- Effective
- July 23, 1964
- Models
- F-27, F-27A, F-27B, F-27F, F-27G, F-27J, F-27M
- Data sheet
- TCDS7A1
- Registered aircraft
- 1 matched by model
- Product
- Aircraft · Large airplane
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 | c7faeb45…e6c711a | FAA DRS (API key needed) |
On this page
The airworthiness directive
64-16-03 FAIRCHILD: Amdt. 771 Part 507 Federal Register July 23, 1964. Applies to Model F-27 Series Aircraft.
Compliance required within 300 hours' time in service after the effective date of this AD, unless already accomplished.
Rebalance the rudder in accordance with the procedures specified in Section 2, "Accomplishment Instructions", of Fairchild Service Bulletin 27-38, or an equivalent approved by the Engineering and Manufacturing Branch, FAA Eastern Region.
(Fairchild Service Bulletin 27-38 dated May 4, 1964, covers this same subject.)
This directive effective July 23, 1964.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 1
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.