AD 92-10-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 767-200 Series | Airworthiness Directives; BOEING Model 767 Series Airplanes |
| aircraft | The Boeing Company | 767-300 Series | Airworthiness Directives; BOEING Model 767 Series Airplanes |
| aircraft | The Boeing Company | 767-300F Series | Airworthiness Directives; BOEING Model 767 Series Airplanes |
Unsafe Condition
The overwing escape slide may be damaged by sharp edges of the rub strip on the inboard spoilers.
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Required Actions
Modify the inboard edges of the rub strip on the inboard spoilers in accordance with Boeing Service Bulletin 767-27-0104, Revision 2, dated September 12, 1991. For airplanes with part numbers 113T4100-37, -38, -41, -42, -45, and -46, the modification must be done within 9 months after the effective date of this AD. An alternative method of compliance may be used if approved by the FAA.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the next 9 months after August 29, 1991 (the effective date of amendment 39-7077) for most airplanes, or within the next 9 months after the effective date of this AD (June 11, 1992) for airplanes with specified part numbers.
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Affected Aircraft
Boeing Model 767 series airplanes listed in Boeing Service Bulletin 767-27-0104, Revision 2, dated September 12, 1991; certificated in any category.
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Federal Register Abstract
Inboard Spoilers
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_92-10-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 92-10-01 Document Type: AD Final Rules Docket Number: 91-NM-240-AD Subject Heading: Airworthiness Directives; BOEING Model 767 Series Airplanes Subject: Inboard Spoilers Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 06/11/1992 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767-200 Series | 767-300 Series | 767-300F Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 92-10-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 91-NM-240-AD AMENDMENT: 39-8234 AD NUMBER: 92-10-01 SUBJECT HEADING: Airworthiness Directives; BOEING Model 767 Series Airplanes ACTION: SUMMARY: DATES: Effective June 11, 1992 ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 92-10-01 BOEING: Amendment 39-8234. Docket No. 91-NM-240-AD. Supersedes AD 91-15-13, Amendment 39-7077. Applicability: Model 767 series airplanes, as listed in Boeing Service Bulletin 767-27-0104, Revision 2, dated September 12, 1991; certificated in any category. Compliance: Required as indicated, unless previously accomplished. To prevent the overwing escape slide from being damaged by sharp edges of the rub strip on the inboard spoilers, accomplish the following: (a) Except as provided by paragraph (b) of this AD, within the next 9 months after August 29, 1991 (the effective date of amendment 39-7077), modify the inboard edges of the rub strip on the inboard spoilers in accordance with Boeing Service Bulletin 767-27-0104, dated November 15, 1990, or Revision 1, dated May 30, 1991. (b) For airplanes equipped with inboard spoiler assemblies, part numbers 113T4100-37, -38, -41, -42, -45, and -46: Within the next 9 months after the effective date of this AD, modify the inboard edges of the rub strip on the inboard spoilers in accordance with Boeing Service Bulletin 767-27-0104, Revision 2, dated September 12, 1991. (c) An alternative method 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 (ACO), FAA, Transport Airplane Directorate. The request shall be forwarded through an FAA Principal Maintenance Inspector, who may concur or comment and then send it to the Manager, Seattle ACO. (d) 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. (e) The modification shall be done in accordance with Boeing Service Bulletin 767-27-0104, dated November 15, 1990; or Revision 1, dated May 30, 1991; or Revision 2, dated September 12, 1991; as applicable. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. [The incorporation by reference of Boeing Service Bulletin 767-27-0104, dated November 15, 1990, and Revision 1, dated May 30, 1991, was previously approved by the Director of the Federal Register as of August 29, 1991 (56 FR 34019, July 25, 1991).] Copies may be obtained from Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington; or at the Office of the Federal Register, 1100 L Street NW., Room 8401, Washington, DC. (f) This amendment becomes effective on June 11, 1992. FOOTER:
Document Text
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AD Final Rules - DRS_92-10-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 92-10-01 Document Type: AD Final Rules Docket Number: 91-NM-240-AD Subject Heading: Airworthiness Directives; BOEING Model 767 Series Airplanes Subject: Inboard Spoilers Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 06/11/1992 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: 92-10-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 91-NM-240-AD AMENDMENT: 39-8234 AD NUMBER: 92-10-01 SUBJECT HEADING: Airworthiness Directives; BOEING Model 767 Series Airplanes ACTION: SUMMARY: DATES: Effective June 11, 1992 ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 92-10-01 BOEING: Amendment 39-8234. Docket No. 91-NM-240-AD. Supersedes AD 91-15-13, Amendment 39-7077. Applicability: Model 767 series airplanes, as listed in Boeing Service Bulletin 767-27-0104, Revision 2, dated September 12, 1991; certificated in any category. Compliance: Required as indicated, unless previously accomplished. To prevent the overwing escape slide from being damaged by sharp edges of the rub strip on the inboard spoilers, accomplish the following: (a) Except as provided by paragraph (b) of this AD, within the next 9 months after August 29, 1991 (the effective date of amendment 39-7077), modify the inboard edges of the rub strip on the inboard spoilers in accordance with Boeing Service Bulletin 767-27-0104, dated November 15, 1990, or Revision 1, dated May 30, 1991. (b) For airplanes equipped with inboard spoiler assemblies, part numbers 113T4100-37, -38, -41, -42, -45, and -46: Within the next 9 months after the effective date of this AD, modify the inboard edges of the rub strip on the inboard spoilers in accordance with Boeing Service Bulletin 767-27-0104, Revision 2, dated September 12, 1991. (c) An alternative method 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 (ACO), FAA, Transport Airplane Directorate. The request shall be forwarded through an FAA Principal Maintenance Inspector, who may concur or comment and then send it to the Manager, Seattle ACO. (d) 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. (e) The modification shall be done in accordance with Boeing Service Bulletin 767-27-0104, dated November 15, 1990; or Revision 1, dated May 30, 1991; or Revision 2, dated September 12, 1991; as applicable. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. [The incorporation by reference of Boeing Service Bulletin 767-27-0104, dated November 15, 1990, and Revision 1, dated May 30, 1991, was previously approved by the Director of the Federal Register as of August 29, 1991 (56 FR 34019, July 25, 1991).] Copies may be obtained from Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington; or at the Office of the Federal Register, 1100 L Street NW., Room 8401, Washington, DC. (f) This amendment becomes effective on June 11, 1992. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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