- Effective
- June 14, 1976
- 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
- 39-2609
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 | 5fe3c08e…d467d46 | FAA DRS (API key needed) |
On this page
The airworthiness directive
76-10-07 FAIRCHILD: Amendment 39-2609. Applies to all F-27 airplanes incorporating the outward opening large cargo door installed in accordance with STC No. SA932SW.
Compliance required within the next 300 hours' or 30 days' time in service, whichever occurs first, after the effective date of this AD unless already accomplished.
To prevent inadvertent opening of the large cargo door in flight, accomplish the alteration in paragraph 2, Accomplishment Instructions, in Fairchild Service Bulletin F27-52-31 dated January 8, 1976, for F-27 airplanes or an equivalent alteration approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Southwest Region.
This amendment becomes effective June 14, 1976.
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.
By model
Aircraft
NTSB investigations that cite this AD · 1
Their narratives or probable cause name AD 76-10-07, often to say whether the aircraft complied with it.