- Effective
- May 8, 1965
- 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
- 39-64
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 | 24d278ed…a118bba | FAA DRS (API key needed) |
On this page
The airworthiness directive
65-10-01 FAIRCHILD: Amdt. 39-64 Part 39 Federal Register May 8, 1965. Applies to Model F-27 Aircraft with Center Hinge Wing Flap Asymmetry Switches, P/N 658-001.
Compliance required within 25 hours' time in service after the effective date of this AD, unless already accomplished.
(a) Modify aircraft in accordance with Fairchild Service Bulletin No. 27-19, dated June 6, 1960, or Service Bulletin No. 27-26, dated September 9, 1960, Revision 1, dated March 1, 1965, or an equivalent approved by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region.
(b) Upon request of an operator, an FAA maintenance inspector, subject to prior approval of the Chief, Engineering and Manufacturing Branch, FAA Eastern Region, may adjust the compliance time specified in this AD if the request contains substantiating data to justify the increase for such operator.
This directive effective upon publication in the Federal Register for all persons except those to whom it was madeeffective immediately by telegram dated April 23, 1965.
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.