This list of airworthiness instructions and technical notes is for information only. Definitive information can be found on the DG website here or from your national authority. For the UK, this is the British Gliding Association.
| DG Technical Note & Date | Type & Production No. | Subject | Optional or Mandatory | Due By Date | |
|---|---|---|---|---|---|
| DG-200 serial numbers 1-78 except 57, 65, 74 | Wing spar reinforcement. Superceded by 323/01. | M | Immediately | ||
| 323/01 | DG-200 serial numbers 1-86 except 57, 65, 74, 81, 84 | Wing spar reinforcement. | M | Immediately | |
| 323/02 | DG-200 exports to the Netherlands | Deviations from German type. | none | ||
| 323/03 | DG-200 all versions | Installation of ELT. | O | as required | |
| 323/04 | DG-200 all versions | Installation of oxygen equipment. | O | as required | |
| 323/05 | DG-200 all versions | Flight manual, maintenance manual amendments for emergency
release of 1-piece canopy. Inspection of rudder bottom hinge. |
M | 30 days | |
| 323/06 | DG-200 all versions | Marking of canopy emergency release and ventilation controls. | M | before next flight | |
| 323/07 | DG-200 all versions | Safety device(s) for l'hotellier connectors. | O | on request | |
| 323/08 | DG-200 all versions | Instructions for new seat harnesses. | O | with installation of new harness | |
| 323/09 | DG-200 all versions | Inspection and possible modification of airbrakes. | M | before next flight | |
| 323/10 | DG-200 all versions | Additional (nose) hook for aerotow. | O | as required | |
| DG-200 all versions | Extension of service life over 3000 hours. | M | 3000 hours | ||
| 323/11 | DG-200 all versions | Improved 1-piece canopy securing system for safer emergency release (similar to Röger-hook). | O | as required | |
| 323/12 | DG-200 all versions | Piggott-hook parking brake and airbrake securing device. | O | as required | |
| 323/13 | DG-200 all versions | Installation of NOAH emergency bale-out aid. | O | as required | |
| 323/14 | DG-200 all versions |
|
M | 31/12/2004 | |
| 323/15 | DG-200 all versions |
|
M | at next annual check | |
| 323/16 | DG-200 all versions | Rod End in Control Column | M | Inspection prior to next take-off Exchange (if required) by 31/12/2009 |
|
| TN-DG-SS-01 | DG-200 all versions | Manual revisions | O* | prior to next maintenance /inspection* Latest 31/08/2010* |
Important note: The following general TN’s are applicable for
this type.
You will find these TN’s on the DG-web site / technical notes in
the directory “General - general TN’s for all DG and LS types”
| TN Number |
Subject |
Due By Date |
|
| DG-G-01 | Approved repair methods according to EU Commission regulation 1702/2003, part 21, subpart M | O | as required |
| DG-G-02 | Installation of transponder and aerial for transponder | O | as required |
| DG-G-07 | Installation of instruments and equipment which are not part of the minimum equipment | O | as required |
| DG-G-08 | Installation of 406MHz ELTs | O | as required |
* I'm unsure about this TN. It appears to be part of DG's initiative to force owners to take out a service agreement and is more or less a rehash of previous documentation. It does not appear to be acknowledged by EASA as an airworthiness requirement. As with other information presented here this is the owner's responsibility to verify.
back to DG-200 page
or back to DG-202 page
©2002-20012 Page last updated by on 10th October 2012