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 |
| aircraft | Textron Aviation Inc. | C23 | 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. | M19A | 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.
Federal Register Abstract
Aileron Control
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_76-25-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 76-25-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BEECH Models A23-19, 19A, M19A, B19, 23, A23, A23A, B23, C23, A-23-24, A2...Show more Subject: Aileron Control Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 01/24/1977 Make: Textron Aviation Inc. Model: 19A | 23 | A23 | A23-19 | A23-24 | A23A | A24 | A24R | B19 | B23 | C23 | M19A Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 76-25-05 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-2789 AD NUMBER: 76-25-05 SUBJECT HEADING: Airworthiness Directives; BEECH Models A23-19, 19A, M19A, B19, 23, A23, A23A, B23, C23, A-23-24, A24, and A24R Airplanes ACTION: SUMMARY: DATES: Effective January 24, 1977. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 76-25-05 BEECH: Amendment 39-2789. Applies to Models A23-19, 19A, M19A and 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) airplanes. Compliance: Required as indicated, unless already accomplished. To prevent interchanging left and right ailerons during reinstallation and resulting reversed aileron control response, accomplish the following: A) 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, 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. B) Any alternate method of compliance with this AD must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region. This amendment becomes effective January 24, 1977. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_76-25-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 76-25-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BEECH Models A23-19, 19A, M19A, B19, 23, A23, A23A, B23, C23, A-23-24, A2...Show more Subject: Aileron Control Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 01/24/1977 Make: Textron Aviation Inc. Model: 19A | 23 | A23 | A23-19 | A23-24 | A23A | A24 | A24R | B19 | B23 | C23 | M19A Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 76-25-05 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-2789 AD NUMBER: 76-25-05 SUBJECT HEADING: Airworthiness Directives; BEECH Models A23-19, 19A, M19A, B19, 23, A23, A23A, B23, C23, A-23-24, A24, and A24R Airplanes ACTION: SUMMARY: DATES: Effective January 24, 1977. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 76-25-05 BEECH: Amendment 39-2789. Applies to Models A23-19, 19A, M19A and 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) airplanes. Compliance: Required as indicated, unless already accomplished. To prevent interchanging left and right ailerons during reinstallation and resulting reversed aileron control response, accomplish the following: A) 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, 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. B) Any alternate method of compliance with this AD must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region. This amendment becomes effective January 24, 1977. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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