AD 85-12-09
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | British Aerospace (Commercial Aircraft) Ltd | Argosy AW.650 Series 101 | Airworthiness Directives; BRITISH AEROSPACE ARGOSY Model AW-650 Series 100 and 200 Aircraft |
Unsafe Condition
Cracks in tailboom frame skin doubler plates items 5, 6, 7, and 8 on drawing BBH 2702 could lead to possible loss of the vertical fin.
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Required Actions
Within 350 flying hours after the effective date, visually inspect doubler plates items 5-8 for cracks per British Aerospace SB 55/41. If no cracks, repeat inspection every 700 flying hours. If cracks found, incorporate repair scheme BBH 2733 within 700 flying hours which eliminates repetitive inspections.
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Compliance Time
within 350 flying hours after the effective date of this AD
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Affected Aircraft
British Aerospace (Commercial Aircraft) Ltd Argosy AW.650 Series 101 aircraft serial numbers 6651, 6652, 6653, 6656, 6660, 6801, 6802, 6803, and 6805
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Federal Register Abstract
Tailboom Frame
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_85-12-09.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 85-12-09 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRITISH AEROSPACE ARGOSY Model AW-650 Series 100 and 200 Aircraft Subject: Tailboom Frame Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 07/22/1985 Make: British Aerospace (Commercial Aircraft) Ltd Model: Argosy AW.650 Series 101 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 85-12-09 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5082 AD NUMBER: 85-12-09 SUBJECT HEADING: Airworthiness Directives; BRITISH AEROSPACE ARGOSY Model AW-650 Series 100 and 200 Aircraft ACTION: SUMMARY: DATES: Effective July 22, 1985. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 85-12-09 BRITISH AEROSPACE ARGOSY: Amendment 39-5082. Applies to Argosy Model AW-650 Series 100 and 200 aircraft Serial Numbers 6651, 6652, 6653, 6656, 6660, 6801, 6802, 6803, and 6805, certificated in all categories. To prevent possible loss of the vertical fin, accomplish the following: A. Within 350 flying hours after the effective date of this AD, visually inspect the tail boom frame skin doubler plates, items 5, 6, 7, and 8 on drawing BBH 2702 for cracks in accordance with British Aerospace Service Bulletin 55/41 dated May 1984. B. If no cracks are found, repeat the inspection at intervals not to exceed 700 flying hours. C. If any cracks are found, incorporate repair scheme BBH 2733 within the next 700 flying hours. Incorporation of BBH 2733 eliminates the requirement for the repetitive inspections required by paragraph A., above. D. Alternate means of compliance which provide an acceptable level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. E. 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 modifications required by this AD. All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to British Aerospace, Inc., Box 17414, Dulles International Airport, Washington, D.C. 20041. These documents also may be examined at FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. This amendment becomes effective July 22, 1985. FOOTER:
Document Text
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AD Final Rules - DRS_85-12-09.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 85-12-09 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRITISH AEROSPACE ARGOSY Model AW-650 Series 100 and 200 Aircraft Subject: Tailboom Frame Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 07/22/1985 Make: British Aerospace (Commercial Aircraft) Ltd Model: Argosy AW.650 Series 101 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: 85-12-09 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5082 AD NUMBER: 85-12-09 SUBJECT HEADING: Airworthiness Directives; BRITISH AEROSPACE ARGOSY Model AW-650 Series 100 and 200 Aircraft ACTION: SUMMARY: DATES: Effective July 22, 1985. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 85-12-09 BRITISH AEROSPACE ARGOSY: Amendment 39-5082. Applies to Argosy Model AW-650 Series 100 and 200 aircraft Serial Numbers 6651, 6652, 6653, 6656, 6660, 6801, 6802, 6803, and 6805, certificated in all categories. To prevent possible loss of the vertical fin, accomplish the following: A. Within 350 flying hours after the effective date of this AD, visually inspect the tail boom frame skin doubler plates, items 5, 6, 7, and 8 on drawing BBH 2702 for cracks in accordance with British Aerospace Service Bulletin 55/41 dated May 1984. B. If no cracks are found, repeat the inspection at intervals not to exceed 700 flying hours. C. If any cracks are found, incorporate repair scheme BBH 2733 within the next 700 flying hours. Incorporation of BBH 2733 eliminates the requirement for the repetitive inspections required by paragraph A., above. D. Alternate means of compliance which provide an acceptable level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. E. 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 modifications required by this AD. All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to British Aerospace, Inc., Box 17414, Dulles International Airport, Washington, D.C. 20041. These documents also may be examined at FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. This amendment becomes effective July 22, 1985. FOOTER:
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