- Effective
- March 12, 1982
- Models
- SA-360C Dauphin, SA-365C, SA-365C1, SA-365C2
- Product
- Aircraft · Rotorcraft
- Amendment
- 39-4331
- Docket
- 82-ASW-4
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 | a9859fdd…7df7b79 | FAA DRS (API key needed) |
On this page
The airworthiness directive
82-05-04 SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE (SNIAS): Amendment 39-4331. Applies to Model SA360C and SA365C series helicopters certificated in all categories (Airworthiness Docket No. 82-ASW-4).
Compliance is required within 30 days after the effective date of this AD.
To prevent possible excessive deformation of the pilot's and copilot's seat long slides and resulting tilt of the seats, accomplish the following modification unless already accomplished.
(a) Add doublers to the 4 long slides as prescribed in Aerospatiale Dauphin Service Bulletin No. 25.08, dated March 23, 1981, or as prescribed in an equivalent modification approved by Chief, Aircraft Certification Staff, FAA, Europe, Africa, and Middle East Office.
(b) Aircraft may be flown in accordance with FAR 21.197 and 21.199 to a base where the slide doublers may be installed.
This amendment becomes effective March 12, 1982.
Affected TCDS · 2
The type certificate data sheets for the models this AD names, matched by model and maker.