AD 90-21-21
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 747-100 Series | Airworthiness Directives; BOEING Model 747 Series Airplanes |
| aircraft | The Boeing Company | 747-100B Series | Airworthiness Directives; BOEING Model 747 Series Airplanes |
| aircraft | The Boeing Company | 747-100B SUD Series | Airworthiness Directives; BOEING Model 747 Series Airplanes |
| aircraft | The Boeing Company | 747-200B Series | Airworthiness Directives; BOEING Model 747 Series Airplanes |
| aircraft | The Boeing Company | 747-200C Series | Airworthiness Directives; BOEING Model 747 Series Airplanes |
| aircraft | The Boeing Company | 747-200F Series | Airworthiness Directives; BOEING Model 747 Series Airplanes |
| aircraft | The Boeing Company | 747-300 Series | Airworthiness Directives; BOEING Model 747 Series Airplanes |
| aircraft | The Boeing Company | 747-400 Series | Airworthiness Directives; BOEING Model 747 Series Airplanes |
| aircraft | The Boeing Company | 747-400D Series | Airworthiness Directives; BOEING Model 747 Series Airplanes |
| aircraft | The Boeing Company | 747-400F Series | Airworthiness Directives; BOEING Model 747 Series Airplanes |
| aircraft | The Boeing Company | 747SP Series | Airworthiness Directives; BOEING Model 747 Series Airplanes |
| aircraft | The Boeing Company | 747SR Series | Airworthiness Directives; BOEING Model 747 Series Airplanes |
Unsafe Condition
Potential for an engine fire due to a fuel leak caused by aluminum pneumatic duct brackets, P/N 69B94023-1, in the outboard struts.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace aluminum pneumatic duct brackets (P/N 69B94023-1) with steel brackets (P/N 69B94023-2) in accordance with Boeing Service Letter 747-SL-54-32.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the next 60 days or 450 hours time-in-service 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
Model 747 series airplanes equipped with General Electric CF6-45 and CF6-50 engines, as listed in Boeing Service Letter 747-SL-54-32 dated December 4, 1989.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Pneumatic Duct Brackets
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_90-21-21.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 90-21-21 Document Type: AD Final Rules Docket Number: 90-NM-108-AD Subject Heading: Airworthiness Directives; BOEING Model 747 Series Airplanes Subject: Pneumatic Duct Brackets Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 11/16/1990 Make: The Boeing Company Model: 747-100 Series | 747-100B Series | 747-100B SUD Series | 747-200B Series | 747-200C Series | 747-200...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: 90-21-21 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 90-NM-108-AD AMENDMENT: 39-6766 AD NUMBER: 90-21-21 SUBJECT HEADING: Airworthiness Directives; BOEING Model 747 Series Airplanes ACTION: SUMMARY: DATES: DATE: Effective November 16, 1990. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 90-21-21 BOEING: Amendment 39-6766. Docket No. 90-NM-108-AD. Applicability: Model 747 series airplanes, equipped with General Electric CF6-45 and CF6-50 engines, as listed in Boeing Service Letter 747-SL-54-32, dated December 4, 1989, certificated in any category. Compliance: Required as indicated, unless previously accomplished. To eliminate the potential for an engine fire due to a fuel leak, accomplish the following: A. Within the next 60 days or 450 hours time-in-service after the effective date of this AD, whichever occurs first, replace the aluminum pneumatic duct brackets, P/N 69B94023- 1, in the outboard struts, with steel brackets, P/N 69B94023-2, in accordance with Boeing Service Letter 747-SL-54-32, dated December 4, 1989. B. An alternate means 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. NOTE: The request should be submitted directly to the Manager, Seattle ACO, and a copy sent to the cognizant FAA Principal Inspector (PI). The PI will then forward comments or concurrence to the Seattle ACO. 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 Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington 98055-4056. This amendment (39-6766, AD 90-21-21) becomes effective on November 16, 1990. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_90-21-21.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 90-21-21 Document Type: AD Final Rules Docket Number: 90-NM-108-AD Subject Heading: Airworthiness Directives; BOEING Model 747 Series Airplanes Subject: Pneumatic Duct Brackets Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 11/16/1990 Make: The Boeing Company Model: 747-100 Series | 747-100B Series | 747-100B SUD Series | 747-200B Series | 747-200C Series | 747-200...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: 90-21-21 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 90-NM-108-AD AMENDMENT: 39-6766 AD NUMBER: 90-21-21 SUBJECT HEADING: Airworthiness Directives; BOEING Model 747 Series Airplanes ACTION: SUMMARY: DATES: DATE: Effective November 16, 1990. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 90-21-21 BOEING: Amendment 39-6766. Docket No. 90-NM-108-AD. Applicability: Model 747 series airplanes, equipped with General Electric CF6-45 and CF6-50 engines, as listed in Boeing Service Letter 747-SL-54-32, dated December 4, 1989, certificated in any category. Compliance: Required as indicated, unless previously accomplished. To eliminate the potential for an engine fire due to a fuel leak, accomplish the following: A. Within the next 60 days or 450 hours time-in-service after the effective date of this AD, whichever occurs first, replace the aluminum pneumatic duct brackets, P/N 69B94023- 1, in the outboard struts, with steel brackets, P/N 69B94023-2, in accordance with Boeing Service Letter 747-SL-54-32, dated December 4, 1989. B. An alternate means 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. NOTE: The request should be submitted directly to the Manager, Seattle ACO, and a copy sent to the cognizant FAA Principal Inspector (PI). The PI will then forward comments or concurrence to the Seattle ACO. 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 Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington 98055-4056. This amendment (39-6766, AD 90-21-21) becomes effective on November 16, 1990. 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.