LBA
AD-No.: |
TN-No.:
|
Subject |
Urgency |
Download |
| 75-168/2 |
206-1 |
Reinforcement of guide plates on
elevator actuating bracket, up to and incl. SN107 |
latest 29.02.1976 |
 |
|
| |
206-2 |
Improvement of shear web, SN 22, 23, 25
and up |
|
|
 |
| |
206-3 |
Lower wing
shell without hard core foam, Production improvement, SN 27 and up |
|
|
|
| |
206-4 |
Reduced
travel of rudder pedals, SN 78 and up, optional |
|
|
|
| |
206-5 |
Single-piece canopy as used on „Mosquito“, optional |
|
|
|
| |
206-6 |
Modified
airbrake drive mechanism, SN 89 only |
|
|
|
| |
206-7 |
Use of
wings originating from „Club Libelle“ to „Hornet“ fuselage, SN 89
only (operational limits of Club Libelle ) |
|
|
|
| |
206-8 |
Lead
ballast compartment in nose bulkhead, optional |
|
|
|
| 80-221 |
206-9 |
Aileron
ballance mass, Hornet C all SN |
|
|
|
| |
206-10 |
Deviation
of Netherland registered sailplanes from German TCDS |
at C of A inspection |
|
|
| 84-11 |
206-11 |
Possible
damage of wing structure with water ballast bags installed. Revision
of flight manual |
Latest 30.04.1984 |
|
|
| 88-28 |
206-12 |
Elevator
drive bracket: replacement or reinforcement |
Latest 30.04.1988 |
|
|
| 88-280/2 |
206-13 |
Extension
of service life limit to 6000 hours, |
until 31.05.89 when reaching 3000h |
|
|
| |
206-14 |
Elevator
drive bracket: Possibility of replacement by elevator drive bracket
acc. to drawing No. 201-33-4 |
|
|
|
| |
206-15 |
Tow
releases: Optional use of model E85 instead of E72/E75 |
|
|
|
| 91-111 |
206-16 |
Insperction
of canopy lifting / tilting mechanism |
Annual Inspection |
|
|
| 96-132 |
206-17 |
Inspection
of glass fiber laminate on spar stub fitting |
Annual Inspection |
|
|
| 97-311 |
206-18 |
Weights and
moments of control surfaces, Hornet C only, all SN |
Until 31.08.1998 |
|
|
| 97-311/2 |
206-19 |
Change of
weights and moments of control surfaces, Hornet C only, all SN |
until 30.11.1999 |
|
|
| |
206-20 |
Optional
installation of winglets ( Hornet only ) |
|
|
|
| 2003-003 |
206-21 |
Replacement
of aft rudder gimbal drive- rear actuator arm |
Latest 31.03.2003 |
|
|
| |
206-22 |
Single-piece up-tilting canopy with „Roeger-Hook“ Hornet SN 54 only |
|
|
|
| |
206-23 |
Extension
of service life limit to 12000 hours, |
until 31.03.2006 when reaching 6000 h |
|
|
| |
206-23 |
Manual |
|
|
|
| |
206-24 |
Installation of Mode-S-Transponder and Transponder Antennas |
|
|
|
| |
206-25 |
Spar stub
fitting replacement, standardisation of fittings |
|
|
|
EASA AD
2011-213 |
206-26 |
Inspection
/ replacement of elevator control rod in vertical fin |
30 Days /
latest 31.12.2012 |
|
|
| |
206-26 |
Authorised
service facilities for TN 206-26 |
|
|
|
| 2018-0143-E |
5-2018 |
Deflector-angles at the C.G. release
Usage of connection ring pair meeting
LN 65091 |
annually |
|
|
| |
206-28 |
Installation of new winglets optional |
|
|
|
