- Effective
- July 5, 1968
- Model
- S.205 - 22/R
- Data sheet
- TCDSA9EU
- Registered aircraft
- 22 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-607
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 | ed7e0c03…6a317f6 | FAA DRS (API key needed) |
On this page
The airworthiness directive
68-12-01 SIAI-MARCHETTI: Amdt. 39-607. Applies to Model S.205/22R airplanes, Serial Numbers 213 through 4-125.
Compliance required as indicated.
To avoid the possibility of flames or harmful gases passing from the engine compartment into the cockpit or other parts of the airplane, within the next 200 hours' time in service after the effective date of this AD, unless already accomplished, incorporate sealing plates and apply fireproof sealant "Stabond HT-4" or an FAA-approved equivalent at the firewall and nose wheel well, in accordance with Siai-Marchetti Service Bulletin No. 205B19, dated January 13, 1968, or later RAI-approved issue, or FAA-approved equivalent.
This amendment becomes effective July 5, 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