- Effective
- March 11, 1967
- 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
- Amendment
- 39-365
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 | a25eb73f…b56e461 | FAA DRS (API key needed) |
On this page
The airworthiness directive
67-08-05 FAIRCHILD-HILLER: Amdt. 39-365 Part 39 Federal Register March 11, 1967. Applies to Model F-27 Series Airplanes Incorporating Stewardess Seat Assembly, Fairchild Drawings No. 27-770633 and 27-770634.
Compliance required within the next 50 hours' time in service after the effective date of this AD unless already accomplished.
To prevent injury to occupants of stewardess seat assemblies, accomplish the following:
(a) Conspicuously post in the vicinity of the stewardess seat and in full view of the seat occupant a placard reading as follows:
"Do not occupy stewardess jump seat during take-off or landing."
(b) The placard required in (a) may be removed when there has been incorporated into the seat assembly a modification approved by the Chief, Engineering and Manufacturing Branch, Eastern Region.
This directive effective March 11, 1967.
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.