AD 87-04-22
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 767-200 Series | BOEING Model 767 Series Airplanes |
| aircraft | The Boeing Company | 767-300 Series | BOEING Model 767 Series Airplanes |
| aircraft | The Boeing Company | 767-300F Series | BOEING Model 767 Series Airplanes |
Unsafe Condition
Flammable fluid leaking into the engine strut systems raceway may drain onto the engine core.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Within 30 days after the effective date, inspect the underside of the engine strut system raceway and fill any unsealed openings per Boeing Alert Service Bulletin 767-54A0024. Alternate compliance may be approved by the Manager, Seattle Aircraft Certification Office.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 30 days after the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Boeing Model 767 series airplanes equipped with General Electric CF6-80 series engines listed in Boeing Alert Service Bulletin 767-54A0024 dated December 23, 1986.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Engine Strut Systems Raceway
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_87-04-22.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 87-04-22 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: BOEING Model 767 Series Airplanes Subject: Engine Strut Systems Raceway Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 03/13/1987 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767-200 Series | 767-300 Series | 767-300F Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 87-04-22 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5566 AD NUMBER: 87-04-22 SUBJECT HEADING: BOEING Model 767 Series Airplanes ACTION: SUMMARY: DATES: Effective March 13, 1987. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 87-04-22 BOEING: Amendment 39-5566. Applies to Model 767 series airplanes, equipped with General Electric CF6-80 series engines, listed in Boeing Alert Service Bulletin 767- 54A0024 dated December 23, 1986, certificated in any category. Compliance required as indicated, unless previously accomplished. To preclude flammable fluid leaking into the engine strut systems raceway from draining onto the engine core, accomplish the following: A. Within 30 days after the effective date of this AD, inspect the underside of the engine strut system raceway and fill any unsealed openings identified in accordance with Boeing Alert Service Bulletin 767-54A0024 dated December 23, 1986, or later FAA-approved revision. B. An alternate means of compliance or adjustment of 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 in order to comply with the requirements of this AD. All persons affected by this directive who have not already received the appropriate service information from the manufacturer may obtain copies upon request to the Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98124-2207. This information may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, FAA, Northwest Mountain Region, 9010 East Marginal Way South, Seattle, Washington. This amendment becomes effective March 13, 1987. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_87-04-22.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 87-04-22 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: BOEING Model 767 Series Airplanes Subject: Engine Strut Systems Raceway Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 03/13/1987 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: 87-04-22 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5566 AD NUMBER: 87-04-22 SUBJECT HEADING: BOEING Model 767 Series Airplanes ACTION: SUMMARY: DATES: Effective March 13, 1987. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 87-04-22 BOEING: Amendment 39-5566. Applies to Model 767 series airplanes, equipped with General Electric CF6-80 series engines, listed in Boeing Alert Service Bulletin 767- 54A0024 dated December 23, 1986, certificated in any category. Compliance required as indicated, unless previously accomplished. To preclude flammable fluid leaking into the engine strut systems raceway from draining onto the engine core, accomplish the following: A. Within 30 days after the effective date of this AD, inspect the underside of the engine strut system raceway and fill any unsealed openings identified in accordance with Boeing Alert Service Bulletin 767-54A0024 dated December 23, 1986, or later FAA-approved revision. B. An alternate means of compliance or adjustment of 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 in order to comply with the requirements of this AD. All persons affected by this directive who have not already received the appropriate service information from the manufacturer may obtain copies upon request to the Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98124-2207. This information may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, FAA, Northwest Mountain Region, 9010 East Marginal Way South, Seattle, Washington. This amendment becomes effective March 13, 1987. FOOTER:
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.