- Effective
- August 15, 1975
- Models
- F.260, F.260B
- Data sheet
- TCDSA10EU
- Registered aircraft
- 11 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-2307
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 | 20 KB | 07c8eefc…34dacab | FAA DRS (API key needed) |
On this page
The airworthiness directive
75-17-06 SIAI-MARCHETTI: Amendment 39-2307. Applies to Models F.260 and F.260B, all serial numbers, certificated in all categories.
Compliance is required within the next 10 hours time in service after the effective date of this AD, unless already accomplished.
To provide instructions for the correct operation of the emergency landing gear control, replace the "Emergency Landing Gear Extension" procedure set forth on page 9 of the airplane Flight Manual with a copy of the procedure set forth in SIAI Service Bulletin S.B.No.260B5, dated December 23, 1970, or an FAA-approved equivalent. Retain a copy of the procedure of Service Bulletin S.B.No. 260B5, or an FAA-approved equivalent, in the airplane Flight Manual until the procedure has been incorporated by the approved revision dated August 9, 1973 into the airplane Flight Manual.
This amendment becomes effective August 15, 1975.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 11
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1968 | 2 |
|---|---|
| 1969 | 2 |
| 1970 | 1 |
| 1971 | 1 |
| 1972 | 1 |
4 with no year recorded
By model
Aircraft
NTSB investigations that cite this AD · 1
Their narratives or probable cause name AD 75-17-06, often to say whether the aircraft complied with it.