- Effective
- July 21, 1970
- Models
- 19A, 23, A23, A23-19, A23-24, A23A, B23
- Data sheet
- TCDSA1CE
- Registered aircraft
- 579 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-1037
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.
| File | Size | SHA-256 | Original |
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| FAA DRS HTML | 20 KB | 834e05d7…14b43e3 | FAA DRS (API key needed) |
On this page
The airworthiness directive
70-15-03 BEECH: Amdt. 39-1037. Applies to Models 23, A23, A23A and B23 (Serial Numbers M-1 through M-1162); A23-24 (Serial Numbers MA-1 through MA-333); and A23-19 and 19A (Serial Numbers MB-1 through MB-392) Airplanes.
Compliance: Required as indicated, unless already accomplished.
To prevent stiff operation, binding and seizing of Beech P/N 169-920000-127 fuel selector valve assembly, accomplish the following:
Within 25 hours' time in service after the effective date of this AD, modify Beech P/N 169-920000-127 fuel selector valve assembly in accordance with Beechcraft Service Instructions No. 0364-289, or later FAA approved revision, or an equivalent method approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.
This amendment becomes effective July 21, 1970.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 579
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 | 57 |
| 1966 | 101 |
| 1967 | 67 |
| 1968 | 69 |
| 1969 | 42 |
111 with no year recorded