AD 82-18-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 747-100 Series | BOEING Model 747 Series Airplanes |
| aircraft | The Boeing Company | 747-100B Series | BOEING Model 747 Series Airplanes |
| aircraft | The Boeing Company | 747-100B SUD Series | BOEING Model 747 Series Airplanes |
| aircraft | The Boeing Company | 747-200B Series | BOEING Model 747 Series Airplanes |
| aircraft | The Boeing Company | 747-200C Series | BOEING Model 747 Series Airplanes |
| aircraft | The Boeing Company | 747-200F Series | BOEING Model 747 Series Airplanes |
| aircraft | The Boeing Company | 747-300 Series | BOEING Model 747 Series Airplanes |
| aircraft | The Boeing Company | 747-400 Series | BOEING Model 747 Series Airplanes |
| aircraft | The Boeing Company | 747-400D Series | BOEING Model 747 Series Airplanes |
| aircraft | The Boeing Company | 747-400F Series | BOEING Model 747 Series Airplanes |
| aircraft | The Boeing Company | 747SP Series | BOEING Model 747 Series Airplanes |
| aircraft | The Boeing Company | 747SR Series | BOEING Model 747 Series Airplanes |
Unsafe Condition
Rudder cable possible hangup on the smoke detection tube.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify the smoke detection tube in accordance with Boeing Service Bulletin No. 747-26-2083, Revision 1, or later FAA approved revisions. Alternate means of compliance may be used if approved by the FAA.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the next 1,500 hours time-in-service after the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Boeing Model 747 series freighter airplanes as listed in Boeing Service Bulletin No. 747-26-2083, Revision 1, or later FAA approved revisions.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Smoke Detection Tube Modification
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_82-18-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 82-18-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: BOEING Model 747 Series Airplanes Subject: Smoke Detection Tube Modification Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 09/30/1982 Make: The Boeing Company Model: 747-100 Series | 747-100B Series | 747-100B SUD Series | 747-200B Series | 747-200C Series | 747-200...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: 82-18-05 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4444 AD NUMBER: 82-18-05 SUBJECT HEADING: BOEING Model 747 Series Airplanes ACTION: SUMMARY: DATES: Effective September 30, 1982. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 82-18-05 BOEING: Amendment 39-4444. Applies to Model 747 series freighter airplanes as listed in Boeing Service Bulletin No. 747-26-2083, Revision 1, or later FAA approved revisions, certificated in all categories. To prevent the rudder cable from possible hangup on the smoke detection tube, accomplish the following: A. Within the next 1,500 hours time-in-service after the effective date of this AD, unless previously accomplished, modify the smoke detection tube in accordance with Boeing Service Bulletin No. 747-26-2083, Revision 1, or later FAA approved revision. B. Alternate means of compliance with the AD which provide an equivalent level of safety may be used when approved by the Manager, Seattle Area 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 for the accomplishment of inspections and/or modifications required by this AD. The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made part hereof pursuant to 5 U.S.C. 552(a)(1). All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98124. These documents may also be examined at FAA Northwest Mountain Region, 9010 East Marginal Way South, Seattle, Washington. This amendment becomes effective September 30, 1982. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_82-18-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 82-18-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: BOEING Model 747 Series Airplanes Subject: Smoke Detection Tube Modification Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 09/30/1982 Make: The Boeing Company Model: 747-100 Series | 747-100B Series | 747-100B SUD Series | 747-200B Series | 747-200C Series | 747-200...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: 82-18-05 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4444 AD NUMBER: 82-18-05 SUBJECT HEADING: BOEING Model 747 Series Airplanes ACTION: SUMMARY: DATES: Effective September 30, 1982. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 82-18-05 BOEING: Amendment 39-4444. Applies to Model 747 series freighter airplanes as listed in Boeing Service Bulletin No. 747-26-2083, Revision 1, or later FAA approved revisions, certificated in all categories. To prevent the rudder cable from possible hangup on the smoke detection tube, accomplish the following: A. Within the next 1,500 hours time-in-service after the effective date of this AD, unless previously accomplished, modify the smoke detection tube in accordance with Boeing Service Bulletin No. 747-26-2083, Revision 1, or later FAA approved revision. B. Alternate means of compliance with the AD which provide an equivalent level of safety may be used when approved by the Manager, Seattle Area 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 for the accomplishment of inspections and/or modifications required by this AD. The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made part hereof pursuant to 5 U.S.C. 552(a)(1). All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98124. These documents may also be examined at FAA Northwest Mountain Region, 9010 East Marginal Way South, Seattle, Washington. This amendment becomes effective September 30, 1982. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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