- Effective
- March 20, 1975
- Models
- 60, A60
- Data sheet
- TCDSA12CE
- Registered aircraft
- 75 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-2129
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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| FAA DRS HTML | 20 KB | 5289a4bd…cf0643e | FAA DRS (API key needed) |
On this page
The airworthiness directive
75-06-09 BEECH: Amendment 39-2129. Applies to Models 60 and A60 (Serial Numbers P-3 through P-200) airplanes with more than 150 hours' time in service.
Compliance: Required as indicated, unless already accomplished.
To prevent malfunctions of the elevator inboard hinge supports, within the next 100 hours' time in service after the effective date of this AD, accomplish the following:
Remove the left and right elevator inboard hinge supports (P/N 60-524078-1 and 60- 524078-2) and install improved supports in accordance with Beech Kit No. 60-4005 or any equivalent modification approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.
Beechcraft Service Instruction No. 0342-132, Revision III, or later revision refers to this subject.
This amendment supersedes Amendment 39-1463, AD 72-13-01.
This amendment becomes effective March 20, 1975.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 75
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1968 | 7 |
|---|---|
| 1969 | 15 |
| 1970 | 10 |
| 1971 | 5 |
| 1972 | 9 |
| 1973 | 12 |
| 1975 | 1 |
16 with no year recorded