2 0 0 20 0 00 20 0 00 2 0 0 00 1 0 0 20 A 2 7 0 85 00 1 0 0 20 1 5 0 7 28 2 0 9 0 0 0 3 025 5 0 1 02 0 5 25 2 0 H 5 0 0 0 H 02 ...

Страница 230: ... 0 0 0 0 2 0 7 2 8 0 5 0 0 0 2 5 0 7 8 2 0 7 8 0 5 B 7 9 D8 7 74 8 9 D 3 8 4 2 0 0 2 0 2 0 J 2 7 0 5 2 0 8 00 7 8 1 5 0 5 4 00 0 1 0 2 25 ...

Страница 231: ... 2 0 2 A 0 0 5 9 0 H K 9 K 4 1 K 1 16 2 5 0 0 K A 25 0 A 25 1994 9 0 5 3 9 149 79 85 0 6 1 16 445 1994 9 00 20 7 8 ...

Страница 232: ... 7 2 0 44 2 25 9 J 0 0 0 0 0 0 I 0 25 0 0 2 0 0 9 ...

Страница 233: ...Flight Manual STEMME S6 RT Doc No P400 006 001 FAA Page 9 1 Revision Date of Issue 18 November 2011 Date of Rev ...

Страница 234: ...to the aircraft configuration If not otherwise specified the supplements to the basic model S6 Doc No P400 006 000 FAA are also valid for the Flight Manual in hand for the model S6 RT Doc No P400 006 001 FAA The installation of supplemental or alternative equipment or accessories is based on a service bulletin SB if equipment is not already installed at delivery The necessary supplemental informat...

Страница 235: ...talled supplemental or alternative equipment of the aircraft has to be marked in the table below with date and check note This applies to alternative equipment already installed at delivery as well as for equipment later installed This directory serves as a table of contents for section 9 Supplements Serial No 77777 Registration 77777 No Title Pages Revision Date Inst Check Note P400 006 000 FAA S...

Страница 236: ...Flight Manual STEMME S6 RT Doc No P400 006 001 FAA Page 9 4 Revision Date of Issue 18 November 2011 Date of Rev Supplements No Title Pages Revision Date Inst Check Note mark as appropriate ...

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