- Effective
- April 18, 1970
- Model
- Fan Jet Falcon
- Data sheet
- TCDSA7EU
- Registered aircraft
- 24 matched by model
- Product
- Aircraft · Large airplane
- Amendment
- 39-958
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 | 5f78786f…a457039 | FAA DRS (API key needed) |
On this page
The airworthiness directive
70-06-07 AVIONS MARCEL DASSAULT/SUD-AVIATION: Amdt. 39-958. Applies to all series Fan Jet Falcon airplanes with Microturbo Saphir I and II APU's installed.
Compliance is required within the next 75 hours of APU operation, unless already accomplished.
To prevent a fire hazard due to continued operation of the APU oil pump motor after APU shutdown, replace Equipment Construction Electrique (ECE) relay P/N 1475-7 with ECE contactor P/N 100CC01-A in accordance with Microturbo Saphir I Service Bulletin 49.10.39, dated September 30, 1969; or Microturbo Saphir II Service Bulletin 49.11.08, Revision No. 1, dated September 30, 1969, as applicable, or later SGAC-approved issues, or FAA-approved equivalents.
This amendment becomes effective April 18, 1970.
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