LBA
AD-No.: |
TN-No.:
|
Subject |
Urgency |
Download |
| |
205-1 |
Elevator control bracket, SN 1up to incl. SN19 |
|
 |
 |
| |
205-2 |
Forward fuselage main bulkhead SN’s 1 up to incl.17,
exept SN 14 |
|
|
|
| |
205-3 |
Parachute rip cord attachment, all SN |
|
|
|
| |
205-4 |
Attachment of airbrake hinges Up to and incl. SN 61 |
|
|
|
| |
205-5 |
FRP cover of parallelogram control stick, up to and
incl. SN 65 |
latest 01.05.1975 |
|
|
| 75-168/2 |
205-6 |
Reinforcement of guide plates on elevator actuating
bracket, up to and incl. SN107 |
latest 29.02.1976 |
|
|
| |
205-7 |
Modification of landing gear to reduce angle of
attack on ground, up to and incl. SN125, exept SN 1 and SN 66 |
|
|
|
| |
205-8 |
Modification of tail gear to reduce angle of attack
on ground, SN 66, 125 and on |
|
|
|
| |
205-9 |
Rear canopy tilt-up support SN 66 and 125 and up |
|
|
|
| |
205-10 |
Shortened airbrakes on inner side, SN 138 and up |
|
|
|
| |
205-11 |
Improvement of shear web, SN 140 and up |
|
|
|
| |
205-12 |
Reduced travel of rudder pedals, SN 170 and up,
optional |
|
|
|
| |
205-13 |
Deviation of Netherland registered sailplanes from
German TCDS |
at C of A
inspection |
|
|
| |
205-14 |
Retrofit of center of gravity towrelease |
|
|
|
| 88-280/2 |
205-15 |
Extension of service life limit to 6000 hrs. |
latest 31.05.1989 when reaching 3000 h |
|
|
| 88-28 |
205-16 |
Elevator drive bracket, Reinforcement or replacement |
latest 30.04.1988 |
|
|
| |
205-17 |
Elevator drive bracket: Possibility of replacement
by elevator drive bracket acc. to drawing No. 201-33-4 |
|
|
|
| |
205-18 |
Tow releases: Optional use of model E85 instead of
E72/E75 |
|
|
|
| 96-132 |
205-19 |
Inspection of glas |
Annual insp. |
|
|
| 96-138 |
205-20 |
Weight and static moments of control surfaces after
repainting and repair |
latest 31.03.1996 |
|
|
| |
205-21 |
Optional installation of winglets |
|
|
|
| 2003-003 |
205-22 |
Rudder gimbal drive – rear actuator arm |
latest 31.03.2003 |
|
|
| |
205-23 |
Extension of service life limit to 12000 hours |
latest 31.03.2006 when reaching 6000 h |
|
|
| |
205-23 |
Manual |
|
|
|
| |
205-24 |
Reinforcement of main landing gear frame |
|
|
|
| |
205-25 |
Installation of Mode-S-Transponder and Transponder
Antennas |
|
|
|
| |
205-26 |
Spar stub fitting replacement, standardisation of
fittings |
|
|
|
EASA AD
2011-213 |
205-27 |
Inspection
/ replacement of elevator control rod in vertical fin |
30 Days /
latest 31.12.2012 |
|
|
| |
205-27 |
Authorised
service facilities for TN 205-27 |
|
|
|
| 2018-0143-E |
5-2018 |
Deflector-angles at the C.G. release
Usage of connection ring pair meeting
LN 65091 |
annually |
|
|
| |
205-28 |
Installation of new winglets optional |
|
|
|
