SCHEMPP-HIRTH FLUGZEUGBAU GmbH., KIRCHHEIM/TECK Duo ...
SCHEMPP-HIRTH FLUGZEUGBAU GmbH., KIRCHHEIM/TECK Duo ...
SCHEMPP-HIRTH FLUGZEUGBAU GmbH., KIRCHHEIM/TECK Duo ...
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<strong>SCHEMPP</strong>-<strong>HIRTH</strong> <strong>FLUGZEUGBAU</strong> <strong>GmbH</strong>., <strong>KIRCHHEIM</strong>/<strong>TECK</strong><br />
<strong>Duo</strong> Discus T WARTUNGSHANDBUCH / MAINTENANCE MANUAL<br />
0.1 Erfassung der Berichtigungen / Record of Revisions<br />
Lfd.Nr.<br />
Rev.No.<br />
9<br />
10<br />
Benennung<br />
Reference<br />
Änderungsblatt Nr. 890-6<br />
Winglets, Hinterkantenklappen (Werk-Nr. 126)<br />
und gefedertes Fahrwerk (ab Werk-Nr. 128)<br />
Modification Bulletin No. 890-6<br />
Winglets, trailing edge flap (S/N 126) and<br />
landing gear with shock absorber struts<br />
(S/N 128 and on)<br />
Technische Mitteilung Nr. 890-7<br />
Winglets wahlweise, Werk-Nr. 1 bis 125<br />
Technical Note 890-7<br />
Winglets optional, S/N 1 through 125<br />
Seite<br />
Page<br />
Deckblatt /<br />
cover sheet<br />
0.2.1<br />
0.2.2*)<br />
0.2.3<br />
1.2.2<br />
1.2.3*)<br />
2.1.2<br />
2.3<br />
3.1.2<br />
3.2.1<br />
3.2.4<br />
5.4.1.1*)<br />
5.4.1.2*)<br />
5.4.2*)<br />
6.2.2*)<br />
6.4.2*)<br />
6.4.3*)<br />
6.6.2*)<br />
6.7*)<br />
8.6*)<br />
8.7*)<br />
Diagr. 1<br />
Diagr. 3<br />
Diagr. 4*)<br />
Diagr. 5<br />
Farbkennz.<br />
Rep. 1, 2<br />
*) entfällt bei<br />
Werk-Nr. 126<br />
not applicable<br />
for S/N 126<br />
0.2.1<br />
2.1.2<br />
Diagr. 3<br />
Farbkennz. /<br />
Anti collisions<br />
marking<br />
Datum<br />
Date<br />
September<br />
2005<br />
November<br />
2005<br />
Rep. 1<br />
MB: Modification Bulletin – Änderungsblatt<br />
TN: Technical Note – Technische Mitteilung<br />
0.1.3
<strong>SCHEMPP</strong>-<strong>HIRTH</strong> <strong>FLUGZEUGBAU</strong> <strong>GmbH</strong>., <strong>KIRCHHEIM</strong>/<strong>TECK</strong><br />
<strong>Duo</strong> Discus T MAINTENANCE MANUAL<br />
AILERONS:<br />
Up:<br />
71 ± 5 mm<br />
[2.80 ± 0.20 in.]<br />
Down:<br />
36 ± 5 mm<br />
[1.42 ± 0.20 in.]<br />
RIGGING DATA AND<br />
CONTROL SURFACE DEFLECTIONS<br />
November 2005<br />
Revision 10 TN-No. 890-7 2.1.2
<strong>SCHEMPP</strong>-<strong>HIRTH</strong> <strong>FLUGZEUGBAU</strong> <strong>GmbH</strong>., <strong>KIRCHHEIM</strong>/<strong>TECK</strong><br />
<strong>Duo</strong> Discus T MAINTENANCE MANUAL<br />
WING CONTROLS<br />
1. Aileron<br />
2. Airbrake<br />
November 2005<br />
Revision 10 TN-No. 890-7 DIAGRAM 3
<strong>SCHEMPP</strong>-<strong>HIRTH</strong> <strong>FLUGZEUGBAU</strong> <strong>GmbH</strong>., <strong>KIRCHHEIM</strong>/<strong>TECK</strong><br />
<strong>Duo</strong> Discus T MAINTENANCE MANUAL<br />
November 2005<br />
Revision 10 TN-No. 890-7<br />
ANTI-COLLISION MARKINGS (optional)<br />
20°
<strong>SCHEMPP</strong>-<strong>HIRTH</strong> <strong>FLUGZEUGBAU</strong> <strong>GmbH</strong>., <strong>KIRCHHEIM</strong>/<strong>TECK</strong><br />
<strong>Duo</strong> Discus T REPAIR INSTRUCTIONS<br />
REPAIR INSTRUCTIONS FOR „<strong>Duo</strong> Discus T“<br />
The components of this aircraft are constructed as follows:<br />
1. Inboard wing panels<br />
GFRP/foam-sandwich, with HEREX C 70.55,<br />
thickness 8 mm (0.31 in.)<br />
Wing tip extension<br />
GFRP/foam-sandwich,<br />
with HEREX C 70.55,<br />
thickness 6 mm (0.24 in.)<br />
with winglets<br />
Pure GFRP/CFRP-shell<br />
2. Ailerons<br />
Inboard: GFRP/foam-sandwich, with HEREX C 70.55,<br />
thickness 4 mm (0.16 in.)<br />
Outboard: Pure GFRP/CFRP-shell<br />
3. Fuselage<br />
Forward section: Pure CFRP/Kevlar/GFRP-shell<br />
Aft section: Pure CFRP-shell<br />
4. Fin<br />
GFRP/foam-sandwich, with HEREX C 70.55,<br />
thickness 6 mm (0.24 in.)<br />
5. Rudder<br />
GFRP/foam-sandwich, with HEREX C 70.55,<br />
thickness 4 mm (0.16 in.)<br />
6. Horizontal stabilizer<br />
GFRP/foam-sandwich, with HEREX C 70.55,<br />
thickness 6 mm (0.24 in.)<br />
7. Elevator halves<br />
Pure CFRP-shell<br />
November 2005<br />
Revision 10 TN-No. 890-7 - 1 -
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