AD 87-22-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| 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.
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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.
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Compliance Time
within the next 4,500 hours time-in-service or 2 years after the effective date of this AD, whichever occurs first
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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.
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Federal Register Abstract
Main Landing Gear Lever
Applicability Source Text
Show captured applicability text from the source AD
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Series | 727-200F Series | 727 Series | 727C Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 87-22-06 CITATION: This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:
Document Text
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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:
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