AD 87-24-08
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
Shutdown of the power transfer unit and inability to extend the landing gear.
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Required Actions
Modify the hydraulic system in accordance with Boeing Alert Service Bulletin 757-29A0035, Revision 1, dated September 10, 1987, or later FAA-approved revision. Alternate means of compliance or adjustment of compliance time may be used with FAA concurrence.
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Compliance Time
within the next one year after the effective date of this AD, unless previously accomplished
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Affected Aircraft
Boeing Model 757 series airplanes, line position 0002 through 0138, certificated in any category.
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Federal Register Abstract
Hydraulic System
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_87-24-08.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 87-24-08 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BOEING Model 757 Series Airplanes Subject: Hydraulic System Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 12/29/1987 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Series | 757-200PF Series | 757-300 Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 87-24-08 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5775 AD NUMBER: 87-24-08 SUBJECT HEADING: Airworthiness Directives; BOEING Model 757 Series Airplanes ACTION: SUMMARY: DATES: Effective December 29, 1987. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 87-24-08 BOEING: Amendment 39-5775. Applies to Model 757 series airplanes, line position 0002 through 0138, certificated in any category. Compliance required within the next one year after the effective date of this AD, unless previously accomplished. To prevent shutdown of the power transfer unit and inability to extend the landing gear, accomplish the following: A. Modify the hydraulic system in accordance with Boeing Alert Service Bulletin 757-29A0035, Revision 1, dated September 10, 1987, or later FAA-approved revision. B. An alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, and which has the concurrence of an FAA Principal Maintenance Inspector, may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. 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. All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to the Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98124-2207. These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. This amendment becomes effective December 29, 1987. FOOTER:
Document Text
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AD Final Rules - DRS_87-24-08.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 87-24-08 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BOEING Model 757 Series Airplanes Subject: Hydraulic System Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 12/29/1987 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: 87-24-08 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5775 AD NUMBER: 87-24-08 SUBJECT HEADING: Airworthiness Directives; BOEING Model 757 Series Airplanes ACTION: SUMMARY: DATES: Effective December 29, 1987. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 87-24-08 BOEING: Amendment 39-5775. Applies to Model 757 series airplanes, line position 0002 through 0138, certificated in any category. Compliance required within the next one year after the effective date of this AD, unless previously accomplished. To prevent shutdown of the power transfer unit and inability to extend the landing gear, accomplish the following: A. Modify the hydraulic system in accordance with Boeing Alert Service Bulletin 757-29A0035, Revision 1, dated September 10, 1987, or later FAA-approved revision. B. An alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, and which has the concurrence of an FAA Principal Maintenance Inspector, may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. 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. All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to the Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98124-2207. These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. This amendment becomes effective December 29, 1987. FOOTER:
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