AD 82-25-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Dassault Aviation | Falcon 10 | AVIONS MARCEL DASSAULT - BREGUET AVIATION Model AMD-BA Falcon 10 Airplanes |
Unsafe Condition
Potential failure of the landing gear to extend or retract due to issues with the pilot valve ball pushrod, selector solenoid valve, or spring in the landing gear control selector solenoid valve assembly.
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Required Actions
Inspect and modify or replace the pilot valve ball pushrod, selector solenoid valve, and spring in the landing gear control selector solenoid valve assembly per Service Bulletins F10-0149, F10-0168, F10-0173, and F10-0174. Alternate means of compliance may be approved by the FAA.
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Compliance Time
within the next 250 hours time in service or 90 days, whichever occurs first, after the effective date of this AD
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Affected Aircraft
All AMD-BA Falcon 10 airplanes certificated in all categories
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Federal Register Abstract
Landing Gear Retraction System
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_82-25-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 82-25-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: AVIONS MARCEL DASSAULT - BREGUET AVIATION Model AMD-BA Falcon 10 Airplanes Subject: Landing Gear Retraction System Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 12/06/1982 Make: Dassault Aviation Model: Falcon 10 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 82-25-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4502 AD NUMBER: 82-25-02 SUBJECT HEADING: AVIONS MARCEL DASSAULT - BREGUET AVIATION Model AMD-BA Falcon 10 Airplanes ACTION: SUMMARY: DATES: Effective December 6, 1982. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 82-25-02 AVIONS MARCEL DASSAULT - BREGUET AVIATION: Amendment 39-4502. Applies to all AMD-BA Falcon 10 airplanes certificated in all categories. Compliance is required within the next 250 hours time in service or 90 days, whichever occurs first, after the effective date of this AD, unless already accomplished. 1. To prevent the potential failure of the landing gear to extend or retract, inspect and modify or replace, if necessary, (a) the pilot valve ball pushrod; (b) the selector solenoid valve; and (c) the spring in the landing gear control selector solenoid valve assembly in accordance with the Accomplishment Instructions of Avions Marcel Dassault-Breguet Aviation Service Bulletin Nos. F10-0149, Revision 1, dated November 22, 1978; F10-0168, Revision 1, dated February 8, 1979; F10-0173 dated November 22, 1978; and F10-0174 dated November 22, 1978. 2. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. 3. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD. The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1). This amendment becomes effective December 6, 1982. FOOTER:
Document Text
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AD Final Rules - DRS_82-25-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 82-25-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: AVIONS MARCEL DASSAULT - BREGUET AVIATION Model AMD-BA Falcon 10 Airplanes Subject: Landing Gear Retraction System Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 12/06/1982 Make: Dassault Aviation Model: Falcon 10 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: 82-25-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4502 AD NUMBER: 82-25-02 SUBJECT HEADING: AVIONS MARCEL DASSAULT - BREGUET AVIATION Model AMD-BA Falcon 10 Airplanes ACTION: SUMMARY: DATES: Effective December 6, 1982. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 82-25-02 AVIONS MARCEL DASSAULT - BREGUET AVIATION: Amendment 39-4502. Applies to all AMD-BA Falcon 10 airplanes certificated in all categories. Compliance is required within the next 250 hours time in service or 90 days, whichever occurs first, after the effective date of this AD, unless already accomplished. 1. To prevent the potential failure of the landing gear to extend or retract, inspect and modify or replace, if necessary, (a) the pilot valve ball pushrod; (b) the selector solenoid valve; and (c) the spring in the landing gear control selector solenoid valve assembly in accordance with the Accomplishment Instructions of Avions Marcel Dassault-Breguet Aviation Service Bulletin Nos. F10-0149, Revision 1, dated November 22, 1978; F10-0168, Revision 1, dated February 8, 1979; F10-0173 dated November 22, 1978; and F10-0174 dated November 22, 1978. 2. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. 3. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD. The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1). This amendment becomes effective December 6, 1982. FOOTER:
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