AD 67-27-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Dassault Aviation | Fan Jet Falcon | Airworthiness Directives; AVIONS MARCEL DASSAULT Model Fan Jet Falcon Airplanes |
Unsafe Condition
Jamming of the engine power lever due to the type MF 2006 pressurization control microswitch installation.
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Required Actions
Modify the pressurization control microswitch installation by adding support P/N MY.20.240.3801 and leaf spring P/N MY.20.240.3802 per Avions Marcel Dassault Service Bulletin No. 211, (76-4), revision 1, or later SGAC-approved revision.
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Compliance Time
within the next 200 hours' time in service after the effective date of this AD
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Affected Aircraft
AVIONS MARCEL DASSAULT Model Fan Jet Falcon Airplanes, Serial Numbers 1 thru 94
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Federal Register Abstract
Engine Power Lever
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_67-27-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 67-27-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; AVIONS MARCEL DASSAULT Model Fan Jet Falcon Airplanes Subject: Engine Power Lever Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 10/09/1967 Make: Dassault Aviation Model: Fan Jet Falcon Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 67-27-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-474 AD NUMBER: 67-27-01 SUBJECT HEADING: Airworthiness Directives; AVIONS MARCEL DASSAULT Model Fan Jet Falcon Airplanes ACTION: SUMMARY: DATES: Effective October 9, 1967. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 67-27-01 AVIONS MARCEL DASSAULT: Amdt. 39-474, Part 39, Federal Register September 9, 1967. Applies to Fan Jet Falcon Airplanes, Serial Numbers 1 thru 94. Compliance required within the next 200 hours' time in service after the effective date of this AD, unless already accomplished. To prevent jamming of the engine power lever, modify the type MF 2006 pressurization control microswitch installation by the addition of a support, P/N MY.20.240.3801, and a leaf spring, P/N MY.20.240.3802, in accordance with Avions Marcel Dassault Service Bulletin No. 211, (76-4), revision 1, dated April 4, 1967, or later SGAC-approved revision, or an equivalent approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa and Middle East Region. This amendment effective October 9, 1967. FOOTER:
Document Text
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AD Final Rules - DRS_67-27-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 67-27-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; AVIONS MARCEL DASSAULT Model Fan Jet Falcon Airplanes Subject: Engine Power Lever Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 10/09/1967 Make: Dassault Aviation Model: Fan Jet Falcon 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: 67-27-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-474 AD NUMBER: 67-27-01 SUBJECT HEADING: Airworthiness Directives; AVIONS MARCEL DASSAULT Model Fan Jet Falcon Airplanes ACTION: SUMMARY: DATES: Effective October 9, 1967. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 67-27-01 AVIONS MARCEL DASSAULT: Amdt. 39-474, Part 39, Federal Register September 9, 1967. Applies to Fan Jet Falcon Airplanes, Serial Numbers 1 thru 94. Compliance required within the next 200 hours' time in service after the effective date of this AD, unless already accomplished. To prevent jamming of the engine power lever, modify the type MF 2006 pressurization control microswitch installation by the addition of a support, P/N MY.20.240.3801, and a leaf spring, P/N MY.20.240.3802, in accordance with Avions Marcel Dassault Service Bulletin No. 211, (76-4), revision 1, dated April 4, 1967, or later SGAC-approved revision, or an equivalent approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa and Middle East Region. This amendment effective October 9, 1967. FOOTER:
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Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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