AD 89-13-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 757-200 Series | Airworthiness Directives; BOEING Model 757 Series Airplanes |
| aircraft | The Boeing Company | 757-200CB Series | Airworthiness Directives; BOEING Model 757 Series Airplanes |
| aircraft | The Boeing Company | 757-200PF Series | Airworthiness Directives; BOEING Model 757 Series Airplanes |
| aircraft | The Boeing Company | 757-300 Series | Airworthiness Directives; BOEING Model 757 Series Airplanes |
Unsafe Condition
Partial loss of braking and potentially complete loss of braking due to aluminum brake metering valve actuation shafts.
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Required Actions
Replace aluminum brake metering valve actuation shafts with steel shafts in accordance with Boeing Service Bulletin 757-32-0083. An alternate means of compliance or adjustment of compliance time may be used if approved by the Manager, Seattle Aircraft Certification Office.
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Compliance Time
Within the next 750 landings after the effective date of this AD or prior to the accumulation of 10,000 landings, whichever occurs later, unless previously accomplished.
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Affected Aircraft
BOEING Model 757 series airplanes listed in Boeing Service Bulletin 757-32-0083, dated December 15, 1988, certificated in any category.
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Federal Register Abstract
Brake Shafts
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_89-13-08.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 89-13-08 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BOEING Model 757 Series Airplanes Subject: Brake Shafts Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 07/24/1989 Make: The Boeing Company Model: 757-200 Series | 757-200CB Series | 757-200PF Series | 757-300 Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 89-13-08 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-6241 AD NUMBER: 89-13-08 SUBJECT HEADING: Airworthiness Directives; BOEING Model 757 Series Airplanes ACTION: SUMMARY: DATES: Effective July 24, 1989. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 89-13-08 BOEING: Amendment 39-6241. Applicability: Model 757 series airplanes, listed in Boeing Service Bulletin 757-32- 0083, dated December 15, 1988, certificated in any category. Compliance: Required within the next 750 landings after the effective date of this AD or prior to the accumulation of 10,000 landings, whichever occurs later, unless previously accomplished. To prevent the partial loss of braking and, potentially, the complete loss of braking, accomplish the following: A. Replace aluminum brake metering valve actuation shafts with steel shafts, in accordance with Boeing Service Bulletin 757-32-0083, dated December 15, 1988. B. An alternate means 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, FAA, Northwest Mountain Region. NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who will either concur or comment and then send it to the Manager, Seattle Aircraft Certification Office. C. 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 the inspections and/or modifications required by this AD. All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. This amendment (39-6241, AD 89-13-08) becomes effective on July 24, 1989. FOOTER:
Document Text
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AD Final Rules - DRS_89-13-08.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 89-13-08 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BOEING Model 757 Series Airplanes Subject: Brake Shafts Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 07/24/1989 Make: The Boeing Company Model: 757-200 Series | 757-200CB Series | 757-200PF Series | 757-300 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: 89-13-08 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-6241 AD NUMBER: 89-13-08 SUBJECT HEADING: Airworthiness Directives; BOEING Model 757 Series Airplanes ACTION: SUMMARY: DATES: Effective July 24, 1989. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 89-13-08 BOEING: Amendment 39-6241. Applicability: Model 757 series airplanes, listed in Boeing Service Bulletin 757-32- 0083, dated December 15, 1988, certificated in any category. Compliance: Required within the next 750 landings after the effective date of this AD or prior to the accumulation of 10,000 landings, whichever occurs later, unless previously accomplished. To prevent the partial loss of braking and, potentially, the complete loss of braking, accomplish the following: A. Replace aluminum brake metering valve actuation shafts with steel shafts, in accordance with Boeing Service Bulletin 757-32-0083, dated December 15, 1988. B. An alternate means 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, FAA, Northwest Mountain Region. NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who will either concur or comment and then send it to the Manager, Seattle Aircraft Certification Office. C. 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 the inspections and/or modifications required by this AD. All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. This amendment (39-6241, AD 89-13-08) becomes effective on July 24, 1989. FOOTER:
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