AD 86-05-06

final rule

BOEING Model 757-200 Series Airplanes

AD Number
86-05-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
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 BOEING Model 757-200 Series Airplanes

Unsafe Condition

The elevator control forward override assembly cam could become jammed, which could prevent proper elevator control operation.

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

Required Actions

Remove and replace the elevator control forward override assembly cam with a revised cam in accordance with Boeing Service Bulletin 757-27-0057, Revision 1, dated October 17, 1985, or later FAA-approved revision. Special flight permits may be issued to operate airplanes to a base for the modification.

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

Compliance Time

Within the next 60 days after the effective date of this AD

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

Affected Aircraft

All Model 757-200 series airplanes listed in Boeing Service Bulletin 757-27-0057, Revision 1, dated October 17, 1985

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

Federal Register Abstract

Elevator Control Forward Override Assembly Cam

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_86-05-06.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
86-05-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
BOEING Model 757-200 Series Airplanes
Subject:
Elevator Control Forward Override Assembly Cam
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/10/1986
Make:
The Boeing Company
Model:
757-200 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Superseded AD: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Superseded By: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: 86-05-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5244

AD NUMBER:   86-05-06

SUBJECT HEADING:   BOEING Model 757-200 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective April 10, 1986.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
86-05-06 BOEING: Amendment 39-5244. Applies to all Model 757-200 series airplanes listed in Boeing Service Bulletin 757-27-0057, Revision 1, dated October 17, 1985, certificated in any category.

To eliminate the possibility of the elevator forward override mechanism becoming jammed, accomplish the following, unless already accomplished:

A. Within the next 60 days after the effective date of this AD, remove and replace the elevator control forward override assembly cam with a revised cam in accordance with Boeing Service Bulletin 757-27-0057, Revision 1, dated October 17, 1985, or later FAA- approved revision.

B. 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 the modifications required by this AD.

All persons affected by this proposal who have not already received the appropriate service document from the manufacturer may obtain copies upon request to the Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98124-2207. This document may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington.

This amendment becomes effective April 10, 1986.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_86-05-06.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
86-05-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
BOEING Model 757-200 Series Airplanes
Subject:
Elevator Control Forward Override Assembly Cam
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/10/1986
Make:
The Boeing Company
Model:
757-200 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: 86-05-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5244

AD NUMBER:   86-05-06

SUBJECT HEADING:   BOEING Model 757-200 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective April 10, 1986.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
86-05-06 BOEING: Amendment 39-5244. Applies to all Model 757-200 series airplanes listed in Boeing Service Bulletin 757-27-0057, Revision 1, dated October 17, 1985, certificated in any category.

To eliminate the possibility of the elevator forward override mechanism becoming jammed, accomplish the following, unless already accomplished:

A. Within the next 60 days after the effective date of this AD, remove and replace the elevator control forward override assembly cam with a revised cam in accordance with Boeing Service Bulletin 757-27-0057, Revision 1, dated October 17, 1985, or later FAA- approved revision.

B. 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 the modifications required by this AD.

All persons affected by this proposal who have not already received the appropriate service document from the manufacturer may obtain copies upon request to the Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98124-2207. This document may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington.

This amendment becomes effective April 10, 1986.

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.