AD 92-19-16
final rule
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 737-100 Series | Airworthiness Directives; BOEING Model 737 Series Airplanes |
| aircraft | The Boeing Company | 737-200 Series | Airworthiness Directives; BOEING Model 737 Series Airplanes |
| aircraft | The Boeing Company | 737-200C Series | Airworthiness Directives; BOEING Model 737 Series Airplanes |
| aircraft | The Boeing Company | 737-300 Series | Airworthiness Directives; BOEING Model 737 Series Airplanes |
| aircraft | The Boeing Company | 737-400 Series | Airworthiness Directives; BOEING Model 737 Series Airplanes |
| aircraft | The Boeing Company | 737-500 Series | Airworthiness Directives; BOEING Model 737 Series Airplanes |
| aircraft | The Boeing Company | 737-600 Series | Airworthiness Directives; BOEING Model 737 Series Airplanes |
| aircraft | The Boeing Company | 737-700 Series | Airworthiness Directives; BOEING Model 737 Series Airplanes |
| aircraft | The Boeing Company | 737-800 Series | Airworthiness Directives; BOEING Model 737 Series Airplanes |
| aircraft | The Boeing Company | 757-200 Series | Airworthiness Directives; BOEING Model 737 Series Airplanes |
| aircraft | The Boeing Company | 757-200CB Series | Airworthiness Directives; BOEING Model 737 Series Airplanes |
| aircraft | The Boeing Company | 757-200PF Series | Airworthiness Directives; BOEING Model 737 Series Airplanes |
| aircraft | The Boeing Company | 757-300 Series | Airworthiness Directives; BOEING Model 737 Series Airplanes |
Unsafe Condition
Overhead stowage bins may separate from their attachments and injure passengers in the event of an accident or emergency landing.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify Phase I overhead stowage bins within 8 months; modify Phase II, III, or IV bins within 31 months; replace drag link and tie rod assemblies for bins over 67 inches long within 31 months; install a doubler on specified forty-five inch stowage compartments within 31 months; install a doubler/diagonal strut assembly within 8 months. Compliance must follow specified Boeing service bulletins.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 8 or 31 months after the effective date of this AD, as specified.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Boeing Model 737 series airplanes listed in specified Boeing Alert Service Bulletins 737-25A1283, 737-25-1291, 737-25-1294 and Model 757 series listed in Bulletins 757-25A0121, 757-25-0130, 757-53-0056.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Overhead Stowage Bins
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_92-19-16.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 92-19-16 Document Type: AD Final Rules Docket Number: 91-NM-171-AD Subject Heading: Airworthiness Directives; BOEING Model 737 Series Airplanes Subject: Overhead Stowage Bins Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 11/20/1992 Make: The Boeing Company Model: 737-100 Series | 737-200 Series | 737-200C Series | 737-300 Series | 737-400 Series | 737-500 Series...Show more 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: Updated RGL applicability to match AD applicability; CAR C-11-185 AIRWORTHINESS DIRECTIVES FINAL RULES: 92-19-16 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 91-NM-171-AD AMENDMENT: 39-8374 AD NUMBER: 92-19-16 SUBJECT HEADING: Airworthiness Directives; BOEING Model 737 Series Airplanes ACTION: SUMMARY: DATES: Effective November 20, 1992. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 92-19-16 BOEING: Amendment 39-8374. Docket No. 91-NM-171-AD. Applicability: Model 737 series airplanes listed in Boeing Alert Service Bulletin 737-25A1283, Revision 1, dated March 19, 1992, Boeing Service Bulletin 737-25-1291, dated December 18, 1991, and Boeing Service Bulletin 737-25-1294, dated February 20, 1992; and Model 757 series airplanes listed in Boeing Alert Service Bulletin 757-25A0121, Revision 1, dated March 19, 1992, Boeing Service Bulletin 757-25-0130, dated December 18, 1991, Boeing Service Bulletin 757-25-0130, Revision 1, dated June 4, 1992, and Boeing Service Bulletin 757-53-0056, dated September 27, 1990; certificated in any category. Compliance: Required as indicated, unless accomplished previously. To prevent overhead stowage bins from separating from their attachments and injuring passengers in the event of an accident or emergency landing, accomplish the following: (a) For Boeing Model 737 series airplanes listed in Boeing Alert Service Bulletin 737-25A1283, Revision 1, dated March 19, 1992; and Model 757 series airplanes listed in Boeing Alert Service Bulletin 757-25A0121, Revision 1, dated March 19, 1992; accomplish paragraph (a)(1), (a)(2), or (a)(3) of this AD, as applicable: (1) For overhead stowage bins defined as Phase I in Section III, Note 5.a, of the applicable alert service bulletin, or any other stowage bin that contains a life raft or video equipment: Within 8 months after the effective date of this AD, modify those