AD 2000-11-19 R1
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 767-200 Series | Airworthiness Directives; Boeing Model 767-200 and -300 Series Airplanes |
| aircraft | The Boeing Company | 767-300 Series | Airworthiness Directives; Boeing Model 767-200 and -300 Series Airplanes |
Unsafe Condition
Worn or damaged door latches and disconnect housings in the off-wing escape slide compartments could result in non-deployment of an escape slide during an emergency evacuation or unexpected deployment during maintenance, leading to passenger/flightcrew injury or maintenance personnel injury.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Repetitive inspections must be conducted to detect wear or damage of door latches and disconnect housings in the off-wing escape slide compartments, with replacement of any discrepant components with new components.
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Compliance Time
before further flight
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Affected Aircraft
Boeing Model 767-200 and -300 series airplanes equipped with Goodrich off-wing ramp/slide having basic part numbers 101630, 101654, 101655, or 101656.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Door latches
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - 2000-11-19 R1.pdf Copy URL Document Versions Feedback DetailsAttachments/Public Comments AD Number: 2000-11-19 R1 Document Type: AD Final Rules Docket Number: FAA-2005-22488 Subject Heading: Airworthiness Directives; Boeing Model 767-200 and -300 Series Airplanes Subject: Door latches Status: Current Citation: (Federal Register: June 12, 2006 (Volume 71, Number 112)) Citation Publish Date: 06/12/2006 Effective Date: 07/18/2000 Make: The Boeing Company Model: 767-200 Series | 767-300 Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: Automatic Zoom Actual Size Page Fit Page Width 50% 75% 100% 125% 150% 200% 300% 400% 125% of 9 1 [Federal Register: June 12, 2006 (Volume 71, Number 112)] [Rules and Regulations] [Page 33608-33611] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr12jn06-7] ––––––––––––––––––––––––––––––––––– DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-22488; Directorate Identifier 2005-NM-151-AD; Amendment 39-14637; AD 2000-11-19 R1] RIN 2120-AA64 Airworthiness Directives; Boeing Model 767-200 and -300 Series Airplanes AGENCY: Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. ––––––––––––––––––––––––––––––––––– SUMMARY: The FAA is revising an existing airworthiness directive (AD) that applies to certain Boeing Model 767-200 and -300 series airplanes. That AD currently requires repetitive inspections to detect wear or damage of the door latches and disconnect housings in the off-wing escape slide compartments, and replacement of any discrepant component with a new component. This new AD revises the applicability of the existing AD to refer to a later revision of the referenced service bulletin, which removes airplanes that are not subject to the identified unsafe condition. This AD results from reports of worn and damaged door latches and disconnect housings in the off-wing escape slide compartments. We are issuing this AD to ensure deployment of an escape slide during an emergency evacuation. Non-deployment of an escape slide during an emergency could slow down the evacuation of the airplane and result in injury to passengers or flightcrew. We are also issuing this AD to detect damaged disconnect housings in the off-wing escape slide compartments, which could result in unexpected deployment of an escape slide during maintenance, and consequent injury to maintenance personnel. DATES: The effective date of this AD is July 18, 2000. The Director of the Federal Register approved the incorporation by reference of Boeing Service Bulletin 767-25A0260, Revision 1, dated January 25, 2001; Boeing Service Bulletin 767-25A0260, Revision 2, dated August 26, 2004; Boeing Service Bulletin 767-25A0260, Revision 3, dated July 7, 2005; and Boeing Service Bulletin 767-25A0275, Revision 3, dated April 24, 2003; listed in the AD as of July 17, 2006. On July 18, 2000 (65 FR 37015, June 13, 2000), the Director of the Federal Register approved the incorporation by reference of Boeing Alert Service Bulletin 767-25A0260, dated July 9, 1998. ADDRESSES: You may examine the AD docket on the Internet at http://dms.dot.gov or in person at the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street SW., Nassif Building, Room PL-401, Washington, DC. 2 Contact Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124-2207, for service information identified in this AD. FOR FURTHER INFORMATION CONTACT: Victor Wicklund, Aerospace Engineer, Cabin Safety and Environmental Systems Branch, ANM-150S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 917-6458; fax (425) 917- 6590. SUPPLEMENTARY INFORMATION: Examining the Docket You may examine the AD docket on the Internet at http://dms.dot.gov or in person at the Docket Management Facility office between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The Docket Management Facility office (telephone (800) 647-5227) is located on the plaza level of the Nassif Building at the street address stated in the ADDRESSES section. Discussion The FAA proposed to amend part 39 of the Federal Aviation Regulations (14 CFR part 39) with an airworthiness directive (AD) to revise AD 2000-11-19, amendment 39-11767 (65 FR 37015, June 13, 2000). The existing AD applies to certain Boeing Model 767-200 and -300 series airplanes. The proposed AD was published in the Federal Register on September 21, 2005 (70 FR 55323) to continue to require repetitive inspections to detect wear or damage of the door latches and disconnect housings in the off-wing escape slide compartments, and replacement of any discrepant component with a new component. The proposed AD also proposed to revise the applicability of the existing AD to refer to a later revision of the referenced service bulletin, which removes airplanes that are not subject the identified unsafe condition. Comments We provided the public the opportunity to participate in the development of this AD. We have considered the comments received. Support for the Proposed AD United Airlines and the National Transportation Safety Board support the proposed AD. Request to Revise the Applicability Boeing requests that the applicability of the proposed AD be revised to ''Boeing Model 767-200 and -300 series airplanes, equipped with Goodrich off-wing ramp/slide having basic part numbers (P/N) 101630, 101654, 101655, or 101656. * * *'' Boeing states that this change would clearly identify that the proposed AD is only applicable to the Goodrich off-wing slide system. Boeing further states that if that system is removed or replaced, the proposed inspection would no longer be necessary and, as a result, the airplane would not be applicable to the AD. We agree and have revised the AD accordingly.
