LBA AD Number TN Number Subject Urgency Download Link
75/168/2 206-1 Reinforcement of guide plates on elevator actuating bracket, up to and incl. SN107 Before 29/2/1976 Deutsch
206-2 Improvement of shear web, SN 22, 23, 25 and up Deutsch English
206-3 Lower wing shell without hard core foam, Production improvement, SN 27 and up Deutsch English
206-4 Reduced travel of rudder pedals, SN 78 and up, optional Deutsch
206-5 Single-piece canopy as used on “Mosquito”, optional Deutsch
206-6 Modified airbrake drive mechanism, SN 89 only Deutsch
206-7 Use of wings originating from “Club Libelle” to “Hornet” fuselage, SN 89 only (operational limits of Club Libelle ) Deutsch
206-8 Lead ballast compartment in nose bulkhead, optional Deutsch English
80-221 206-9 Aileron ballance mass, Hornet C all SN Deutsch English
206-10 Deviation of Netherland registered sailplanes from German TCDS Annual Inspection Deutsch
84-11 206-11 Possible damage of wing structure with water ballast bags installed. Revision of flight manual Before 30/4/1984 Deutsch English
88-28 206-12 Elevator drive bracket: replacement or reinforcement Before 30/4/1988 Deutsch English
8-280/2 206-13 Extension of service life limit to 6000 hours Before 31/5/89 or when reaching 3000h Deutsch English
206-14 Elevator drive bracket: Possibility of replacement by elevator drive bracket acc. to drawing No. 201-33-4 Deutsch English
206-15 Tow releases: Optional use of model E85 instead of E72/E75 Deutsch English
91-111 206-16 Inspection of canopy lifting / tilting mechanism Annual Inspection Deutsch English
96-132 206-17 Inspection of glass fiber laminate on spar stub fitting Annual Inspection Deutsch English
97-311 206-18 Weights and moments of control surfaces, Hornet C only, all SN Before 31/8/1998 Deutsch English
97-311/2 206-19 Change of weights and moments of control surfaces, Hornet C only, all SN Before 30/11/1999 Deutsch English
206-20 Optional installation of winglets (Hornet only) Deutsch English
2003-003 206-21 Replacement of aft rudder gimbal drive- rear actuator arm Before 31/3/2003 Deutsch English
206-22 Single-piece up-tilting canopy with “Roeger-Hook” Hornet SN 54 only
206-23 Extension of service life limit to 12000 hours Before 31/3/2006 or when reaching 6000h Deutsch English
206-23 Manual Deutsch English
206-24 Installation of Mode-S-Transponder and Transponder Antennas Deutsch English
206-25 Spar stub fitting replacement, standardisation of fittings English
EASA AD 2011-213 206-26 Inspection/replacement of elevator control rod in vertical fin 30 days/before 31/12/2012 Deutsch English
206-27 Optional Installation of backrest with integrated headrest Deutsch English
2018-0143-E 5-2018 Deflector-angles at the C.G. release
Usage of connection ring pair meeting LN 65091
Annual Inspection Deutsch English
206-28 Installation of new winglets optional Deutsch English