- Effective
- September 22, 1970
- Model
- S.205 - 22/R
- Data sheet
- TCDSA9EU
- Registered aircraft
- 22 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-1081
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 | 8a366ba8…21682e7 | FAA DRS (API key needed) |
On this page
The airworthiness directive
70-20-01 SIAI-MARCHETTI: Amdt. 39-1081. Applies to Model 205-22/R airplanes.
To prevent malfunction of the flap position locking mechanism, within the next 25 hours' time in service after the effective date of this AD, unless already accomplished, replace the flap system locking pawl (P/N 205-6-052-22) and cup (P/N 205-6-052-23) with a modified locking pawl (P/N 205-6-052-22/A) and modified cup (P/N 205-6-052-23/A) in accordance with SIAI Marchetti Technical Instruction No. 205 I-13, dated 3 April 1970, or an FAA-approved equivalent.
(SIAI Marchetti Service Bulletin No. 205B25 refers to this subject).
This amendment becomes effective September 22, 1970.
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