AD 82-18-02

final rule

Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 Series 400 Airplanes

AD Number
82-18-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Airbus SAS BAC 1-11 400 Series Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 Series 400 Airplanes

Unsafe Condition

Overloads and possible failure of the spoiler operating rods caused by corroded turnbarrels

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

Required Actions

Inspect the internal threads of the spoiler operating rod turnbarrels for corrosion and excessive thread truncation, replace the turnbarrel if necessary, and follow British Aerospace Alert Service Bulletin 27-A-PM5732, Issue No. 2.

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

Compliance Time

Within the next 1200 landings or 6 months after the effective date of this AD, whichever occurs first, and thereafter at intervals not exceeding 10,000 landings or 5 years from the last inspection

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

Affected Aircraft

British Aerospace Model BAC 1-11 series 400 airplanes certificated in all categories

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

Federal Register Abstract

Turnbarrels Inspection

Applicability Source Text

Show captured applicability text from the source AD
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Details
AD Number:
82-18-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 Series 400 Airplanes
Subject:
Turnbarrels Inspection
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
09/27/1982
Make:
Airbus SAS
Model:
BAC 1-11 400 Series
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Superseded AD: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Superseded By: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: 82-18-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4443

AD NUMBER:   82-18-02

SUBJECT HEADING:   Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 Series 400 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective September 27, 1982.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   82-18-02 BRITISH AEROSPACE, AIRCRAFT GROUP (formerly British Aircraft Corporation): Amendment 39-4443. Applies to Model BAC 1-11 series 400 airplanes certificated in all categories. Compliance required as indicated unless already accomplished. To prevent overloads and possible failure of the spoiler operating rods caused by corroded turnbarrels, accomplish the following:

1. Within the next 1200 landings or 6 months after the effective date of this AD, whichever occurs first, and thereafter at intervals not exceeding 10,000 landings or 5 years from the last inspection, inspect the internal threads of the spoiler operating rod turnbarrels for corrosion and excessive thread truncation and replace the turnbarrel, if necessary, in accordance with paragraph 2, Accomplishment Instructions, of British Aerospace, Aircraft Group, BAC 1-11 Alert Service Bulletin 27-A-PM5732, Issue No. 2, dated November 13, 1980.

2. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Chief, Seattle Area 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 September 27, 1982.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_82-18-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
82-18-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 Series 400 Airplanes
Subject:
Turnbarrels Inspection
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
09/27/1982
Make:
Airbus SAS
Model:
BAC 1-11 400 Series
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: 82-18-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4443

AD NUMBER:   82-18-02

SUBJECT HEADING:   Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 Series 400 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective September 27, 1982.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   82-18-02 BRITISH AEROSPACE, AIRCRAFT GROUP (formerly British Aircraft Corporation): Amendment 39-4443. Applies to Model BAC 1-11 series 400 airplanes certificated in all categories. Compliance required as indicated unless already accomplished. To prevent overloads and possible failure of the spoiler operating rods caused by corroded turnbarrels, accomplish the following:

1. Within the next 1200 landings or 6 months after the effective date of this AD, whichever occurs first, and thereafter at intervals not exceeding 10,000 landings or 5 years from the last inspection, inspect the internal threads of the spoiler operating rod turnbarrels for corrosion and excessive thread truncation and replace the turnbarrel, if necessary, in accordance with paragraph 2, Accomplishment Instructions, of British Aerospace, Aircraft Group, BAC 1-11 Alert Service Bulletin 27-A-PM5732, Issue No. 2, dated November 13, 1980.

2. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Chief, Seattle Area 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 September 27, 1982.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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