AD 82-03-06

final rule

Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C-9A, C-9B, VC-9C Airplanes

AD Number
82-03-06
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-9-10, -20, -30, -40, -50, and -80 Series, including C-9A, C-9B, VC-9C Airplanes
aircraft The Boeing Company DC-9-12 Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C-9A, C-9B, VC-9C Airplanes
aircraft The Boeing Company DC-9-13 Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C-9A, C-9B, VC-9C Airplanes
aircraft The Boeing Company DC-9-14 Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C-9A, C-9B, VC-9C Airplanes
aircraft The Boeing Company DC-9-15 Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C-9A, C-9B, VC-9C Airplanes
aircraft The Boeing Company DC-9-15F Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C-9A, C-9B, VC-9C Airplanes
aircraft The Boeing Company DC-9-21 Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C-9A, C-9B, VC-9C Airplanes
aircraft The Boeing Company DC-9-31 Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C-9A, C-9B, VC-9C Airplanes
aircraft The Boeing Company DC-9-32 Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C-9A, C-9B, VC-9C Airplanes
aircraft The Boeing Company DC-9-32 (VC-9C) Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C-9A, C-9B, VC-9C Airplanes
aircraft The Boeing Company DC-9-32F Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C-9A, C-9B, VC-9C Airplanes
aircraft The Boeing Company DC-9-32F (C-9A) Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C-9A, C-9B, VC-9C Airplanes
aircraft The Boeing Company DC-9-32F (C-9B) Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C-9A, C-9B, VC-9C Airplanes
aircraft The Boeing Company DC-9-33F Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C-9A, C-9B, VC-9C Airplanes
aircraft The Boeing Company DC-9-34 Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C-9A, C-9B, VC-9C Airplanes
aircraft The Boeing Company DC-9-34F Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C-9A, C-9B, VC-9C Airplanes
aircraft The Boeing Company DC-9-41 Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C-9A, C-9B, VC-9C Airplanes
aircraft The Boeing Company DC-9-51 Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C-9A, C-9B, VC-9C Airplanes
aircraft The Boeing Company DC-9-81 (MD-81) Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C-9A, C-9B, VC-9C Airplanes
aircraft The Boeing Company DC-9-82 (MD-82) Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C-9A, C-9B, VC-9C Airplanes
aircraft The Boeing Company DC-9-83 (MD-83) Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C-9A, C-9B, VC-9C Airplanes
aircraft The Boeing Company DC-9-87 (MD-87) Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C-9A, C-9B, VC-9C Airplanes

Unsafe Condition

Failure of the tailcone emergency exit release mechanism due to improper operation caused by tailcone assemblies with part numbers 5910233-505 or 5910233-507.

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

Required Actions

Replace or modify the tailcone lock housing as per McDonnell Douglas DC-9 Service Bulletin 53-158 dated July 15, 1981, or later revisions approved by the Chief, Los Angeles Area Aircraft Certification Office. Alternate means of compliance may be used if approved by the same authority.

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

Compliance Time

within the next 900 hours time-in-service from 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-9-10, -20, -30, -40, -50, and -80 series airplanes, including C-9A, C-9B, and VC-9C airplanes, equipped with Kevlar tailcones.

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

Federal Register Abstract

Tail Cone Lock Housing Modification

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_82-03-06.html
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Details
AD Number:
82-03-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C...Show more
Subject:
Tail Cone Lock Housing Modification
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/11/1982
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: 82-03-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4311

AD NUMBER:   82-03-06

SUBJECT HEADING:   Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C-9A, C-9B, VC-9C Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective March 11, 1982.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
82-03-06 MCDONNELL DOUGLAS: Amendment 39-4311. Applies to McDonnell Douglas Model DC-9-10, -20, -30, -40, -50, and -80 series airplanes, including C-9A, C-9B, and VC-9C airplanes, certificated in all categories, equipped with Kevlar tailcones. Compliance required within the next 900 hours time-in-service from the effective date of this AD, unless already accomplished. To assure proper operation of the tailcone emergency exit release mechanism on aircraft utilizing tailcone assemblies P/N 5910233-505 or P/N 5910233-507, accomplish the following:

A. Replace or modify the tailcone lock housing as outlined in the Accomplishment Instructions of McDonnell Douglas DC-9 Service Bulletin 53-158 dated July 15, 1981, or later revisions approved by the Chief, Los Angeles Area Aircraft Certification Office, Northwest Mountain Region.

B. Alternate means of compliance with the AD which provide an equivalent level of safety may be used when approved by the Chief, Los Angeles Area Aircraft Certification Office, Northwest Mountain Region.

Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD.

This Amendment becomes effective March 11, 1982.


FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_82-03-06.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
82-03-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C...Show more
Subject:
Tail Cone Lock Housing Modification
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/11/1982
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: 82-03-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4311

AD NUMBER:   82-03-06

SUBJECT HEADING:   Airworthiness Directives; MCDONNELL DOUGLAS DC-9-10, -20, -30, -40, -50, and -80 Series, including C-9A, C-9B, VC-9C Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective March 11, 1982.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
82-03-06 MCDONNELL DOUGLAS: Amendment 39-4311. Applies to McDonnell Douglas Model DC-9-10, -20, -30, -40, -50, and -80 series airplanes, including C-9A, C-9B, and VC-9C airplanes, certificated in all categories, equipped with Kevlar tailcones. Compliance required within the next 900 hours time-in-service from the effective date of this AD, unless already accomplished. To assure proper operation of the tailcone emergency exit release mechanism on aircraft utilizing tailcone assemblies P/N 5910233-505 or P/N 5910233-507, accomplish the following:

A. Replace or modify the tailcone lock housing as outlined in the Accomplishment Instructions of McDonnell Douglas DC-9 Service Bulletin 53-158 dated July 15, 1981, or later revisions approved by the Chief, Los Angeles Area Aircraft Certification Office, Northwest Mountain Region.

B. Alternate means of compliance with the AD which provide an equivalent level of safety may be used when approved by the Chief, Los Angeles Area Aircraft Certification Office, Northwest Mountain Region.

Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD.

This Amendment becomes effective March 11, 1982.


FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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