AD 86-15-06
final rule
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Dassault Aviation | Falcon 10 | AVIONS MARCEL DASSAULT - BREGUET AVIATION Model AMD Falcon 10 Series Airplanes |
Unsafe Condition
The rudder servo actuator hydraulic lines may not be properly installed, which could result in hydraulic fluid leakage and loss of rudder control.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify the rudder servo actuator system in accordance with AMD-BA Service Bulletin F10-27-028 (0237). An alternate means of compliance or adjustment of compliance time may be used if approved by the FAA Manager, Standardization Branch, ANM-113.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within 60 days after the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
AMD Falcon 10 series airplanes, serial numbers 1 thru 196 inclusive, and 198 thru 201 inclusive, certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Rudder Servo Actuator System
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_86-15-06.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 86-15-06 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: AVIONS MARCEL DASSAULT - BREGUET AVIATION Model AMD Falcon 10 Series Airplanes Subject: Rudder Servo Actuator System Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 08/25/1986 Make: Dassault Aviation Model: Falcon 10 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 86-15-06 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5363 AD NUMBER: 86-15-06 SUBJECT HEADING: AVIONS MARCEL DASSAULT - BREGUET AVIATION Model AMD Falcon 10 Series Airplanes ACTION: SUMMARY: DATES: Effective August 25, 1986. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 86-15-06 AVIONS MARCEL DASSAULT - BREGUET AVIATION: Amendment 39-5363. Applies to AMD Falcon 10 series airplanes, serial numbers 1 thru 196 inclusive, and 198 thru 201 inclusive, certificated in any category. Compliance is required within 60 days after the effective date of this AD. To ensure the proper installation of the rudder servo actuator hydraulic lines, accomplish the following, unless already accomplished: A. Modify the rudder servo actuator system in accordance with AMD-BA Service Bulletin F10-27-028 (0237), dated June 24, 1983. 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, Standardization Branch, ANM-113, FAA, Northwest Mountain Region. C. 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. All persons affected by this directive, who have not already received the appropriate service bulletin from the manufacturer, may obtain copies upon request to the AMD-BA Representative, c/o F.J.C., Teterboro Airport, Teterboro, New Jersey 07608. This document may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. This amendment, 39-5363, becomes effective August 25, 1986. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_86-15-06.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 86-15-06 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: AVIONS MARCEL DASSAULT - BREGUET AVIATION Model AMD Falcon 10 Series Airplanes Subject: Rudder Servo Actuator System Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 08/25/1986 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: 86-15-06 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5363 AD NUMBER: 86-15-06 SUBJECT HEADING: AVIONS MARCEL DASSAULT - BREGUET AVIATION Model AMD Falcon 10 Series Airplanes ACTION: SUMMARY: DATES: Effective August 25, 1986. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 86-15-06 AVIONS MARCEL DASSAULT - BREGUET AVIATION: Amendment 39-5363. Applies to AMD Falcon 10 series airplanes, serial numbers 1 thru 196 inclusive, and 198 thru 201 inclusive, certificated in any category. Compliance is required within 60 days after the effective date of this AD. To ensure the proper installation of the rudder servo actuator hydraulic lines, accomplish the following, unless already accomplished: A. Modify the rudder servo actuator system in accordance with AMD-BA Service Bulletin F10-27-028 (0237), dated June 24, 1983. 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, Standardization Branch, ANM-113, FAA, Northwest Mountain Region. C. 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. All persons affected by this directive, who have not already received the appropriate service bulletin from the manufacturer, may obtain copies upon request to the AMD-BA Representative, c/o F.J.C., Teterboro Airport, Teterboro, New Jersey 07608. This document may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. This amendment, 39-5363, becomes effective August 25, 1986. 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.