- 2 b – Ventus bT WARTUNGSHANDBUCH ... - Schempp-Hirth
- 2 b – Ventus bT WARTUNGSHANDBUCH ... - Schempp-Hirth
- 2 b – Ventus bT WARTUNGSHANDBUCH ... - Schempp-Hirth
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- 2 b –<br />
<strong>Ventus</strong> <strong>bT</strong> <strong>WARTUNGSHANDBUCH</strong> / MAINTENANCE MANUAL<br />
0.1 Erfassung der Berichtigungen / Records of revisions<br />
Lfd.<br />
Nr.<br />
Benennung<br />
Rev. Reference / short title<br />
No.<br />
14. Technische Mitteilung Nr. 825-12<br />
Schleppkupplungen<br />
Technical Note No. 825-12<br />
Nose and C/G tow release mechanism<br />
15. Technische Mitteilung Nr. 825-14<br />
- wahlweise -<br />
Nachträglicher Einbau eines unteren Aluminium-<br />
Kraftstofftanks, nur in Verbindung mit<br />
Änderungsblatt Nr. 825-1.<br />
Für Flugzeuge ohne TM-Nr. 825-5 kann der alte<br />
GFK-Tank nicht weiter verwendet werden.<br />
Technical Note No. 825-14<br />
Optional lower fixed aluminium fuel tank (only for<br />
aircraft complying with MB 825-1. Upper tank<br />
may additionally be used when in compliance<br />
with TN-No. 825-5)<br />
16. Technische Mitteilung Nr. 825-11<br />
Winglets<br />
-wahlweise –<br />
Technical Note No. 825-11<br />
Winglets<br />
-optional-<br />
17. Technische Mitteilung Nr. 825-21<br />
Prüfungsablauf zur Erhöhung der Betriebszeit<br />
auf 12.000 Stunden<br />
Technical Note No. 825-21<br />
Inspection program for extending the service<br />
time to 12.000 hours<br />
18. Technische Mitteilung Nr. 825-26<br />
Kraftstoffhahn-Betätigung<br />
- wahlweise alle Werknummern -<br />
Technical Note No. 825-26<br />
Fuel cock mechanism<br />
- optional all serial numbers -<br />
Seite<br />
Page<br />
27, 39<br />
5, 6, 8, 12, 21B,<br />
21D, 21E, 32,<br />
37, 45, 46, 47,<br />
Fehlers. Bl 11<br />
(Trouble<br />
shooting page 11)<br />
6, 7, 8, 23, 42<br />
40 A<br />
40 B<br />
12, 45, 47<br />
Datum<br />
Date<br />
Dezember<br />
1989<br />
Dezember<br />
1990<br />
Juni<br />
Juni<br />
1992<br />
1999<br />
Januar<br />
2001
- 12 -<br />
<strong>Ventus</strong> <strong>bT</strong> MAINTENANCE MANUAL<br />
2.2.2 Fuel system<br />
For refuelling the tank has to be removed from the fuselage by<br />
disengaging the spring-loaded lock(s), removing the quick-connector<br />
of the fuel line and disconnecting the vent line. Then a looped blind<br />
plug is connected to the tank vent to prevent fuel escaping through<br />
the vent hole. The fuel tank outlet has two built-in fuel finders also<br />
acting as filters.<br />
Fuel is supplied to the engine from the fuselage tank via its quick<br />
connector to the shut off valve and via the diaphragm<br />
pump to the carburetors.<br />
Fuel contents are read off directly from the transparent<br />
GFRP-tank.<br />
See fuel system, page 47.<br />
2.3 Electrical System<br />
2.3.1 Gliding Instrumentation<br />
For the prescribed minimum equipment no power supply is<br />
required.<br />
Additional electrical instruments are connected with a power supply<br />
according the “wiring diagram for gliding instrumentation” page 41,<br />
and in correspondence with the manufacturer’s instructions for the<br />
individual instruments.<br />
On request a separate master switch for the gliding instrumentation<br />
is provided, but standard is only a single master switch combining<br />
gliding instrumentation and engine control box according to section<br />
2.3.2.<br />
Modification Bulletin No. 825-1 April 1984<br />
Technical Note No. 825-26 January 2001
SCHEMPP-HIRTH FLUGZEUGBAU GmbH., KIRCHHEIM/TECK<br />
<strong>Ventus</strong> <strong>bT</strong> - 45 - MAINTENANCE MANUAL<br />
POWER PLANT - INSTALLATION AND CONTROLS<br />
MB-No. 825-1 - April 1984<br />
MB-No. 825-5 - March 1985<br />
TN-No. 825-26 - January 2001
SCHEMPP-HIRTH FLUGZEUGBAU GmbH., KIRCHHEIM/TECK<br />
<strong>Ventus</strong> <strong>bT</strong> - 47 - MAINTENANCE MANUAL<br />
TN-No. 825-5 - July 1987<br />
TN-No. 825-26 - January 2001
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