- Effective
- September 7, 1968
- Model
- S.205 - 22/R
- Data sheet
- TCDSA9EU
- Registered aircraft
- 22 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-628
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 | 07186eca…8684da2 | FAA DRS (API key needed) |
On this page
The airworthiness directive
68-16-02 SIAI-MARCHETTI: Amdt. 39-628. Applies to Model S.205/22R airplanes - Serial Nos. 213, 370, 371, 372, 373, 374, 379, 380, 381, 382, and 384.
Compliance required within the next 200 hours' time in service after the effective date of this AD, unless already accomplished.
To provide a position indicating means for the main landing gear, install a Burgess MK4BR microswitch on the right and left wing in accordance with Siai-Marchetti Service Bulletin No. 205B5A, dated April 11, 1968, or later RAI-approved issue, or an FAA-approved equivalent.
This amendment becomes effective September 7, 1968.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 22
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1967 | 5 |
|---|---|
| 1968 | 9 |
| 1969 | 5 |
3 with no year recorded