AD 89-10-10

final rule

Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes

AD Number
89-10-10
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company DC-9-11 Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-12 Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-13 Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-14 Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-15 Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-15F Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-21 Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-31 Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-32 Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-32 (VC-9C) Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-32F Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-32F (C-9A) Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-32F (C-9B) Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-33F Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-34 Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-34F Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-41 Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-51 Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-81 (MD-81) Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-82 (MD-82) Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-83 (MD-83) Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes
aircraft The Boeing Company DC-9-87 (MD-87) Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes
aircraft The Boeing Company MD-88 Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes

Unsafe Condition

Failure of the evacuation slide girt bar forward stowage clip could result in an unusable emergency exit.

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

Required Actions

Replace the evacuation slide girt bar forward stowage clip within 6 months after the effective date of this AD in accordance with McDonnell Douglas Alert Service Bulletin A25-299, Revision 1. An alternate means of compliance or adjustment of compliance time may be approved by the Manager, Los Angeles Aircraft Certification Office.

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

Compliance Time

Within 6 months after the effective date of this AD

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

Affected Aircraft

McDonnell Douglas Model DC-9 Series, Model DC-9-80 series, including Model MD-88, and C-9 (Military) series airplanes equipped with hinged evacuation slide cover assemblies as listed in McDonnell Douglas Alert Service Bulletin A25-299, Revision 1, dated September 23, 1988.

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

Federal Register Abstract

Evacuation Slide Assemblies

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_89-10-10.html
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Details
AD Number:
89-10-10
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Mili...Show more
Subject:
Evacuation Slide Assemblies
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
06/12/1989
Make:
The Boeing Company
Model:
DC-9-11 | DC-9-12 | DC-9-13 | DC-9-14 | DC-9-15 | DC-9-15F | DC-9-21 | DC-9-31 | DC-9-32 | DC-9-32 (...Show more
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: 89-10-10
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-6209

AD NUMBER:   89-10-10

SUBJECT HEADING:   Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective June 12, 1989.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
89-10-10 McDONNELL DOUGLAS: Amendment 39-6209.

Applicability: McDonnell Douglas Model DC-9 Series, Model DC-9-80 series, including Model MD-88, and C-9 (Military) series airplanes, equipped with hinged evacuation slide cover assemblies, as listed in McDonnell Douglas Alert Service Bulletin A25-299, Revision 1, dated September 23, 1988, certificated in any category.

Compliance: Required as indicated, unless previously accomplished.

To minimize the possibility of an unusable emergency exit, accomplish the following:

A. Within 6 months after the effective date of this AD, replace the evacuation slide girt bar forward stowage clip in accordance with the Accomplishment Instructions of McDonnell Douglas Alert Service Bulletin A25-299, Revision 1, dated September 23, 1988.

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, Los Angeles Aircraft Certification Office, 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, Los Angeles Aircraft Certification Office.

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 McDonnell Douglas Corporation, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Director of Publications, CL-100 (54-60). These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or the Los Angeles Aircraft Certification Office, 3229 East Spring Street, Long Beach, California.

This amendment (39-6209, AD 89-10-10) becomes effective on June 12, 1989.


FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_89-10-10.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
89-10-10
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Mili...Show more
Subject:
Evacuation Slide Assemblies
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
06/12/1989
Make:
The Boeing Company
Model:
DC-9-11 | DC-9-12 | DC-9-13 | DC-9-14 | DC-9-15 | DC-9-15F | DC-9-21 | DC-9-31 | DC-9-32 | DC-9-32 (...Show more
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: 89-10-10
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-6209

AD NUMBER:   89-10-10

SUBJECT HEADING:   Airworthiness Directives; McDONNELL DOUGLAS DC-9 Series, Model DC-9-80 Series, MD-88, and C-9 (Military) Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective June 12, 1989.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
89-10-10 McDONNELL DOUGLAS: Amendment 39-6209.

Applicability: McDonnell Douglas Model DC-9 Series, Model DC-9-80 series, including Model MD-88, and C-9 (Military) series airplanes, equipped with hinged evacuation slide cover assemblies, as listed in McDonnell Douglas Alert Service Bulletin A25-299, Revision 1, dated September 23, 1988, certificated in any category.

Compliance: Required as indicated, unless previously accomplished.

To minimize the possibility of an unusable emergency exit, accomplish the following:

A. Within 6 months after the effective date of this AD, replace the evacuation slide girt bar forward stowage clip in accordance with the Accomplishment Instructions of McDonnell Douglas Alert Service Bulletin A25-299, Revision 1, dated September 23, 1988.

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, Los Angeles Aircraft Certification Office, 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, Los Angeles Aircraft Certification Office.

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 McDonnell Douglas Corporation, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Director of Publications, CL-100 (54-60). These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or the Los Angeles Aircraft Certification Office, 3229 East Spring Street, Long Beach, California.

This amendment (39-6209, AD 89-10-10) becomes effective on June 12, 1989.


FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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