- Effective
- June 11, 1970
- Model
- Do 28 D-1
- Data sheet
- TCDSA16EU
- Registered aircraft
- 1 matched by model
- Product
- Aircraft · Small/large airplane
- Amendment
- 39-1005
Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
| File | Size | SHA-256 | Original |
|---|---|---|---|
| FAA DRS HTML | 19 KB | 2d7f56fc…0149943 | FAA DRS (API key needed) |
On this page
The airworthiness directive
70-12-10 DORNIER, AG: Amdt. 39-1005. Applies to Model DO-28D-1 airplanes with Serial Numbers 0401, and 4002 through 4039.
To prevent disconnection of the right hand elevator trim tab system, within the next 50 hours' time in service after the effective date of this AD, unless already accomplished, replace washer P/N MS20002-C5 on the right hand elevator trim tab actuator bellcrank with a larger washer P/N 28.01.303 -111.43 in accordance with Dornier Alert Service Bulletin A024-1303, dated 23 February 1970, or later ARB-approved issue or an FAA-approved equivalent.
This amendment becomes effective June 11, 1970.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 1
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.