- Effective
- August 22, 1967
- Model
- FH 76-1
- Data sheet
- TCDSP1IN
- Product
- Propeller
- Amendment
- 39-467
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 | c9543786…7a5816e | FAA DRS (API key needed) |
On this page
The airworthiness directive
67-24-04 RATIER-FIGEAC: Amdt. No. 39-467, Part 39, Federal Register August 22, 1967. Applies to Model FH 76-1-7 Propellers Installed on Pilatus PC-6a Series Aircraft.
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 pitch change actuator, replace the bronze actuator socket, P/N FH 76-1-120-02, with a steel actuator socket, P/N FH 76-2-120-02, in accordance with Ratier Figeac Service Bulletin 64-45, dated October 1966, or later SGAC-approved issue, or an FAA-approved equivalent.
This amendment effective August 22, 1967.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.