AD 85-12-09

final rule

Airworthiness Directives; BRITISH AEROSPACE ARGOSY Model AW-650 Series 100 and 200 Aircraft

AD Number
85-12-09
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
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.

AI-generated summary from the source AD text. Verify against the official source before acting.

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.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

within 350 flying hours after the effective date of this AD

AI-generated summary from the source AD text. Verify against the official source before acting.

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

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

Tailboom Frame

Applicability Source Text

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AD Final Rules - DRS_85-12-09.html
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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Superseded AD: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Superseded By: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

Show stored source text (verify against official source)
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:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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