AD 85-05-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Lockheed Martin Corporation | L-1011-385-1 | LOCKHEED-CALIFORNIA COMPANY Model L-1011-385 Series Airplanes |
| aircraft | Lockheed Martin Corporation | L-1011-385-1-14 | LOCKHEED-CALIFORNIA COMPANY Model L-1011-385 Series Airplanes |
| aircraft | Lockheed Martin Corporation | L-1011-385-1-15 | LOCKHEED-CALIFORNIA COMPANY Model L-1011-385 Series Airplanes |
| aircraft | Lockheed Martin Corporation | L-1011-385-3 | LOCKHEED-CALIFORNIA COMPANY Model L-1011-385 Series Airplanes |
Unsafe Condition
Loss of flight control capability due to loss of three out of four hydraulic systems.
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Required Actions
Modify hydraulic system 'C' by installing a hydraulic fuse and associated hydraulic tubing, replace aluminum return lines with steel lines in accordance with specified service bulletins.
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Compliance Time
Within one year after the effective date of this AD
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Affected Aircraft
Lockheed Model L-1011-385 series airplanes, certificated in all categories.
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Federal Register Abstract
Hydraulic System
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_85-05-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 85-05-04 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: LOCKHEED-CALIFORNIA COMPANY Model L-1011-385 Series Airplanes Subject: Hydraulic System Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 04/01/1985 Make: Lockheed Martin Corporation Model: L-1011-385-1 | L-1011-385-1-14 | L-1011-385-1-15 | L-1011-385-3 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 85-05-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5010 AD NUMBER: 85-05-04 SUBJECT HEADING: LOCKHEED-CALIFORNIA COMPANY Model L-1011-385 Series Airplanes ACTION: SUMMARY: DATES: Effective April 1, 1985. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 85-05-04 LOCKHEED-CALIFORNIA COMPANY: Amendment 39-5010. Applies to Lockheed Model L-1011-385 series airplanes, certificated in all categories. Compliance required as indicated unless previously accomplished. To minimize potential for the loss of flight control capability due to the loss of three out of four hydraulic systems accomplish the following: A. Within one year after the effective date of this AD, modify hydraulic system "C" by installing a hydraulic fuse and associated hydraulic tubing and replace aluminum return lines with steel lines in accordance with Lockheed L-1011 Service Bulletins Number 093-29-065, Revision 4, dated August 9, 1983, and 093-29-085, dated December 8, 1983, or later revisions approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. B. Alternate means of compliance which provide an acceptable level of safety may be used when approved by the Manager, Los Angeles 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 these documents from the manufacturer may obtain copies upon request to Lockheed-California Company, P.O. Box 551, Burbank, California 91520, Attention: Commercial Support Contracts, Dept. 63-11, U-33, B-1. These documents also may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington or the Los Angeles Aircraft Certification Office, 4344 Donald Douglas Drive, Long Beach, California. This amendment becomes effective April 1, 1985. FOOTER:
Document Text
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AD Final Rules - DRS_85-05-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 85-05-04 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: LOCKHEED-CALIFORNIA COMPANY Model L-1011-385 Series Airplanes Subject: Hydraulic System Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 04/01/1985 Make: Lockheed Martin Corporation Model: L-1011-385-1 | L-1011-385-1-14 | L-1011-385-1-15 | L-1011-385-3 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: 85-05-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5010 AD NUMBER: 85-05-04 SUBJECT HEADING: LOCKHEED-CALIFORNIA COMPANY Model L-1011-385 Series Airplanes ACTION: SUMMARY: DATES: Effective April 1, 1985. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 85-05-04 LOCKHEED-CALIFORNIA COMPANY: Amendment 39-5010. Applies to Lockheed Model L-1011-385 series airplanes, certificated in all categories. Compliance required as indicated unless previously accomplished. To minimize potential for the loss of flight control capability due to the loss of three out of four hydraulic systems accomplish the following: A. Within one year after the effective date of this AD, modify hydraulic system "C" by installing a hydraulic fuse and associated hydraulic tubing and replace aluminum return lines with steel lines in accordance with Lockheed L-1011 Service Bulletins Number 093-29-065, Revision 4, dated August 9, 1983, and 093-29-085, dated December 8, 1983, or later revisions approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. B. Alternate means of compliance which provide an acceptable level of safety may be used when approved by the Manager, Los Angeles 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 these documents from the manufacturer may obtain copies upon request to Lockheed-California Company, P.O. Box 551, Burbank, California 91520, Attention: Commercial Support Contracts, Dept. 63-11, U-33, B-1. These documents also may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington or the Los Angeles Aircraft Certification Office, 4344 Donald Douglas Drive, Long Beach, California. This amendment becomes effective April 1, 1985. FOOTER:
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