AD 90-02-12

final rule

Airworthiness Directives: BOEING Model 757 Series Airplanes

AD Number
90-02-12
Status
final_rule
Effective Date
Product Category
aircraft
Docket
89-NM-160-AD
FR Citation
This information is not available.
Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company 757-200 Series Airworthiness Directives: BOEING Model 757 Series Airplanes
aircraft The Boeing Company 757-200CB Series Airworthiness Directives: BOEING Model 757 Series Airplanes
aircraft The Boeing Company 757-200PF Series Airworthiness Directives: BOEING Model 757 Series Airplanes
aircraft The Boeing Company 757-300 Series Airworthiness Directives: BOEING Model 757 Series Airplanes

Unsafe Condition

Loose objects lodging in the control quadrant assembly could cause aileron control system jamming.

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

Required Actions

Install flexible deflectors in accordance with Boeing Service Bulletin 757-27-0072 or Revision 1 dated June 29, 1989. Alternate means of compliance or adjustment may be used if approved by the FAA 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 12 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

BOEING Model 757 series airplanes listed in Boeing Service Bulletin 757-27-0072, Revision 1, dated June 29, 1989

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

Federal Register Abstract

Aileron Control System

Applicability Source Text

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AD Number:
90-02-12
Document Type:
AD Final Rules
Docket Number:
89-NM-160-AD
Subject Heading:
Airworthiness Directives: BOEING Model 757 Series Airplanes
Subject:
Aileron Control System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
02/09/1990
Make:
The Boeing Company
Model:
757-200 Series | 757-200CB Series | 757-200PF Series | 757-300 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Superseded AD: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Superseded By: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:
AIRWORTHINESS DIRECTIVES FINAL RULES: 90-02-12
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   89-NM-160-AD

AMENDMENT:   39-6439

AD NUMBER:   90-02-12

SUBJECT HEADING:   Airworthiness Directives: BOEING Model 757 Series Airplanes


ACTION:  

SUMMARY:  

DATES:   Effective February 9, 1990.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
90-02-12 BOEING: Amendment 39-6439. Docket No. 89-NM-160-AD.

Applicability: Model 757 series airplanes, as listed in Boeing Service Bulletin 757-27- 0072, Revision 1, dated June 29, 1989, certificated in any category.

Compliance: Required within the next 12 months, after the effective date of this AD, unless previously accomplished.

To reduce the possibility of aileron control system jamming due to loose objects being lodged in the control quadrant assembly, accomplish the following:

A. Install flexible deflectors in accordance with Boeing Service Bulletin 757-27-0072, dated February 5, 1987, or Revision 1, dated June 29, 1989.

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 documents from the manufacturer may obtain copies upon request to Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124. These documents 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 (39-6439, AD 90-02-12) becomes effective on February 9, 1990.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_90-02-12.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
90-02-12
Document Type:
AD Final Rules
Docket Number:
89-NM-160-AD
Subject Heading:
Airworthiness Directives: BOEING Model 757 Series Airplanes
Subject:
Aileron Control System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
02/09/1990
Make:
The Boeing Company
Model:
757-200 Series | 757-200CB Series | 757-200PF Series | 757-300 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:
AIRWORTHINESS DIRECTIVES FINAL RULES: 90-02-12
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   89-NM-160-AD

AMENDMENT:   39-6439

AD NUMBER:   90-02-12

SUBJECT HEADING:   Airworthiness Directives: BOEING Model 757 Series Airplanes


ACTION:  

SUMMARY:  

DATES:   Effective February 9, 1990.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
90-02-12 BOEING: Amendment 39-6439. Docket No. 89-NM-160-AD.

Applicability: Model 757 series airplanes, as listed in Boeing Service Bulletin 757-27- 0072, Revision 1, dated June 29, 1989, certificated in any category.

Compliance: Required within the next 12 months, after the effective date of this AD, unless previously accomplished.

To reduce the possibility of aileron control system jamming due to loose objects being lodged in the control quadrant assembly, accomplish the following:

A. Install flexible deflectors in accordance with Boeing Service Bulletin 757-27-0072, dated February 5, 1987, or Revision 1, dated June 29, 1989.

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 documents from the manufacturer may obtain copies upon request to Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124. These documents 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 (39-6439, AD 90-02-12) becomes effective on February 9, 1990.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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