| AD Number | 65-10-01 | Status | Active |
| Effective Date | May 08, 1965 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-64 |
| Product Type | ["Aircraft"] | Product Subtype | ["Large Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Maryland Air Industries, Inc. |
| Model(s) | F-27 F-27A F-27B F-27F F-27G F-27J F-27M |
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.