bins in accordance with Section III of Boeing Alert Service Bulletin 737-25A1283, Revision 1, dated March 19, 1992; or Boeing Alert Service Bulletin 757-25A0121, Revision 1, dated March 19, 1992; as applicable. (2) For overhead stowage bins defined as Phase II, III, or IV in Section III, Notes 5.b., 5.c., and 5.d., of the applicable alert service bulletin: Within 31 months after the effective date of this AD, modify those bins in accordance with Section III of Boeing Alert Service Bulletin 737-25A1283, Revision 1, dated March 19, 1992; or Boeing Alert Service Bulletin 757-25A0121, Revision 1, dated March 19, 1992; as applicable. (3) For overhead stowage bins greater than 67 inches long: Within 31 months after the effective date of this AD, replace the applicable drag link and tie rod assemblies in accordance with Boeing Service Bulletin 737-25-1291, dated December 18, 1991; or Boeing Service Bulletin 757-25-0130, dated December 18, 1991, or Revision 1, dated June 4, 1992; as applicable. (b) For Boeing Model 737 series airplanes listed in Boeing Service Bulletin 737-25-1294, dated February 20, 1992: Within 31 months after the effective date of this AD, install a doubler on the specified forty-five inch stowage compartment, in accordance with that service bulletin. (c) For Boeing Model 757 series airplanes listed in Boeing Service Bulletin 757-53-0056, dated September 27, 1990: Within 8 months after the effective date of this AD, install a doubler/diagonal strut assembly in accordance with that service bulletin. (d) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Seattle Aircraft Certification Office (ACO), FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Seattle ACO. NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Seattle ACO. (e) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished. (f) The installations, modifications, and replacement shall be done in accordance with the following Boeing service bulletins, which contain the following specified effective pages: Service Bulletin Referenced Page Number Revision Level Shown on Page Date Shown on Page 737-25A1283, 1-9, 11, 13-17, 1 March 19, 1992 Revision 1, 19-21, 23-24, March 19, 1992 26-27, 29-30, 32-33, 35-36, 38-39, 41-42, 44-45, 48-49, 51-52, 55-60, 246-257 10, 12, 18, 22, Original September 19, 1991 25, 28, 31, 34, 37, 40, 43, 46-47, 50, 53-54, 61-245 737-25-1291, 1-25 Original December 18, 1991 December 18, 1991 737-25-1294, 1-11 Original February 20, 1992 February 20, 1992 757-25A0121, 1-5, 7, 9-12, 1 March 19, 1992 Revision 1, 15-17, 19-20, March 19, 1992 22-23, 25-26, 28-29, 31-32, 35-36, 38-41, 110-115 6, 8, 13-14, 18, Original September 19, 1991 21, 24, 27, 30, 33-34, 37, 42-109 757-25-0130, 1-7, 12, 14-17, 1 June 4, 1992 Revision 1, 24-26, 29, 31, June 4, 1992 33-35, 37, 40-43 8-11, 13, 18-23, Original December 18, 1991 27-28, 30, 32, 36, 38-39 757-53-0056, 1-13 Original September 27, 1990 September 27, 1990 This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies may be obtained from Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. (g) This amendment becomes effective on November 20, 1992. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_92-19-16.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 92-19-16 Document Type: AD Final Rules Docket Number: 91-NM-171-AD Subject Heading: Airworthiness Directives; BOEING Model 737 Series Airplanes Subject: Overhead Stowage Bins Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 11/20/1992 Make: The Boeing Company Model: 737-100 Series | 737-200 Series | 737-200C Series | 737-300 Series | 737-400 Series | 737-500 Series...Show more 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: Updated RGL applicability to match AD applicability; CAR C-11-185 AIRWORTHINESS DIRECTIVES FINAL RULES: 92-19-16 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 91-NM-171-AD AMENDMENT: 39-8374 AD NUMBER: 92-19-16 SUBJECT HEADING: Airworthiness Directives; BOEING Model 737 Series Airplanes ACTION: SUMMARY: DATES: Effective November 20, 1992. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 92-19-16 BOEING: Amendment 39-8374. Docket No. 91-NM-171-AD. Applicability: Model 737 series airplanes listed in Boeing Alert Service Bulletin 737-25A1283, Revision 1, dated March 19, 1992, Boeing Service Bulletin 737-25-1291, dated December 18, 1991, and Boeing Service Bulletin 737-25-1294, dated February 20, 1992; and Model 757 series airplanes listed in Boeing Alert Service Bulletin 757-25A0121, Revision 1, dated March 19, 1992, Boeing Service Bulletin 757-25-0130, dated December 18, 1991, Boeing Service Bulletin 757-25-0130, Revision 1, dated June 4, 1992, and Boeing Service Bulletin 757-53-0056, dated September 27, 1990; certificated in any category. Compliance: Required as indicated, unless accomplished previously. To prevent overhead stowage bins from separating from their attachments and injuring passengers in the event of an accident or emergency landing, accomplish the following: (a) For Boeing Model 737 series airplanes listed in Boeing Alert Service Bulletin 737-25A1283, Revision 1, dated March 19, 1992; and Model 757 series airplanes listed in Boeing Alert Service Bulletin 757-25A0121, Revision 1, dated March 19, 1992; accomplish paragraph (a)(1), (a)(2), or (a)(3) of this AD, as applicable: (1) For overhead stowage bins defined as Phase I in Section III, Note 5.a, of the applicable alert service bulletin, or any other stowage bin that contains a life raft or video equipment: Within 8 months after the effective date of this AD, modify those bins in accordance with Section III of Boeing Alert Service Bulletin 737-25A1283, Revision 1, dated March 19, 1992; or Boeing Alert Service Bulletin 757-25A0121, Revision 1, dated March 19, 1992; as applicable. (2) For overhead stowage bins defined as Phase II, III, or IV in Section III, Notes 5.b., 5.c., and 5.d., of the applicable alert service bulletin: Within 31 months after the effective date of this AD, modify those bins in accordance with Section III of Boeing Alert Service Bulletin 737-25A1283, Revision 1, dated March 19, 1992; or Boeing Alert Service Bulletin 757-25A0121, Revision 1, dated March 19, 1992; as applicable. (3) For overhead stowage bins greater than 67 inches long: Within 31 months after the effective date of this AD, replace the applicable drag link and tie rod assemblies in accordance with Boeing Service Bulletin 737-25-1291, dated December 18, 1991; or Boeing Service Bulletin 757-25-0130, dated December 18, 1991, or Revision 1, dated June 4, 1992; as applicable. (b) For Boeing Model 737 series airplanes listed in Boeing Service Bulletin 737-25-1294, dated February 20, 1992: Within 31 months after the effective date of this AD, install a doubler on the specified forty-five inch stowage compartment, in accordance with that service bulletin. (c) For Boeing Model 757 series airplanes listed in Boeing Service Bulletin 757-53-0056, dated September 27, 1990: Within 8 months after the effective date of this AD, install a doubler/diagonal strut assembly in accordance with that service bulletin. (d) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Seattle Aircraft Certification Office (ACO), FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Seattle ACO. NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Seattle ACO. (e) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished. (f) The installations, modifications, and replacement shall be done in accordance with the following Boeing service bulletins, which contain the following specified effective pages: Service Bulletin Referenced Page Number Revision Level Shown on Page Date Shown on Page 737-25A1283, 1-9, 11, 13-17, 1 March 19, 1992 Revision 1, 19-21, 23-24, March 19, 1992 26-27, 29-30, 32-33, 35-36, 38-39, 41-42, 44-45, 48-49, 51-52, 55-60, 246-257 10, 12, 18, 22, Original September 19, 1991 25, 28, 31, 34, 37, 40, 43, 46-47, 50, 53-54, 61-245 737-25-1291, 1-25 Original December 18, 1991 December 18, 1991 737-25-1294, 1-11 Original February 20, 1992 February 20, 1992 757-25A0121, 1-5, 7, 9-12, 1 March 19, 1992 Revision 1, 15-17, 19-20, March 19, 1992 22-23, 25-26, 28-29, 31-32, 35-36, 38-41, 110-115 6, 8, 13-14, 18, Original September 19, 1991 21, 24, 27, 30, 33-34, 37, 42-109 757-25-0130, 1-7, 12, 14-17, 1 June 4, 1992 Revision 1, 24-26, 29, 31, June 4, 1992 33-35, 37, 40-43 8-11, 13, 18-23, Original December 18, 1991 27-28, 30, 32, 36, 38-39 757-53-0056, 1-13 Original September 27, 1990 September 27, 1990 This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies may be obtained from Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. (g) This amendment becomes effective on November 20, 1992. 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.
Related Airworthiness Directives
2025-02-02 Recurring
final ruleAirworthiness Directives; The Boeing Company Airplanes
Unsafe Condition: cracks in the frame inner chord and web at station (STA) 727 between S-11L and S-13L, which could result in the inability of a principal structural element to sustain limit load, and adversely affe...
2023-13-12 Recurring
final ruleAirworthiness Directives; The Boeing Company Airplanes
Unsafe Condition: premature aging of certain passenger chemical oxygen generators, which could fail to deliver oxygen during an emergency, possibly resulting in injury to the airplane occupants.
2023-12-13
final ruleAirworthiness Directives; The Boeing Company Airplanes
Unsafe Condition: Radio altimeters cannot be relied upon to perform their intended function if they experience interference from wireless broadband operations in the 5G C-Band. This interference can cause other airp...
2023-10-02
final ruleAirworthiness Directives; Transport and Commuter Category Airplanes
Unsafe Condition: Radio altimeter anomalies that are undetected by the automation or pilot, particularly close to the ground (e.g., landing flare), could lead to loss of continued safe flight and landing. Additional...