AD 90-11-11

final rule

Airworthiness Directives; BOEING Model 747-400 Series Airplanes

AD Number
90-11-11
Status
final_rule
Effective Date
Product Category
aircraft
Docket
90-NM-70-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company 747-400 Series Airworthiness Directives; BOEING Model 747-400 Series Airplanes

Unsafe Condition

Disablement of the passenger oxygen system due to the passenger oxygen/yaw damper module.

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

Required Actions

Remove and replace the passenger oxygen/yaw damper module in accordance with Boeing Alert Service Bulletin 747-35A2067. An alternate means of compliance or adjustment may be used if approved by the Manager, Seattle Aircraft Certification Office.

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

Compliance Time

within the next 500 hours time-in-service after the effective date of this AD, unless previously accomplished

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

Affected Aircraft

Boeing Model 747-400 series airplanes listed in Boeing Alert Service Bulletin 747-35A2067 dated March 15, 1990.

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

Federal Register Abstract

Oxygen/Yaw Damper Module

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_90-11-11.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
90-11-11
Document Type:
AD Final Rules
Docket Number:
90-NM-70-AD
Subject Heading:
Airworthiness Directives; BOEING Model 747-400 Series Airplanes
Subject:
Oxygen/Yaw Damper Module
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
06/11/1990
Make:
The Boeing Company
Model:
747-400 Series
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Superseded AD: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Superseded By: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:
Updated RGL applicability to match AD applicability; CAR C-11-185
AIRWORTHINESS DIRECTIVES FINAL RULES: 90-11-11
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   90-NM-70-AD

AMENDMENT:   39-6610

AD NUMBER:   90-11-11

SUBJECT HEADING:   Airworthiness Directives; BOEING Model 747-400 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective June 11, 1990.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
90-11-11 BOEING: Amendment 39-6610. Docket No. 90-NM-70-AD.

Applicability: Model 747-400 series airplanes, listed in Boeing Alert Service Bulletin 747-35A2067, dated March 15, 1990, certificated in any category.

Compliance: Required within the next 500 hours time-in-service after the effective date of this AD, unless previously accomplished.

To prevent disablement of the passenger oxygen system, accomplish the following:

A. Remove and replace the passenger oxygen/yaw damper module in accordance with Boeing Alert Service Bulletin 747-35A2067, dated March 15, 1990.

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, Seattle 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, Seattle 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 information from the manufacturer may obtain copies upon request to Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124. This information may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington.

This amendment (39-6610, AD 90-11-11) becomes effective on June 11, 1990.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_90-11-11.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
90-11-11
Document Type:
AD Final Rules
Docket Number:
90-NM-70-AD
Subject Heading:
Airworthiness Directives; BOEING Model 747-400 Series Airplanes
Subject:
Oxygen/Yaw Damper Module
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
06/11/1990
Make:
The Boeing Company
Model:
747-400 Series
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:
Updated RGL applicability to match AD applicability; CAR C-11-185
AIRWORTHINESS DIRECTIVES FINAL RULES: 90-11-11
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   90-NM-70-AD

AMENDMENT:   39-6610

AD NUMBER:   90-11-11

SUBJECT HEADING:   Airworthiness Directives; BOEING Model 747-400 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective June 11, 1990.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
90-11-11 BOEING: Amendment 39-6610. Docket No. 90-NM-70-AD.

Applicability: Model 747-400 series airplanes, listed in Boeing Alert Service Bulletin 747-35A2067, dated March 15, 1990, certificated in any category.

Compliance: Required within the next 500 hours time-in-service after the effective date of this AD, unless previously accomplished.

To prevent disablement of the passenger oxygen system, accomplish the following:

A. Remove and replace the passenger oxygen/yaw damper module in accordance with Boeing Alert Service Bulletin 747-35A2067, dated March 15, 1990.

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, Seattle 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, Seattle 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 information from the manufacturer may obtain copies upon request to Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124. This information may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington.

This amendment (39-6610, AD 90-11-11) becomes effective on June 11, 1990.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.