AD 82-25-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | BAE Systems (Operations) Limited | HS 748 Series 2A | Airworthiness Directives; BRITISH AEROSPACE Model H.S. 748 Airplanes |
| aircraft | BAE Systems (Operations) Limited | HS 748 Series 2B | Airworthiness Directives; BRITISH AEROSPACE Model H.S. 748 Airplanes |
Unsafe Condition
The presence of two cable assemblies (Parts No. 2V19699 and 3V19699) or resistor assemblies (Part No. 10V15130) may create a heat source which could cause a fire in the cabin wiring.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Remove the specified cable or resistor assemblies in accordance with British Aerospace H.S. 748 Service Bulletin No. 21/106. Alternate means of compliance may be used if approved by the FAA. Special flight permits may be issued under FAR 21.197 and 21.199.
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Compliance Time
within the next 100 hours time in service or 60 days, whichever occurs first, after the effective date of this AD
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Affected Aircraft
BRITISH AEROSPACE Model H.S. 748 airplanes with Modifications 2743 or 5263 incorporated
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Federal Register Abstract
Cabin Wiring
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_82-25-06.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 82-25-06 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRITISH AEROSPACE Model H.S. 748 Airplanes Subject: Cabin Wiring Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 12/06/1982 Make: BAE Systems (Operations) Limited Model: HS 748 Series 2A | HS 748 Series 2B Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 82-25-06 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4503 AD NUMBER: 82-25-06 SUBJECT HEADING: Airworthiness Directives; BRITISH AEROSPACE Model H.S. 748 Airplanes ACTION: SUMMARY: DATES: Effective December 6, 1982. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 82-25-06 BRITISH AEROSPACE (formerly Hawker Siddeley): Amendment 39-4503. Applies to all H.S. 748 airplanes with Modifications 2743 or 5263 incorporated. Compliance is required as indicated unless already accomplished. To eliminate a heat source which may cause a fire in the cabin wiring accomplish the following within the next 100 hours time in service or 60 days, whichever occurs first, after the effective date of this AD: 1. Remove two cable assemblies (including resistors), Parts No. 2V19699 and 3V19699, for aircraft having Modification 6318 incorporated or, on aircraft without Modification 6318 incorporated, remove two resistor assemblies, Part No. 10V15130, in accordance with the Accomplishment Instructions of British Aerospace H.S. 748 Service Bulletin No. 21/106, dated March 23, 1981. 2. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. 3. 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 a part hereof pursuant to 5 U.S.C. 552(a)(1). This amendment becomes effective December 6, 1982. FOOTER:
Document Text
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AD Final Rules - DRS_82-25-06.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 82-25-06 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRITISH AEROSPACE Model H.S. 748 Airplanes Subject: Cabin Wiring Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 12/06/1982 Make: BAE Systems (Operations) Limited Model: HS 748 Series 2A | HS 748 Series 2B 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: 82-25-06 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4503 AD NUMBER: 82-25-06 SUBJECT HEADING: Airworthiness Directives; BRITISH AEROSPACE Model H.S. 748 Airplanes ACTION: SUMMARY: DATES: Effective December 6, 1982. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 82-25-06 BRITISH AEROSPACE (formerly Hawker Siddeley): Amendment 39-4503. Applies to all H.S. 748 airplanes with Modifications 2743 or 5263 incorporated. Compliance is required as indicated unless already accomplished. To eliminate a heat source which may cause a fire in the cabin wiring accomplish the following within the next 100 hours time in service or 60 days, whichever occurs first, after the effective date of this AD: 1. Remove two cable assemblies (including resistors), Parts No. 2V19699 and 3V19699, for aircraft having Modification 6318 incorporated or, on aircraft without Modification 6318 incorporated, remove two resistor assemblies, Part No. 10V15130, in accordance with the Accomplishment Instructions of British Aerospace H.S. 748 Service Bulletin No. 21/106, dated March 23, 1981. 2. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. 3. 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 a part hereof pursuant to 5 U.S.C. 552(a)(1). This amendment becomes effective December 6, 1982. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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