AD 84-11-02 R2
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 767-200 Series | BOEING Model 767-200 Series Airplanes |
Unsafe Condition
Failure of the engine fuel feed hose and engine flame out or engine nacelle fire.
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Required Actions
Inspect and replace, as necessary, the engine fuel feed hose in accordance with Boeing Service Bulletin 767-73-11 or later FAA-approved revision. The repetitive inspection requirement is terminated by installing fuel feed hose P/N S332TO12-11 per Service Bulletin 767-73-11, Revision 2, or later FAA-approved revisions.
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Compliance Time
Within the next 200 landings or 30 days, whichever occurs first, after the effective date of this AD, and thereafter at intervals not to exceed 200 landings.
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Affected Aircraft
Boeing Model 767-200 series airplanes equipped with CF6 engines as listed in Boeing Service Bulletin 767-73-11 dated March 28, 1984, or later FAA-approved revision.
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Federal Register Abstract
Engine Fuel Feed Hose
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_84-11-02_R.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 84-11-02 R2 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: BOEING Model 767-200 Series Airplanes Subject: Engine Fuel Feed Hose Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 09/16/1985 Make: The Boeing Company Model: 767-200 Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 84-11-02 R2 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5117 AD NUMBER: 84-11-02 R2 SUBJECT HEADING: BOEING Model 767-200 Series Airplanes ACTION: SUMMARY: DATES: Effective September 16, 1985. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 84-11-02 R2 BOEING: Amendment 39-4873 as amended by Amendment 39-4979, is further amended by Amendment 39-5117. Applies to the Model 767-200 series airplanes equipped with CF6 engines as listed in Boeing Service Bulletin 767-73-11 dated March 28, 1984, or later FAA approved revision, certificated in all categories. Compliance is required as indicated unless previously accomplished. To prevent failure of the engine fuel feed hose and engine flame out or engine nacelle fire, accomplish the following: A. Within the next 200 landings or 30 days, whichever occurs first, after the effective date of this AD, and thereafter at intervals not to exceed 200 landings, inspect and replace, as necessary, the engine fuel feed hose in accordance with Boeing Service Bulletin 767-73-11 dated March 28, 1984, or later FAA approved revision. NOTE: It is anticipated that this AD will be amended when a new reinforced hose or equivalent terminating action is available. B. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. C. For the purpose of this AD, and when approved by an FAA maintenance inspector, the number of landings may be computed by dividing each airplane's time in service by the operator's fleet average time from takeoff to landing for the aircraft type. D. 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 inspections and/or modifications required by this AD. E. Installation of fuel feed hose P/N S332TO12-11 in accordance with Service Bulletin 767-73-11, Revision 2, dated May 25, 1984, or later FAA-approved revisions, terminates the repetitive inspection requirement of paragraph A., above. Amendment 39-4873 became effective June 4, 1984. Amendment 39-4979 became effective January 24, 1985. This amendment 39-5117 becomes effective September 16, 1985. FOOTER:
Document Text
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AD Final Rules - DRS_84-11-02_R.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 84-11-02 R2 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: BOEING Model 767-200 Series Airplanes Subject: Engine Fuel Feed Hose Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 09/16/1985 Make: The Boeing Company Model: 767-200 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: 84-11-02 R2 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5117 AD NUMBER: 84-11-02 R2 SUBJECT HEADING: BOEING Model 767-200 Series Airplanes ACTION: SUMMARY: DATES: Effective September 16, 1985. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 84-11-02 R2 BOEING: Amendment 39-4873 as amended by Amendment 39-4979, is further amended by Amendment 39-5117. Applies to the Model 767-200 series airplanes equipped with CF6 engines as listed in Boeing Service Bulletin 767-73-11 dated March 28, 1984, or later FAA approved revision, certificated in all categories. Compliance is required as indicated unless previously accomplished. To prevent failure of the engine fuel feed hose and engine flame out or engine nacelle fire, accomplish the following: A. Within the next 200 landings or 30 days, whichever occurs first, after the effective date of this AD, and thereafter at intervals not to exceed 200 landings, inspect and replace, as necessary, the engine fuel feed hose in accordance with Boeing Service Bulletin 767-73-11 dated March 28, 1984, or later FAA approved revision. NOTE: It is anticipated that this AD will be amended when a new reinforced hose or equivalent terminating action is available. B. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. C. For the purpose of this AD, and when approved by an FAA maintenance inspector, the number of landings may be computed by dividing each airplane's time in service by the operator's fleet average time from takeoff to landing for the aircraft type. D. 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 inspections and/or modifications required by this AD. E. Installation of fuel feed hose P/N S332TO12-11 in accordance with Service Bulletin 767-73-11, Revision 2, dated May 25, 1984, or later FAA-approved revisions, terminates the repetitive inspection requirement of paragraph A., above. Amendment 39-4873 became effective June 4, 1984. Amendment 39-4979 became effective January 24, 1985. This amendment 39-5117 becomes effective September 16, 1985. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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