canopy - Schempp-Hirth Flugzeugbau GmbH

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SCHEMPP-HIRTH FLUGZEUGBAU <strong>GmbH</strong>., KIRCHHEIM/TECK Duo Discus T MAINTENANCE MANUAL UNDERCARRIAGE WITH RETRACTING LINKAGE AND HYDRAULIC DISC BRAKE 1. Front retracting linkage 2. Rear retracting linkage 3. Brake handle on front control stick 4. Brake handle on rear control stick 5. Brake master cylinder with reservoir February 2008 MB 396-15 Revision 20 TN 396-16 (x) DIAGRAM 4
SCHEMPP-HIRTH FLUGZEUGBAU <strong>GmbH</strong>., KIRCHHEIM/TECK Duo Discus REPAIR INSTRUCTIONS REPAIR INSTRUCTIONS FOR „Duo Discus “ The components of this aircraft are constructed as follows: 1. Inboard wing panels GFRP/foam-sandwich, with HEREX C 70.55, thickness 8 mm (0.31 in.) Wing tip extension GFRP/foam-sandwich, with HEREX C 70.55, thickness 6 mm (0.24 in.) 2. Ailerons Inboard: GFRP/foam-sandwich, with HEREX C 70.55, thickness 4 mm (0.16 in.) Outboard: Pure GFRP/CFRP-shell 3. Fuselage Forward section: Pure CFRP/Kevlar/GFRP-shell Aft section: Pure CFRP-shell 4. Fin GFRP/foam-sandwich, with HEREX C 70.55, thickness 6 mm (0.24 in.) 5. Rudder GFRP/foam-sandwich, with HEREX C 70.55, thickness 4 mm (0.16 in.) 6. Horizontal stabilizer GFRP/foam-sandwich, with HEREX C 70.55, thickness 6 mm (0.24 in.) 7. Elevator halves Pure CFRP-shell February 2008 Revision 20 TN-No. 396-16 (x + xL) - 1 -
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canopy - Schempp-Hirth Flugzeugbau GmbH

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