AD 91-18-10
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
Loss of main landing gear braking effectiveness due to insufficient brake wear limits in the maintenance inspection program.
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Required Actions
Incorporate the specified maximum brake wear limits into the FAA-approved maintenance inspection program within 180 days after the effective date. Alternative methods may be used if 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 180 days after the effective date of this AD
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Affected Aircraft
Boeing Model 767 series airplanes equipped with brake part numbers (P/N) 2607092-1, 2607092-2, 2607092-3, 2607092-4, 2608812-4, or 2608812-6.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Brake Wear Limits
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_91-18-10.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 91-18-10 Document Type: AD Final Rules Docket Number: 90-NM-206-AD Subject Heading: Airworthiness Directives; BOEING Model 767 Series Airplanes Subject: Brake Wear Limits Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 11/12/1991 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767-200 Series | 767-300 Series | 767-300F Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 91-18-10 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 90-NM-206-AD AMENDMENT: 39-8013 AD NUMBER: 91-18-10 SUBJECT HEADING: Airworthiness Directives; BOEING Model 767 Series Airplanes ACTION: SUMMARY: DATES: Effective November 12, 1991. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 91-18-10 BOEING: Amendment 39-8013. Docket No. 90-NM-206-AD. Applicability: Model 767 series airplanes equipped with brake part numbers (P/N) identified in paragraph (a) of this AD, certificated in any category. Compliance: Required as indicated, unless previously accomplished. To prevent the loss of main landing gear braking effectiveness, accomplish the following: (a) Within 180 days after the effective date of this AD, incorporate the maximum brake wear limits, shown below, into the FAA-approved maintenance inspection program. Brake Mfr. Brake P/N Boeing P/N Max. Wear Limit Bendix 2607092-1 S160T200-12 2.15 inches Bendix 2607092-2 S160T200-13 2.15 inches Bendix 2607092-3 S160T200-14 2.15 inches Bendix 2607092-4 S160T200-15 2.15 inches Bendix 2608812-4 S160T300-12 2.56 inches Bendix 2608812-6 S160T300-14 2.90 inches (b) 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. NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector, who may concur or comment and then send it to the Manager, Seattle ACO. (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. This amendment (39-8013, AD 91-18-10) becomes effective on November 12, 1991. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_91-18-10.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 91-18-10 Document Type: AD Final Rules Docket Number: 90-NM-206-AD Subject Heading: Airworthiness Directives; BOEING Model 767 Series Airplanes Subject: Brake Wear Limits Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 11/12/1991 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: 91-18-10 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 90-NM-206-AD AMENDMENT: 39-8013 AD NUMBER: 91-18-10 SUBJECT HEADING: Airworthiness Directives; BOEING Model 767 Series Airplanes ACTION: SUMMARY: DATES: Effective November 12, 1991. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 91-18-10 BOEING: Amendment 39-8013. Docket No. 90-NM-206-AD. Applicability: Model 767 series airplanes equipped with brake part numbers (P/N) identified in paragraph (a) of this AD, certificated in any category. Compliance: Required as indicated, unless previously accomplished. To prevent the loss of main landing gear braking effectiveness, accomplish the following: (a) Within 180 days after the effective date of this AD, incorporate the maximum brake wear limits, shown below, into the FAA-approved maintenance inspection program. Brake Mfr. Brake P/N Boeing P/N Max. Wear Limit Bendix 2607092-1 S160T200-12 2.15 inches Bendix 2607092-2 S160T200-13 2.15 inches Bendix 2607092-3 S160T200-14 2.15 inches Bendix 2607092-4 S160T200-15 2.15 inches Bendix 2608812-4 S160T300-12 2.56 inches Bendix 2608812-6 S160T300-14 2.90 inches (b) 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. NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector, who may concur or comment and then send it to the Manager, Seattle ACO. (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. This amendment (39-8013, AD 91-18-10) becomes effective on November 12, 1991. FOOTER:
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Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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