AD 91-14-10

final rule

Airworthiness Directives; British Aerospace Model BAe 146-300A Series Airplanes

AD Number
91-14-10
Status
final_rule
Effective Date
Product Category
aircraft
Docket
91-NM-36-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft BAE Systems (Operations) Limited BAe 146-300A Airworthiness Directives; British Aerospace Model BAe 146-300A Series Airplanes

Unsafe Condition

The stall identification (stick push) could occur at a higher angle of attack than the design specification, adversely affecting controllability.

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

Required Actions

Install two signal summing units, Part Number C81606-6, in accordance with British Aerospace Service Bulletin 27-114-01028B. An alternative method of compliance or adjustment of the compliance time may be used if approved by the Manager, Standardization Branch, ANM-113.

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, unless previously accomplished

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

Affected Aircraft

British Aerospace Model BAe 146-300A series airplanes with serial numbers E3118 through E3161, E3163, E3165, and E3169, certificated in any category.

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

Federal Register Abstract

Signal Summing Units

Applicability Source Text

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AD Number:
91-14-10
Document Type:
AD Final Rules
Docket Number:
91-NM-36-AD
Subject Heading:
Airworthiness Directives; British Aerospace Model BAe 146-300A Series Airplanes
Subject:
Signal Summing Units
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/06/1991
Make:
BAE Systems (Operations) Limited
Model:
BAe 146-300A
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Superseded AD: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Superseded By: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: 91-14-10
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   91-NM-36-AD

AMENDMENT:   39-7051

AD NUMBER:   91-14-10

SUBJECT HEADING:   Airworthiness Directives; British Aerospace Model BAe 146-300A Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective on August 6, 1991.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
91-14-10 BRITISH AEROSPACE: Amendment 39-7051. Docket No. 91-NM-36-AD.
Applicability: Model BAe 146-300A series airplanes; Serial numbers E3118 through E3161, E3163, E3165, and E3169; certificated in any category.

Compliance: Required within 180 days after the effective date of this AD, unless previously accomplished.

To prevent the stall identification (stick push) from occurring at a higher angle of attack than the angle called for in the design specification which could adversely affect the controllability of the airplane, accomplish the following:

A. Install two signal summing units, Part Number C81606-6, in accordance with British Aerospace Service Bulletin 27-114-01028B, dated September 26, 1990.

B. An alternative method 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 forwarded through an FAA Principal Maintenance Inspector, who may concur or comment and then send it 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.

D. The installation requirements shall be done in accordance with British Aerospace Service Bulletin 27-114-01028B, dated September 26, 1990. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies may be obtained from British Aerospace, PLC, Librarian for Service Bulletins, P.O. Box 17414, Dulles International Airport, Washington, D.C. 20041. Copies may be inspected at the FAA, Transport Airplane Directorate, Renton, Washington; or at the Office of the Federal Register, 1100 L Street N.W., Room 8401, Washington, D.C.

This amendment (39-7051, AD 91-14-10) becomes effective on August 6, 1991.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_91-14-10.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
91-14-10
Document Type:
AD Final Rules
Docket Number:
91-NM-36-AD
Subject Heading:
Airworthiness Directives; British Aerospace Model BAe 146-300A Series Airplanes
Subject:
Signal Summing Units
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/06/1991
Make:
BAE Systems (Operations) Limited
Model:
BAe 146-300A
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: 91-14-10
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   91-NM-36-AD

AMENDMENT:   39-7051

AD NUMBER:   91-14-10

SUBJECT HEADING:   Airworthiness Directives; British Aerospace Model BAe 146-300A Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective on August 6, 1991.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
91-14-10 BRITISH AEROSPACE: Amendment 39-7051. Docket No. 91-NM-36-AD.
Applicability: Model BAe 146-300A series airplanes; Serial numbers E3118 through E3161, E3163, E3165, and E3169; certificated in any category.

Compliance: Required within 180 days after the effective date of this AD, unless previously accomplished.

To prevent the stall identification (stick push) from occurring at a higher angle of attack than the angle called for in the design specification which could adversely affect the controllability of the airplane, accomplish the following:

A. Install two signal summing units, Part Number C81606-6, in accordance with British Aerospace Service Bulletin 27-114-01028B, dated September 26, 1990.

B. An alternative method 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 forwarded through an FAA Principal Maintenance Inspector, who may concur or comment and then send it 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.

D. The installation requirements shall be done in accordance with British Aerospace Service Bulletin 27-114-01028B, dated September 26, 1990. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies may be obtained from British Aerospace, PLC, Librarian for Service Bulletins, P.O. Box 17414, Dulles International Airport, Washington, D.C. 20041. Copies may be inspected at the FAA, Transport Airplane Directorate, Renton, Washington; or at the Office of the Federal Register, 1100 L Street N.W., Room 8401, Washington, D.C.

This amendment (39-7051, AD 91-14-10) becomes effective on August 6, 1991.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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