AD 83-06-03

final rule

Airworthiness Directives; MCDONNELL DOUGLAS DC-9-30, -40, and -50 Series Airplanes

AD Number
83-06-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company DC-9-31 Airworthiness Directives; MCDONNELL DOUGLAS DC-9-30, -40, and -50 Series Airplanes
aircraft The Boeing Company DC-9-32 Airworthiness Directives; MCDONNELL DOUGLAS DC-9-30, -40, and -50 Series Airplanes
aircraft The Boeing Company DC-9-32 (VC-9C) Airworthiness Directives; MCDONNELL DOUGLAS DC-9-30, -40, and -50 Series Airplanes
aircraft The Boeing Company DC-9-32F Airworthiness Directives; MCDONNELL DOUGLAS DC-9-30, -40, and -50 Series Airplanes
aircraft The Boeing Company DC-9-32F (C-9A) Airworthiness Directives; MCDONNELL DOUGLAS DC-9-30, -40, and -50 Series Airplanes
aircraft The Boeing Company DC-9-32F (C-9B) Airworthiness Directives; MCDONNELL DOUGLAS DC-9-30, -40, and -50 Series Airplanes
aircraft The Boeing Company DC-9-33F Airworthiness Directives; MCDONNELL DOUGLAS DC-9-30, -40, and -50 Series Airplanes
aircraft The Boeing Company DC-9-34 Airworthiness Directives; MCDONNELL DOUGLAS DC-9-30, -40, and -50 Series Airplanes
aircraft The Boeing Company DC-9-34F Airworthiness Directives; MCDONNELL DOUGLAS DC-9-30, -40, and -50 Series Airplanes
aircraft The Boeing Company DC-9-41 Airworthiness Directives; MCDONNELL DOUGLAS DC-9-30, -40, and -50 Series Airplanes
aircraft The Boeing Company DC-9-51 Airworthiness Directives; MCDONNELL DOUGLAS DC-9-30, -40, and -50 Series Airplanes

Unsafe Condition

Failure of the main landing gear support structure due to improperly heat treated restrictor support tubes.

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

Required Actions

Perform an eddy current inspection of the restrictor support tube per McDonnell Douglas Service Bulletin 32-186. Replace restrictor tubes if improperly heat treated. Use special flight permits under FAR 21.197/21.199 to operate to a base for compliance.

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

Compliance Time

prior to December 14, 1983

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

Affected Aircraft

McDonnell Douglas DC-9-30, -40, -50 series airplanes with MLG strut serial numbers R4429N, R4430-R4436, R4438-R4449, R4462-R4469, R5415-R5420, R7475, R7476, R7478-R7526, R8734, R8736, R8742, R8743.

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

Federal Register Abstract

MLG Support Structure

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_83-06-03.html
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AD Number:
83-06-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; MCDONNELL DOUGLAS DC-9-30, -40, and -50 Series Airplanes
Subject:
MLG Support Structure
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/28/1983
Make:
The Boeing Company
Model:
DC-9-31 | DC-9-32 | DC-9-32 (VC-9C) | DC-9-32F | DC-9-32F (C-9A) | DC-9-32F (C-9B) | DC-9-33F | DC-9...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: 83-06-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4590

AD NUMBER:   83-06-03

SUBJECT HEADING:   Airworthiness Directives; MCDONNELL DOUGLAS DC-9-30, -40, and -50 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective April 28, 1983.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
83-06-03 MCDONNELL DOUGLAS: Amendment 39-4590. Applies to McDonnell Douglas Model DC-9-30, -40, and -50 series airplanes, with the following MLG strut serial numbers installed: R4429N, R4430 through R4436, R4438 through R4449, R4462 through R4469, R5415 through R5420, R7475, R7476, R7478 through R7526, R8734, R8736, R8742, and R8743, certificated in all categories. Compliance required prior to December 14, 1983, unless previously accomplished.

To prevent failure of the main landing gear support structure, accomplish the following:

A. Perform an eddy current inspection to determine the heat treat condition of the restrictor support tube in accordance with the Accomplishment Instructions of McDonnell Douglas DC-9 Service Bulletin 32-186, original issue, dated January 29, 1982, or later revisions approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region.

B. Replace restrictor tubes if any are found to be improperly heat treated in accordance with the above service bulletin.

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. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region.

All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to McDonnell Douglas Corporation, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Director, Publications and Training, C1-750 (54-60). These documents also may be examined at FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington 98168, or Los Angeles Aircraft Certification Office, 4344 Donald Douglas Drive, Long Beach, California 90808.

This amendment becomes effective April 28, 1983.


FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_83-06-03.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
83-06-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; MCDONNELL DOUGLAS DC-9-30, -40, and -50 Series Airplanes
Subject:
MLG Support Structure
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/28/1983
Make:
The Boeing Company
Model:
DC-9-31 | DC-9-32 | DC-9-32 (VC-9C) | DC-9-32F | DC-9-32F (C-9A) | DC-9-32F (C-9B) | DC-9-33F | DC-9...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: 83-06-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4590

AD NUMBER:   83-06-03

SUBJECT HEADING:   Airworthiness Directives; MCDONNELL DOUGLAS DC-9-30, -40, and -50 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective April 28, 1983.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
83-06-03 MCDONNELL DOUGLAS: Amendment 39-4590. Applies to McDonnell Douglas Model DC-9-30, -40, and -50 series airplanes, with the following MLG strut serial numbers installed: R4429N, R4430 through R4436, R4438 through R4449, R4462 through R4469, R5415 through R5420, R7475, R7476, R7478 through R7526, R8734, R8736, R8742, and R8743, certificated in all categories. Compliance required prior to December 14, 1983, unless previously accomplished.

To prevent failure of the main landing gear support structure, accomplish the following:

A. Perform an eddy current inspection to determine the heat treat condition of the restrictor support tube in accordance with the Accomplishment Instructions of McDonnell Douglas DC-9 Service Bulletin 32-186, original issue, dated January 29, 1982, or later revisions approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region.

B. Replace restrictor tubes if any are found to be improperly heat treated in accordance with the above service bulletin.

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. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region.

All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to McDonnell Douglas Corporation, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Director, Publications and Training, C1-750 (54-60). These documents also may be examined at FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington 98168, or Los Angeles Aircraft Certification Office, 4344 Donald Douglas Drive, Long Beach, California 90808.

This amendment becomes effective April 28, 1983.


FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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