- Effective
- February 17, 1976
- Models
- 35-B33, 35-C33, E33, F33, G33, P35
- Data sheet
- TCDS3A15
- Registered aircraft
- 913 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-2510
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 |
|---|---|---|---|
| FAA DRS HTML | 20 KB | 8e421ad1…e4f6604 | FAA DRS (API key needed) |
On this page
The airworthiness directive
76-03-05 BEECH: Amendment 39-2510. Applies to Models 35-B33, 35-C33, E-33, F-33 and G-33 (Serial Numbers CD-388 thru CD-981 and CD-983 thru CD-1304); and Model P-35 (Serial Numbers D-6842 thru D-7139 and D-7141 thru D-7309) airplanes.
Compliance: Required as indicated unless already accomplished.
To preclude contact of the tachometer cable housing with the battery relay, within the next 50 hours' time in service after the effective date of this AD, install a tachometer cable housing stand-off bracket on the battery box and secure the tachometer cable housing to this bracket in accordance with Beechcraft Service Instruction No. 0784-241 or later FAA-approved revisions or by any equivalent method approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.
This amendment becomes effective February 17, 1976.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 913
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1961 | 80 |
|---|---|
| 1962 | 202 |
| 1963 | 191 |
| 1964 | 68 |
| 1965 | 104 |
| 1966 | 36 |
| 1967 | 34 |
| 1968 | 29 |
| 1969 | 16 |
| 1970 | 10 |
| 1971 | 12 |
| 1972 | 25 |
106 with no year recorded