AD 91-03-11

final rule

Airworthiness Directives; British Aerospace Model BAe 146 100A and 200A Series Airplanes.

AD Number
91-03-11
Status
final_rule
Effective Date
Product Category
aircraft
Docket
90-NM-193-AD
FR Citation
This information is not available.
Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

Applicability

TypeManufacturerModelDetails
aircraft BAE Systems (Operations) Limited BAe 146-100A Airworthiness Directives; British Aerospace Model BAe 146 100A and 200A Series Airplanes.
aircraft BAE Systems (Operations) Limited BAe 146-200A Airworthiness Directives; British Aerospace Model BAe 146 100A and 200A Series Airplanes.

Unsafe Condition

Oscillations (flutter) of the elevators

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

Required Actions

Install additional mass balance weights to the elevators forward of the hinge line in accordance with British Aerospace Service Bulletin 55-7-00955D, Revision 2. An alternate means of compliance or adjustment of the compliance time may be used if approved by the FAA. Special flight permits may be issued under FAR 21.197 and 21.199 to operate airplanes to a base for compliance.

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

Compliance Time

Within 180 days 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 Model BAe 146 100A and 200A series airplanes listed in British Aerospace Service Bulletin 55-7-00955D, Revision 2

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

Federal Register Abstract

Elevators

Applicability Source Text

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AD Number:
91-03-11
Document Type:
AD Final Rules
Docket Number:
90-NM-193-AD
Subject Heading:
Airworthiness Directives; British Aerospace Model BAe 146 100A and 200A Series Airplanes.
Subject:
Elevators
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/04/1991
Make:
BAE Systems (Operations) Limited
Model:
BAe 146-100A | BAe 146-200A
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Superseded AD: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Superseded By: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: 91-03-11
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   90-NM-193-AD

AMENDMENT:   39-6873

AD NUMBER:   91-03-11

SUBJECT HEADING:   Airworthiness Directives; British Aerospace Model BAe 146 100A and 200A Series Airplanes.

ACTION:  

SUMMARY:  

DATES:   Effective on March 4, 1991.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
91-03-11 BRITISH AEROSPACE: Amendment 39-6873. Docket No. 90-NM-193-AD.
Applicability: Model BAe 146 100A and 200A series airplanes, as listed in British Aerospace Service Bulletin 55-7-00955D, Revision 2, dated January 22, 1990, certificated in any category.

Compliance: Required as indicated, unless previously accomplished.

To prevent oscillations (flutter) of the elevators, accomplish the following:

A. Within 180 days after the effective date of this AD, install additional mass balance weights to the elevators forward of the hinge line, in accordance with British Aerospace Service Bulletin 55-7-00955D, Revision 2, dated January 22, 1990.

B. An alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Standardization Branch, ANM-113, FAA, Transport Airplane Directorate.

NOTE: The request should be submitted directly to the Manager, Standardization Branch, ANM-113, and a copy sent to the cognizant FAA Principal Inspector (PI). The PI will then forward comments or concurrence to the Manager, Standardization Branch, ANM-113.

C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD.

All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to British Aerospace, PLC, Librarian for Service Bulletins, P.O. Box 17414, Dulles International Airport, Washington, D.C. 20041-0414. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 1601 Lind Avenue S.W., Renton, Washington.

This amendment (39-6873, AD 91-03-11) becomes effective on March 4, 1991.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_91-03-11.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
91-03-11
Document Type:
AD Final Rules
Docket Number:
90-NM-193-AD
Subject Heading:
Airworthiness Directives; British Aerospace Model BAe 146 100A and 200A Series Airplanes.
Subject:
Elevators
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/04/1991
Make:
BAE Systems (Operations) Limited
Model:
BAe 146-100A | BAe 146-200A
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: 91-03-11
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   90-NM-193-AD

AMENDMENT:   39-6873

AD NUMBER:   91-03-11

SUBJECT HEADING:   Airworthiness Directives; British Aerospace Model BAe 146 100A and 200A Series Airplanes.

ACTION:  

SUMMARY:  

DATES:   Effective on March 4, 1991.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
91-03-11 BRITISH AEROSPACE: Amendment 39-6873. Docket No. 90-NM-193-AD.
Applicability: Model BAe 146 100A and 200A series airplanes, as listed in British Aerospace Service Bulletin 55-7-00955D, Revision 2, dated January 22, 1990, certificated in any category.

Compliance: Required as indicated, unless previously accomplished.

To prevent oscillations (flutter) of the elevators, accomplish the following:

A. Within 180 days after the effective date of this AD, install additional mass balance weights to the elevators forward of the hinge line, in accordance with British Aerospace Service Bulletin 55-7-00955D, Revision 2, dated January 22, 1990.

B. An alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Standardization Branch, ANM-113, FAA, Transport Airplane Directorate.

NOTE: The request should be submitted directly to the Manager, Standardization Branch, ANM-113, and a copy sent to the cognizant FAA Principal Inspector (PI). The PI will then forward comments or concurrence to the Manager, Standardization Branch, ANM-113.

C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD.

All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to British Aerospace, PLC, Librarian for Service Bulletins, P.O. Box 17414, Dulles International Airport, Washington, D.C. 20041-0414. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 1601 Lind Avenue S.W., Renton, Washington.

This amendment (39-6873, AD 91-03-11) becomes effective on March 4, 1991.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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