AD 74-16-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | 65-B80 | Airworthiness Directives; BEECH Models 65-B80, C90 and E90 Airplanes |
| aircraft | Textron Aviation Inc. | C90 | Airworthiness Directives; BEECH Models 65-B80, C90 and E90 Airplanes |
| aircraft | Textron Aviation Inc. | E90 | Airworthiness Directives; BEECH Models 65-B80, C90 and E90 Airplanes |
Unsafe Condition
Restricted elevator travel
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Required Actions
Install a MS20365-428 self-locking nut on the threaded portion of each of the four elevator control stop bolts in accordance with the attached sketch and Part I of Beechcraft Service Instruction 0618-152 or subsequent revisions or by any equivalent method of compliance approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.
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Compliance Time
within the next 100 hours' time in service after the effective date of this AD
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Affected Aircraft
BEECH Models 65-B80 (Serial Numbers LD-452 through LD-468), C90 (Serial Numbers LJ-552 through LJ-588), and E90 (Serial Numbers LW-1 through LW-56) airplanes.
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Federal Register Abstract
Restricted Elevator Travel
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_74-16-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 74-16-04 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BEECH Models 65-B80, C90 and E90 Airplanes Subject: Restricted Elevator Travel Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 08/06/1974 Make: Textron Aviation Inc. Model: 65-B80 | C90 | E90 Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 74-16-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-1908 AD NUMBER: 74-16-04 SUBJECT HEADING: Airworthiness Directives; BEECH Models 65-B80, C90 and E90 Airplanes ACTION: SUMMARY: DATES: Effective August 6, 1974. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 74-16-04 BEECH: Amendment 39-1908. Applies to Models 65-B80 (Serial Numbers LD-452 through LD-468), C90 (Serial Numbers LJ-552 through LJ-588) and E90 (Serial Numbers LW-1 through LW-56) airplanes. Compliance: Required as indicated, unless already accomplished. To prevent restricted elevator travel, within the next 100 hours' time in service after the effective date of this AD, accomplish the following: Install a MS20365-428 self-locking nut on the threaded portion of each of the four elevator control stop bolts in accordance with the attached sketch and Part I of Beechcraft Service Instruction 0618-152 or subsequent revisions or by any equivalent method of compliance approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region. This amendment becomes effective August 6, 1974. FOOTER:
Document Text
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AD Final Rules - DRS_74-16-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 74-16-04 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BEECH Models 65-B80, C90 and E90 Airplanes Subject: Restricted Elevator Travel Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 08/06/1974 Make: Textron Aviation Inc. Model: 65-B80 | C90 | E90 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: 74-16-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-1908 AD NUMBER: 74-16-04 SUBJECT HEADING: Airworthiness Directives; BEECH Models 65-B80, C90 and E90 Airplanes ACTION: SUMMARY: DATES: Effective August 6, 1974. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 74-16-04 BEECH: Amendment 39-1908. Applies to Models 65-B80 (Serial Numbers LD-452 through LD-468), C90 (Serial Numbers LJ-552 through LJ-588) and E90 (Serial Numbers LW-1 through LW-56) airplanes. Compliance: Required as indicated, unless already accomplished. To prevent restricted elevator travel, within the next 100 hours' time in service after the effective date of this AD, accomplish the following: Install a MS20365-428 self-locking nut on the threaded portion of each of the four elevator control stop bolts in accordance with the attached sketch and Part I of Beechcraft Service Instruction 0618-152 or subsequent revisions or by any equivalent method of compliance approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region. This amendment becomes effective August 6, 1974. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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