AD 92-01-10
final rule
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Dassault Aviation | Fan Jet Falcon Series G | Airworthiness Directives; DASSAULT AVIATION Model Fan Jet Falcon Series G and Mystere Falcon 200 Series Airplanes |
| aircraft | Dassault Aviation | Mystere-Falcon 200 | Airworthiness Directives; DASSAULT AVIATION Model Fan Jet Falcon Series G and Mystere Falcon 200 Series Airplanes |
Unsafe Condition
In-flight separation of the engine cowls due to failure of hinges and fasteners (latches and aprons).
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Required Actions
Within 14 days after the effective date, and every 7 days thereafter, inspect hinges and fasteners on engine cowls per the maintenance manual. Replace discrepant parts before further flight. Reinforce latches per SB F200-59, install new hinge pin latching systems per SB F200-78, and reinforce small aprons/modify hinged cowl attachments per SB F200-87.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 14 days after the effective date of this AD, and thereafter at intervals not to exceed 7 days
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Dassault Aviation Model Fan Jet Falcon Series G and Mystere Falcon 200 series airplanes, certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Engine Cowls
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_92-01-10.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 92-01-10 Document Type: AD Final Rules Docket Number: 91-NM-256-AD Subject Heading: Airworthiness Directives; DASSAULT AVIATION Model Fan Jet Falcon Series G and Mystere Falcon 200 Ser...Show more Subject: Engine Cowls Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 01/24/1992 Make: Dassault Aviation Model: Fan Jet Falcon Series G | Mystere-Falcon 200 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 92-01-10 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 91-NM-256-AD AMENDMENT: 39-8134 AD NUMBER: 92-01-10 SUBJECT HEADING: Airworthiness Directives; DASSAULT AVIATION Model Fan Jet Falcon Series G and Mystere Falcon 200 Series Airplanes ACTION: SUMMARY: DATES: Effective January 24, 1992. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 92-01-10 DASSAULT AVIATION (formerly Avions Marcel Dassault-Breguet Aviation): Amendment 39-8134. Docket 91-NM-256-AD. Applicability: Model Fan Jet Falcon Series G and Mystere Falcon 200 series airplanes, certificated in any category. Compliance: Required as indicated, unless accomplished previously. To prevent in-flight separation of the engine cowls, accomplish the following: (a) Within 14 days after the effective date of this AD, and thereafter at intervals not to exceed 7 days, perform an inspection of the hinges and fasteners (latches and aprons) on the engine cowls to verify their integrity, in accordance with the airplane maintenance manual (refer to Work Card 741-0, Revision A-1-b, dated December 1990). Replace discrepant hinges or fasteners (latches or aprons) prior to further flight, in accordance with the airplane maintenance manual. (b) Accomplishment of subparagraphs (b)(1), (b)(2), and (b)(3) of this AD constitutes terminating action for the repetitive inspections required by paragraph (a) of this AD. (1) Reinforce the latches in accordance with Dassault Aviation Service Bulletin F200- 59 (ATA Number F200-54-4), Revision 1, dated September 18, 1991. (2) Install new hinge pin latching systems in accordance with Dassault Aviation Service Bulletin F200-78 (ATA Number F200-54-7), Revision 1, dated September 18, 1991. (3) Reinforce the small aprons and modify the hinged cowl attachments in accordance with Dassault Aviation Service Bulletin F200-87 (ATA Number F200-54-10), dated September 18, 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, Standardization Branch, ANM- 113, 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, Standardization Branch, ANM-113. (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 required by this AD shall be done in accordance with Dassault Aviation Service Bulletin F200-59 (ATA Number F200-54-4), Revision 1, dated September 18, 1991; Dassault Aviation Service Bulletin F200-78 (ATA Number F200-54-7), Revision 1, dated September 18, 1991; and Dassault Aviation Service Bulletin F200-87 (ATA Number F200-54-10), dated September 18, 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 Falcon Jet Corporation, Customer Support Department, Teterboro Airport, Teterboro, New Jersey 07608. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue S.W., Renton, Washington; or at the Office of the Federal Register, 1100 L Street N.W., Room 8401, Washington, D.C. (g) This amendment (39-8134, AD 92-01-10) becomes effective on January 24, 1992. FOOTER:
Document Text
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AD Final Rules - DRS_92-01-10.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 92-01-10 Document Type: AD Final Rules Docket Number: 91-NM-256-AD Subject Heading: Airworthiness Directives; DASSAULT AVIATION Model Fan Jet Falcon Series G and Mystere Falcon 200 Ser...Show more Subject: Engine Cowls Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 01/24/1992 Make: Dassault Aviation Model: Fan Jet Falcon Series G | Mystere-Falcon 200 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: 92-01-10 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 91-NM-256-AD AMENDMENT: 39-8134 AD NUMBER: 92-01-10 SUBJECT HEADING: Airworthiness Directives; DASSAULT AVIATION Model Fan Jet Falcon Series G and Mystere Falcon 200 Series Airplanes ACTION: SUMMARY: DATES: Effective January 24, 1992. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 92-01-10 DASSAULT AVIATION (formerly Avions Marcel Dassault-Breguet Aviation): Amendment 39-8134. Docket 91-NM-256-AD. Applicability: Model Fan Jet Falcon Series G and Mystere Falcon 200 series airplanes, certificated in any category. Compliance: Required as indicated, unless accomplished previously. To prevent in-flight separation of the engine cowls, accomplish the following: (a) Within 14 days after the effective date of this AD, and thereafter at intervals not to exceed 7 days, perform an inspection of the hinges and fasteners (latches and aprons) on the engine cowls to verify their integrity, in accordance with the airplane maintenance manual (refer to Work Card 741-0, Revision A-1-b, dated December 1990). Replace discrepant hinges or fasteners (latches or aprons) prior to further flight, in accordance with the airplane maintenance manual. (b) Accomplishment of subparagraphs (b)(1), (b)(2), and (b)(3) of this AD constitutes terminating action for the repetitive inspections required by paragraph (a) of this AD. (1) Reinforce the latches in accordance with Dassault Aviation Service Bulletin F200- 59 (ATA Number F200-54-4), Revision 1, dated September 18, 1991. (2) Install new hinge pin latching systems in accordance with Dassault Aviation Service Bulletin F200-78 (ATA Number F200-54-7), Revision 1, dated September 18, 1991. (3) Reinforce the small aprons and modify the hinged cowl attachments in accordance with Dassault Aviation Service Bulletin F200-87 (ATA Number F200-54-10), dated September 18, 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, Standardization Branch, ANM- 113, 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, Standardization Branch, ANM-113. (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 required by this AD shall be done in accordance with Dassault Aviation Service Bulletin F200-59 (ATA Number F200-54-4), Revision 1, dated September 18, 1991; Dassault Aviation Service Bulletin F200-78 (ATA Number F200-54-7), Revision 1, dated September 18, 1991; and Dassault Aviation Service Bulletin F200-87 (ATA Number F200-54-10), dated September 18, 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 Falcon Jet Corporation, Customer Support Department, Teterboro Airport, Teterboro, New Jersey 07608. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue S.W., Renton, Washington; or at the Office of the Federal Register, 1100 L Street N.W., Room 8401, Washington, D.C. (g) This amendment (39-8134, AD 92-01-10) becomes effective on January 24, 1992. FOOTER:
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Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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