AD 92-07-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 737-100 Series | Airworthiness Directives; BOEING Model 737 Airplanes |
| aircraft | The Boeing Company | 737-200 Series | Airworthiness Directives; BOEING Model 737 Airplanes |
| aircraft | The Boeing Company | 737-200C Series | Airworthiness Directives; BOEING Model 737 Airplanes |
| aircraft | The Boeing Company | 737-300 Series | Airworthiness Directives; BOEING Model 737 Airplanes |
| aircraft | The Boeing Company | 737-400 Series | Airworthiness Directives; BOEING Model 737 Airplanes |
| aircraft | The Boeing Company | 737-500 Series | Airworthiness Directives; BOEING Model 737 Airplanes |
| aircraft | The Boeing Company | 737-600 Series | Airworthiness Directives; BOEING Model 737 Airplanes |
| aircraft | The Boeing Company | 737-700 Series | Airworthiness Directives; BOEING Model 737 Airplanes |
| aircraft | The Boeing Company | 737-800 Series | Airworthiness Directives; BOEING Model 737 Airplanes |
Unsafe Condition
Chafing of wires and electrical overload of wires, which could lead to a potential fire in the cockpit.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify wire bundles and install a capped quick release receptacle and nutplate per Boeing Service Bulletin 737-24-1077, or replace undersized wire with 12 gauge wire in the P6-2 circuit breaker panel per Boeing Service Bulletin 737-24-1084.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within 6 months after the effective date of this AD, unless accomplished previously
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Model 737 airplanes listed in Boeing Service Bulletins 737-24-1077 (Rev 2) and 737-24-1084 (Rev 1), certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Wire Bundles
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_92-07-10.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 92-07-10 Document Type: AD Final Rules Docket Number: 91-NM-93-AD Subject Heading: Airworthiness Directives; BOEING Model 737 Airplanes Subject: Wire Bundles Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 05/04/1992 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: AIRWORTHINESS DIRECTIVES FINAL RULES: 92-07-10 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 91-NM-93-AD AMENDMENT: 39-8206 AD NUMBER: 92-07-10 SUBJECT HEADING: Airworthiness Directives; BOEING Model 737 Airplanes ACTION: SUMMARY: DATES: Effective May 4, 1992. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 92-07-10 BOEING: Amendment 39-8206. Docket No. 91-NM-93-AD. Applicability: Model 737 airplanes, as listed in Boeing Service Bulletin 737-24-1077, Revision 2, dated July 25, 1991, and Boeing Service Bulletin 737-24-1084, Revision 1, dated March 21, 1991; certificated in any category. Compliance: Required within 6 months after the effective date of this AD, unless accomplished previously. To prevent chafing of wires and electrical overload of wires, and to remove the potential for a fire in the cockpit, accomplish the following: (a) For airplanes listed in Boeing Service Bulletin 737-24-1077, Revision 2, dated July 25, 1991: Modify the wire bundles and install a capped quick release receptacle and nutplate, in accordance with Boeing Service Bulletin 737-24-1077, dated August 17, 1989; or Revision 1, dated August 16, 1990; or Revision 2, dated July 25, 1991. (b) For airplanes listed in Boeing Service Bulletin 737-24-1084, Revision 1, dated March 21, 1991: Replace the undersized wire with a 12 gauge wire in the P6-2 circuit breaker panel, in accordance with Boeing Service Bulletin 737-24-1084, dated October 11, 1990; or Revision 1, dated March 21, 1991. (c) An alternative method 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. The request shall be forwarded through an FAA Principal Maintenance Inspector, who may concur or comment and then send it to the Manager, Seattle ACO. (d) 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. (e) The modifications shall be done in accordance with Boeing Service Bulletin 737- 24-1077, dated August 17, 1989, or Revision 1, dated August 16, 1990, or Revision 2, dated July 25, 1991; and in accordance with Boeing Service Bulletin 737-24-1084, dated October 11, 1990, or Revision 1, dated March 21, 1991. 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, Northwest Mountain Region, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington; or at the Office of the Federal Register, 1100 L Street NW., Room 8401, Washington, DC. (f) This amendment becomes effective on May 4, 1992. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_92-07-10.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 92-07-10 Document Type: AD Final Rules Docket Number: 91-NM-93-AD Subject Heading: Airworthiness Directives; BOEING Model 737 Airplanes Subject: Wire Bundles Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 05/04/1992 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: AIRWORTHINESS DIRECTIVES FINAL RULES: 92-07-10 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 91-NM-93-AD AMENDMENT: 39-8206 AD NUMBER: 92-07-10 SUBJECT HEADING: Airworthiness Directives; BOEING Model 737 Airplanes ACTION: SUMMARY: DATES: Effective May 4, 1992. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 92-07-10 BOEING: Amendment 39-8206. Docket No. 91-NM-93-AD. Applicability: Model 737 airplanes, as listed in Boeing Service Bulletin 737-24-1077, Revision 2, dated July 25, 1991, and Boeing Service Bulletin 737-24-1084, Revision 1, dated March 21, 1991; certificated in any category. Compliance: Required within 6 months after the effective date of this AD, unless accomplished previously. To prevent chafing of wires and electrical overload of wires, and to remove the potential for a fire in the cockpit, accomplish the following: (a) For airplanes listed in Boeing Service Bulletin 737-24-1077, Revision 2, dated July 25, 1991: Modify the wire bundles and install a capped quick release receptacle and nutplate, in accordance with Boeing Service Bulletin 737-24-1077, dated August 17, 1989; or Revision 1, dated August 16, 1990; or Revision 2, dated July 25, 1991. (b) For airplanes listed in Boeing Service Bulletin 737-24-1084, Revision 1, dated March 21, 1991: Replace the undersized wire with a 12 gauge wire in the P6-2 circuit breaker panel, in accordance with Boeing Service Bulletin 737-24-1084, dated October 11, 1990; or Revision 1, dated March 21, 1991. (c) An alternative method 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. The request shall be forwarded through an FAA Principal Maintenance Inspector, who may concur or comment and then send it to the Manager, Seattle ACO. (d) 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. (e) The modifications shall be done in accordance with Boeing Service Bulletin 737- 24-1077, dated August 17, 1989, or Revision 1, dated August 16, 1990, or Revision 2, dated July 25, 1991; and in accordance with Boeing Service Bulletin 737-24-1084, dated October 11, 1990, or Revision 1, dated March 21, 1991. 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, Northwest Mountain Region, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington; or at the Office of the Federal Register, 1100 L Street NW., Room 8401, Washington, DC. (f) This amendment becomes effective on May 4, 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.
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