- Effective
- October 9, 1967
- Model
- Fan Jet Falcon
- Data sheet
- TCDSA7EU
- Registered aircraft
- 24 matched by model
- Product
- Aircraft · Large airplane
- Amendment
- 39-474
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 | 7bb1d80a…c6f5260 | FAA DRS (API key needed) |
On this page
The airworthiness directive
67-27-01 AVIONS MARCEL DASSAULT: Amdt. 39-474, Part 39, Federal Register September 9, 1967. Applies to Fan Jet Falcon Airplanes, Serial Numbers 1 thru 94.
Compliance required within the next 200 hours' time in service after the effective date of this AD, unless already accomplished.
To prevent jamming of the engine power lever, modify the type MF 2006 pressurization control microswitch installation by the addition of a support, P/N MY.20.240.3801, and a leaf spring, P/N MY.20.240.3802, in accordance with Avions Marcel Dassault Service Bulletin No. 211, (76-4), revision 1, dated April 4, 1967, or later SGAC-approved revision, or an equivalent approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa and Middle East Region.
This amendment effective October 9, 1967.
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