AD 88-06-04

final rule

Airworthiness Directives; BOEING Model 757 Series Airplanes

AD Number
88-06-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of a riveted aircraft structural panel and frame
Problem area Airframe structure

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

Structural failure of the vertical fin and horizontal stabilizers in the event of a failure of the aft pressure bulkhead.

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

Required Actions

Install a vertical fin access door and horizontal stabilizer covers in accordance with Boeing Service Bulletin 757-53-0038 or later FAA-approved revision. Alternate means of compliance or adjustment of compliance time may be used with FAA concurrence.

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

Compliance Time

within 18 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 757-53-0038, dated August 27, 1987, certificated in any category.

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

Federal Register Abstract

Vertical Fin & Horizontal Stabilizers

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_88-06-04.html
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AD Number:
88-06-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BOEING Model 757 Series Airplanes
Subject:
Vertical Fin & Horizontal Stabilizers
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/22/1988
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: 88-06-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5872

AD NUMBER:   88-06-04

SUBJECT HEADING:   Airworthiness Directives; BOEING Model 757 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective April 22, 1988.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
88-06-04 BOEING: Amendment 39-5872. Applies to Model 757 series airplanes listed in Boeing Service Bulletin 757-53-0038, dated August 27, 1987, certificated in any category. Compliance required within 18 months after the effective date of this AD, unless previously accomplished.

To prevent structural failure of the vertical fin and horizontal stabilizers in the event of a failure of the aft pressure bulkhead, accomplish the following:

A. Install a vertical fin access door and horizontal stabilizer covers in accordance with Boeing Service Bulletin 757-53-0038, dated August 27, 1987, or later FAA-approved revision.

B. An alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety and which has the concurrence of an FAA Principal Maintenance Inspector, may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region.

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 the Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98124. These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or Seattle Aircraft Certification Office, FAA, Northwest Mountain Region, 9010 East Marginal Way South, Seattle, Washington.

This amendment becomes effective April 22, 1988.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_88-06-04.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
88-06-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BOEING Model 757 Series Airplanes
Subject:
Vertical Fin & Horizontal Stabilizers
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/22/1988
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: 88-06-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5872

AD NUMBER:   88-06-04

SUBJECT HEADING:   Airworthiness Directives; BOEING Model 757 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective April 22, 1988.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
88-06-04 BOEING: Amendment 39-5872. Applies to Model 757 series airplanes listed in Boeing Service Bulletin 757-53-0038, dated August 27, 1987, certificated in any category. Compliance required within 18 months after the effective date of this AD, unless previously accomplished.

To prevent structural failure of the vertical fin and horizontal stabilizers in the event of a failure of the aft pressure bulkhead, accomplish the following:

A. Install a vertical fin access door and horizontal stabilizer covers in accordance with Boeing Service Bulletin 757-53-0038, dated August 27, 1987, or later FAA-approved revision.

B. An alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety and which has the concurrence of an FAA Principal Maintenance Inspector, may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region.

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 the Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98124. These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or Seattle Aircraft Certification Office, FAA, Northwest Mountain Region, 9010 East Marginal Way South, Seattle, Washington.

This amendment becomes effective April 22, 1988.

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.