- Effective
- April 7, 1977
- Model
- Fan Jet Falcon
- Data sheet
- TCDSA7EU
- Registered aircraft
- 24 matched by model
- Product
- Aircraft · Large airplane
- Amendment
- 39-2857
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 | 1356020b…bd4360c | FAA DRS (API key needed) |
On this page
The airworthiness directive
77-07-02 AVIONS MARCEL DASSAULT (AMD): Amendment 39-2857. Applies to all Fan Jet Falcon airplanes, all series, certificated in all categories, not incorporating AMD Modification No. 2092.
Compliance is required within the next 300 hours time in service after the effective date of this AD, unless already accomplished.
To prevent possible horizontal stabilizer trim runaway, remove the positive voltage wire from the normally-closed contacts of the pilot's and copilot's horizontal stabilizer trim control switches in accordance with paragraphs 2B through 2F of the section entitled "Accomplishment Instructions" of AMD Service Bulletin No. 568, Revision 1 dated October 25, 1976, or an FAA- approved equivalent.
This amendment becomes effective April 7, 1977.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 24
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1966 | 3 |
|---|---|
| 1967 | 5 |
| 1968 | 2 |
| 1969 | 3 |
| 1970 | 1 |
| 1971 | 1 |
| 1972 | 1 |
| 1974 | 1 |
| 1977 | 2 |
5 with no year recorded