AD 82-04-06

final rule

Airworthiness Directives; MCDONNELL DOUGLAS DC-10-40 Airplanes

AD Number
82-04-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company DC-10-40 Airworthiness Directives; MCDONNELL DOUGLAS DC-10-40 Airplanes
aircraft The Boeing Company DC-10-40F Airworthiness Directives; MCDONNELL DOUGLAS DC-10-40 Airplanes

Unsafe Condition

Separation of the nose cowl from the aircraft in the event of fan blade failure.

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

Required Actions

Replace the nose cowl attaching bolts and nuts on engines 1 and 3 as outlined in McDonnell Douglas DC-10 Service Bulletin 71-123 dated June 23, 1981, or later revisions approved by the FAA. Alternate means of compliance may be used if approved by the FAA.

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

Compliance Time

within twelve (12) calendar months 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-10-40 airplanes equipped with Pratt and Whitney JT9D-20 series engines

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

Federal Register Abstract

Nose Cowl Separation

Applicability Source Text

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AD Final Rules - DRS_82-04-06.html
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Details
AD Number:
82-04-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; MCDONNELL DOUGLAS DC-10-40 Airplanes
Subject:
Nose Cowl Separation
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/04/1982
Make:
The Boeing Company
Model:
DC-10-40 | DC-10-40F
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Superseded AD: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Superseded By: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: 82-04-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4320

AD NUMBER:   82-04-06

SUBJECT HEADING:   Airworthiness Directives; MCDONNELL DOUGLAS DC-10-40 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective March 4, 1982.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
82-04-06 MCDONNELL DOUGLAS: Amendment 39-4320. Applies to McDonnell Douglas Model DC-10-40 airplanes equipped with Pratt and Whitney JT9D-20 series engines, certificated in all categories. Compliance required within twelve (12) calendar months from the effective date of this AD, unless already accomplished.

To minimize the possibility of separation of the nose cowl from the aircraft in the event of fan blade failure, accomplish the following:

A. Replace the nose cowl attaching bolts and nuts on engines 1 and 3 as outlined in the Accomplishment Instructions and Material Information in McDonnell Douglas DC-10 Service Bulletin 71-123 dated June 23, 1981, or later revisions approved by the Chief, Los Angeles Area Aircraft Certification Office, FAA Northwest Mountain Region.

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

The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1).

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 the FAA Northwest Mountain Region, 9010 East Marginal Way South, Seattle, Washington 98108, or 4344 Donald Douglas Drive, Long Beach, California 90808.

This amendment becomes effective March 4, 1982.


FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_82-04-06.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
82-04-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; MCDONNELL DOUGLAS DC-10-40 Airplanes
Subject:
Nose Cowl Separation
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/04/1982
Make:
The Boeing Company
Model:
DC-10-40 | DC-10-40F
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: 82-04-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4320

AD NUMBER:   82-04-06

SUBJECT HEADING:   Airworthiness Directives; MCDONNELL DOUGLAS DC-10-40 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective March 4, 1982.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
82-04-06 MCDONNELL DOUGLAS: Amendment 39-4320. Applies to McDonnell Douglas Model DC-10-40 airplanes equipped with Pratt and Whitney JT9D-20 series engines, certificated in all categories. Compliance required within twelve (12) calendar months from the effective date of this AD, unless already accomplished.

To minimize the possibility of separation of the nose cowl from the aircraft in the event of fan blade failure, accomplish the following:

A. Replace the nose cowl attaching bolts and nuts on engines 1 and 3 as outlined in the Accomplishment Instructions and Material Information in McDonnell Douglas DC-10 Service Bulletin 71-123 dated June 23, 1981, or later revisions approved by the Chief, Los Angeles Area Aircraft Certification Office, FAA Northwest Mountain Region.

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

The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1).

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 the FAA Northwest Mountain Region, 9010 East Marginal Way South, Seattle, Washington 98108, or 4344 Donald Douglas Drive, Long Beach, California 90808.

This amendment becomes effective March 4, 1982.


FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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