AD 90-09-04

final rule

Airworthiness Directives; MCDONNELL DOUGLAS DC-9-81, -82, -83, and -87 Series and Model MD-88 Airplanes

AD Number
90-09-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
89-NM-240-AD
FR Citation
This information is not available.
Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company DC-9-81 (MD-81) Airworthiness Directives; MCDONNELL DOUGLAS DC-9-81, -82, -83, and -87 Series and Model MD-88 Airplanes
aircraft The Boeing Company DC-9-82 (MD-82) Airworthiness Directives; MCDONNELL DOUGLAS DC-9-81, -82, -83, and -87 Series and Model MD-88 Airplanes
aircraft The Boeing Company DC-9-83 (MD-83) Airworthiness Directives; MCDONNELL DOUGLAS DC-9-81, -82, -83, and -87 Series and Model MD-88 Airplanes
aircraft The Boeing Company DC-9-87 (MD-87) Airworthiness Directives; MCDONNELL DOUGLAS DC-9-81, -82, -83, and -87 Series and Model MD-88 Airplanes
aircraft The Boeing Company MD-88 Airworthiness Directives; MCDONNELL DOUGLAS DC-9-81, -82, -83, and -87 Series and Model MD-88 Airplanes

Unsafe Condition

Potential fire ignition source due to arcing, burning, or chafing of electrical wiring in the overhead stowage compartment rail assemblies near electrical bonding straps.

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

Required Actions

Visually inspect left and right overhead stowage compartment rail assemblies for damage to electrical wiring, repair damaged wires as specified, and modify the electrical bonding strap installation per MD-80 Alert Service Bulletin A25-309. Alternate compliance may be approved by the FAA Manager.

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

Compliance Time

within 18 months after the effective date of this airworthiness directive (May 29, 1990), unless previously accomplished

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

Affected Aircraft

McDonnell Douglas Model DC-9-81, -82, -83, -87 series and MD-88 airplanes, Fuselage Numbers 1071 through 1644

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

Federal Register Abstract

Overhead Stowage Assemblies

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_90-09-04.html
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AD Number:
90-09-04
Document Type:
AD Final Rules
Docket Number:
89-NM-240-AD
Subject Heading:
Airworthiness Directives; MCDONNELL DOUGLAS DC-9-81, -82, -83, and -87 Series and Model MD-88 Airplanes
Subject:
Overhead Stowage Assemblies
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
05/29/1990
Make:
The Boeing Company
Model:
DC-9-81 (MD-81) | DC-9-82 (MD-82) | DC-9-83 (MD-83) | DC-9-87 (MD-87) | MD-88
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: 90-09-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   89-NM-240-AD

AMENDMENT:   39-6584

AD NUMBER:   90-09-04

SUBJECT HEADING:   Airworthiness Directives; MCDONNELL DOUGLAS DC-9-81, -82, -83, and -87 Series and Model MD-88 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective May 29, 1990.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
90-09-04 MCDONNELL DOUGLAS: Amendment 39-6584. Docket No. 89-NM-240-AD.

Applicability: McDonnell Douglas Model DC-9-81, -82, -83, and -87 series airplanes and Model MD-88 airplanes, Fuselage Numbers 1071 through 1644, certificated in any category.

Compliance: Required within 18 months after the effective date of this airworthiness directive (AD), unless previously accomplished.

To eliminate a potential fire ignition source in the main cabin above the overhead stowage compartment area, accomplish the following:

A. Visually inspect the left and right overhead stowage compartment rail assemblies in the vicinity of each electrical bonding strap for evidence of arcing, burning, or chafing to electrical wiring. If damage is found, prior to further flight, repair the electrical wires in accordance with McDonnell Douglas MD-80 Maintenance Manual, Chapters 20-50-01 and 20-50-02.

B. Modify the electrical bonding strap installation of the left and right overhead stowage compartment rail assemblies in accordance with the Accomplishment Instructions of McDonnell Douglas MD-80 Alert Service Bulletin A25-309, dated October 30, 1989.

C. 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, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region.

NOTE: The request should be forwarded through an FAA Principal Avionics Inspector (PAI), who will either concur or comment and then send it to the Manager, Los Angeles Aircraft Certification Office.

D. 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 McDonnell Douglas Corporation, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Business Unit Manager, Technical Publications, C1-HCW (54-60). These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or at the Los Angeles Aircraft Certification Office, 3229 East Spring Street, Long Beach, California.

This amendment (39-6584, AD 90-09-04) becomes effective on May 29, 1990.


FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_90-09-04.html
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Document Versions
 Feedback
Details
AD Number:
90-09-04
Document Type:
AD Final Rules
Docket Number:
89-NM-240-AD
Subject Heading:
Airworthiness Directives; MCDONNELL DOUGLAS DC-9-81, -82, -83, and -87 Series and Model MD-88 Airplanes
Subject:
Overhead Stowage Assemblies
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
05/29/1990
Make:
The Boeing Company
Model:
DC-9-81 (MD-81) | DC-9-82 (MD-82) | DC-9-83 (MD-83) | DC-9-87 (MD-87) | MD-88
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: 90-09-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   89-NM-240-AD

AMENDMENT:   39-6584

AD NUMBER:   90-09-04

SUBJECT HEADING:   Airworthiness Directives; MCDONNELL DOUGLAS DC-9-81, -82, -83, and -87 Series and Model MD-88 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective May 29, 1990.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
90-09-04 MCDONNELL DOUGLAS: Amendment 39-6584. Docket No. 89-NM-240-AD.

Applicability: McDonnell Douglas Model DC-9-81, -82, -83, and -87 series airplanes and Model MD-88 airplanes, Fuselage Numbers 1071 through 1644, certificated in any category.

Compliance: Required within 18 months after the effective date of this airworthiness directive (AD), unless previously accomplished.

To eliminate a potential fire ignition source in the main cabin above the overhead stowage compartment area, accomplish the following:

A. Visually inspect the left and right overhead stowage compartment rail assemblies in the vicinity of each electrical bonding strap for evidence of arcing, burning, or chafing to electrical wiring. If damage is found, prior to further flight, repair the electrical wires in accordance with McDonnell Douglas MD-80 Maintenance Manual, Chapters 20-50-01 and 20-50-02.

B. Modify the electrical bonding strap installation of the left and right overhead stowage compartment rail assemblies in accordance with the Accomplishment Instructions of McDonnell Douglas MD-80 Alert Service Bulletin A25-309, dated October 30, 1989.

C. 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, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region.

NOTE: The request should be forwarded through an FAA Principal Avionics Inspector (PAI), who will either concur or comment and then send it to the Manager, Los Angeles Aircraft Certification Office.

D. 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 McDonnell Douglas Corporation, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Business Unit Manager, Technical Publications, C1-HCW (54-60). These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or at the Los Angeles Aircraft Certification Office, 3229 East Spring Street, Long Beach, California.

This amendment (39-6584, AD 90-09-04) becomes effective on May 29, 1990.


FOOTER:

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Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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