| AD Number | 65-22-02 | Status | Active |
| Effective Date | September 29, 1965 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-139 |
| Product Type | ["Aircraft"] | Product Subtype | ["Large Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Lockheed Martin Corporation |
| Model(s) | 1329-23A 1329-23D |
65-22-02 LOCKHEED: Amdt. 39-139 Part 39 Federal Register September 29, 1965. Applies to Model 1329 Airplanes, Serial Numbers 5001 through 5063.
Compliance required within the next 10 hours' time in service after the effective date of this AD, unless already accomplished.
To prevent uncontrolled pitch trim actuation, accomplish the inspection and repair as described in Lockheed Alert Service Bulletin No. 329-218, "Horizontal Stabilizer Trim System- Inspection of A-723L, A-723LA, A-723LD, and A-723N Stabilizer Trim Contactors," or perform an equivalent FAA-approved inspection and repair.
This directive effective September 29, 1965.