AD 86-07-05

final rule

Airworthiness Directives; BRITISH AEROSPACE Model HS 748 Airplanes

AD Number
86-07-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft BAE Systems (Operations) Limited HS 748 Series 2A Airworthiness Directives; BRITISH AEROSPACE Model HS 748 Airplanes
aircraft BAE Systems (Operations) Limited HS 748 Series 2B Airworthiness Directives; BRITISH AEROSPACE Model HS 748 Airplanes

Unsafe Condition

Cracks in the wing structure at rib 134.366 and adjacent areas.

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

Required Actions

Inspect the wing structure at rib 134.366 and adjacent areas in accordance with BAe Service Bulletin 57/75, Revision 1, dated August 1984. Repair any damage found as specified in the service bulletin.

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

Compliance Time

within the next 750 hours time in service after the effective date of this AD, or upon accumulating the service threshold as specified in paragraph 1.D of BAe Service Bulletin 57/75, Revision 1, dated August 1984, whichever occurs later; and thereafter at the intervals as specified in the service bulletin

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

Affected Aircraft

BAE Systems (Operations) Limited Model HS 748 Series 2A and HS 748 Series 2B airplanes, certificated in any category

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

Federal Register Abstract

Wing Structure

Applicability Source Text

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Details
AD Number:
86-07-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BRITISH AEROSPACE Model HS 748 Airplanes
Subject:
Wing Structure
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
05/08/1986
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Superseded AD: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Superseded By: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: 86-07-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5271

AD NUMBER:   86-07-05

SUBJECT HEADING:   Airworthiness Directives; BRITISH AEROSPACE Model HS 748 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective May 8, 1986.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   86-07-05 BRITISH AEROSPACE AIRCRAFT GROUP (BAe): Amendment 39-5271. Applies to all BAe Model HS 748 airplanes, certificated in any category. Compliance is required within the next 750 hours time in service after the effective date of this AD, or upon accumulating the service threshold as specified in paragraph 1.D of BAe Service Bulletin 57/75, Revision 1, dated August 1984, whichever occurs later; and thereafter at the intervals as specified in the service bulletin. To detect cracks in the wing structure, accomplish the following, unless already accomplished:

A. Inspect the wing structure at rib 134.366 and adjacent areas in accordance with BAe Service Bulletin 57/75, Revision 1, dated August 1984. Repair any damage found in accordance with the requirements specified in the service bulletin.

B. Alternate means of compliance which provide an acceptable level of safety may be used when approved by the Manager, Standardization Branch, ANM-113, 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.

All persons affected by this directive who have not already received the appropriate service document from the manufacturer may obtain copies upon request to British Aerospace, Inc., Librarian, Box 17414, Dulles International Airport, Washington, D.C. 20041. This document may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington.

This amendment becomes effective May 8, 1986.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_86-07-05.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
86-07-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BRITISH AEROSPACE Model HS 748 Airplanes
Subject:
Wing Structure
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
05/08/1986
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: 86-07-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5271

AD NUMBER:   86-07-05

SUBJECT HEADING:   Airworthiness Directives; BRITISH AEROSPACE Model HS 748 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective May 8, 1986.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   86-07-05 BRITISH AEROSPACE AIRCRAFT GROUP (BAe): Amendment 39-5271. Applies to all BAe Model HS 748 airplanes, certificated in any category. Compliance is required within the next 750 hours time in service after the effective date of this AD, or upon accumulating the service threshold as specified in paragraph 1.D of BAe Service Bulletin 57/75, Revision 1, dated August 1984, whichever occurs later; and thereafter at the intervals as specified in the service bulletin. To detect cracks in the wing structure, accomplish the following, unless already accomplished:

A. Inspect the wing structure at rib 134.366 and adjacent areas in accordance with BAe Service Bulletin 57/75, Revision 1, dated August 1984. Repair any damage found in accordance with the requirements specified in the service bulletin.

B. Alternate means of compliance which provide an acceptable level of safety may be used when approved by the Manager, Standardization Branch, ANM-113, 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.

All persons affected by this directive who have not already received the appropriate service document from the manufacturer may obtain copies upon request to British Aerospace, Inc., Librarian, Box 17414, Dulles International Airport, Washington, D.C. 20041. This document may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington.

This amendment becomes effective May 8, 1986.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.