AD 91-07-13

final rule

Airworthiness Directives; BOEING Model 757 Series Airplanes

AD Number
91-07-13
Status
final_rule
Effective Date
Product Category
aircraft
Docket
90-NM-213-AD
FR Citation
This information is not available.
Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

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

Latent failure of the alternate landing gear extension system.

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

Required Actions

Install a bracket and attach the hydraulic tubing in accordance with Boeing Service Bulletin 757-29-0042. 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 3,000 hours time-in-service 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 757-29-0042 dated August 9, 1990

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

Federal Register Abstract

Alternate Landing Gear

Applicability Source Text

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AD Number:
91-07-13
Document Type:
AD Final Rules
Docket Number:
90-NM-213-AD
Subject Heading:
Airworthiness Directives; BOEING Model 757 Series Airplanes
Subject:
Alternate Landing Gear
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/29/1991
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Superseded AD: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Superseded By: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: 91-07-13
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   90-NM-213-AD

AMENDMENT:   39-6948

AD NUMBER:   91-07-13

SUBJECT HEADING:   Airworthiness Directives; BOEING Model 757 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective April 29, 1991.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
91-07-13 BOEING: Amendment 39-6948. Docket No. 90-NM-213-AD.

Applicability: Model 757 series airplanes, listed in Boeing Service Bulletin 757-29- 0042, dated August 9, 1990, certificated in any category.

Compliance: Required within 3,000 hours time-in-service after the effective date of this AD, unless previously accomplished.

To prevent a latent failure of the alternate landing gear extension system, accomplish the following:

A. Install a bracket and attach the hydraulic tubing in accordance with Boeing Service Bulletin 757-29-0042, dated August 9, 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 (ACO), FAA, Transport Airplane Directorate.

NOTE: The request should be submitted directly to the Manager, Seattle ACO, and a copy sent to the cognizant FAA Principal Inspector (PI). The PI will then forward comments or concurrence to the Seattle ACO.

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 Airplane Group, P.O. Box 3707, Seattle, Washington 98124. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 1601 Lind Avenue S.W., Renton, Washington.

This amendment (39-6948, AD 91-07-13) becomes effective on April 29, 1991.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_91-07-13.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
91-07-13
Document Type:
AD Final Rules
Docket Number:
90-NM-213-AD
Subject Heading:
Airworthiness Directives; BOEING Model 757 Series Airplanes
Subject:
Alternate Landing Gear
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/29/1991
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: 91-07-13
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   90-NM-213-AD

AMENDMENT:   39-6948

AD NUMBER:   91-07-13

SUBJECT HEADING:   Airworthiness Directives; BOEING Model 757 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective April 29, 1991.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
91-07-13 BOEING: Amendment 39-6948. Docket No. 90-NM-213-AD.

Applicability: Model 757 series airplanes, listed in Boeing Service Bulletin 757-29- 0042, dated August 9, 1990, certificated in any category.

Compliance: Required within 3,000 hours time-in-service after the effective date of this AD, unless previously accomplished.

To prevent a latent failure of the alternate landing gear extension system, accomplish the following:

A. Install a bracket and attach the hydraulic tubing in accordance with Boeing Service Bulletin 757-29-0042, dated August 9, 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 (ACO), FAA, Transport Airplane Directorate.

NOTE: The request should be submitted directly to the Manager, Seattle ACO, and a copy sent to the cognizant FAA Principal Inspector (PI). The PI will then forward comments or concurrence to the Seattle ACO.

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 Airplane Group, P.O. Box 3707, Seattle, Washington 98124. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 1601 Lind Avenue S.W., Renton, Washington.

This amendment (39-6948, AD 91-07-13) becomes effective on April 29, 1991.

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.