- Effective
- August 22, 1977
- Model
- Falcon 10
- Data sheet
- TCDSA33EU
- Registered aircraft
- 59 matched by model
- Product
- Aircraft · Large airplane
- Amendment
- 39-2981
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 | 7d517761…7b09c8c | FAA DRS (API key needed) |
On this page
The airworthiness directive
77-15-08 AVIONS MARCEL DASSAULT-BREGUET AVIATION (AMD-BA): Amendment 39-2981. Applies to Model Falcon 10 airplanes, certificated in all categories, incorporating SICMA AERO-SEAT pilot seat, P/N 376-2, or copilot seat, P/N 376-3.
Compliance is required within the next 100 hours time in service after the effective date of this AD unless already accomplished.
To prevent possible unwanted movement of a pilot or copilot seat when operating in turbulence or when performing high-g maneuvers, for SICMA AERO-SEAT pilot seats, P/N 376-2, and copilot seats, P/N 376-3, modify the seat rails and reidentify the seats in accordance with SICMA AERO-SEAT Service Bulletin 376/F10/BS01, dated June 5, 1975, including Revision "A", dated July 1975, or an FAA-approved equivalent.
(AMD-BA Service Bulletin No. F10/0093 (ATA No. F10/25/007), dated July 18, 1975, pertains to this subject.)
This amendment becomes effective August 22, 1977.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 59
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1974 | 8 |
|---|---|
| 1975 | 2 |
| 1976 | 1 |
| 1977 | 4 |
| 1978 | 1 |
| 1979 | 5 |
| 1980 | 7 |
| 1981 | 5 |
| 1982 | 3 |
| 1987 | 2 |
| 1988 | 4 |
| 1989 | 1 |
| 1990 | 1 |
15 with no year recorded