- Effective
- August 26, 1965
- Published
- August 26, 1965
- Models
- 23, A23
- Data sheet
- TCDSA1CE
- Registered aircraft
- 232 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-125
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 January 21, 2026.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
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On this page
The airworthiness directive
65-19-02 BEECH: Amdt. 39-125 Part 39 Federal Register August 26, 1965. Applies to Model 23 Airplanes, Serial Numbers M-225 through M-554 except M-344, M-381, M-387, M- 389, and M-390; and Model A23 Airplanes, Serial Numbers M-556 through M-791 except M- 737, M-742, M-763, N-764, M-777, and M-780.
Compliance required within the next 50 hours' time in service after the effective date of this AD unless already accomplished.
To prevent failure of the aileron control column links due to insufficient edge distance and resultant loss of aileron control, accomplish the following:
Visually inspect the four links, P/N 169-524040-15, that attach the aileron cable to the chain on the control column for edge distance. Replace each link with edge distance less than 0.16 inch, measured from the center of the attach hole to the edge of the link, with a link with edge distance of 0.16 inch or greater or an FAA-approved equivalent.
(Beech Service Bulletin No. 65-13, dated July1965, covers this same subject.)
This directive effective August 26, 1965.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 232
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1962 | 30 |
|---|---|
| 1963 | 81 |
| 1964 | 21 |
| 1965 | 44 |
| 1966 | 2 |
54 with no year recorded