AD 92-10-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 707-100 Long Body | Airworthiness Directives; BOEING Model 707 and 720 Series Airplanes |
| aircraft | The Boeing Company | 707-100B Long Body | Airworthiness Directives; BOEING Model 707 and 720 Series Airplanes |
| aircraft | The Boeing Company | 707-100B Short Body | Airworthiness Directives; BOEING Model 707 and 720 Series Airplanes |
| aircraft | The Boeing Company | 707-200 | Airworthiness Directives; BOEING Model 707 and 720 Series Airplanes |
| aircraft | The Boeing Company | 707-300 Series | Airworthiness Directives; BOEING Model 707 and 720 Series Airplanes |
| aircraft | The Boeing Company | 707-300B Series | Airworthiness Directives; BOEING Model 707 and 720 Series Airplanes |
| aircraft | The Boeing Company | 707-300C Series | Airworthiness Directives; BOEING Model 707 and 720 Series Airplanes |
| aircraft | The Boeing Company | 707-400 Series | Airworthiness Directives; BOEING Model 707 and 720 Series Airplanes |
| aircraft | The Boeing Company | 720 Series | Airworthiness Directives; BOEING Model 707 and 720 Series Airplanes |
| aircraft | The Boeing Company | 720B Series | Airworthiness Directives; BOEING Model 707 and 720 Series Airplanes |
Unsafe Condition
Loss of main landing gear braking effectiveness due to main landing gear brakes exceeding maximum wear limits.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect main landing gear brakes with specified part numbers for wear; replace any brake worn beyond the listed maximum wear limits (e.g., 0.60 inch for Bendix P/N 150550) before further flight. Incorporate the maximum wear limits into the FAA-approved maintenance inspection program.
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 (July 2, 1992)
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Affected Aircraft
Boeing Model 707 and 720 series airplanes equipped with brake part numbers listed in paragraph (a) of the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Main Landing Gear Brakes
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_92-10-10.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 92-10-10 Document Type: AD Final Rules Docket Number: 91-NM-216-AD Subject Heading: Airworthiness Directives; BOEING Model 707 and 720 Series Airplanes Subject: Main Landing Gear Brakes Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 07/02/1992 Make: The Boeing Company Model: 707-100 Long Body | 707-100B Long Body | 707-100B Short Body | 707-200 | 707-300 Series | 707-300B S...Show more 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: 92-10-10 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 91-NM-216-AD AMENDMENT: 39-8244 AD NUMBER: 92-10-10 SUBJECT HEADING: Airworthiness Directives; BOEING Model 707 and 720 Series Airplanes ACTION: SUMMARY: DATES: Effective July 2, 1992 ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 92-10-10 BOEING: Amendment 39-8244. Docket No. 91-NM-216-AD. Applicability: Model 707 and 720 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, accomplish paragraphs (a)(1) and (a)(2) of this AD: (1) Inspect the main landing gear brakes, having brake part numbers shown below, for wear. Any brake worn more than the maximum wear limit specified below must be replaced, prior to further flight, with a brake within that limit. Brake Mfr. Brake P/N Boeing P/N Maximum Wear Limit Bendix 150550 10-3072-1,-11 0.60 inch Bendix 2601775 None 0.70 inch BFGoodrich 2-756-2 10-60228-1 0.51 inch BFGoodrich 2-784-1 10-3379-11 0.35 inch BFGoodrich 2-991 10-60228-8 0.51 inch ABS 9560569 10-60818-1 0.528 inch (2) Incorporate the maximum brake wear limits specified in paragraph (a)(1) of this AD into the FAA-approved maintenance inspection program. (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. 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. (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. (d) This amendment becomes effective on July 2, 1992. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_92-10-10.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 92-10-10 Document Type: AD Final Rules Docket Number: 91-NM-216-AD Subject Heading: Airworthiness Directives; BOEING Model 707 and 720 Series Airplanes Subject: Main Landing Gear Brakes Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 07/02/1992 Make: The Boeing Company Model: 707-100 Long Body | 707-100B Long Body | 707-100B Short Body | 707-200 | 707-300 Series | 707-300B S...Show more 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: 92-10-10 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 91-NM-216-AD AMENDMENT: 39-8244 AD NUMBER: 92-10-10 SUBJECT HEADING: Airworthiness Directives; BOEING Model 707 and 720 Series Airplanes ACTION: SUMMARY: DATES: Effective July 2, 1992 ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 92-10-10 BOEING: Amendment 39-8244. Docket No. 91-NM-216-AD. Applicability: Model 707 and 720 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, accomplish paragraphs (a)(1) and (a)(2) of this AD: (1) Inspect the main landing gear brakes, having brake part numbers shown below, for wear. Any brake worn more than the maximum wear limit specified below must be replaced, prior to further flight, with a brake within that limit. Brake Mfr. Brake P/N Boeing P/N Maximum Wear Limit Bendix 150550 10-3072-1,-11 0.60 inch Bendix 2601775 None 0.70 inch BFGoodrich 2-756-2 10-60228-1 0.51 inch BFGoodrich 2-784-1 10-3379-11 0.35 inch BFGoodrich 2-991 10-60228-8 0.51 inch ABS 9560569 10-60818-1 0.528 inch (2) Incorporate the maximum brake wear limits specified in paragraph (a)(1) of this AD into the FAA-approved maintenance inspection program. (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. 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. (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. (d) This amendment becomes effective on July 2, 1992. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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