AD 90-07-07

final rule

Airworthiness Directives; British Aerospace Model BAe-146 Series Airplanes

AD Number
90-07-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
89-NM-257-AD
FR Citation
This information is not available.
Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

Applicability

TypeManufacturerModelDetails
aircraft BAE Systems (Operations) Limited BAe 146-100A Airworthiness Directives; British Aerospace Model BAe-146 Series Airplanes
aircraft BAE Systems (Operations) Limited BAe 146-200A Airworthiness Directives; British Aerospace Model BAe-146 Series Airplanes
aircraft BAE Systems (Operations) Limited BAe 146-300A Airworthiness Directives; British Aerospace Model BAe-146 Series Airplanes

Unsafe Condition

Brake drag or complete loss of braking due to loose quick-disconnect couplings in the yellow and auxiliary systems hydraulic lines to the wheel brake units on the left and right main landing gear.

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

Required Actions

Inspect the quick-disconnect couplings in the yellow and auxiliary systems hydraulic lines to the wheel brake units on the left and right main landing gear for tightness, retighten to finger-tight torque, and secure with a corrosion-resistant steel lockwire per British Aerospace Service Bulletin 32-A101. Alternate compliance or time adjustment may be approved by the Manager, Standardization Branch, ANM-113, FAA, Northwest Mountain Region.

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

Compliance Time

within 30 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 series airplanes with Modification HCM50075A, B, and C incorporated

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

Federal Register Abstract

Wheel Brake Units

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_90-07-07.html
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AD Number:
90-07-07
Document Type:
AD Final Rules
Docket Number:
89-NM-257-AD
Subject Heading:
Airworthiness Directives; British Aerospace Model BAe-146 Series Airplanes
Subject:
Wheel Brake Units
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/30/1990
Make:
BAE Systems (Operations) Limited
Model:
BAe 146-100A | BAe 146-200A | 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: 90-07-07
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   89-NM-257-AD

AMENDMENT:   39-6553

AD NUMBER:   90-07-07

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

ACTION:  

SUMMARY:  

DATES:   Effective on April 30, 1990.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
90-07-07 BRITISH AEROSPACE, PLC: Amendment 39-6553. Docket No. 89-NM-257-AD.
Applicability: Model BAe-146 series airplanes, on which Modification HCM50075A, B, and C have been incorporated, certificated in any category.

Compliance: Required within 30 days after the effective date of this AD, unless previously accomplished.

To prevent brake drag or complete loss of braking, accomplish the following:

A. Inspect the quick-disconnect couplings in the yellow and auxiliary systems hydraulic lines to the wheel brake units on the left and right main landing gear for tightness, retighten to finger-tight torque, and secure the quick-disconnect couplings with a corrosion-resistant steel lockwire, in accordance with British Aerospace Service Bulletin 32-A101, dated September 1, 1989.

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, Northwest Mountain Region.

NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who will either 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.

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. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or the Standardization Branch, 9010 East Marginal Way South, Seattle, Washington.

This amendment (39-6553, AD 90-07-07) becomes effective on April 30, 1990.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_90-07-07.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
90-07-07
Document Type:
AD Final Rules
Docket Number:
89-NM-257-AD
Subject Heading:
Airworthiness Directives; British Aerospace Model BAe-146 Series Airplanes
Subject:
Wheel Brake Units
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/30/1990
Make:
BAE Systems (Operations) Limited
Model:
BAe 146-100A | BAe 146-200A | 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: 90-07-07
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   89-NM-257-AD

AMENDMENT:   39-6553

AD NUMBER:   90-07-07

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

ACTION:  

SUMMARY:  

DATES:   Effective on April 30, 1990.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
90-07-07 BRITISH AEROSPACE, PLC: Amendment 39-6553. Docket No. 89-NM-257-AD.
Applicability: Model BAe-146 series airplanes, on which Modification HCM50075A, B, and C have been incorporated, certificated in any category.

Compliance: Required within 30 days after the effective date of this AD, unless previously accomplished.

To prevent brake drag or complete loss of braking, accomplish the following:

A. Inspect the quick-disconnect couplings in the yellow and auxiliary systems hydraulic lines to the wheel brake units on the left and right main landing gear for tightness, retighten to finger-tight torque, and secure the quick-disconnect couplings with a corrosion-resistant steel lockwire, in accordance with British Aerospace Service Bulletin 32-A101, dated September 1, 1989.

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, Northwest Mountain Region.

NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who will either 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.

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. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or the Standardization Branch, 9010 East Marginal Way South, Seattle, Washington.

This amendment (39-6553, AD 90-07-07) becomes effective on April 30, 1990.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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