AD 84-04-01
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
Electrical arcing in the cockpit windshield and side window heating electrical wire bundle
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Required Actions
Perform an aircraft wiring inspection and modification within 300 flight hours after the effective date, following Service Bulletin 093-30-055 or approved alternate. Alternate means of compliance may be used with approval.
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Compliance Time
Within 300 flight hours after the effective date of this AD
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Affected Aircraft
Lockheed-California Company Model L-1011-385 series airplanes, certificated in all categories
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Federal Register Abstract
Aircraft Wiring Insp. and Mod.
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_84-04-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 84-04-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: LOCKHEED-CALIFORNIA COMPANY Model L-1011-385 Series Airplanes Subject: Aircraft Wiring Insp. and Mod. Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 02/27/1984 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| L-1011-385-1-14 | L-1011-385-1-15 | L-1011-385-3 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 84-04-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4815 AD NUMBER: 84-04-01 SUBJECT HEADING: LOCKHEED-CALIFORNIA COMPANY Model L-1011-385 Series Airplanes ACTION: SUMMARY: DATES: Effective February 27, 1984. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 84-04-01 LOCKHEED-CALIFORNIA COMPANY: Amendment 39-4815. Applies to Lockheed Model L-1011-385 series airplanes, certificated in all categories. Compliance required as indicated unless previously accomplished. To prevent the possibility of electrical arcing in the cockpit windshield and side window heating electrical wire bundle, accomplish the following: A. Within 300 flight hours after the effective date of this AD, perform the aircraft wiring inspection and modification, if required, in accordance with Part 2, Accomplishment Instructions, in Lockheed-California Company L-1011 Service Bulletin 093-30-055, dated July 1, 1983, or later revision approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. B. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. NOTE: Airplanes previously inspected in accordance with the procedures specified in Lockheed L-1011 Service Bulletin 093-30-055, dated July 1, 1983, or in accordance with alternate inspection procedures since June 6, 1983, approved by an FAA Principal Maintenance Inspector (PMI), are considered to comply with the inspection requirements of this AD. 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 February 27, 1984. FOOTER:
Document Text
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AD Final Rules - DRS_84-04-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 84-04-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: LOCKHEED-CALIFORNIA COMPANY Model L-1011-385 Series Airplanes Subject: Aircraft Wiring Insp. and Mod. Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 02/27/1984 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: 84-04-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4815 AD NUMBER: 84-04-01 SUBJECT HEADING: LOCKHEED-CALIFORNIA COMPANY Model L-1011-385 Series Airplanes ACTION: SUMMARY: DATES: Effective February 27, 1984. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 84-04-01 LOCKHEED-CALIFORNIA COMPANY: Amendment 39-4815. Applies to Lockheed Model L-1011-385 series airplanes, certificated in all categories. Compliance required as indicated unless previously accomplished. To prevent the possibility of electrical arcing in the cockpit windshield and side window heating electrical wire bundle, accomplish the following: A. Within 300 flight hours after the effective date of this AD, perform the aircraft wiring inspection and modification, if required, in accordance with Part 2, Accomplishment Instructions, in Lockheed-California Company L-1011 Service Bulletin 093-30-055, dated July 1, 1983, or later revision approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. B. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. NOTE: Airplanes previously inspected in accordance with the procedures specified in Lockheed L-1011 Service Bulletin 093-30-055, dated July 1, 1983, or in accordance with alternate inspection procedures since June 6, 1983, approved by an FAA Principal Maintenance Inspector (PMI), are considered to comply with the inspection requirements of this AD. 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 February 27, 1984. FOOTER:
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