Document Text
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AD Final Rules - 2000-11-19 R1.pdf Copy URL Document Versions Feedback DetailsAttachments/Public Comments AD Number: 2000-11-19 R1 Document Type: AD Final Rules Docket Number: FAA-2005-22488 Subject Heading: Airworthiness Directives; Boeing Model 767-200 and -300 Series Airplanes Subject: Door latches Status: Current Citation: (Federal Register: June 12, 2006 (Volume 71, Number 112)) Citation Publish Date: 06/12/2006 Effective Date: 07/18/2000 Make: The Boeing Company Model: 767-200 Series | 767-300 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: Automatic Zoom Actual Size Page Fit Page Width 50% 75% 100% 125% 150% 200% 300% 400% 125% of 9 1 [Federal Register: June 12, 2006 (Volume 71, Number 112)] [Rules and Regulations] [Page 33608-33611] From the Federal Register Online via GPO Access [wais.access.gpo.gov] [DOCID:fr12jn06-7] ––––––––––––––––––––––––––––––––––– DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-22488; Directorate Identifier 2005-NM-151-AD; Amendment 39-14637; AD 2000-11-19 R1] RIN 2120-AA64 Airworthiness Directives; Boeing Model 767-200 and -300 Series Airplanes AGENCY: Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. ––––––––––––––––––––––––––––––––––– SUMMARY: The FAA is revising an existing airworthiness directive (AD) that applies to certain Boeing Model 767-200 and -300 series airplanes. That AD currently requires repetitive inspections to detect wear or damage of the door latches and disconnect housings in the off-wing escape slide compartments, and replacement of any discrepant component with a new component. This new AD revises the applicability of the existing AD to refer to a later revision of the referenced service bulletin, which removes airplanes that are not subject to the identified unsafe condition. This AD results from reports of worn and damaged door latches and disconnect housings in the off-wing escape slide compartments. We are issuing this AD to ensure deployment of an escape slide during an emergency evacuation. Non-deployment of an escape slide during an emergency could slow down the evacuation of the airplane and result in injury to passengers or flightcrew. We are also issuing this AD to detect damaged disconnect housings in the off-wing escape slide compartments, which could result in unexpected deployment of an escape slide during maintenance, and consequent injury to maintenance personnel. DATES: The effective date of this AD is July 18, 2000. The Director of the Federal Register approved the incorporation by reference of Boeing Service Bulletin 767-25A0260, Revision 1, dated January 25, 2001; Boeing Service Bulletin 767-25A0260, Revision 2, dated August 26, 2004; Boeing Service Bulletin 767-25A0260, Revision 3, dated July 7, 2005; and Boeing Service Bulletin 767-25A0275, Revision 3, dated April 24, 2003; listed in the AD as of July 17, 2006. On July 18, 2000 (65 FR 37015, June 13, 2000), the Director of the Federal Register approved the incorporation by reference of Boeing Alert Service Bulletin 767-25A0260, dated July 9, 1998. ADDRESSES: You may examine the AD docket on the Internet at http://dms.dot.gov or in person at the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street SW., Nassif Building, Room PL-401, Washington, DC. 2 Contact Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124-2207, for service information identified in this AD. FOR FURTHER INFORMATION CONTACT: Victor Wicklund, Aerospace Engineer, Cabin Safety and Environmental Systems Branch, ANM-150S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 917-6458; fax (425) 917- 6590. SUPPLEMENTARY INFORMATION: Examining the Docket You may examine the AD docket on the Internet at http://dms.dot.gov or in person at the Docket Management Facility office between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The Docket Management Facility office (telephone (800) 647-5227) is located on the plaza level of the Nassif Building at the street address stated in the ADDRESSES section. Discussion The FAA proposed to amend part 39 of the Federal Aviation Regulations (14 CFR part 39) with an airworthiness directive (AD) to revise AD 2000-11-19, amendment 39-11767 (65 FR 37015, June 13, 2000). The existing AD applies to certain Boeing Model 767-200 and -300 series airplanes. The proposed AD was published in the Federal Register on September 21, 2005 (70 FR 55323) to continue to require repetitive inspections to detect wear or damage of the door latches and disconnect housings in the off-wing escape slide compartments, and replacement of any discrepant component with a new component. The proposed AD also proposed to revise the applicability of the existing AD to refer to a later revision of the referenced service bulletin, which removes airplanes that are not subject the identified unsafe condition. Comments We provided the public the opportunity to participate in the development of this AD. We have considered the comments received. Support for the Proposed AD United Airlines and the National Transportation Safety Board support the proposed AD. Request to Revise the Applicability Boeing requests that the applicability of the proposed AD be revised to ''Boeing Model 767-200 and -300 series airplanes, equipped with Goodrich off-wing ramp/slide having basic part numbers (P/N) 101630, 101654, 101655, or 101656. * * *'' Boeing states that this change would clearly identify that the proposed AD is only applicable to the Goodrich off-wing slide system. Boeing further states that if that system is removed or replaced, the proposed inspection would no longer be necessary and, as a result, the airplane would not be applicable to the AD. We agree and have revised the AD accordingly.
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Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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