AD 86-25-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 767-200 Series | BOEING Model 767 Airplanes |
| aircraft | The Boeing Company | 767-300 Series | BOEING Model 767 Airplanes |
| aircraft | The Boeing Company | 767-300F Series | BOEING Model 767 Airplanes |
Unsafe Condition
Uncommanded deployment of spoiler panels in flight as a result of a rotary variable differential transducer (RVDT) separation.
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Required Actions
Modify the flight control forward control quadrants in accordance with Boeing Alert Service Bulletin 767-27A0062, dated January 24, 1986, or later FAA-approved revisions. An alternate means of compliance or adjustment of the compliance time may be used when approved by the FAA Manager.
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Compliance Time
within six months after the effective date of this AD
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Affected Aircraft
Boeing Model 767-200 Series, 767-300 Series, 767-300F Series airplanes identified in Boeing Alert Service Bulletin 767-27A0062, dated January 24, 1986.
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Federal Register Abstract
Flight Control Quadrants
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_86-25-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 86-25-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: BOEING Model 767 Airplanes Subject: Flight Control Quadrants Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 01/12/1987 Make: The Boeing Company Model: 767-200 Series | 767-300 Series | 767-300F Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 86-25-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5479 AD NUMBER: 86-25-02 SUBJECT HEADING: BOEING Model 767 Airplanes ACTION: SUMMARY: DATES: Effective January 12, 1987. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 86-25-02 BOEING: Amendment 39-5479. Applies to Boeing Model 767 airplanes identified in Boeing Alert Service Bulletin 767-27A0062, dated January 24, 1986, certificated in any category. To prevent the uncommanded deployment of spoiler panels in flight as a result of a rotary variable differential transducer (RVDT) separation, accomplish the following within six months after the effective date of this AD, unless already accomplished: A. Modify the flight control forward control quadrants in accordance with Boeing Alert Service Bulletin 767-27A0062, dated January 24, 1986, or later FAA-approved revisions. B. An alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of the replacements required by this AD. All persons affected by this directive who have not already received the above specified service bulletin from the manufacturer may obtain copies upon request from the Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98124. It may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. This amendment becomes effective January 12, 1987. FOOTER:
Document Text
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AD Final Rules - DRS_86-25-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 86-25-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: BOEING Model 767 Airplanes Subject: Flight Control Quadrants Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 01/12/1987 Make: The Boeing Company Model: 767-200 Series | 767-300 Series | 767-300F Series Product Type: Aircraft Product Subtype: Large 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: 86-25-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5479 AD NUMBER: 86-25-02 SUBJECT HEADING: BOEING Model 767 Airplanes ACTION: SUMMARY: DATES: Effective January 12, 1987. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 86-25-02 BOEING: Amendment 39-5479. Applies to Boeing Model 767 airplanes identified in Boeing Alert Service Bulletin 767-27A0062, dated January 24, 1986, certificated in any category. To prevent the uncommanded deployment of spoiler panels in flight as a result of a rotary variable differential transducer (RVDT) separation, accomplish the following within six months after the effective date of this AD, unless already accomplished: A. Modify the flight control forward control quadrants in accordance with Boeing Alert Service Bulletin 767-27A0062, dated January 24, 1986, or later FAA-approved revisions. B. An alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of the replacements required by this AD. All persons affected by this directive who have not already received the above specified service bulletin from the manufacturer may obtain copies upon request from the Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98124. It may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. This amendment becomes effective January 12, 1987. FOOTER:
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