AD 76-25-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | 19A | Airworthiness Directives; BEECH Models A23-19, 19A, M19A, B19, 23, A23, A23A, B23, C23, A-23-24, A24, and A24R Airplanes |
| aircraft | Textron Aviation Inc. | 23 | Airworthiness Directives; BEECH Models A23-19, 19A, M19A, B19, 23, A23, A23A, B23, C23, A-23-24, A24, and A24R Airplanes |
| aircraft | Textron Aviation Inc. | A23 | Airworthiness Directives; BEECH Models A23-19, 19A, M19A, B19, 23, A23, A23A, B23, C23, A-23-24, A24, and A24R Airplanes |
| aircraft | Textron Aviation Inc. | A23-19 | Airworthiness Directives; BEECH Models A23-19, 19A, M19A, B19, 23, A23, A23A, B23, C23, A-23-24, A24, and A24R Airplanes |
| aircraft | Textron Aviation Inc. | A23-24 | Airworthiness Directives; BEECH Models A23-19, 19A, M19A, B19, 23, A23, A23A, B23, C23, A-23-24, A24, and A24R Airplanes |
| aircraft | Textron Aviation Inc. | A23A | Airworthiness Directives; BEECH Models A23-19, 19A, M19A, B19, 23, A23, A23A, B23, C23, A-23-24, A24, and A24R Airplanes |
| aircraft | Textron Aviation Inc. | A24 | Airworthiness Directives; BEECH Models A23-19, 19A, M19A, B19, 23, A23, A23A, B23, C23, A-23-24, A24, and A24R Airplanes |
| aircraft | Textron Aviation Inc. | A24R | Airworthiness Directives; BEECH Models A23-19, 19A, M19A, B19, 23, A23, A23A, B23, C23, A-23-24, A24, and A24R Airplanes |
| aircraft | Textron Aviation Inc. | B19 | Airworthiness Directives; BEECH Models A23-19, 19A, M19A, B19, 23, A23, A23A, B23, C23, A-23-24, A24, and A24R Airplanes |
| aircraft | Textron Aviation Inc. | B23 | Airworthiness Directives; BEECH Models A23-19, 19A, M19A, B19, 23, A23, A23A, B23, C23, A-23-24, A24, and A24R Airplanes |
Unsafe Condition
Interchanging left and right ailerons during reinstallation could result in reversed aileron control response.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install one each Beech P/N 169-110000-481 strap in the left and right wing trailing edge in accordance with Beechcraft Service Instruction 0510-032 or later approved revisions. Any alternate method of compliance must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the next 100 hours' time in service after the effective date of this AD or at the next removal of the ailerons or within one year after the effective date of this AD, whichever occurs first
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
BEECH Models A23-19, 19A, M19A, B19 (Serial Numbers MB-1 thru MB-545 and MB-547), Models 23, A23, A23A, B23 and C23 (Serial Numbers M-2 thru M-1415), Models A-23-24 and A24 (Serial Numbers MA-1 thru MA-368), and Models A24R (Serial Numbers MC-2 thru MC-127)
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.