- Effective
- May 11, 1967
- Model
- FH 76-1
- Data sheet
- TCDSP1IN
- Product
- Propeller
- Amendment
- 39-393
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 | 074e61c2…5c4e60e | FAA DRS (API key needed) |
On this page
The airworthiness directive
67-14-08 RATIER-FIGEAC: Amdt. 39-393, Part 39, Federal Register April 11, 1967. Applies to Model FH 76-1 Propellers Installed on Pilatus Model PC-6 Series Airplanes.
Compliance required within the next 200 hours' time in service after the effective date of this AD, unless already accomplished, or previously modified by Ratier Fageac (Amendment No. 1018).
To prevent failure of the magnesium pitch change reduction gear housing, P/N 76-300- 01, rework the housing in accordance with Ratier Figeac Service Bulletin 61-44, dated December 1966, or later SGAC-approved revision.
This directive effective May 11, 1967.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.