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This text is OCR from a scan. OCR can misread letters and numbers. © Glasfaser-Flugzeug-Service. Filed by the FAA in regulations.gov docket FAA-2019-0560; AD 2020-19-12 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.
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Glasfaser-Flugzeug-Service GmbH Technical Note Page: 01 von 02 Hansjörg Streifeneder No. 5-2018 Hofener Weg 61 72582 Grabenstetten Subject: Deflector-angles at the C.G. release Usage of connection ring pair meeting standard LN 65091 Affected: All glider manufactured by Glasfügel Type H301 Libelle Model: H 301 B Standard Libelle Standard Libelle 201 B Standard Libelle 203 Standard Libelle 204 Type: Glasflügel 604 Type: BS 1 Type : Kestrel Club Libelle 205 Model : Hornet Hornet-C Mosquito Model : Mosquito B Glasflügel 304 Falcon Urgency: Before the next winch launch.
Each annual inspection.
Reason: Jamming of the double-ring pair between the deflector-angles at the C.G. release.
Actions: 1. Verification of the distances and the parallelism of the deflector-angles by means of a caliper or gauge with 36 mm width as shown in the attached drawing
2. If the distance between the deflector-angles is less than 36 mm, remove the deflector-angles and file the holes till the distance is right.
Pull the deflector-angles with a distance-piece of 36 mm together and support them with filling material as resin with cotton flocks or polyester putty. Positioning it with the screws.
After curing, screw the release and the deflector-angles as shown on the drawing.
Finally, a function test and release test must be done.
Glasfaser-Flugzeug-Service GmbH Technical Note Page: 02 von 02 Hofener Weg Hansjörg Streifeneder No. 5-2018 72582 Grabenstetten
3. Insert the following Note into the flight- and maintenancemanual under winch tow: „Winch launching is permissible only with connecting ring pair according to LN 65091" Schnitt C-D Schrawba 116x18 DIN 931,80 Sechskantmutter Schaibe M6 LN 9348 64 DIN 125 Schraubenkopf geundet 36*1 C.G. and mass: Differences negligible Note: For action 1 and 3 accomplishment and issue CRS may be executed by pilot-owner within the scope of M.A. 801 For action 2 the CRS must be issued by a certifying staff according to M.A.801.
Grabenstetten, 25.06.2018 The technical content of this TN No. 5-2018 is EASA approved.
Issued:.. Ze Steitenedes EASA No.: 0010055705 Glasfaser-Flugzeug-Service Date: 03.07.2018 Hansjörg Streifeneder