AD 87-22-06

final rule

Airworthiness Directives; BOEING Model 727 Series Airplanes

AD Number
87-22-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
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 727-100 Series Airworthiness Directives; BOEING Model 727 Series Airplanes
aircraft The Boeing Company 727-100C Series Airworthiness Directives; BOEING Model 727 Series Airplanes
aircraft The Boeing Company 727-200 Series Airworthiness Directives; BOEING Model 727 Series Airplanes
aircraft The Boeing Company 727-200F Series Airworthiness Directives; BOEING Model 727 Series Airplanes
aircraft The Boeing Company 727 Series Airworthiness Directives; BOEING Model 727 Series Airplanes
aircraft The Boeing Company 727C Series Airworthiness Directives; BOEING Model 727 Series Airplanes

Unsafe Condition

The main landing gear door release lever may move to the door open position during flight.

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

Required Actions

Modify the left and right main landing gear door release levers in accordance with Boeing Service Bulletin 727-32-267, Revision 1, dated June 15, 1984, or later FAA-approved revision. Alternate means of compliance or adjustment may be used with FAA concurrence.

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

Compliance Time

within the next 4,500 hours time-in-service or 2 years after the effective date of this AD, whichever occurs first

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

Affected Aircraft

Boeing Model 727 series airplanes as listed in Boeing Service Bulletin 727-32-267, Revision 1, dated June 15, 1984, certificated in any category.

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

Federal Register Abstract

Main Landing Gear Lever

Applicability Source Text

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AD Final Rules - DRS_87-22-06.html
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AD Number:
87-22-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BOEING Model 727 Series Airplanes
Subject:
Main Landing Gear Lever
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/20/1987
Make:
The Boeing Company
Model:
727-100 Series | 727-100C Series | 727-200 Series | 727-200F Series | 727 Series | 727C 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: 87-22-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5743

AD NUMBER:   87-22-06

SUBJECT HEADING:   Airworthiness Directives; BOEING Model 727 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective November 20, 1987.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
87-22-06 BOEING: Amendment 39-5743. Applies to Model 727 series airplanes, as listed in Boeing Service Bulletin 727-32-267, Revision 1, dated June 15, 1984, certificated in any category. Compliance is required within the next 4,500 hours time-in-service or 2 years after the effective date of this AD, whichever occurs first, unless previously accomplished.

To prevent the main landing gear door release lever from moving to the door open position during flight, accomplish the following:

A. Modify the left and right main landing gear door release levers in accordance with the Accomplishment Instructions of Boeing Service Bulletin 727-32-267, Revision 1, dated June 15, 1984, 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 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 November 20, 1987.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_87-22-06.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
87-22-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BOEING Model 727 Series Airplanes
Subject:
Main Landing Gear Lever
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/20/1987
Make:
The Boeing Company
Model:
727-100 Series | 727-100C Series | 727-200 Series | 727-200F Series | 727 Series | 727C 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: 87-22-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5743

AD NUMBER:   87-22-06

SUBJECT HEADING:   Airworthiness Directives; BOEING Model 727 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective November 20, 1987.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
87-22-06 BOEING: Amendment 39-5743. Applies to Model 727 series airplanes, as listed in Boeing Service Bulletin 727-32-267, Revision 1, dated June 15, 1984, certificated in any category. Compliance is required within the next 4,500 hours time-in-service or 2 years after the effective date of this AD, whichever occurs first, unless previously accomplished.

To prevent the main landing gear door release lever from moving to the door open position during flight, accomplish the following:

A. Modify the left and right main landing gear door release levers in accordance with the Accomplishment Instructions of Boeing Service Bulletin 727-32-267, Revision 1, dated June 15, 1984, 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 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 November 20, 1987.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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