AD 89-24-09
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | 19A | Airworthiness Directives; Beech Model A23-19, 19A, M19A, B19, 23, A23, A23A, B23, C23, A23-24, A24, A24R and B24R Airplanes |
| aircraft | Textron Aviation Inc. | 23 | Airworthiness Directives; Beech Model A23-19, 19A, M19A, B19, 23, A23, A23A, B23, C23, A23-24, A24, A24R and B24R Airplanes |
| aircraft | Textron Aviation Inc. | A23 | Airworthiness Directives; Beech Model A23-19, 19A, M19A, B19, 23, A23, A23A, B23, C23, A23-24, A24, A24R and B24R Airplanes |
| aircraft | Textron Aviation Inc. | A23-19 | Airworthiness Directives; Beech Model A23-19, 19A, M19A, B19, 23, A23, A23A, B23, C23, A23-24, A24, A24R and B24R Airplanes |
| aircraft | Textron Aviation Inc. | A23-24 | Airworthiness Directives; Beech Model A23-19, 19A, M19A, B19, 23, A23, A23A, B23, C23, A23-24, A24, A24R and B24R Airplanes |
| aircraft | Textron Aviation Inc. | A23A | Airworthiness Directives; Beech Model A23-19, 19A, M19A, B19, 23, A23, A23A, B23, C23, A23-24, A24, A24R and B24R Airplanes |
| aircraft | Textron Aviation Inc. | A24 | Airworthiness Directives; Beech Model A23-19, 19A, M19A, B19, 23, A23, A23A, B23, C23, A23-24, A24, A24R and B24R Airplanes |
| aircraft | Textron Aviation Inc. | A24R | Airworthiness Directives; Beech Model A23-19, 19A, M19A, B19, 23, A23, A23A, B23, C23, A23-24, A24, A24R and B24R Airplanes |
| aircraft | Textron Aviation Inc. | B19 | Airworthiness Directives; Beech Model A23-19, 19A, M19A, B19, 23, A23, A23A, B23, C23, A23-24, A24, A24R and B24R Airplanes |
| aircraft | Textron Aviation Inc. | B23 | Airworthiness Directives; Beech Model A23-19, 19A, M19A, B19, 23, A23, A23A, B23, C23, A23-24, A24, A24R and B24R Airplanes |
Unsafe Condition
Separation of aileron push rods and possible loss of aileron control due to corrosion and restricted movement of the rod ends.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Within 100 hours time-in-service, install inspection openings in the wing lower skins, inspect aileron rod ends for corrosion and freedom of movement, lubricate serviceable rod end bearings, and replace corroded rod ends with new P/N 169-380082-3 rod ends as specified in Beech Service Bulletin No. 2198. Flights may be conducted under FAR 21.197 to reach a location for AD compliance.
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 (TIS) after the effective date of this AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Beech Models A23-19, 19A, M19A, B19 (MB-1 through MB-816 except MB-814), 23, A23, A23A, B23, C23 (M-1 through M-1879 except M-1875), A23-24, A24 (MA-1 through MA-368), A24R (MC-2 through MC-150), B24R (MC-152 through MC-451 except MC-311 and MC-449).
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
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